(1992) T.O. 1F-117A-1 Utility Flight Manual USAF Series F-117A Aircraft

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TO 1F-117A-1

UTILITY FU GHT MANUAL USAF SERIES

F- 117A AIRCRAFT

DISTRIBUTlON STATEMENT

This publication is required for offiCial use or for administrative or operational purposes onty. Distribution is limited to U.S. Government Agencies. Other requests for this documerrt must be referred to SM-ALC/QL See reverse side {PageT-2) for discJoswe notice, handUng and destruction notice, supplemental notice, and supersedure notice. Commanders are respons ble for bringing th s pub ication to the attention of all affected personnel.

TO 1F-117A-1

DISClOSURE NOTICE

If this dlx:uman is app oved for release 10 a foreign pemment, it is fumisbed upon the cooditiolllbal it 'iliiiJ - be released to aDOthcr Datioll wilhoot specific authority ollhe Department ollhe Air Force ol the United Slates, thai it will be used focmililalypwposesoaly,lbal iDdividual orWipcuterigluoriginatingin the information. wbetbeqxue•ncd or DOl. will be respected, lball.be w will report promptly to the U.S.. UIJ t:nowD or suspected axnpromise. and lballhe infomoation ..,ill be JI"''idcd snbqantia!Jy the same degree ol security afforded it by l.be Dcpanmcnt ol Ddmse ol the United States.

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HANDUNG AND OESTRUcnoN NOTICE l:laadle in compl.iaoce 'lrith cfisuilcuioa statement and desuOJ by any method that will ~· cfisrlosm~ ol the

eonterus or recoasuuctioo ollhe docv!!lft!J SUPPl.EJ.IEHTAL NOTICE This manual is incomplete witbout TO 1F-117A-1A a.nd TO 1F-117A-l-L SUPERSEDURE NOTICE SJIY I99Z

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FUGHT MANUAL,. SAFETY SUPPLEMENT, AND OPERATIONAL SUPPLEMENT STATUS This supplement swus page is based on information a-mJallle as ol3 l'dlru:uy 1992. It is Dill an official SUl11S page. flight Manual

Basic Date

TO 1F-117A- l

3Fd>92

Supplemental Fligbt ~fanual

Basic Date

TO 1F-117A-IA TO 1F-ll7A-l-l

3Fd>92 3Feb92

Flight Crew C'Ju:d:l jq

Basic Date

TO 1F-ll7A-ICL-1

3Feb92

Cllante No. and Date

Olange No. and Date

OUTSTANDING SAFETY AND OPERATIONAL SUPPLEMENTS Short Tille

Number

INCORPORATED SAFErt AND OPERATIONAL SUPPLEMENTS Date

Short Tille

Fliglu ~fanual

Seaions Affected

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TO 1F-117A-1

CHANGE DATA SUMMARY "The followin& Womaatioa is added, deleted. oc revised i.o this reissue. Engine blow-iiHioor incficaroc lights desc:ripcioa revised ECS owerbcat light description ~ Throttle pand illusuatioo ~ • ECS pand illnurarm revised Cootrol stict switches illusuatioo revised • New brake S)'Siem data added

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NAV ALERT PWR S'l'ild> dcsuipi.xl revised --.~1>:-:;t:..:. asrer test system 'tted. Comments. COO''"' •• •IS, aDd questions regazding lllis manual are wdalmed Please forward any commeots. c:or:recUoo.s. oc reqaest fer inftwmation through mmmand beadquacten 10 Saaamen10 ALCIQL. McOd1an AFB, CA

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TABLE OF COl'.'TENTS

SECTION •••.•••.•••...•.••• TTn..£ •••••••••••••••••••••••••••••••••••••••••••••••••••• PACE

SECllOS I ••.•.•• • ••• . • . .•. DESCJUPTJON •..••.•.••..••.••••..•••.••••••...•.•..•••••.• 1-1 SECTION D • . • • • • • • • • . • • • . • • ORMAl.. I'ROCEDURES ........ . ............................ l-1 SECTIOS m ................ DIERCENCY PROC£Dl/RES .um ABSOIL\tAL OPERATIONS

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3-l

Sll:11()Srv .••..•.....•...• A~Y~~'r .....••...•.•.••••••••••.•••...••••. 4-1 SECllOS V ................. OPI:RATI:SC UMJTATIONS ...................................

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SECTION \1 ................ n.JCKT O«ARA.CTEIUSl1CS ................................. .._, S£CT10S \11 ............... ADVERSE VI'EAniE.R OPI:RATION ............................ 7-l

APPL''DIX A ••••••••••••.•• PERFORMANCE DATA .•..••••..•...........••.••.••..••••.•. A-I APPL''DIX II ............... PERFORMANCE DATA ...................................... lA-1 (RCS D-'HA.""CERS ISSTAU..ED)

Gl OSSARY ........................................................................ CIMsa ,-1 Al.PHA.IIETlCAL I!"DEX .............................................................. lada-1

FOLDOUT .................. FOLDOUT lU.USTRATIOSS ................................ F0-1

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THE AIRCRAFT

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SECTION I DESCRIPTION TABLE OF CONTENTS Air0"8ft ···················· · ···-··--·- ·--· 1- 1

FAP- -- .... -............... -............

1-2

~ T.-.diJic Awl E..p.. ·~

SJSbOa (~IS) •••••.••.••.•••••••..• l-10 Air0"8ft F..t s~ 1-10 AUfra.o Mo.•led ... ' ' .. 'T DriTe l-18

_____ ......... ___ .....

s,..... (.\.\tAD)---------·----·--------

s~ -----·--·--·-·--·-----·-~ eo.tro1 s~ CECS> .... ...

EDeod AJr

t- 19 t-19

Ami""ry ~ u.it (APU) • .. ... . • • • • • • • • 1-23 E "f""lcated oa the tluotlle and stidt grips. Four majoo" CRf displa)'S in llle axtpit iDdudc left and ri&Jtt mniQpwpose display in1a1tin& t1oe APU wtDcb thee so.,. r t , adeqra•e air Dow to t1oe AT'S ror eap.e a:an.

ENGLNE STARTING SYSTEM CONTROLS AND INDICATORS

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ENGINE START£R ENGAGED LIGHTS

Two STARTER ENGAGED (L-R) li&hts. located oo tbe aas~er teP pend (sec r tprc 1-3) 011 tbe left tide pad. QliDe . . ~ e.p.e swt wtaeso tbe ~ aated esopae • • ""'es 10 40110t.o45'1o rpm (appor· .-ely). Tile lip~ &OCS off wt.ao tbe CDgiDe swter djsco~ as l.be mpoe CIOtt rpm ina lboYe S4'1o. START£R ENGAGED UGHT

ENGINE START SWTTCH£5

Two (LJR) STAKT AMAD RUN swilcftcs .-.= lex e.:ll esogix. are Joc:uecl oa t1oe UuouJe pud ca tloe ldt cnmrAe (see rC!ft 1-~ 1bol: IDOIDetW!tJ' macaaic-llold S'trildl ....p.es l.be AT'S wbit:b is dri'I'CII by p Sr >ol ....., ctur., me Slat\ qcle ill &be 1..STAJIT or R-STAJrr pW4•• Rll'l'riso& ~ menl (aasla Cllll&t) 0{ lbe AT'S C3ll be & I I 0 lij !l&Stled ..nu-t damaze op 10 301' rpm. 1bol: switch also opcm the APU irolatiocl vUve:s and doses tbe CIM-

Tbe START ENGD amber caa101 iiabt 011 tbe anavnnator pmd (see r....,.e 1-3) and the ID3Sler CAIJJlON 1igbt (see rll'ft fO...J)a:meoa nacillocr ot tbe two STAJUER ENGAGED (l.JR) 1iJb1$ Joc:uecl 011 tbe iUStet teSI pud il1amiaate

Iftbe START ENG D tiaJt:t tema.ins 011 after tbe stan switcb mums 10 O FF and l.be ENGII\'E START J.icbt is out, the swter datdt ID2J baTe f"ailcd t.odjscopge and the eso,me sllou)d DOt be wrdentcd I! the STAKT ENGD ¥t reaams 08 after tbe eap.e tpa1 Slabiljzrs at Idle(oppc · w•ely 64'1o CIOtt rpm). -n•Dy tfismpge tbe swter by teua:W.C tbe START/AMAD RUN switdlto the olJ (ceatet) pw;.;..,

roameatal IXIIltrOf sys~ea (ECS) isobtiocl •'alves as well as opesoiq tbe SUtter u vahu d:lrilt& Cllzjne s:tart. 1a tbe ENGINE STAKT/A.\lAD RUN sridl bas prionly alllltOI ooe- tbe l!S!!OCOted cupor b1ee:! aaUIIJ vUve:s (a.Jess tbe ESG BL£ED AIR S'lritdliS ill tbe OFF • h tit •t). the STAKT p&ti• ot tbe ENGil'fE START/AMAD RUN mu:ll is selettcd. tbe cqille blee:! u ~ opcso. O+dtidin& tbe """"''~ (WOG) swudL Rder to Eapnc Bleed Air Syst~ this see·

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mame sbutdolrn is

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ENGINE BLEED AIR SWTTCHES

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ENGINE START INDICATOR LIGHT An ENGINE START tw1caw liglt:t Jocatcd OD the t.bnxtle pud oa t1oe ldt awsole (see r~ 1- 3)

e bleed pan. the asqxwred ill the OFF po111ion. eup.e bleed air and APU &Jt c:aJUIO( be SUJlJlUed manllllly ~ automatically r~ aMroc:rmanal CXJDUl!l system fur• •i"*> and.,.. caJ1DOI be Prpplird 10 the eapes r~ swtift&- (Rder 10 Bleed AJz s,-stem, this S-1 IIESIQoO'D CW'-liiDIGIWD ClEMO ll!S'liiiAllQI 5ll.lt"D

NP''1Bl' S8fti'S •RE fn!l Of \'Ill

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II GAJIC

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Ar. ax:BI

MIII!ICS

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OH:IIU5£S IZAOS GAl

'Ol•SES

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1'IMSIUl - ~IUCAt)QO II!ID\'t 1 K - MIEKI* tiMSMD

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.,.. I FIGURE 1-6

1-9

TO 1F-117A- 1 SW1Idl slloa.ld be lldd for at lcasl1X?: blf sccoad 10 emure tbt data is tt:Wided.

ENGJHE BlOW-IN DOOR INDICATOR LIGHTS

Two a.p.e blooHn do« incficauv liahU. L BID and R BID. are loc:aled oo 1be lcfl atarcsJlield qcbipiDd. T1lese tipus aae on 10 iadicate 10 lbe pilot lballbe doors are - fully doled. Tile L BID and R BID J.ipts are a ""':d o-ly wtoee lbe RCS MON SWIIdl c. 1be Gll5ler tes:t pud is ill IKON I"..;.;. • ENGIN~BLEED

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HOTE Wllca au data frames bve beeD atilized. liCIMtioD ol the ENGINE o.ide appOiliiDatdy 1-"' ol the fa-

~ fuel for engine~

FUEL CROSSFEED A atllllfeed valve~ 1loe Jc(t and ripu CDpc feed JBanifokls,allowseithcr, or both~ 10 obwD fuel from either or both feed tanks. The ~ is opened by a sipal C.rom the law fud wamin&

tbenlmlors iR cilhc:r feed Wits or by the FEED SOURCE swiu:ll em llae fod CX!Ilii'OI paod (see F"~t ure 1-8). Ant""""ic: ope:nina ol the aossfeed ~ ca.a be mhib:eed by IIJC d 1loe atllllfeed .vUrde

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FUEL CROSSFEED VALVE OPEN INDICATOR

_..,. -..... -..... ....... ..- t

,.._I ' ~ I•~

................. "Ul-1

~-

I ,..._.-..... - . o

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-.. .....-... .-... ....._.,.-__,. __ - .....-.. .:.j

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FIGURE 1- t

AIR REFUEUNG CONTROLS AND

NOTE

INDICATORS Willi fuel may $bow lUI oo-lold mdir;ujnn ol 100 10 200 poutlds ol Cud wotb FUS ONLY sdeaioe ~air refoelitla-

AIR REF\JEUHG SELECTO R

'The Wu posjojnn (~Al.L-FUS 0!-o"JY/ PULL) air nf r & (AIR) r:' a«. loc:a1cd oa 111e fad mauo1 paad F,.are 1~ oa lloe ldi aiDsole. a.aoh llle apetaUOil olllle ARR ad !be air refoeliA&sigaalaxanmniratjnnump!;roc:r. WbeaiD the C1 OSED l"'sjojoo tbc ref~ ruepcl!de is stoWed aad all Ji&IIIS ate ofi. \\'bell llle pilol sdcc:ls the AU. or FUSOI'o'U' post- !lie reflldm&rec:epcadc roc&lCS ad 'lrbca tt.e i 14 k S ,..,. is ill the (lilly opea p osjlicw tbc "'W'optiue icfodwa 5talUS Ji&llts, the ~ bpls, aad llle twO Side and ODe aft-lootmc fixed imeastty refueling flood!iehiS Ql!!De oo automatically. AD adjuslable inteiiSlty APEX flood!ial!l abo is lhea ·~

d (see F'"lple F0-1), pnMdes for manual opcni>)& ol tbe air rdudma I e :e. cdc Pulling lhe T-llandlc tonrds the caner cl tbc cxd:pit ano-s lhe rccepcade 10 be unlocted. Sprir>& pcsswe tllaa ..;n rowe il 10 lhe qx:a poAtirw n.e T4wldlc ..;n mmu 10 the SUIWcd posrrion YDell rd ' ~. lhe Tlludle IS atiliza! after dccUnl udlor ~ pcwu •e ee 1aqet •• 3 'h ud then oa1) after a failwe ollhe 1eflrctizc 1 10 opal after seleaJIIIIhe AIR switcb 10 fUS ONLY or AlL positiDD. If lhe T -bandle is bdd CllUidcd (wttlllrydmulic aDd deruica1 JXl"'U :n'ailable 011 tbc airaaft aDd Wlth the air reflldinz (AIR) swildl srlcacd to the CLOSED p)'ition). lhe reczpcadc will cnct penia1ly opea. tben qde closed. c:ootm-.s!y, prcoauin& the l"'""'q''ade attaiDin& a !uDy opa1 poPiion The mlldin& re ••• k C3JUIOl be doled il it 11as beea c u rdadinz READY blue tipt on lhe ~ wmdsllidd pea comes on wbeD the rdadiDz recq>tadc bas routed to lhe proper positioe to ~lhe Wiker boca oozzle. IJIIhe eoeat that adisnmnen OCOIIJ'Sbf pilot aam•ed 1 ea Wiker boca disa-nen, « ~ sate chr-rrt, lhe U'JOi . . . ril JDOIIl aad tile ••

DISC Jiclll ri!CDDeOD...lbn:tet lheAEI\DY fill''

.r~er pilot disnmnen (NWSIAR DlleoazaZe peddle l'l'!ldl jM 1). lhe -.dl ud press tile ~ SWIIdl apia to re--ill-iea•c lhe READY !aPt (« another rdadiD& booblp wulllhe Wiker. I[a boom or aut~ clisalBnecl occutS, press

me-

tile Jadlfle switdl 0111:e aDd release to re-&IIIDiDatt lhe READY light f« anolhe:r rdodiltc auemp (The READY light -r also be reset b7 qcliD& lhe doot clolcd. tben m'IIOiilla to lhe proper p

lSi••·· )

.....,......... post (see Fiprc F0-1) eo.es ext wtw:a lhe Wlkc:rbooe DOZZJc 1atcbes •10 tile rdadinz rc-

cepcac:tc.lhe READY tipt JDe50UI. udureCad:inz an bqjD. AIR REFUEUNG DISCONNECT UGHT

11>c u rdoc!inz ydlow DISC (.._.nca) Ji&bt oa lhe riz)n Jriedshjr!d pos:t (sec Feaze F0-1) comes .. wlot8 a cl19 1 "C a oa:ms bctweea lhe taD1tt boom aoz:zk _, tile n::fadiDc I " *I" ....

MANUAl OVERRIDE ON SWrTCHUGHT 1bc MAN ORIDE (man!W ooulidt) altemate-ec. lion ON switcbliaht is loc:lted adj8centto the slipway IICbts control on lhe fuel COGtrOI ped(sec F"rgurc 14). lt pooidcs man!W oou1idt c:ootrol ollhe air refueliaz sipla1 Ulptif.cr if the llllpll".cr Wls 'IIbera tbc lir rcftldiDZ srtm« IS Rt lO lhe AlL « fUS 01\'l.Y posrtjne Iflhe READY IJIItl bls toccmcoa after ld tbc AlL« fUS 0!'-'l.Y p Mi•• tbc __.. owen ide switd!IJbN ca be pressed 10 rqaira -oCtile rdoeliri&SW11S tipts. Opemioa ol tbc r:efoet.c ~will be oor.u cu:qJl thM tile tallkaairaaft c:armol dcc:trically .........,_, lhe rdlldiDz booaL The O N light aJmCS on wbeD the swiachlight Is pressed to incfica te that orc:rridc has beea srlcaed.

u1"

ENERGEHCY AIR REFUEL T - HANDLE

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Rdcr to Exterior LiiJus, APEX Rdoclilt& Lip:r. this socc:tion, for APEX ~t Control cfisr:nssjne

FUEL SYSTEM MISCELLANEOUS CONTROLS AND INDICATORS EHGJH£ AND APU FUEL CUTOFF

SWITCHUGKTS Tbc APU roc~ ...m and the kft aDd rleht eap.e rue~ valves are slim all bJ pra:sin& lhe UR EXG PUSH, or APU PUSH ...-i1diligbts whic:ll are loc:lted . . the ta:SU\IftiCftt paDd -'jaceot 10 the FIRE wanting li&hl$. Narmally, tllese soritcllblbts are used 10 shut all fuel Dow aDd bleed air 10 an enpe. or Cud flow to tbc APU 10 lhe ~ a ~ oc:curs. Whel lhe FIRE !.ipt comes oa.lhe UR EXG PUSH, or APU PUSH bpts also caac . . to rndic:atc wbcre the fire • - = 4 Wbultlle pilot presses tbc swnmfiaht tile O.'lll&J>t will caac 011 ..S tbc a• Wed '03lfts wi1 dose ...., raaaiD ex-~ ""til tbc swnr!rr~t is ... cw:d ..., aDd the '¥3lves opaL If lhe ~ ClliJ>. plSbes aDd the ()VI!Jbe:ai mnc!rt. . no 1o1tacr CIISl5, the FIRE l.ipll aDd UR ENG PUSH.« AP'll PUSH h&Jits will tp all. Rder to F'"tre Wanwl&IDeuaioo Sysaem. thiS sec:tion, fO£ addlbOCial tnformatioo. NOTE

Doc 10 lhe dose prtlli!lllly cl the APU PUSH ..S R ENG PUSH sontr!olipiS, cllcd"for uw:rect sa 2 s-et- ..... to tEJIIDI wnll the a-taster "Rst Panel

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FUR. OUAH1TTY INDICATOR A fud quantity indicator(see ficute 1-10). placarded FUEL QUA.'"TITY,IS located ora lhe npu side of lhe Cftter illstrameDt paDd. A similar mdjraoor, ~ cated m the right maia wbt:dwcll, IS IISCd duria& pvuud foelmg. 1bW fuel quutily iD pounds iS illdicatcd a.1111110US!y by lhe pae a.! lhe dipW rcaOOCL ne L(ldl) &lid R{..pt) qilaJ teacfocts irodicate !be pounds ol fud .....,.mq m the lank mdi:ated by p6i1MWI!Q@lhe fn~(FUSTUJ: WING. FEED. FWO XFR. AFTXFR) rowy selet: -:;-

tor. Tbe BINGO SET tDob is IISCd by lhe pilol10 Mljusl !lie 1"6it ilw ollhe triaJJ&olu BINGO llldez a. the fuel qu:u>btypge. When llleflld mumq .-:be$ !lie sdeded •-aloe ol (ud. lhe red BINGO~ lip! aaes ora.

1lle volame olfud m eadl fad tan1t is ._mon=dby fuel~ smsors•iudl send Slpl!ls 10 !lie fudquanbl)' pOGLW aniL Tbe fud qauwy pwfir:ator S)~ lela can be dM:cted by premq aad lllllclm& the buillIll-test (Bri) s..-tldi. The cage &lid the dicJtal P•\ * IS &re uac:isa! iDa Rq'IH e t lest. T'be cipW ud -toe •• •· s wil 10 =o. Ailee reacl!in& zero, left ud right fuelqts311lityclisjAa]s ril ~ from am. uoo. 2200, 3300 c:ontinW.C 10 91JW.IXXO ud TOTAL LBS mdin!!or will seqoaoce rna IBID. 22201. 21ue ol!Xro ora lhe left and ,.Jlt fud quantity mdicurn &lid oo the 1Dial quantily indicator. The aMJoc poioller will ClOiatst''OG) swisda ialerloct. AUAD UNCOUPLE SWITCHES

Two parded A.\.IAO lll"COUPLE sorild>e5. 011e for cacb eagjDelAMAD. ate located 011 eitbersille ctllhe lbroule qtradnn! 011 the tbroule pand on the left console (see F'~ 1-1 1). The swildles an: gu:arded 10 !be NORM posiaion iWsul& tbe prd aDd poD.__, the S'lrildl forward will cause the A.' JAD 1.0 n+"*'l*" from the cupx; lw>wcua. the AMAD 5llooold 1101 be n• • ••pled aatiii'OWJOII rlabe ~ 11as c1tu •10 abe Jooooest pcin& p WCi a:el'l- soan:es lor a.iraaft s,sums "'!"?rire DvriD& abe APU SWt qdc. pe.wnaed a>£ front lhe ~ IVc Scatt System (PASS) is meted 10 the APU ur -.e ~ (AVS). Wilb abe APU opera!iq. air is rn.ilallle lor EPU opcmion, aircraft =&iDe Sl3tt, aad envirorunerual c:onttol System (ECS) air coaditionina rcquiremen!S{see F'II!Jre F0-2). In odditloa 10 =&iDe bleed air aad APU tt snpplies, d eq• 4 co• allliiDJ if mjQIRd. Separate CXllltTOis oo the ECS panel an: available 10sllut olf either llle lclft « ,..,, eap.e bleed . . and the aire swt. The enzme START/A.">iAD RUN saitches (wben seleaed 10 S1JYU) hm: priority CXIIIUOI and wil ope• the ~ bleed a •"ah-cs, ~ the weigh~~ (WOG) i1rildL

LEFT AND RIGHT DUCT OVERHEAT UGHTS

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T...., left and n&ftt daa ~ red wamin1 lights, plac:arded UR DUCTOVHTare located on the ECS ~J (see FlflUCl-12). Tbacli&Jltsmmeoowbe:n.....,. a ,. .pcrarure CODCitioa ...,., 3to•F (400" F ~a

1-22

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tbe atpAe beys). caused by a ~ leak. IS se:nscd A leak iD the riPt or left manafold ben een the enpte and the 1espean-e isolation valve trill iDuminate the associated DUCT OVHT JcbL A leak in the a ossbl ' ' :1 mamfold. bel'ftell llac i>olation •"ah-cs, Mil triger both lJR DUCT OVHT lipo.. Eap>e bleed air 10 llac af(eacd dloa sllooakl be slntt oii by plac:Uic llac L or R ENGINE BlEED AIR swidl to the OFF pooition; thisdoKs the left or ncht bleed air shutoff \'al\-e, the left or 'llbt aCIISbleed shutOff vah-e, and the left or right APU jsolation val\'e.

alocJ allacr bleed air duct.

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WARHING

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IJiuminalion of either or both UR DUCT OVHT liJhts indx:ales the possibility ol a bleed au leak. Ibis u can be as hoc as 150"F wbida is caplble ol dormP>& cntic:al aircraft " \ - •IS and po~entully c:amm& loss o( llac aaraaft ECS OVERtiEAT UGKT An ECS o.., beat red •-unin& light, placarded ECS the EC:S pa:ld ( - ~

ovm; .. loc:a1cif on

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TO 1F-117A-1SS-1

I

1-12). 11m li:bt Wt the APU which -ny will swt within IS lealllds. If tlte PASS syuem is utibzcd to swt the APU ill fli&ht, tlte PASS boule is aedw&ed ~-

A lt)odntl.lica!J operated APU exhaw door is ;,. sWied 10 ,;vi•ai•e abomt: ~ ol u.e APU. If tlte APU £ails 1D aia1art. the c:xhanu ll,pus door is DOl commanded 1D close and no jncfinta- IS pooided iD the mctpd' bowe>a-, the door can be blown closed by ao::c:deatial& the aircnft at>cwe .wl KCAS 10 ooerpowu the ooer-a:t~ter door sprin&:s. ODce dosed. u.e l!lriDcs will hold tlte door in the closed p +ia i w If tlte APU • u • ed> taaperatcre Jiluils, tlte APU wil shat dowD aauxuatlcally. If tbe EPU bas been aai.ated automamny (both tcnerator> ol1 tbe line). or il the PASS bottle IS redluJiug. the automatic APU sbGidowD feature is mhtiled and the APU .,;n rw1 IMIIil • fa& II Uoe EPU bas been aaivated mant:ally. lllc •mogptjc slnndow1l feature 1 • iD dlect. Aa amber cmtioa bcbt a. tlte annoncialor pud iDdi:ale> APU sbtddcJora.. Ill ac»rww u APU fad al1df (APU, PUSHJO;o.') switdllipu IS localed on the upper riiJlt Cetlltr mstrument panel adjx=t 1D the FIRE onrnD!g liJbL Wbea an APU o-~1 o:aus. the FIRE lizbtlllld tbe APU, PUSH liglll ea.oe oa. PI essiaig tlte swrildl will slm:t dowD the APU. nod foe the APU IS supplaed by the APU boost pump ia the oaJil fad auDOk1. Caatrols foe the APU ~ locued on the EPUIAPU pud on the left a>mole. 'The mctpd battely SWIIdl must be tumed on prior to aueupcing a >b1t fi'OIII cilher the mctpd oe the pound mrmal amUOI panel

APU CONTROLS AND INDICATORS APU FUEL SWITCH

The l'tiOpmrion {JuardedOPEN-Cl.SO) APU Fuel SW'ddl located oa the EPUfAPU J*'d oa the left a.ae (see Feon 1-14). QJIUrOis tbe APU slmtoff .aM "' the APU foci SOipply liDe. Wllell the swildl is placed;, the CLSD p•i•i"' tbe mutoli .-aM is dosed and the APU and APU cuapanment are isolated from the APU fuel Sllpply soun:e. The APU sbuldf vah"e is aiJo closed wbeo the APU fllel al1df swrtcblieh' is pressed. APU START SWITCH

1lle twO-p05ibon (ON-OFF) APU sun saitdl. located on the EPU/APU panel on the left CDaSO!e (see Ftpn: 1-14). elearicallyactuateSorshutSdown the APU through the dectronir conUOI WUI (ECU) ol u.e APU. wen: tbe -.c~o aplaced•tlte O.'~.pclli. tia.. tlte ECU allow$ the 1*e5SUi iz.ed air SWt syuem

1-23

TO 1F-117A-1

EPU/ APU CONTROLS AND INDICATORS NIUICwtiiPA.'n

•

AGUR£ 1-1 4

(PASS) 10apply air10 the APU Slart motor and sdledules proper fuel and ignirioo seqo.eocillg 10 Sl3rt the APU. Wbal the switcb is placed 10 the OFF position. the ECU ans oii fuel10 the APU and the APU sbuts dl)oo.~ If the APU sun switcb in the ldt main -.bed wdl bas beea otiliml 10 Sial! the APU. sbotdoto-o contrOl d the APU cu be uansferrccl 10 the CXldqlil by placing the CXldqlil panel APU Slart switcb 10 the 0~ J" osj• w., prior 10 sdeaio& the OFF p osj!OMI d the APU sun s-"iu:b in the left main -..bed -n. The APU switcb is magoeU:ally bdd in the ON J""'i'jon and will autaNnially mum 10 the OFF posit jon if the APU flames out or fails 10 stan. APU OFF CA11T10H UGKT All APU OFF amber cautjon fi&bt Joc:ated"" the annllDCiata- panel oa the lower right instrument panel comes on ~the APU is DOt runnill&- Noocbtt iftdkatjon of APU operation is P""ided. The cautjon iWU is disabled if the APU fod Striu:h is dosed.

APU FIRE WARNING DETECTION SYSTEM

-

TbIdl &Dd c- 1tydraDiic presane ~ "The t.n.e!nc pre5SIIre .-..itdl opalS as the ailtr.!ft diiDbs tllrouJil 11,an rea liDII close> as the aircraft dua:ods lhroup JS.(O) feet. loci:iaa out the auxiliary~­ tor cm1ess the bydtaulic pressure switches >ease tlw dlher cape fliJitt bydralilic pump is produc::lq suf. liOeat poorer.

wm

11oe EPU c:an be ased OD the poaDd to mpply eka.rical poorer or~~~ 1lyca the c:maJCDCy pump is ope:miq.

s-a

EPU AUXIUARY GENERATOR SWJTCH

• .., • wily sdeacd to the TEST poetjon the APU MODE SEQ Ji&bt C01DC$ Oft for approoamatc1y S510C· .-is wbilc tbe APU shifts modes due 10 added EPU load.

HYORAUUC SYSTEMS H)dqlllic powu- is supplied"' two separate syst~ The i*W1 Utiliry H)drcJie System ud the pr:imaoy Fbpl tfJdmllic s,stem are cadi cli>1dcd i:to- oadary~RYD A. lfllLR\l'I'D't-8, Fl.T HYD A, and fl.T HYD 8). Rn MJir IC'rd • • & • empo,ed iD cacll system for the p'dops, a valve seasn the i=:hou IC'f'd dtucasitiJand sllutsoll R> O'*"'YSJStcm A ol the affeetcd Utility or fli&hl hydraulic sys-

"idiioaeaoJeACY~po-uuddearicaiJIO'I'­ tt [I'(D tk mdia.ry g"e and tbe EPU will .ac run iA tbe ttst mode.

EMERGENCY HYDRAUUC SYSTEM

v.ru doe APU npeatin& the EPU eaa pnJO'itk esacr&C'CY b)dd liltll musr be unad all marually ,.,_,lan"en with bolh en3fne teneratOn inoperatiYe if the utilily bydtaulic system is in operation and the amilia!y (AUX GEN) elearical power is being sopptied by the APUIEPU (both ac and de power are required). The bol bntel)' bas supplies elearical power for aoti-5l:id aaioD w'beD the EMER BRAKE PWR is selected. NOTE

The antHDI system (c:a:ept locl:ed wbc:d toae:bdownprotectioo)rilopenteincon· jrmctioo with the eme.geocy bake system Dllless il is deacli\ated (Anli-&id switcb - OFF).

•

'

TO 1F-117A-1

ELECTRICAL POWER SUPPLY SYSTEM Tbc dearicl1 powa- supply S)Slea . , _ . ol two maiD ac ~ u amiliuy ac ~ two ~&tid a benay. E:aawal clooaricaJ P""'tt can be appliCII oo the !JOOIDd lluoolp a plug-in recepcade ID the IIOSeWbed wdJ.

AC ELECTRICAL SYSTEM T-ac~a«lhe ......ysowceoldtnriral

powa- (see F"care R>-3). Eadt JeKdl« is • "'""'' ol suppor1mlthe toW det:n ical ad.

AC ELECTRICAL SYSTEM CONTROLS AND INDICATORS Tbc fW0-90111J011 (ON-OFF} ~ swircbeo. placarded GEN L a:od R. are oo 1k do ••i:ao! aJ11U01 paDd (see F"ocare 1-20) oo the rip!_.. Datilt3 . . - I operauans. t1oese two swUIIes are left in the ON pos:itJOn. ~ aJIIbtt cautioa !ljpts (lJR GEN) a« located oo the amnmc:it.t« paDd 10 indicate a failure of the appqwiate ~Min~­ Wbca aeoentor fails. the Olllu cena&t« auU>mariraDy pds ap lhe toW lood.

'*'

DC ELECTRICAL SYST£M

t-

Main de eledncaJ powa- is supplied by x-w-dc CDDVerteR. 8otb cnmeners supply de pG'Ii'e< to the left and ri&)lt main de buses, the left and o&Jat esseotial buses, &tid tile batter)' bas (see F"!CUfe FO-3).

DUAL LEAD AaD BAil E1lfES

Tbc DaaJ Lead Acid 8aneJy l!tSU"a!- (Sc:mce BulleUD N-Z777 IIISI3IIed). pO>ides iooacased pl

OOIC.\1011 UQil'S

lO IAI.U lli!IICAitll IST SW1101 II UfTNII RIQ!Ja!EIAJilii!Al1T llCIICAIO!IS

&

ll UfT IJttJ i i Q ! J - Cllll:tiClllR fA...'U l!lniCAIO!IS IJ

1a OEIEC10I TEST UGomt lllSU1UDents. CllllUCII paads. aDd other lipl.iDs ""hponmts. suewdli>ts adjusl· able controls for lllllintcaoce use are poflded. lllaeadjasuDc:Dt CODtrolsare located on !he left aDd Iicht rear bnlthe*! ol the mctpd

•

RIGHT SlOE PAH£1.

COCKPfT LIGHTS CUTOUT SWITCH

A S"Oilldl 011 me ldt tlltottk pip C

•

•

o.:.•- I

~l~ =''~' ln.

(c~,

IGf

--.a

~-"""'

i \ ~ e.:3~~

B

~

-·o·fi ~~ n ~

a ')

FIGURE 1-·23

SET wtrite switdilight adjacent 10 lhe panel Other lipl.sOG lhe pa.aehrill remain 011 until !he indiea•ed fanh llasbeal rorreaed. Each ollhe i.ndividmJ anomriuor pu>d liJb.IS is desctibed illlhe applirabl-. SJSlCill desu iptiuu. The anniiJicialorpu>d lipiSare powued 1J!Y lhe essential de bClS.

ANNUNCIATOR •RESET SWITCHUGKT

The annanciauw •RESET white S'lriui!li&ht, located adjanmt to lhe annn•rinnr panel illlhe lower ri8Jit insltumenl panel is used 10 reset (for a 51iJscquent alert) only lhose lqeDd lipiS "" lhe annunciator pu>e1 lhaJ are preceded IJ!Y lhe S)Tllbol • _ If "no). san::e· fauliS occur and no "bani'" failures are preseDt. "SNGL FCS and • ADC ligb.IScan be reset 011 lhe ~ as well as iD lhe air, bowe-. lhe "HYD, "ECS.and "IR AOTcanlioo lightscatUIO(be rese1 oo lhe ~ wi1b wei&Jlt-G>-'Id Ji&bts (wilhocn asluists) will always remaiD Ji&bted until !he indicated fanh has beal corn:aed..

ill&. cautioa, and ach>isOiy fi8111S.

The ....Ucb is 001 fnnctMloal anless lhe INST ligln switch is on and lhe sronn fi8111Sareo1J(FLOODISTORM fi8llt51 I IIOO eeable fins (see FigUre 1-216). Si:a: inlqxated dual scn'OaauaIOIS power l.be SUifaccs; ooe for eacb devou seaiou

andoaeforeacblio.. Utilitylf)ldraulicsa:udalysystem 8, and fli&bt Hydraulic d for~ Tbe word AI:RSPEED is repeated continuously and at ran rtllume (not acljuslable) as long as lhe aircraft rauaiDs below lhis speed. Tbe low ainpecd a.len is inbilited 'OOilh weipl 011 wheels. The MEA ''Oioe alert is present wileD lhe aircraft de~below! minimum altitude determined clnring llli$5IOil planning and progtammed into lhe compeller with bas mntrol, oormally lhe W- WSC Yia lhe EDTM, or manually keyed iD 0111he CDU ke)b:ran1. The minimum esuoute altitude must be propammcd for each l, """'eou, altar the dc:ice ODid pump energizes, pt esswe is built ap and ODid flows tlutlugb ODid shutoff vaiYes to the grid. The va!Yesopea oolywbeo the •espectite ~ is s•t:Cjliq. Wben lhe 'll'ipersare in lhe srowed posilioa be1•etJI sweeps. lhe vaNes dose. Jn>-enting ODidlosstluougbthe~manifold. Wltalewerthe

Wlper operation

caJJy as soon as the airaa£1 becomes aiibome. "The A and C prabe beaters are ptTNetopy dc!O!,Sing is 1101 a\'3ilable wbeo INLET GRID DEICER CONTROLS the ECS mode seJee:tor is set to ALL RAM.)

AND INDICATORS

DEFOG HOT UGHT

ENGINE INLET WIPER swrrCH "The ENG INLET WIPER switdl is loca!ed oo theantH:eldc:ice panel oo the rigbt side panel (see F'l'lf'C J-~ WbeD the switdl is placed in the WIPER positioo. operalioa of the left and right eogine inlet grid IJI"dpniral wipers are initiated In lhe WIPER & FL position the switdl activates the wipers and the a1mbo1 deicing DDid did•t!IJdc are bolh ~ ihea1be piU: uses the $1itt bJ am the aiauaft; but the S"!Oilc:bes are not turned 10 the O FF posi1ion Af.

1-S3

-

TO 1F-117A-1 ter CIOIIlrOI stict SleeriD&. man 10 t1oese modes is.,. '"""""'.......,by lhe pilot 1M "'I tloe auiOpiloc rdercnce cnP&f! switd> 011 lbe cooii'OI Sl.ict.

Iori& IS lbe amopiloc is ~ tloe ainraft is maonta!IM:d at pi1cb aDd bent uaJCS c:allcd lhe rdttcnce pildl ud bllllk (see F"!pte 1-31). These angles ue~frooalheattnaded lbeairaaftalbe ~..e t1w t1oe pilot CJii&4!CS lhe aUIOpiloc. IS l'd1ooos: • If tloe iailia1 bent . . . cqmliO (W less JU

OWI~rderacetant(remn)"ugle15

o•

ud 1 s.,, 1aold • aU'cwatjr;tJJy caaqec1 This is tbc beSIC auiOpiloc IIIOde. Boc.b anttade aDd beadin& are mainlaiaed. • U lbe initial t.nt aDak is between J• aDd 10•. lbe baDl: aqle eriaina at ~ is maizlw-1 by tbc auiOpilot. Headin& is aotbdd.

• u tloe iiWalballk . . .. e f t lhu J08,1be

CONTROL STICK STEERING lateral Sl.ict; mc:M:mlUI

,__.

I€A!l"' lH.D

I FIGURE 1-31

Coauol stick stccrioz ooeuidei llaas CXJaUOI axle and causes lbe AlP mcH li&IJtl.o aae on Ready. The altilude hold or Madl bold tDOde remains selecU4 ben is 110 1oazcr ~ The aluradelll:lacb bold SW11da remains ;, lbe sekaed poRtion duriD& a.uolllidt saeerin& as looo& as lbat ~does not !' Pte lk at!lq:lilnl Wbea CXlDllOI stick steeririJ ifdi5caat;;..u..t 1be AlP PITCH li&IJt • em. aDd lbe aiiiOpilol reon::ns ~.oauirode lldd. Pt • eu.e... lopilot rdere:acr ~ SWIIO 0C1 lbe aJDtrol stick ..... u.ea reeapJeS lbe sdeaed coauol dQie aDd 111n1S olf lbe NP PITCH lipL Moo1q lbe A!TMACH hold sridll.o lbe OFF P""'- ' lip 'Mlllt:m; lbe axle and 1be AlP PITCH blbtllasbes. Tbeflasbq IJ&bt is turned oil by pt essina lbe 1iaJat- Autopilot cliseApceme< lor ury reuoo returns lhe AlTMACH hold SW11da 10 1be OFF J1011101. and tmnsoo tile AlP DISC fialtt Ready. Tbe alurude bold and Mxllloold modc:s reqorire a .ucldaaete lroaa tile air dma coaopater. Tbe Madl hold axle is Otba-trise,.. -.oral. Tlle altitode hold axle "' 'PCJ!Iirored by _ _ _ cbon • dRone! se:1ca swa is • t11e DUAL poRtjae Eiltle:r ..,deriatiatlialk~

1-56

a ~ bdweea lbe rwo data IOUJces, or a Wltn cl OCie cl tJacse SOWeti detected by lbe tz10Gi.. tor, dtseapces 111e altitude bold ~ llasbes 111e AlP PITCH Iicht. and returns lbe ALT-MACH bold SWIIdlto 1be OFF pusitit.,

NOTE

I

TO 1F-117A- 1 When !be clwmd sdea swiu:h is in !be CH I ..- CH

2 posi•inn !be altitude .-leis nnmonitoml. bot a Jossollbe a.r data ipl'ioe IIDid mode~ ill&. tbe navipiDt ldd switdl miiDiillc 10 the OFF poP'-. aad the AlP ROLL lipt fb.!rin& The AlP ROLL li&Ju is t1lrDed olfbypoa~U~~ tbe li&I>L Failure ol boO JSSJ data basses beJ Weest tbe autopilol and tile a•pmer alllttOilin& st~ """"Ancls or fail. are ollbe somee mot!p"er ilsdl'alsD ends UV1ptiaa bold mode. and relllnl5 tbe .......... bold S'II1Ida 10 lbe OFF posiliaR. Bas or N-WSC computer Cailure is identified 011 lbe 51atus display, bot DOt the associated 5 .,.. eal ol ~ bold mode. lboe

amopilol i s - d

"

la&ed-

Tile twO-j)OQUIJil (NAV-()FF) Nav Hold s-ildo is.

cated 011 tbe auwpilot mntrol pud (sre rmgwe 1- 30). w.e. set to tbe NAV pl"ition !be aD'opiloc I I 51" w!s 10 IJal1t angie SlCaia&' ' Is fna tile w~ S}1lem Coalpater (N-~ The Nav Hold (NAV) SWtldl will mom to !be OFF posit..~'er tbe auwpilot IS mea,~ lt is used 10 cause tile auwpilot 10 1upood 10 SlectlDJ cgmm3nds tile N-WSC whea dcs!jparioe steeriRt, a.ne bDe stecilot is operatiiiJ in dual cban4d or dwmd ttro mode, and !he AHRS validity apaJ islosL 6. The autopilot is opentiq Ill dual dwu:ld mode and llle axapuatorS delea a sipirtC3Jit cliffermce bd•eeo tbc ttro data

•

TO 1F- 117A-1

&. Tberc is a lass ol power 10 lbc outnpi!o« 9. Tberc IS UJY powu ttaDSiefttiO lbc autopilot .... allows deancally bdd swildaes 10 ~ lllnl 10 1bc

bas a fued scale ud a IDOOillc poioter &l'ld IS placllided ANGLE OF ATTACK. The scale is cali)rated -10• 10 20• in ioa-ts.

rn.

z•

OFF p.;,;.

BETA INDICATOR Al1TOP1LOT SlHGLE-cHANNEl. UGKT (see Ffllltt J-:Jl) c. lite --=ia&or pud, p.c. arded AlP SNGL CR. CODeS oa 'llilmlbe aatqlilx IS~ &l'ld t!ieCH I::O~sdc:i:t swi:dl IS oot ill lbe DUAL poUboo.

The beta indicator (see Ftgme 1-32). on the main inSliowut paDd.mnpqsof a fixed scale witb a~ poiater ud is placarded BETA L. R. The sale is aJin.led fnD o- 10 16" ldt ud riglll ill iDaeAklllS: Tbepoiater , _ ldtor rich* rrdjcatinc oose depees ol yaw.

FUGHT INSTRUMENTS

AIRSPEED INDICATOR (STANDBY)

n.e autOpilot ~ pea ..,.,"isory liP!

N a bllct-ap 10 lbc cathode ray lllbe (CIO')dispays oa the center illstrumeat paDd. a - ol CXJII\'elltioul dean w ' · •I f1cht iasuumeBis is jXOWidcci wlUdl iDdade aa ADl, aa HSI.. u ah · u:r, u aarspccd jecficator. aDd a -u:aJ •c:Joc:4) jryljcator, • tuc:b are poapc::d JDCe!beroa lbc left Ddeol tile msuument p&lld in lbc md:pit AOA aad BETA (Ddesl.ip) jncficaton are locaUd oa either Side ol tile~ [tQGl CDlUOI pud (UFCP) locaud iallte 1!ppCrccater iiiStrwWllt puw:l. A radualtiaaeler, Utude incfieotor, aDd ~ iadicato£ &emisphere ., wtuda llle ain:raft is MAGNETlC VARIAT10N SWTTCli

AHRS CONTROLS AND INDICATORS SYNCHRONIZAT10N INDICATOR METER "Tloe sttdu : ·

ar;.. iec!icuor (SYN lND) meter is a

WJGC:U::C: l:l!lft'...S&e

fi atei)'"'

""'jrujgnof

AHRS lleadia& with tile MAD rdc:n::ace sipaL

The magne'5lem by p1XIild JlU"90"nd Oae bandle is located ilia I E~ pmd 011 tbe Jdi side ol the fasdqe below tl!c ax:li:pit siD and aDOther is located llllder aA addir_,l pud oa tile lowu left side ol the f I •t:eo •tp fi'IIO tbe forward alae ol ~left wabeel door

c...,DOl be.

.....

to poaiOd pcnoa.nd iltl!c

WEAPONS DELIVERY SYSTEMS Rdu 10 Amilia.ry Eqoipouu.. Section IV and 10 the F-117A Utility Mlm>oc:leac Weapon$ DdNe!y !>fan. aal. (()I" ClOI!tpltte informa•ion CODCelllml the weap-

A _ , . ) aant baa:!le is IIOcated 0111 tbe riPt side pue1 • tbe coctpit (see Fcare J-43). ud cu be used 10 opes oc dose tl!c CIDOI'1 il case ol c:anopy dearical circail failure. A barled collar 011 the lludle is Jp:iat-" eded ud lias a detUII roc !.be opal and stoore1 positions. This c::o11at miiSI be polled 001 10 allow the lwldle 10 cball&e poQtious. ApproDmatdy 322 turns ol the lw>dle are reqwred 10 fully opal 01" dose tbe c:aDOp)'.

A bud aut. located benea•h u eaemaJ access pad 0111 the foratd ol ~ ftt1 below ~c:aaopysiD .....,,IOtl!c extc:mal c:uopyswirda. c:a be used by poaad pcnognd 10 opuo 01" dose tbe canopy ..,aally (see F'opre 1-'3). I

r:e

EMERGENCY CANOPY SYSTEM INnRNAL J ETTISON A CIDOp115Cal T -J.arwfle, loca1ed 0111 ~ ldt crmn!c (see Fcare 1-43) !XOu on the right comer of the regulator panel, controls the flow of OIIL)'gell from the regulaior. In ON posit jan the proper mix ol coctpit air and oxyzeu is Sllpplied 10 the mask. In OFF pll5it.iun. breathing is not possible with tbe mast on.

DIU1TER LEVER

or

WEAPONS SAY DOOR GROIJHD CONTROL SWJTCH (COCKPIT MASTER TEST PANEL)

A hiO posit jan diluter Je.u. ill the center the rqulalor, COIItrois tbe mirture ol air and OIXyiCtL In !'ORMALp &1 i•~ thucneduled mirtur-eor air and oggeu is ddiva-ed. In ~ OXYGEN position,

pore Ol)'gCD is delh-en:d. BIIERGENCY LEVER

-

The tJu-ee..positiu (OPEN-OFF-CI.S}. gaarded wcapuu.; bay door poa:nd cootrol (GND COl\TOR) soritdl Oil the masltt lest panel in the left side pand (see FlgW"e 1-45) prorides for coctpit COIItrol ol the weapuo.s baydoor:s wbile tbe airaaft is Oil tbe 8fOIIDd (....,jgbt-o-pr~ The soriu:h is enabled wbc:n tbe LOAD soriu:h on the DC!I5C'Iri>ed wdJ weapons Jood. u.. - - ' (W1..P) is iD tbe OPERATE .....-....,.;,;.., -.. . - WbcD tbecoctpit 8fOIIDdcooUOI swiu:ll isselcaed 10 OPEN. both weapoo bay doors 'llill open to the 9(k!egree positjnn in the inching (slow speed) .-!e. WbcD tbe coctpit 8fOIIDd cootrol switch is so:· lcaed 10 close (Cl.S). any uapcze that is extended _ reuaa and both doors clase.

.nn

1-74

.nn

•

A tJu-ee..positiu emergency le.--er is on the lower left CXIIDtt ol the regulator paneL In NORMAL posi· licm, normal opcratjnn ispttl'ided. In B IERGEN· CY position, COIItinuous positive pressme oxygen is delivered to the mast. In TEST MASK position. positive OIIL)'gell p1 essw e is Sl!Jllllicd. OXYGEN A..OW INDICATOR

The oxyzeu Dow indicator (FLOW) on the rqulalot altematelysbows..-biteforflowaodblactforno-Oow

with car:b breath under oormaJ CXlllditiuos. Continuoas ~ indicate--sT'R aad p ... . t tbe PUSH-TO-

'*

ne

TEST swildL indo10r pointtt ma1es 10 display aaual OX}' pquwil:y-;andtbe OXY WW f®Ugoes~ tbe llldicaur pJBI1er ..,.u upscale past O.S Iller.

1-77

-

TO 1F-117A- 1

EJECTION SEAT SYSTEM (ACES II)

-

The ACES 0 ejeaion seat (see Frg.ure 1-48} is a !ally automatic catapUlt roctet SJstem.. Three qeam modes are autOmatically selected (see FJ~Ure 1-48). Mode I is a low speed mode~ w!Ucb the para· chute is ~'eel almosl i:mmalialdyafter the seat departs the aircraft; M~ 2 is a bigb speed modcdur· ec:hme iHirsi~Ue­ seat, followed by the clq:>loymau d. the pa.racbute; M~ 3 is a bigb altitade DIOde in w!Ucb the sequence d. events is the same as DIOde 2 excqK tbat '""" seat separatiM and c1q:>1oymau d. the puadlute is delayed until a safe altitade is reached. Ca>trols are l*,.ided 10 adjust seat bei&bt and loct the sbooldtt harness. The ejeaion seat S)'Slent is designed 10 provide emerrezq egress from the ainnft at any altitade or speed iDdudin& Zl!rO altitadeand zero forward veloc· ily. Refer 10 Seaioo Three for informatioo 011 seat pedtlnMnce The only aaion required is 10 poD eitberol.the rwoejeaion bandies or the canopy/ seat Tband!e 10 the full uavd e:acmioo 10iniUale the automatic ba.ilout sequence.

EJECTION SEAT NORMAL GROUND EGRESS Ric normal ground egress and~ from the ejeaion seat the pilot must dismn,... the paradime riser, the surriv.!l tit rdease lint med!anjsnK and the lap bdt (see Frg.ure 1-48).

EJECTION SEAT SAFETY DEVICES The ejeaion seat safety deftocs are shown in F.gure 1-48. EMERGBICY OXYGEN SUPPLY An emagcucy oxygeo Sllpply is Qllltained in a ()'lin· der asq ... . , located 011 the ld"t side d. the ejeaioo seat bad< Sll1IClUre. 1'beoxygeo bose is routed 10 the con,...or 011 the tono bamess. The system is actuated au•nm•uicaDyclu.t'iqan ejo ti•• by a lanyard anchored 10 the coctpit suuctiiJe. lD addjrioa, the oxyl"' can be -a in a adpit emergmcy by polling 011 a emergency oxygeo ring located 011 the left side d. the seat buctet (sec F.gure 1-48). A pressure pae-lkcyliiiQuis silwled IO.pa'l'lit ~loring

sreeu

d. oxygeo pressure.

1- 78

EJECTION SEAT CONTROLS AND INDICATORS Tbe ACES o primal)' ejo ti •• seat controls and indicatooS are shown in Frg.ure 1-48. EJECTION CONTROl HANDLES There are rwo ejeaion control baDdies.~ mounted oo eactt fonraro upper side o1. the seat. The Qllltrols are.interconnected ~that aaualioo ol eith«_control in.itiates eju •i•a The ejo •i•a control pull is w•uinwrely 4.S poands.

roroe

EJECTION CONTROLS SAFETY LEVER Tbe ejection controls safety leva- is located immedialdy aft 011 the left ejeaiuo O)ntroi baDdle. Wtth the safety (e.er rowed up and forward boch ejeaioa con· tro1 bandies are med!anicai'Jiocted, and a yellow md blact c:llect;Clbaud placald is displa)-ed 10 the seat ocrnpant readin& EJEcnON CO~OLS LOCKED. Wtth the safety leva- rotated aft and doro. the ejeaioo O)ntroi handles are nnJocted and a blact and wftite placanl isdisplajed reading EJEC· TION CONTROLS ARMED. S'HOULDER HARNESS INERTlA REEL

l'ilol sboulcl« harness resaaint is prtJ'"ided by a dual SllOp sboulcl« harness inertia n:d mocmted in the seal below the headn:sl pads. Automatic locting d. the inertia n:d oa:ms .men the red semes excessn-e rate d. suap pa)'OOL Manuallocting and unlocting d. the red is COIUlOiled by the sboolder harness loci:/ unloct bandle. SHOULDER HARNESS LOCI(JIJNLOCK HANDLE Tbe inettia n:d control bandle on the left arm rest oltheseat is~ and has two positions: • LOCKED - The inertia red !X""-eats the reel SliiiJl5 from IJeiD& e:aended, md ratcbers any s1act in the suaps bact intO the reeL This pn:o-ents the pilot from leaning forward 'lrithoo1 first unlocting the red. • Uh'LOCKED- The red allows the pilot to lean forward Tbe inertia portioo ol the n:d will aotomatically loct the n:d when it

0oce the red has locted automatically, the locted condition ma5l be released by cycling the cootrol (e.er 10 lod:ed and bact to unlocted.

sense5 t II es I. P a CDUIIrl ua thc frnat oC the seat pan. n.c sd "" is a rocter sw1tch. When tbe left arm (as __.s by the seat ocaopant) is pressed. MAN is selected. When thc Jiclu arm is pCS5Cd. AlJTO is selected. Io MAN posirinn the tadio beaala willaatVateat • seaurpno•inp Io AlJTOpnsitjnn thc radio beaa>n liCliY8le5 at e;a sea• P'p'mim

CAHOPY/SEAT AlTERHATE E.JECT10N T- HANOlE A c:aaopy/scat T -baDdle (labeled CANOPY SE.tcr). located oa tbe ldt .....,...(see F~ F0-1 ud F~g­ tue I ...C) it tbe mct:po pooi:lts tbe pib wi1b the apob"ily oCbed:-op seal ej< IH"' i( tbe .,.-.y sysICIII fails. Wbeu thc T ~e is puDed stmpt "Po thec:aaopywil jetnm Tbe T-lwldle reqt1li'CS an appnwimare U 10 1>-plwld pull for the rllSI threeei&bts iDcb o( tr.avd 10 take up slad: present in thc liMs. II theD teql1iles a~ paD o-cr one indl o( ua-.-d toaamte thc caDDpJ jettisoa illliator. thc T-lwldle is mmed 91)- QlOAtM:Iooc:biK after tile c:a.DOpy is jet I jq •rl -.l palled up fanber, seat ejectioa will OCDII-"The pull toaamte seat qcaioa is also app0i>iU111ely a S0-1)0IIIId pull aCft oC ttaYeL N. tbe lRipletjnn oC the seat aauatjnn ll'avel. the T -llandle isdisr::onnec:ted tn.a !be aircn!t so lint the pilol·s baDd ril - be IAJUI'ed if tbe T-llaadle is -

u

re'

r 'as eju ••• oc:nau.

BATTERY INDICATOR

The t.nay iftdicator IS located on tbe ri&Jlt side oC tbe seat aboo-e thc resuauu rdease reRt lmob (see

Frcure

1~

A nile bmay coodnioa mdic:ates

tllat the bm:tay is opaatioa:IL A ted a-dniop indicates tllat thc bm:tay IS e 'P' r•irc! and must be rep!Ked. U-teplwed, theseqac:aca is •••• rat~e aad ao se:alhuD sepanuon wil oa::u.r upon ejection.

1-79

TO 1F-117A-1

ACES II EJECTION SEAT

YIIW

8

... c

IKAAa gti!IJ ... E

I GRWIID MUIIlii\NICE PI!\ asstMCIY

1 E.Kl10I SLU

SNDYI!ml

3

RGURE 1-48 (Sheet 1 of%)

1-80

TO 1F-117A-1

EJECTION SEAT MODES OF OPERATION

_ , _ ,I --.... .. ... ...

(V'Oil..a..... SfCOUKl

l

,....,.,_,__

MODE I OPERATION

(j) @ @

0 0

as (!)

_.........,,_

------

I

'""""""""

......

I

o.u

... .. ..L. ... u

Ul

---~,.. !Dl SO:E!..m~..,

... t.U

Ul

~

~

u

~~~~

_...._____

u

~ - ~ .-.-~- )

"-'_.__,_ ... u ..-..,

.......

;.&-----~.._,

®\

~it; MODE 2

..

OP~IATION

®

~

;-

..

~

•

i

!f •

••

-· I

-·

- --.. -

"'

"""""

MODE 3 OPEIATION

- FJGIIBE.l ., (sa-t.t ot 2)._ - - -- - - - - - - - - - - - - -

1-81/ (1-82 Blank)

TO 1F-111A-1

SECTION 0 NORMAL PROCEDURES TABLE OF CONTENTS ~ Fer flicltl. ............. ... .. . . 2--1 PI,..,. a-t< ................ . ..... . .... 2- 1 ~~ 1'.-.n) .................... 2-6

W'SCIOCIP EoiPa Sbt6oon ...• ...•. . . . . .. 2- 14 W'SCIOCIP NAV AlERT up. She'.._, .. 2- 15 W'SCIOCIP .utAD flta. ~ Pleadwe . •. 2-16 Stwlioc E i •••••• u~~----2.2--6-6-.~·~\fldAJ+DI)_{C:_... .......,.,fliDIMIQHtliiJI WI"'to< u-uuuoou • •• u•2-17 W'SCIOCIP Sun-Up F.- NAV 2-8 WSC/OCIP SMred R-'lll&•l~ "' .,.... TaD ........ . .............. . . ...... 2-9 2- 17 TaD . .. . . . . • . • • • • . • • • • • . • • • . • • • . . .. . . . . . . 2-LO W'SCIOCIP 11\S Slend ~ A'~ at . • . 2-18 &fOft Tabolr . . . . . . . . . .. . • • . • • . . . .. . • . . • • 2-LO 00 N...--1 Afip-•t .•.......... . ..• . ... . 2- Ul 'JUMir • . • . . . . . . . . • • • • • • • • • • • • • • • • • • • . • . • 2- 10 INS £iPt ~tiJud.o Rdria .•••.••.••• .••....• 2-18 A1Ur TaRe~!' • • • • • • • • • • • • • • • • • • • • • • • . . • • . • 2-11 I.RADS aJOd Semw DUpbJ ~ ....,_u .-_:.... .....~. ., Preadue .•..........•.•.... ..... . .. . 2-18 •.••. . ... . .••.•...••• 11 ·~ D~ • ~ 2 11 Balmy Sun~ ,... _,I rl-GW tS . . . . . . . . . . . . . . . .. . -e-

n.c

1110\'ed

L

I!IC!Il

Form 131 Chected

1-

EXTEIUOR INSPECTlOH

•

E.derior "'•l'•clion procedUres are based oo a:tainteaanc:e pez30Md ~completed aD tedmjral ....,._ aaJi!tlj •i•u~qwrcmcau. Ouriac walbround.,.. sp-a;, the airaalt be dleckcd few ceneraJ oooditjoe loose panels ew f.aslCDCU. dems. teals. esc. Partialbr ancatioo w.111 be pa to

aan

aaas.

&nd.' ljci••ad ,.,.,.._waD a:a~and cdte

1b:fer1DPI&-e'2-t"fura:reasawd be mspeacd c. tile pilot's ~-arowxl ;asprmon m'xnpls

f'ilo( orifices -

Clear

IL P!loc cbuiC salety pia - l nsWlrd, salery - ued L CaD0pJ power clrNc uail ciraBt bre>ker 0!'1 j. Banery mmcnor - ClJed wllite

T

.,.

t.

Restrain~ em~ rdeasc baDdle-

Down.

locted L Lap belts - AttaChed, pms ttposed m. Sum.aJ ~I select SW\U:IIo - As desired IL Radio bcaale 5dca sorilda - J!.s desired

AERP INGRESS (CW GEAR) L Rallcrre and SlOW blower S' SIJIIS!Iji)C+C,.;isi;;;•;suap ;

2- 1

TO 1F-117A-1

•

EXTERIOR I NSPECTlON

@

RIGHT WEAPONS BAY t 2 :S 41 •

@

OCXJ!I $IIFEJY $IIUril$ • ICXH I B O H ) 0! NSr.IU!D Siii'Ca.EAS - OHX H"J'DDIIM.LC NIB CJEilA P W:CM - o-EClt DOQ!I:COC:UOC • OEDt ~ JIIIIIER.CHI'- c:::cMUl'E

®

LDT~BAY

s

OO&:lA SIIII'OY !iifUottS - !IC1'H: IIIIIS«JJI'E)(Il~ -tiCJCII'WLW • o«JC liPCl.E!IIS -OED(

•

l'ft'tJ!W.IJC RJ'B tElA.,. -

1

2

s

'U!IS -

oe:::x

=-

2 ~

@

~~ - CXJrr,jlllt,£T(

FOII'II'AJIO SECllOII 1

• •• s

•

@

..Em50N ACCESS IXXBS IW"4'"WM0!:"'"99'1i -

.:iMI'OH:J/!#f •• ,.,..., .......as CICJOi'i .

QD5B)

C/IIICP'tcama.llCX:ESSODCB - a.OSED QAfl.a SCI!&JrCS- ~IICSF"B;J R:IIOIIM#IOE

1 2 :S 41

N..C 1liiiE.. ~CXXIf!CCH I I M ·OBX MD PN ... ai$'DUID MD SIJLIJ EXXI&ii5MJN - r - U'"

s

--.....c:.tJW»G ...... SllrMIOG -a:r

l MI

IS y> o"" ICICI"a:_~EIJIM~~--­

-or Ptw ,- ll '

-na. (SICp 8) pri« 10 eo-petas-ON

1•

Caapater LOAI>IRUNIRESTART swiiA::b -

RUN NOTE

lS. MODE/MARK SWMrl!beb• - Press

PI

Mt switdiJilllt pl8ceS lllc INS in swadby.

16. INS- Alipl Refer 10 INS GIOUDII AliCJ'!II('!!t J>rocedure.

LEFT CONSOLE L Cila* breatas - lA « mllared 2. L ud R A.'lAD RDY TO CPl. !iplS- 00 • a. L ud R A.ll.fAD G!'o'D COUPUO swildxs I'ORM. awers down b.. EPU Gh'D TEST S'IIUriP - NOR.\f. CO\U cloom 3. Mesler 1tsl pead - Chedt &ftd olf a. Gl'm co:-rr oRITlU'Z S'IIUriP- OFF. CO'= cloom b.. RCS MON swilrl! - As 1eqwted •c. Masler Testsdea SWlldl- Set aad ICSI. thai OFF 4.. Coctpil aad cnenor JC1US - As 1eqan a:1

•

NudearW~Ddin::ry

' We11• Deli118J Piloc~

Uldaies ill ar:r.ordatwle wtth mjspon ~ ~

7. S. 9.

FCS peel. uim swiJc:b- NORMAL 'Tbtottles - 00 1luoule panel - Set

a. Fdaiw toob- As desired b.. L &ftd R A.>dAD UNCOUPL£ S'lrill::bes -NORM. awers down c. L ud R - STAKf"IJIMAD RUN S'Oritdles-

Coepnter lOad a.11 be venfled by DllliD8 wtlca NAY illformatioo ~ oo dis~ IDformatioa wil appear ill appaai.aldy ~ secoad .U a . . - I laed. If lllc NAV iafomptjgg tales app tdy lS fCICIOI'ds 10appear, c:o.p'ICU 1ft bcia& loeded ~ lllc lSS3 senal dua buses iiii5U:Id d the llicJl speed c:Mnnd If m. formatioo appc:an in less tbaD ~ 5lCall>d. the lOad in memoedt ..S sa

E.

4.

s. 6.

Pi • atlleBITbouoaCDtllefodcpaa~ ry •!c•nor aaiYaies lhe BIT S)'SieJL Selcc:tin& lhe Maslcr Tesl swUdl J:NS"m poAtioa aad pressing lhe PUSH-TO-TEST buuoo will also aaivate lhe BITS)= foe tile fod quantity iodicator.lhe =Peper· fonmoce illdicator, aDd tile ar.y&e~~ SJSiem.

IC SUndJf atlllllde indira tor- UJICIIC(I 15. Radar altJmeter- As ieqtoded 16. Saisor display - ON. cbcdt 8ild sa n UHF and lntaaa puds- 011 and sa RIGHT CONSOLE

I ;.____ z.

I.

Gcaemor swiu:bcs- ON Nf.RS...... ptsd Sa L

Sl.AVE/00 swUdl -SLAVE

u.s -

WARNHG

I

A meam enensioa or re:ti'IICtD c:u c:atiSC

illjluy. Ooect with~ penoud poor to aamrq the anteaaas.

1.

NOTE

L Sapply Jeou- ON b. OXYGEN PSI - ~ 10 l2S p51 c. Diluter le¥er- NORMAL d. EMERGENCY le¥er- NORMAL EMER&AIR REFUEL1' hade ln IFF. TACAN. As required Ante:aaa pBIId - Set

I

ll. Fvd qaaDiit)' panel - a.ca Uld sa L BIOJO mob- Set b. Unt qaantily iodicator cr!toanr - As reqait'ed

Do oot attempt tO COITCCla fod illlbalanc:e (wm& fad cliflereace ol um Ills) wull tile FEED SOURCE swUdl oalhe P'O'Iftd af. ICI" CS1p1C stan. This C311SeS 'll'iq fod 10 bJpus fuD fv:sda&e tanks aDd eaa oia tile ...m IDI:SI.. aeaJiA& a porrntial fire b2zard. GI'OIIIId pu pwmel IDIISl COirCCl Lias lllltoal.a: poor 10 ~ SWt.

SJ51em - 0ec1t and sa

a. Anrmna swildl - EXTEND b. UHF antes~~~a - As desired c. ILSil.OC antetma - As reqwred ECS COJttnll pand - Chcd aDd sa

a. CKPT ~ sdeaor- AVTO COLO or MA''E STAKT Jillll I ies oa. lbc lhrotlle sllould - be arMDc:ed aDd CIIICi*= slnudowa 15 10 1 . m """ Oariils the statU~~~ qde. tAt 4'POf41UC ~comes 011 Ja.e alllpI*Wdy ~axe 1J1111 and the GEN tiptoe the miiiiCia~« pud aoes ofL n.e ClleniBI dcMmt power ON 1iCJU remains oa a:znil the Other ~teo'

mmes oaline at ;,ppt«imldy ~axe rpm.

&pie paiU>CleD duriDg 5Wt ....ncs with atmOsphencc:oaditioas. bowe;er, 3ppltiiie p>ne out. 6. FCS ftl5lslalt BIT- Complete Oblsene lbe SO C

cram Slops 8dva8cie& (test am:lbc:r m

ECS tdtctnr- I'ORM WallpOIIS bay doors - As ttqailtd

(4) FCS pad~ saudi- Slew 10 ENGINE STAKJ""

I w~ I Vtt!ly weapons bay doors area is dear ol

Bold swrill2 ia SLEW poq•ion 1UUi1 pro-

cram Slops~ (test nU!IIbcr 65} 1.

pmonod prior 10 cbanJini door maf!p-

IRADS aDd Sensor Display .. Laser swUt. -Off b. FUJUDUR BRSGT-OFF- TEST swit.cbes

&.

~ Display PWR swildl - ON d. FUJUDUR mode sdect s•Udlc:s - STirY (I) SO SWCS !ipl CXIIIICS Oil (2) lRADS ll'JT1AI.J21NG cispb)'ai Oil SO (3) FUJUDUR COOLING bp!S mme oo ~ u):W:.Zeoot916 liCbb p> out c:oruinne (IS llliautes !Uliutem~

c.

.

Anti-ice - Cbect

a. ENG A.Vll-IC£ nrildl - ON (EGT in·

aease. 2 tipts) b. ENG ANll-IC£ S'lrildl - A1JTO

- Off

_,_:=..- ----

PTIUTISVJIC FIT switdl - ON {li&llt off be· fore tau) Ensure PITU'f tipt oa annunciator pend p>es out bdore taXi.

ralioL

S..

'*"'

If the leSl swildl ma,PICS OG swt: {I) FCS panel lest swt!dl -TEST (2) FCS panel Ad\~ew ,..;tell- ADV (llimes)

LDwe:r zlareSbidd bdore lowerinJ canopy aDd msure caaopr r.Ws are dear.

3.

follows:

9.

SMD - Verily cmrau wc::apOil S1or'CS aDd SUI OS

JQ. Alti::letcr - Set

IL Thill - Set 10 tateoiJ senila& a. Pitcb trim - I llllil -=-don b. Yaw uim - 0 U'IUIS c. Roll aim - 0 mtits

2-9

TO 1F- 117A-1

12. IXS - Atigu

-'1 "

'llik«e

L

l'r.wl0121ickctal!p'Pft!l~and&OIO

dthc:r AUrO 01" MAN NAV. 1l. IRADS test - Complete 14.. vnt - Tdle

B.ate Sdemx- NO!Ut (PRJ BRAKE 1igbt

oO). apply bntcs, b. BJake sder:cY - SECONDARY (PRI BRAKE lipt oa). apply bntes c. BJake sder:cY- NORM

anjgn

-

While holc!jag breath. ctismnnta blowtt from de-mist bose connector and connea to pigtail adapter S'i»>" r•'>ly Switd! CXOI5.'500U vah'e knob to oormaJ ground (bnriznaw) posiljoo

Dismnnea blower e1earicaJ conneaoc and te· tDOVe blower from bractet

W'SC/OCIP AMAD ELECT1'11CAL POWER PROCEDURE

L

APU .,.itch - ON

oooJd oa:ar.

c. Canopy $'lritcb - OPEN ts. Tllroales - 011

2-16

Dismnnea lanyard betweeD the ~ bosle and the oxygen bose Hold breath and disconnect from ooboard O>Cy-

_Extemall}!.supplitd oonditiontd air is required for avionics rooling

--•

TO 1F-117A-1

• The eqine generator sball be turned OFF pn. toAMAO shutdooon to pcectude possible SWtCr sbaft sbearing clalDqe. There is jnw!Trient AMAD eleCiric:al IJO'I'U .nth the ECS mode sdcaor Dill in ALL RAM.

3.

Loc R AMAO UNCOUPLE- NORM S'lrirdl -UNCOUPLE

4-

Lor R ENGINE STAJIT/AMAD RUN $1ritdt -AMADRUN

5..

AVIONICS GND PWR switch - A

6.

EI>Thf - lNat

7.

INS mode switch - STBY

8.

Displa)~ - On

9.

Campo11ers - ance tb.rv step$ S8, 59, 62and63.

NOTE ~ MODEJMARKswiu:IIJisbt at this

point bas 110 elfea.

6.

Computers- OFF

1

Compmer I OAO/RI fNIRFSTAJIT ..;t.d! -

8.

LOAD Computers -ON

9.

Computer LOADJRUNIRESTART switdl -

RUN

Rder 10 FCS PRESTKRT BrT l'tocec:lwe; this seaioo FCS PRESTART 8fT CHECK L Initial CXlllditioas - Set a. External JlO'I'U - On

NOTE

NOTE • Cnmpn1er load can be ,uified by noting wbeo NAV infcymaJion appean Oil displays. lnfonaaJion ri1 appear in appn:wj-

mately one second 'lrith a Jnmal load. If the NAV infomwioD takes awua:iiWtely 15 ... I Hds 10 appear, allllpllteiS an! being loaded throo~ the 155J serial daJa buses instead cl the hi8h speed c:lwmd. If informaJion appears in less than ODe second. the load in weuoy is being used. DO( the desired EDTM load. For this case, attempt a reload by placiD& the LDADI

RUNJRESTAKf switd> 10 l.DAD,tumall WSC OXIIpUICIS OFF lhen all WSC computers ON. Set LDADJRUNJR.ESTARI" swilc:b 10 RUN. • Computet load is lUified by DO(ing ~v informaJion appears Oil the displa)S in oae: second foe a normal load. Oled: the RSI> 10 eDSUre the MARK and SNSR hJDaions are DO( baled. 10. MODE/MARK switc:bligbt - Press IL

SbaiJ be done after engine $l8lt ifencmal JlO'I'U DO( a-~ to a-'Oid au:ssi•e batttty discba.rge. lf the FCS presun BIT is pedDDDc:d after eugine start. the DUAL FCS ligbt will number2L

2. 3.

4.

DO(

illuminate during test

b. BATtERY - ON c. lbrottles- Of( oc Idle (as appopriate) FCS pand test swi1c:b - TEST FCS pand - Cbect displa)S (FAIUBiank) lbe BIT fail li!Jlt comes on and the alpbatlumeric display remains blank. FCS pa!id (AdvaDce-Slew Slritc:b - ADV) -Chect displap (FAilJ ;:~ ) lbe BIT fail 1igbl remains on and lhe radial sq.. merus cl eacb dsala:ter in lhe alphanumeric

,.,

S..

INS - Align

display QliDeuiSol eacb c:baxacu:r in lhe alpbatlnmeric

display come on(:·_.- ). NOTE

Owing INS aligmaent c:bect for and dear any BIT INTERLOCK ligb1s. A properly aliping INS shonld reac:b step 6 in Ulldelr 18 so ••d• and step 23 in less than 12 min-

•n.es. 12. Fud qu:mlily panel - Oled: and se1

13. S!andly attitude incficatoc- UJIOI&e 14.

Radar a.IIimeter- As tequin::d

IFF. TACAN, JlS - As tequin:d 16. FCS Prestan BIT- Pbfcym

15.

6.

FCS pand (AdYance-Siew switc:b - ADV) -Qed displays (FAilJSYSTEM cnmpatilility statement) The BITfail!ipt remains 011. ALL SYSTEMS COMPATIBlE appears in the alphanumeric display if lhe ~'lAC, FLCC, and FCSP are com-

pattie. I( this appears.

p«oceed 'lrith step 7FLCC INCOMPATIBlE or NIAC INCOM· PATIBlE awars. in the alpbatlumeric: display if the installed equipment is DO( eat ................

Bmte Failore • • • • . . • . • • • . • . • • • • 3-44

~36

E CS Aur.omatic Sbutdoom ...•... Avionics Air Bol ..•.••.••.••.•• Arionics Cooling Fan Failure . • . • • ECS Ovcd>eal ..........•......

~37

Failure . • • . • • . • • . • • . . • . . . . • ~35

Coottollabilit)' Ched: •••........ rm Dama&e or LDss • . • • . . • • • • • • ~bl

Eu

C•tnol Srst-

uc• . • ...................

~35 ~35

~36

Single Bleed Air Dua O'beat ..•. ~36

Pilot Prelw Hemr r.mor.

I

~37

Ai''fflUNCIATOR PA..'lEL WARNING, CAunO~ A..'ID ADVISORY LIGHTS

~37

~'I)JCA1riON

~37

..........

~38

INS f ailan (balljpt) •.•...•........

~38

WSCIOOP DaJ ~IDUO.IDI/HtJD Fail.,.. (bllljpt) .........•..........•.• ~38

.... . ................... 3-45

AIRCRAFT ENTRY/PILOT

EMERGENCY EXTRACfiON ...... 3-45 Ncxmal ADa-aft E.atJy • • • • • • • • • • 3-45 Emerzeocy ADa-aft Eally • • • • • • • 3-45 Pilot Ema&c:ocy Exuaaion • . . • . • 3-45

I 3-2

~~~~~~~~~~~~~~~~~~~~~~

TO 1F- 117A-1A

•

EQUIPMENT ALERTS DESCRIPTION

ALERT WSC1 ON

WSC1 FAILED 1J>1D RECONFIGURED TO AHOlHER C()MPUTER

WSC2DN

WSC2 FAILED 1J>1D RECONFIGURED TO ANOlHER C()MPUTER

WSC3DN

WSC3 FAILED NIO RECONFIGURED TO ANOTHER COMPl1Tl:R

WSC1 Rl

WSC1 HAS REl.OAOED ITSB.F; NO OPERATOR AC110N REQUIRED

WSC2Rl

WSC2 HAS REl.OAOED ITSB.F; NO OPERATOR AC110N REOUIRED

WSC3Rl

WSC3 HAS AS O&OED ITSB.F; NO OPERATOR AC110N REOUIRED

NIAC

BOTH BIIS£S FAILED, NIAC FAL BIT SE't AlP BIT SET; NWS FAIL

SMS

SMS PR:MARY OR BAQQ.N> 1liREAD FAILED OR OYEJn'ENP

INS

EU OR IMU 01/ER'TBaP OR ANY CAT 1 OR 2 BITE

IW)$

A A

ADC

A OR 8 BUS FAI.

EDTS

EDTM NOT INSTAU..ED

OSP

CMOI OR DISPLAY PROCESSOR FAI..URES

HUNGSTL

HUNG STORE LEFT STATION

HUNGSTR

HUNG STORE RIGHT STATION

POStJNR

A

I

ANY IRAOS S'l'S I EM BIT FAL

NAVIGAllON POSrTlON liNREASONABlE

N>ATT

AN'f INS CAT 1 BITE FAL

E DATA

~ EDTN

D DATA

UNABl£ TO READ EDTN DIRECTORY

W DATA

UNABl£ TO READ EDTN PREFI..IGHT TABlE

OTSO

FAILED BLOCK COUNT

OOITAL MAP P~ FAL

NOTES:

£ .£_

CAUSED PA!UARI.Y 8'f ATTEMP11NG A VISUAL OR 59/SOR UPOATE AT A RANGE GREATER THAN 120 NM. IF THREE ITERATIONS OCCUR IN tO MINUTES AHRSATTITUOEWIU. BE USED; HOWEVER. IF INS ACeS FRATIONS REMAIN VAllO THEY WILL BE USED.

A EDTN RB..OADING REOUIRED

•

BEf()RE

NEXT~

FIGURE 3-1

3-3/(3... Blanlc)

- TO 1F-117A-1

'

This seclioo ,......,..,mends procedures for we U. lhe

for cbase aiia:aft aodlorground COIUJOI assis'a!V"e for n._...,les'u"c.ing systemS or for ~ procedures will be made.

C'I'CDI of~ orolhcratwwmal COIIditioas. The procedures are~ 10 J&O'Oide a margin of

~ or

INTRODUCTION

safety in 1M e.UII of{unber faiJW'CS. The prooedllln:s sbould be cooside:n:d as eme.gency procedures unless they are labeled sperifrally as abooimaL.

'*"'

ChcctJisu are ided wbcre sperilic ooueaive steps caa be enumemcd for a ~ Aiiritmaator l'iiid WiiJiiii& CiUbllll. aDO tights inw:ing

any ~· emergeney wbeu SUUCiliral f1i&hl Colllrol Sys~em malfuoaioas ezisl

lhal adwusc:IJ a1Iea b;uxUin& qualilirs a axwollability cbcdt sbould be performed (See Ccnuollabiliry Cbc:d, Ibis section)-

LANDING CRITERIA The depee of wgency in la:ndin& lhe aiia:aft duD~!& c:mc:rp:DC1 apcratiom is dt:Cmrxt as folloH: LAND AS SOON AS POSSIBLE AZJ em~ will be declared. A landing sbouldbe acromplis"ed at lhe nearesl suil:able aidield ...... ,_,"'&1M~ of lhe emergency, ftalher CUDditiODs, 6dd facilities, ambinn tigblioa, aitaafl gross~ and avn-nd guida!V"e

LAND AS SOON AS PRACTlCABLE/ PRAcnCAL EmuBe swt cycle mast be carduDy IJIODil«ed until lhe eDgiDe bas a!IDpletdy stat.lizrd at Idk. w1th an aocma1 iDdicatioas.

If !he eapoe fails 10 ligbt~ 'lrilbirt 20.......,.,. EGT rcacbc:s 100. rpm fails 10 modi Idle, oc any Olbtt aboouoal SlaJ1 ......tdjnm. arc nou:d::

c.

1. 2..

Throule- Off Continoe to aant eaaiDe

If awe rpm rcacbc:s zero after a bot swt attempt. doDCM -~ocauempta reswt. Mainlen;nn· aaioa is tt>:juiitd

NOTE • If bot swt (EGr greater than IOO'C). engage swter wben awe 5peed (Nl) is a1 oc below 30'JI. and oonlinue aa.n.tmg until EGr drops below 200" C. A reswt may be attempted aD)~ foiJowin& Ibis proc:edun: ptO¥iding EGr bas 11CM , " ..ded

pa.nd. oc the geen ENGINE START light remain oo after awe rpm bas qabj!izecf a!ldle durinJ the swt anempc (appraUaa.tdy 64$ awe rpm). the swter is DOl disengalecf oc the duu::b has Wled. 1. START/AMAD RUN swi:tcb -Off (c:entered)

If STARIER ENGAGED light remains on: 2.. Throule - Off

ENGINE FIRE DURING START An ~ fire is iDdicated by il.luminatjon olthe

f1RE wam.iD& light and eilhe:r L oc R ENG light oo lhe instrument pond. No fire ~system is prooided foe lhe eagiDe cnmpa.nmenL The fuel

sltalolf wive a! !he fuel Ollltrol DDil caD be daio:d by raardiD& the throale 10 the oiJ positjon The fuel sltalolf wive at the~ firewall caD be shill oiJby pushin& lhe enJine fuel S'Oii!chtizht oothe instrumalt pond.

1.

THRO'nl..ES - OfT

2.

SWrTCIU.JGHT'(S) - PUSH

Ensure appropriate ~swi:tcb'W" ispasbcd and t.bat the ON sqment rlthe SW'ild:llisht is illuminated. If FIRE waming light remains on: 3. APU - OFF "- BAIIERY - OFF S. EXT PWR- OFF 6. Emergenq• GtOIIDd E£=$

APU FIRE (GROUND) 1. 2..

Ailempl

reszan

STARTER NOT DISENGAGED If the START ENGD light oolhe amnmciato£_paDd. STARTER ENGAGED liglus oo lhe master test

Push Ensure t.bat the ON sqmmt rllhe swUc:b.liaht is illumioated.

The guanled APU FUEL sori!dl oo the EPU/APU panel Ollltrols the s:uoe APU artoiJ wive as the APU PUSH switd!lighl oo the instrument pond.

• If wet star!, aanJt eagiDe until tailpipe is ckar rl Cud.

3.

APU-OFF APU PUSH $'1ritd!IWn

NOTE

ru·c.

• If a oold hDDg swt (awe rpm roiiJact 10 apprOlimatdy Sl$ N2..-ith EGrlesstban 400" C). IIIOIOl" eagiDe 2-3 milnnes wilh throale off.

•

EMERGENCY GROUND EGRESS If time is ememety aiticaJ, mnsidetatjon sboo.ld be Otherwise, the evaruatjon ptocedwe is identical 10 normal ecres:s- If canopy jettison is tt>:jlliled, remain in the seat 10 mitrimire pc:>SSiMiy rl injuly as the canopy departs the airaafL

g;.a. 10 ground cjo ti"'

L

Seat- Sate

I

.,.,,.,,.,,.,

•

___ ------------TO 1F-1 17A-1

2.

HanM:s - Release

3.

Seal belt - "'RdCJCiiiK

-Sti:l

SJ1ll3 UIOCIWically swlldla tbe tnte SJ1lem 10 the p"satac -.ode aDd lllniS oo tbc A"'TT SKID ............ bpt.

L

ANll SKID - OFF

BRAKE FAILURE II 110 braboc aaioa: L

•

orr

EMER. BRAKE PWR SWI!dilial>t - Press

PWR ac:tiQted. After SUJp aDd if aD ~are

6.

i••••

uti-te: BAIIERl'-OfF Tam bmery 10 ~ IJIIItery power for tbc ......,.#DCY lnkes oo tbe bot butery bas.

orr

TAKEOFF EMERGENCIES

Ensure tJw tbc $WI!Chl'lbl IS ilbsinated

MISTRJM Durio& Wcolf ~ tbe pilot always bas eDOilgil sua: aUU>Onl)' 10 LES - P\JU.

CoDtiDoe !ricfin& budles ualil after seat-fllllll separabOL

I

WARNING

I

Mlnimum ejatiaualtilocles are clep ""'"'' ~ sink me. ainpecd. alii! roll ao&leR'""""_...v.d miDimwa altitudes are l5,lDl feet AGL iC out d contrOl, allll200) feet AGL iD conuolkd (babL

CANOPY JETT1SON FAILURE If aJIOIIJ' does - jetli!oa. ~ iD p +Qoi•• for qeaX8 ud pttfomathe !olJoonlawllile kttping ldt ana amc.rd iD rc•f ess to at:p*4» De scat cje r; ••

bandle. I. Alt.emate Canopy/ Scat T --baDdk - Pllll

II the c:anopy fails 10 jet..-. do - rawe ud pall the T -'ewk Dep!et- d tbe

psMD!Or 10 lllo: iQ1 c:atap.oh • iD rc:scll.

•

•

'

TO 1F-117A-1

EJECTION PROCEDURES F T1ME AND CONDITIONS PERMIT

• A1RSPEED - REDt.la: TO BELOW 2SO lme OISCbatge te:mperaiU1'e ooaus and mre speed

3-13

TO 1F- 1 17A- 1 is deaeasing; therefore. ai:rstarts are ~ otijuil tx! 0111y .mm an CSigiDe bas been illtaniooally shut down. If an speed rolls bact 'lritbout. auto-alp reszan, Lbe ~ aU'slan must be· initiated Durin& Lbe ~ aiatan prOttdure. lbe tbroule must be p1aatx! ia the off pNoil"' 10 enable the START Strildl10 operate. Refer 10 ~ 3-J. fo< airswt euodopes.

I.

Ifthe pooorertatcoll (PTO) shaft bas failed, l!o!dio& the stall swi1dl in Lbe START position will eause failnre ol Lbe staller. The SW1 attempt may be repeata! 10 ¥erify PTO shaft failure but do 1101 hold Lbe swt swi1dl in position The followin& are iadicatiaas ol PTO shaft failure:

Throl1Je - 00

•

nrouJe s:bould remam ia Lbe off position for s ~~-------5~~foes zero, the a.p.e 1M) due lD lllemlaJ ..,._., u CSip)e does sza.n. ""......,. reswt Oil doe odlct c:ap.e.

1J AMAD OJLcmtinn Ji8bt CtDes a.; L Autotbtoole - 00 (OOP) 2. Fad flow 2100 ppb lllinitn.

If ew.... c:qiae 5WIS (steps 5lhtoap ~ S. EMER HYD- OFF

o.

the

NOTE

• Do - .u. . . . airswt abme J83X) rea Oil lk SLiJdJ!' aJrimcter or loG ol (lcbl ClOII1rOI$ ....,. resall dlle lD ipmff"den• lljdtaulic pme

• Anuns may booA JIUIIII5-

011

dou:K tifl> ON b&lll- f"'locc.trm oil

AMAD OIL temperature sensor dela:u tcmpcnture or low oil presmrc:.

IJ AMAD

on. cautiOil !ipl

3.

Throllle - Idle

4.

Gmcnrtnr- Ot+

rea-

Oil

hi&h

af1tt 2l)

3-19

-

---------~

....

...,...,~....,~~,.,.~

TO 1F- 117A- 1

If AMAD Oll.light goes olf: 5. Tluoule - Use as neo'$$3'Y

C\"CCY effort sbould be made 10 npirrritt APU a.inwt mnctitinns (RdertoFtgme~fortheAPUa.inwt em-dope.)

If AMAD Oll.ligbt remains on: 6. Allilode - 22JlX) feet MSL (2ll,lXXl feet staodby altimeter) or looFer

The AJ'O ainlart sbould only be anempced afier allowia& time for the APU 10 spool down. After APU &ilnre is indicated, wait 15 stronds 'libea altitude isbelow20,1DHeet MSLorwail noo minutes 1ibea a!timde is a1 20.IXXI feet MSL aDd higher, before al1elllpliD& the APU airslan.

OD

NOTE

Ill the C\'al1 ol an~ failure 011 the side

•

:.?'C:.n~.:!:-~linethe~y----L-..J.~JJO::IS-'"D:~ >jlocel ID il!nmimote aDd (eal Wilt fuel will remaia a•aiable by pll'rily feed aDd 10 preoall lhe fad from •apoiila4 II lhe cqiDe ~ wbicb cn:scs D eqiK: Opec OU). a maumm:a fad {low ol 2fD) ppll is leqont ed .,. lhe failed Side. boBber rlwl Ole 1J2Vff1 feal ee.e~opt. a dcsomt is also reqailed. IJ the pcm« IS lamed ali. AMAD beat load is 1educed aDd a hlcbcr alutude is

e..-e _,_

u

pennitted. If lhe (ad uptwb.,... is OOl oorreaed:

l.

U doe aor:sfeed nJore (X FEED VLV) S'1rildl is io Al1IU pc»rim, Ole aoafeed qt,.e .;a al'lmmrnlly « a late~ Snlf.;..,l allltrol poorer is available if lbe apptoadl is JDaik with a mnimum d 1• ADA No difficulties are eocowuend at speeds obowe 2IXJ KCAS in lbe cruise CCIIIfiguraliDD

run

ro.-

2. 3.

TO 1F-117A-1

GENERATOR FAJWRE

A pera10e fallare will be jodicated by iii!JtDinatiOD d lbe apptiJ!Kiate tipt 011 the liDIIunri;nor paoe1. ~CICCtriCil IOidS WiD

La.od as SOOD as p:anira! Fly a 7° AOA (mnimnm)apptoadl

FUEL BOOST AND TRANSFER PUUPS INOPERATIVE (AC POWER LOSS)

Ill !be c-ut that all ain::raft fud boost and traliiS{er pumps become iDopetatNe dee 10 los&d the acpoorer supply. J.f7S pouods daft transfer (f~) fael OD cadi sitlc d tbe ain:r.dt and any fuel rnnainin,g in eiahcr ..-iD& Wilt becomes tl3Jlll"d and unusable. AIR REFUEUNG SY'STEU MALFUNCTlONS

10 F-117A- J-6, AlR R.EFUELJING PROCEDURES wrm KC- llS AND KC-.lllA

Refer

tm1IIY FUGHT MANUAL SUPPJ..EMENT(S). Section V. for Ema&eJIC.t Air RdtJeliD& Proa:du.Rs.

ELECTRICAL EMERGENCIES

iftiOiiiafically be

handled by the owoP'e paa!OC. If the pcra10e falJare was due 10 beat hti!dnl' in the AMAD, a posstie AMAD oil pressureltemperanue malfunaiOD may oc:att. L

Affected~ -

C)de

Iflbe pera10e cavtioo (LGENIR GEN) 1ipd oo the annnncia•or panel remains c:m: 2. Generuo.- - OFF Automatic bus ~ will jliO';.!e ac poorer 10 tbe falJed bus fioollbe oppoQie pcn.10e. 3. Land as sooo as pr.!ClicaJ DUAL GENERATOR FAJWRE

If both gencratot:s fail, the EPU will atUomatirally come otHiDe when the main J:CDCf31Dr5 drop o6-line. "Thr APU au!O-$hutdowu ooertemperatare pro~toioo is inbiited. The EPU atllil:i:a.ry pcra!OC anlOUles.

The SNGL FCS fa:iJ !ipt comes oo io coajunaioa willl tllc • HYO fail IIcht. a:cep1 for bJdraDlic syst- !ailwes !OCID!al by llae ~ faihlre ljpu::

• L lJI1L PUMP orR lJI1L PUMP • lJI1L HYD A

•

• L~«-R FU"PUMP ----~~""''-.=..

,. ~~~~~~~~--

----------~

•

T01F-1 17A- 1

AIRCRAFT OPERATlVE S'fSIEMS/FUNCTlONS DURING EMERGENCY ELECTRICAL POWER DISTRIBUTION CONDfTIONS

ENG1NE/AMADJFUE1. Enginll: A111J-1c:e left Cfaled ID 011

Mi-lcBRiltf Bleed o:r.ol

1'\lotonna. ce 1n•dcabdc..., (EJ'IJ Owethea1l'fQ, 0

• •

;ri(w I

- - -:581

-UGHTS

Map and Ulilily -T851Panel Anli-O:llisicn (Bcalml Aoojand Slam

----~~--~ -·~I--------

X-"--lhln •

8oo6t ~-Forward (l & Ill

•

HoiDoHca

AVIONICS

£ 01S £ IFF £ INS

• HPliiAic Pressue •dcab$

AIRCRAFT

A NCC

APU/S'U rADI N». and Bela Ind.

Slard>r Ah;peed Slard>r AlliUIB (PNBJ) A •AIIamale ADI RADIOS o:r.ol tH'JSeon tH' HAVEOUICK

NAV1GAT10N

--..a

£•AHRS

• -as

£"HSI A "TACAH

NOTE

• Wllh bolh enpe per.uors inopcnlh'e. the emagencygeneratOr(AUX GEN)c:aD maintain power for a minimum oll2 minutes (dve 10 EPU opemioaallimiwjons). • Wllhoal main and amiliaty ~ opaatin&, a fully dw&ed tnnery will supply power oaly to lbe battery buses and tO the left and right CSSCDtial de buses for a minimum oliO minuus.

• If bolh main~ and lbe amiliary pemor are ilqletati>"e and lbeairaaftbaneey is~ ~dearic:al powecfor the fli:&lu contrOl S)'Slem (FCS) is SJ'I'P'itd by four dedicated smndby baUcries, or a lead-acid baueeywith SIB N·2777 jnqatled, whida caD pO< ide 10131 det· tric:aJ requirements tO the FCS for approf ~

3-27

TO 1F- 117A- 1

AIRCRAFT IHOPERAT1VE SVSTDISIFUNCTlOHS DURING ElolERGENCY

El..ECTlUCAL POWER DlSTRl8UT10N COHDmONS

~

~

~

ENGINEIFUEL

NAVIGATIOH

8oclll'lnps - Nl. f-. & Ill , . . , Scut;a Select

•HSI

·~

•llS Rador-

r...t ~mal lCiorJRoiUII 1-

STEMS CEGT HigM.ow Thus! or.! 01. " Low~

"TACAN

AIRCRAFT

AV10NICS

K)A .,..., • iQ Tlet.'llilable.

4.

• Minimize maneuvering NOTE A.ad large control mowemems dl!e 10 limited capacity ol the EPU bydla1llic

pwnp.

s.

Use Landillg Gear Emerge:ucy Extension poc::tdwe Refudin& can be aa:omplisbed by the ernc:rp,eocy air rdoeling system only. No 1'-'WS. pid ...;pers. • eapoo bay doors oo- APU e:dlatm door a>-ailable. Refer to Complete Loss of Eitber Hydnalic S)'Slem puc:edure. this seaioo

Loss e1 f1icld S}'Sl- A Oaid (FLT HYD A Jipt oe) flicllt S~ 8 Ollid (fLT HYD 8 . . . oa)

II[

•

I

3.

Refer to Complete Loss ol Either Hydra:alic 5)~ ~we, tJU. >c-e

S.

!Uform Controllability Cbect Rd'er to Coolplete Loss ol Either Hydraulic

6.

Extr=psiop

System pocedwe, this sectioa SystemS affcaed; DO inlet grid 'll!ipers. weapoo bay dooc opcratiOD. APU exbat!Sl dooc operation. and

emergency airttfodln! oaly. 3-30

I

Centc:r:ing ol up 10 thtee COIIIJ'OI mrfaces em result .nth =tam mmbiruujnns ol IIJdraulic SJS1en1 failures (RESET and DUAL FCS ligb.ts oa). The first ruet attempt sboold be """"""tal)' and the rea:tiw obsel:wd. If a 1aiJe. abrupt. airaaft tranSient 01X11IS, DO funber resel sboold be attempted.

•••nmnbliW'S.

4.

WARNING

1 4.

Coolplete Dual FCS Faa Light l ndjcarion ptoa:dwe. this sectioa Land as soon as paaic:al

If the SNGL FCS fail tiabt ames 011 wttbout any FCS smface tights: S. Coolplae FCS Fail lipllndica•ioo proocdme, dlis StXtiuo

•

TO IF- 117A- 1

I

6.

Refer 10 fbcllt Allon En>dope poc:edwe, this

llCClioD

FUGHT ABORT CRfTERIA Aa abort

fucb1 andopc Ills beeD ckr.cd

few use

foDoow111c fd..-cs • SJ1l... 'lliJida ace critical 10 flcllt W11lua 1lle abort ez;dupc

safay-d..fhpL

• rm,e

aJioo;s-- op-- dlab ~ a1IISC speeds u oplllllaJD ahiiUdcs.

aad pOiides m= poblbilly ol r !IW ejrctine il De C"¥'e8t ol zu eat -..ora case· Wlara.

••e

lD 1lle (ollowJita 5eC'iws fucb1 ....... tbe abort Cll

--

-~ -~

3t0~75-

2DOICCAS 7 0ogr.-

the sezsnrs. Fl.CC. aa:uaton.. ud b)-dtaulic S)'SlUIIS. The SNGL FCS annUDCia10r bpt ud FCS RESET tizjllmmes011wbalc.ecw IIKftol tllele ~ failtats 1o1m: beCII dclec:ttd

Sf

·x

c:111a1 rumu c:u be ""'"' amca1 tbu lhtec

« aoe disuibataS lim failurO';wb~the~~ S~NG~Lij,FCS; fail tight and the

-

scaica U the SNGL FCS and RESET tights stay oo aftes: anrmpred reset, and boob bJdranlic S)'SlUDS are oormal: 6. Annunciator •RESETsoriu:bliglu- Push 7.

• U the DUALFCS fail tight isoo and cannol be ~ wilh the FCS RESET switddigtn, the pilot will baoe DO indicatioa of tbird 01" foanb failure detcaion iD the same viett«. 1be pilot sboold always reset the SNGL FCS fail tipt oo the ammnciatcx plDd foe an jndjratioa of a Sllbseqoeru single failure iD $Oiile othtt pan of the SJS'CIIL Because lhese failmes may be re:senable, lhe pilot sboold pa iodically press lhe FCS RESET switc:bli&f't oo 1be FCS pand wben FCS tights are OIL C¥eD lhoup !here is DO iadit:atioa of subseqaenl failures oc

Continue lliglu

DUAl. FCS FAIL UGHT INDICATION

U an FCS failure can1101 be reset, the FCS RESEr the flight control paDd will remain illuminated latheeoentofasa:ond~ failure in t.be same FCSRkacrortbesamearm:unr. the DUAL FCS fail tight oo the llJlPCI" instcumeal paDd will a:~me on. Refer also 10 FCS Elearical POwer Failures. switd!ligbt 00

H DUAL FCS fail tight ooaoes oa:

• H the DUAL FCS failure tight is oo aftes: !anctin& the pilot must 1101 press the FCS reset buttoo wben !here is weight 00 the PI Wllil the aitaafi 5pCed drops below SO

2seuuis

WARNING

fU} te5eL

Slh c

FCS RESETS'Orildlligbt- Pross and bold at least

1.

I

blots. 011e

Centering of up ID three control pnfac:es caD resoh with cenaift Cn!ijuati()lls of b)Wau6c S)'Stall CaiJures (RESET and DUAL FCS J:i&b.ts oo). The first reset anrmpr sboold be III(IOll'fltmy and the rcaaioa obsened. U a 1atge, abrupt,

airaaft tr1!n5iem oa:ms, .., f1!1ther reset

~and~:~------------

wilh the FCS RESET swiu:bligln, the pilot sbooJd be prepared foe imDM'!diate ejcaitm Flipt wilhm the abort envelope prov;des lhe amimum prdJabiliJy of 5'0 1 r lJ ejeaUa fo~Jowin& the critical tbird failure_

Refer 10 Abort f1igln E.trtdope procedwe, Ibis

S.

-

~

AD attrmp«ed reset migltt cao:se

« more CODuol wrf¥eS 10 go

bard-t Elo>elope

4..

Pafona CoaUOIJIIIiiJly C1ariJl& tile ffi8jlt teSl popam, aa irw1rnt oc:a=ed ..tricla remll.ed in tbe lm5 ol tbe Jdl filL Tile airallft wasaaiullable alii!- aldy JCIIXIftJc:d willa sliPl wodjfw a(

10 tbe .......... Oipl abort proc:edllres

112S floona u 220 ICCAS ..U. --------~~~~~~~~~bc~ueaorex»r~

[~J

Be prqiUc:d for a ' " u. PIO ~ 0a.re. Alter It ... ow a, an.... 10 - - tile ad ill appi • tdy tile aeuua~..-- cspeae!!y •i!ile dqAojq tile draa dune.

SIMULTANEOUS DUAL AIRSPEED FAIUJRE

AJ"-&f> II IS a remote possb'l!ly, d IS awlU\-able tJW a bud SlliU could daJDaae ore or won ol the pdOC probes. While II is Ut!p..W•c 10 predict tile resalts ol iOidl a arite. tile rolloorin, failures may loss ol esther or both the priJB:aJy and SWKIJy linpeul india!OIS. • Pltdl axis osdllations 1112)' oa:ur if dllaJ. simaltancous pilot-static SJ5lcm failures result m tile ~ sdcciOr c:hoo5m,s one ol the failed apa1s ror asc ia tile pou:b Dis QllltrOI laws. nus will resalt • Cthcr a siqJc (SSG L FCS) failarc or chel (DUAL FCS) fail~ bcJlt joc1ir:aJ!Ojl •

L 2.

e

(JinaJ appoadl

MDI- Abort fliPt Ertieed swtS is DOl availallle if the bleed air swild>es are iD the OFFpositim

ECS mode selil pressurization. Loss of

IXScan lie ~Wiiliiii f10l5 llll.IIUt~cs;....--1-­

Go 10 step 3 and reftt 10 Sin&)e £nPx f1iclu - ' sqJe Enpoe ~

~ Oft ambi.

II ECS OVHT JW!t remaiDS em: Land R ENG BLEED AlR swildlc$ - O FF

4.



- - O O(OCU')

"""

6. 7.

A-.aid bixlt power sc:nings Laod as~ as pcssille

• This aaioo forces the reconfiguratioo d the weapon fnnaion into COMPUTER

No.3 PfTOT PROBE HEATER FAILURE

• Ifpotlk:mremainsandiNSisopemiooal. two temau......,ric;dly failsto tbc: DR liiOdc:. a ba10! DR lqend will appear on tbc: VSD, and the snJnpoln« will 1y en~ The tdocity >-eci.Or will be ",~.. d bJ the W symbol 1llc: 8SD and BUD displays are 110t afiected. Navig;atia11 daJa is p.,.idol 10 the NIAC. HSI and ADI bJ tbc: AHRS. If DR does 1101 appear Oil the VSD, the used the SW>1t:Jt instruments is oequioed..

navigation

information

ff autopilol npera!ioo is desiitd:

~

~

~

'' ' '

1.

AII1.0pilot cbaond select - CB2

W"nh a W-WSC or- N-WSC IXllllpUler failure, the sy>tcm reloads au•nmatic!l!y into the X-WSC allllpUICrand DOacboo is..., ry. If the X-WSC IXllllpUler fails, 110 rdmd is available or- Dft"!'SSS'J because it oormaDy is the baclup CWijNter for- a W-WSC or- N-WSC complier failure. With two orthree compouers failed, the 1NS fails and display is DOt available. usc the 5UDCIJy iml:ramcms. Reload the WSC compatas in an

information

ancmp to obcain DR infonna•ioo Oil tbc: displays. rr two or- more CXJGipillers fail: l. 2. 3.

ff EDnUU and/or- EDTM FAIL light(5) on: 4. EDThf balldle - Cycle a. Verify EDTM FAIL fi&bt comes Oil and goes off and wait l.S se£nnds befor-e continuing proc:eduns

2.

If antolbmUJe

operation is desired (OCJP):

3.

Amolbronle manneJ sdea- 01 2

4.

Autothrottle engage- ENG

WSC/OCIP DUAL MDIICMDIIHUO FAIWRE (lNFUGHT)

If both MDS$/O.IDJs fail (llasbin& STANDBY, blaU or- frozal display$, ioaopenot>k swiu:bc:s, de-) and the HUD fails (Dashing STANDBY):

1.

EDTM balldle dowD and locto:l - Cbect EDThflU FAIL fi&bt- Cbect off EDJM FAIL ficbt - Cbect off

C)de power Oil both MDJsiCMDls

6. 1.

&

Computer LOAD/RUN/RESTART swiu:b LOAD Computer 1. 2, and 3 power swilcbes - OFF Computer 1. 2, and 3 power swilcbes - ON Q,mputer LOAD/RUN/RESTART swiu:b -

RUN

If NAV infonnatiall appears on displa)s: 9. Mode S'lritdl - DR 10. MODE/MARK ..,.;td!IWJ! - Press DR oavigatiao appt2rs Oil the displays. VSD disptay sbow$ a DR ad>-isory and the ¥elocity ftClOr is rcplao edt., the W SjmboL HSD and HUD displays are JIOl afieaed. Na-rigatioa infonnatiall is based 011 AHRS.

Foe anrnpo"Joo operation:

~-

-u- ~&m~&tt=on---------~

3-38

TO 1F-117A-1

'

12. Autopilot eotpCe - ENGAGE

NOTE

Few awxbrotlle npem-· 13. AD&odlnxlle ct.annel sdect - CH2

u.s PcJe dope is p r do« is opea.

-aJable lllltil -

14.. ADiodlnxlle e11PCC - ENGAGE ll Nay ..ror-1ioa does - llppQf a. di:stbJs: 1.1. Use SIUCIIy iitiU cuw:uu

DRAG CHUTE DEPlDYED IN FUGHT The c1r1c clime oc MWt•w • tlat 'trillllil ~ !Kc:llale is~ dqllo)ed al JPCC~d&bd weca l7S&al 300 JCCAS. IV. JPCCd& bdow l7S KCAS, tile c:11ate will- (a;l &al .,;a,_ Ill....... to !be amn[L IV. speeds peatCr tllaa 300 KCAS. !be dune may f2jJ eac1 SU"eata bdUDd 111e lliraali.. 1a an ~ 111e chme- be · tMudy ja'-O:Ito JRdllde inu:derence .ntll oc da-ce to lias &al 10 prew:ru loss al CXJeuol allbe aitaait due to !be dnc al tbe

'JZ'ft trim Ched:ect Nalljsfw:d 011 final44"c:all)

0 • (after

4..

.Roll and

S.

Do 111X eoaed 7• ADA IDilil ~is o:1 ('JS ADA 111Uia11a wbea ludiiiC is~

-6..-f>m& chute -

Jettisw decia& ri006;wll {llboal 20

blots grOII8d speed)

SDfGLE-£NGJNE GO-AROUND

L

Tluoole(s)- .,., iwm power

2.

ADA- Mainlllia 7•

I

WARHTNG

I

chute. It may be necess?'J 10 1.-:b dowllto ~ eueotins 7• ADA. After lil""""''*P, allow tbe aitaaflto aa:ld~ to 180 to 200

I! the dra& chu~ dqJio)s m n..pc I.

On& chute - Jetusoo

RoWe the en, chute handle 90 • dod• a and pull to the jeiUSOil poatioiL nus.ruoa WI opea 111e draa chute lint latch. allowul& the dra& diu~ 10 separa~ !10111 the auuafL The handle m:1tf be lodled ia tbe jelliDl po5itioD by roc.arma !be baJadle 90.

KCAS. 3. 4.

CXJIII'mla-cloc::tali(;.

I anding gear - Rema (as 100M as ddiaitdy airtrne) MaimaiD minimwa rate al climb antil airspeed reacbes 200 KCAS

I

LANDING EMERGENCIES

• oir&fe em awo-* speed sboald be 220 KCAS ..U IK ,ear ap. Delay laDdiD& p r me-qw ...u fiMI awocowa c1nran 15 desired. (Rder to F"eutt 34 rooludin& pilie.) 1k IIIIXIIDil:ID 10 • leo' ADA is 7• . Af&er tile M.

acxzleraliou is

2. 3.

GnllllS wacJ11- RedDce EMER HYD- ON ' atwtina pr - Enaxl wbol 1ma1 des::miiS desired

.

' by

~

pit!

eup.

sing!=

the

s• iato !be

(Rder to ApJ: wi A (« .gW: perfcwrMIM r '1~il4y.)

APPROACH-END ARREST1ciEHT The Umft au~ S}Stelll is c::ttplllk al airtJonlc boc* depio;;Wt+l aud I 'ul 8f4li~

' :1 WJtltia tbe andope {see F"p-c ~ll). Due to W!boot lilmts, ......Old enpgemmtS require more precise CXJeuol al Uspccd ud """ lo•u poiat t11aa ...,..,.... e"" capable aircnfL f'l'IVZ ±ema,

if

lf""""*'""d

URSUD=nt

•

t•~

t

SIHGLE- E.NGtHE LANDING I.

.~.

sjrted~ ac:ar zao lnlll t.e~

e.::a"'"''

,...L

I

Any .... ;s;. •• to ~ tro. • tin&'- mpue awocowa sllcoald be ..seas ea:dy as 1* 4 sl.... Best •'C': cmc

SINGLE-ENGINE EMERGENCIES

&ear os k>wucxl. reset !be rca ud ,...- a.a 10 aao if !be auaaft b8d beat u-...cd !or • . s'e . . nus will mpre saee small stJCt '""" pedal Corasc!DnQ& !be • "daaiiK ....,._..,. , . . . . cperabll.& ~ at • relati¥dy . . . pooocz- scaiRc. bet ril resalt • DC1IUal lnm wbea tile pooocz- is rub:al • the Bare.

WARMMG

aw-stid is DOl the caused the brake faiJ:are. AN1l SKID-ON will powide ant>-stid proceajon in all wod:iDg modes p oo ided tttili!y bydm1lic ptsSUte and eru.er primal)'. so 1 ••1aty or emerxencr

dearical power, available.

AIRCRAFT ENTRY/PILOT EMERGENCY EXTRACTION (REFER TO AGURE 3-10) NORMAL AIRCRAFT ENTRY

L

as applirahle, are

2.

• 3.

Canopy external latcll baDdJe - RDiate aft (c:loctwise- left silk; mcnter-dod;wise- right side) Canopy - Open

'l'AILHOO ~if tequued If dep ' cusure that the HOOK and DOWN sqments d the S'lritcbljzln are il]nmjmued.

EME.RGEHCY ArRCRAFT ENTRY

L

If Slill DO braking aaioo:

4.

EMER BRAKE PWR $'1ritcblipt -Press oiJ

S.

Ensure that tbe switcblight is DOl ill:umiaated. AUX GEN - ON Ensure that the AUX GEN ON light is iJ'nmjnatcd

Ldt extema1 fuselaF caacpy jeltisoa baDdle or C3DOp)' jeuison baDdle adjacelu to ii05IeW1Ied .,dJ- Pvll

I

WARHING

I

10 ensure C3DOp)' jettisoo, C3DOp)' dlooJd be jeuisoned only in !be fvlly clotsal posi•jnn

NOTE

AUX G~N will only supply decuical

PilOT EMERGENCY EXTRAC110N

powtt to tbe SO I w>da'Y bl'l!te S)Steal and only if (1) both ain:n:ft engine driYeo ~lOIS are iDopaative or off the line, and (2) EMER BRAKE PWR is 110t aamled or the ta~ has failed 'lri1lt

Do DOl ar:tuate eilhcr qtajon balldles.

EMER BRAKE PWR aamued.

After srop and if all~ are inoperative:

6.

BATICRY - OFF 1bm battesy off to cnnser ooe battay powtt for the emetEeDCY brakes ao the bot banesy bus.

ANNUNCIATOR PANEL WARNING, CAUTION, AND ADVISORY UGHTS INDICATION Annnnri:nor panel \VuDina. Cavtiao, aDd AdYisay ligiUs ilxlic:atiao. cause and tespoosive aaioo tequited by the pilot are outliDed in Fopre 3-9.

•

d tbe nov seat

L

Left and rigln eagiDe FIRE wam.ing switdili&hts -Pusb

2.

3.

APU PUSH switcbligbt - Pusb INERT - ON

4. S.

TbroUles - Off BATICRY -OFF

6.

Ejeaioa seat safety ' - - S3fe Sbooklerlw:ocss- Release 8. Seat belt - Release 9. SarvM~ a suaps- Rdea>e 10. Remo:we pilot

1.

TO 1F-117A-1

•

ANNUNCIATOR PANEl. WARNING, CAunON, AND ADVISORY UGHTS INDICATION

'~ '~ '~ '' ' ~ ~ ~ ~ ~

NOTE THE ACTION AHO OR REMARKS I.JSTB) IN THIS SUNNARV ME NOT CONPLETE NlD ONLY REFRES&IT PILOT INIT1Al ACT10N. REFCH TO APf'ftOf'RIATE EWEl'IIGENCY f'fiOCa)URE FOR COMPlETE PROCEDURE NlD Fed< ol ~ ildic:alUL Sei-ID ldla. 1l'rtR OFF If Jig'lllli'l'ahs en

l(ol) RPUY

Daacfhalbd.

...... , . ahla..

PITOT

llidool&iipOiiiUe~being~ liom

O>ed< ...... leal ..... panel tor specille .....

(CAUTlOfl)

any of 1h9probe haat ma.-s.or 1h9 nasa WII CJili!IUI& I 18ii4J&AQ is 1:)0 t::e*l fS when lhe probe is IDO haL

"ECS

ecs-.041••1Por~

I

(CAUT10N)

Olqogen QRif'Uy at (I' l:leloo!o ()..5 Iiiii; (I' or;oen ~lo&

ICING

Engine Helice ... "91

(CAUTlOH)

.

b1dian. -

-""'""""'-

0>ec1< ecs pane~liQI'iiS tor spedllic l1'dn> lion. Oou ~ ' appoplalie proc::eQns as,.. (JJi'ad. • lb II IICICiO I Cl'1ly.

0>ec1< ice-..... ligl'iiS an -..ice panel ll8rily 8lgine -..a $ldth is in OH or AIJTO r:-:s~·· : L

AHTliCE (CAUTlOH)

Bllw ~-..a- is in any posilion -

......... Wll>i•c:led pciiSiliol•

0>ec1< -..a ligl'iiS an arli-lce panel and I engine anli-loe is oft. do IICii - . . ... and / (I'~ COidlbiiS . . iW6::Ipaled.

fly...,-

FIGURE 3-9 (Sheet 2 of 3)

1-· 3-47 '- ~

I

I

Oil ~n.a 01\

lec,de,.- ar'ITOrG . ,"*"'*" .,_-on

hiRADSCCIWd ...... ~hOFF• la•LSRO!MT

.-vlcr30w NUClEAR

tcAl1T10HI

• IJi CcJ(a og Olh irdCt& ..., uoibJclog las nal

• P1Wiili11Qcfa

p:••••Q ,_ ,_.

• "t'

""'"".....

lfWar IG llclrrO Wailrc:*ln ~ II1CI 07-

I8Cib'llledcn rn,. F-117A-~ 1a.-1,J

; ,...,_,._JAil t:lraa'l cx:aaat•de 0-*..,SIIIilcto '"'""' -vna is .,,~ OFF. On . . grtlllld.l'lalle 011 ldlo, a1. rn ~ l'lalle 011 I 5

3

.., -vne

• b n-.:1 arly, &1girw C8mill be I . . . AMADUUJLC .....

fCtoliTOII OPEN jAIMS()R'(j

O'ed ldlo ard ~

1-ISopen

ClorTaon b8IDor ....,....,.,

....

...,

I I) 8001bs..nenl

01 R FEED SOURCE Is I ~ ..,.,_,lancsdechol-t>-~ "*"Y 500 lbs,

FIGURE 3-1 (ShHt 3 ol 3)

·

•

TO 1F-117A-1

AIRCRAFT ENTRY I Pll..OT EMERGENCY EXTRACTION

NORMAL AIRCRAFT ENTRY

• CNGP'f ..IEI'tKJirrf KlitCI.E: Pi.a:J CN f.DiiiiBI R.ISQ.IIQI: ~ IIQJIICih.l

STMER EXTEJIN.Al CAJIOPt JEI IISOH H1.ND1 E £:U ll.EFT A '58 &GE OR OH LOWER A '58 &GE SUIFAa. NJJICS(T 10 fORWAED 8lGE OF A

1'0~ 1BJQE~~WEU.

NCJSf WHEElWB.lH'W-

1

WAIUUHG

I

10 EHSlJRIO CNfOP'f .E II iSOH. CNfOP'f SHCU.D BE .ETnSONEDONY .. n£ A.UY a osm POSOllOtL

I

WARJUHG

I

00 NOT ACl\JIIJE BTHBI OF 1ltE TWO E.IECT10H HMO ES All E.IECT10H ~ SAf£TY LEVER 10 I.P POSi IIOH 10 SAf£TY THE SEAL

P'tUlT EMFP"'~ EX1"R.AoCt11N UIOTH BIGINES NID N'IJ RIEL SWITOiiJIGHTS - f'l.l9l 2.1HERT swm::H - OH a THAOTT\£5 - OfF C. BATTERY swm::H- OfF 5.E.IECT10H SEAT SAf£TY LEVER - SoV£ &._SIQU)ER H.tJDlESS- RElEASE (.£:!0t~ T.SEAT BE1.1 Ra.EASE 8-!HMVAI. lOT STRAPS - Ra.EASE 9. RBIO'>'E PUrr

-

• ·r~

•

... FlGUReJ-10

c•-• n~

3-411/(3-50 Blank)

TO 1F-11 7A- 1

•

SECilON IV

AUXILIARY EQUIPMEJ\'T

TABLE OF COI\' TENTS AviMic Sf$loas latrodDCtioa - •••••• -- •• -- •• ._I All1ftla8 Srst- -.. ---.--.-.- .. -.--.- -·- .. 4-33 Radar AJti_.t:r . ..... ...... ......... ..... 4-33 Dispb_IS Up-f"ro.t C..tnll Puel ....•.. - --- -. __ - -..•. ~ URF Ca-wwairat; . s,.u. (ANIARC-164\1) - ...... -- ....... 4-36 Air Data (ADC) ---------------- ._24 Soan \-..~ Navlpt* lalft&rr A.!

------..:. :. :-------------------------- ._I c-.-

Aeu,

a'· c-pookr ~'lAC) - - . - ... - - - .. ._24

s~ ~-~

·····---------·--·----- 4-42

........ ._2S ~·-- Srstea (ANIAIC-2:5) • - •• 4-42 C I 'trc.tnii'Dd ................... ._2S 1fT s,.u. CA1 ' :APX-111) ................. 4-44 TACA.'I ~ SJS~ea ................. 4-48 IAirwt4 AcQ • r..; -m ., ., . . S,.u. (lRADS) ------------------·· • 4-27 1-mat l'imptiM s,.._ (ISS) .... ----- .. 4-2 Raaor ~ S,.u. ..................... 4-30 Sns. Update PI eudmes .. -- .... -..... -.. 4-37 I !aecfi-c Srstt- (A1 ' All.'l--111) • 4-92 RMor ~ &'-iser s~ ........ 4-30 lull RCS L.-0 ............ -~ • •.••• 4-30 " " " ' - Dellftry Srstea ..... -- -- . -- ••• -- - 4-93 RCS Eeha • s .•.•.•• •••••.•• ••••••••.••• 4-32 MiMics Sutlsrst-s Oot-Beerd Ttstiea . • • • • . 4-9S V'ocloe T - RW J:Ue Dispby !nc!gonrs (MDis) {F!pte

Tbe Ultqtated a-ftonics cnnfipruioD d Jloe F-117A (5ee Fr&~R 4-1) 1m bem can:r1111y sdo::tcd 1 0 - tile dfeaM:oess d Jloe Uaaft W'llllocn COOiip 1 tile ad nntaganOI ADI wtUda prcsalls AHRS en.c.S.: ud ftipL1 tileaiuu data fOJ" tile TACAN ud llS modes, the HSl wDicb prOate sdea sftdl10 facililate IRADS, BUD.aoo MDI display mnuol (see F'"tgUre 1-~

Ven:ical •'docity is displayed by a fixed scale. a IDO\ing pointer, and a four-digit rQdouL The scale bassbon lidt matt;sat SOOfeeo per minute intenals. and longer mans at !be 0, ... 1000. -liD ), llld - 2000 feet per minute points. The •-ertical •'doc:ily is disjAa)QI as a readout adjal'>/

NO

NO

NO

NO

NO

YES

SlCER

131

141

'YES 'YES 'YES

PfiETRAO(

POINTING (2)

AVT

FREE

PfiETRAO(

loiPT

AVT WPT (7)

I~

MANUAL

LOFT

NONE

aJB)

SEARCH

I..EV9..

IRADS SU8MOOE

(NONE)

ATTACK

SUI'f'ORT

NOTES:

(I) The pi!« may sdea any one ollbe Dine swiu:bes ao the UFC pand lbat CXIDtrol six $leering modes and t1uee auact modes(~ AlA~ and AIG MSI.are inopenlive). or be may aot sdca anycf tbcse modes and opeate lbe airaaft iD a ao-steeriD& mode. (2) AJ IRADS llmHJD. and 110 mode sdeac:d on l.be UFC.

(3) No $leeriliJ or attad: mode. (4) AZf1 $leering mode. (S) IRADS commanded 10 CP upoo sdcaioa oi LVL or LOFJ: The CP Slbuode is 1.be same 5>Jbmode 1bat free sea.rdl wasiD upoo sdcaioa cf the anad: mode. Free sea.rdl can be sdcac:d while iDan anad: mode.

(6} IRADS is oommanded to CPIPT upoo sdcaioa cf urL or LOFt {7) MFT is DO! lmlilable direaly from Free SeudiiPI: System mDSl default out cf AVI; or be sdcac:d oat cl AVT. (8) Sequeoa: and ttact dla.Dzes iporc:d by free sea.rdl mode ...ilen iD AVf or MPT qd•*• «5 Sightlioe remains oo ~ withiD FOR limit$, iD MP1: FIGURE 4-7

HUD CONTROLS The Up-Froru Cootrol (UFC)pand (see F~4-8) indodes l.be {ollovoing CXIDtrols: L

Reticle Depcssioo Sur Wheel The reticle dep< essiou sw W'bed is located oa lbe left side cf the UFC paneL The sw wl!ed CXIDuols the BUD $laDIIJy reticle, 'lll1licb is med in arimntb on the BUD venical axis, and eli$. plays dqxcssioo angles from 0 milJiradiaDS(mr) at lbe (usdage refereoa: line (FRL). dDwn to -250 mr. A numeric readoot oo the reticle in is a WSC oYUride switdl,

•ilich. wllal set to the L position poridcs

IRADS video lbe left MDL When either the L orR position is sdcaed, HUD symbology is aot displa)'c:d. and the a...,.;,tc:d MDI mllSl be in the bactnp 'ideo dearo-opdc:al (EO) display mode. When the swiu:b is iD the N p !Sjrjuo. BUD symbology is pra.ided bJ the WSC. Velocity Vedor Switdl

A no~ C'ORM-cAGE) vdocilyveaor (VV) swiu:b is loc:atc:d on the left center cl the

CXIDuast.'Wbeo'lk"loob'k'ln"lbe"1illi~1:7FCpand.-whentbes•ildlissetWIIIC'0\61!

4-10

TO 1F-117A-1

UP-FRONT CONTROL PANEL

I

aUla! IIEPII£SSIOI StU WilEn

2

IASI'B -

coma.

·(D.U!AST

Gt.ci!R • WGK:l6S

3

l!roliiDAUIIQil SWlTO!

'

lilli!lll CAa \'9.DC1TY V£t1Ui SWITOI

-

----~~S ' 1 S

'

IDICWSIlflil! - 5lllill. Dm.IITlB SW110I I.R: u Qntrot knob. UFC panel lighting is CODtrolled by the rowy HUDIMDI light swittb 011 the left side

pnsiljon !he HUD •doc:ity •-eaor isc:qcd in aDmoth- When i1 is set 10 the I'ORM pnsilion, the HUD velocity- is UJIC3&Cid in 2Zimut.IL

S.

Rai::le and Symbol Bripmess Cooaols

panel

T- CODCeDtric HUD reUde and symbol k!nobJ!¥6d

-

tic:le ••• o-ed

iicle. bl &Ned aogle io o:lc:aD . . moved

n.s ~ 5Zill pi"""""'1

Deduuer I

1.

O»tbiOted

SecadllytoeSV• . .

T~ :o..-iiiQ Slil pro-

iemo>'es:

HUD

a. Venical Ydocity indicatot b. Tune 10 go display

c. GiOWid speed display d

~display

e. Destination anmbc=r Sensor Display

a. Venicallligltt patll jndicamr 1). B'onzoo.taf de\iallOO-tlldi:ator

4-12

d TACAN D ME display

s_.,.- Display a. Le¥d aDd gaiD scales b. ALG acti.-e jndjraroc (A)

DECU1TTER LEVELS

c

c. Bant angle display

MDI DISPLAYS MDI DISPLAY DESCRIPTION

The ~(left and ri&Ju) MD!s are idelltical, and dispia] a variety of geuG2I flisb.t and system iDforma· tioo. and ima&e data under ttrta:in Olilditioas. Eadt !>ofDJ bas fi.-e mulilfuuaiou s1rildJes along cad! of its four sides. There are eight MDI display formats wDicllaredm-en by the WSC. cad! wiih .ari:uioasdepen in the booom row ol tile !>oJDI switelles estl!blisiles wbicll fornw group is seleaedoo that MDL wiih the t,_,poaps simp!] alter• natiJl&. The pilot's display format selections pre-ail. ,.ittluo o:ttplbb. Upon ICllb) 10 an attacl IIIUde;-~--_;o

TO 1F-1 17A-1

dloe SMD is di!:plajed at111 1ita"r oa tile MDI w1bdl b8s lllc HSD poep sdeaecl.

apN!•-

"lbe MDis proo;.Je saaoe blct-llp 10 allcviate P'"!i!i k Wlures d tile SD, or tile VIdeo ,...a 111the IRADS~ Rdcr10 ~ BM:II:op. llus senion These ~ vatioas ctiptal readouts oothe MDI dlspbl)'s. These readon•s ~COftSISI dan tdmtdylll&labd followed br the cum::au numc:ric ~oe ollbe i:ndicated p•amaer.Jf'!IRnlua~~i~ lbcse lfQdouts as -vaibble (for ...,mple, tile ADC is 1101 ~ ~ uw ainpecd). the unmeric valne area oCtile radoat isN.aotrd wbile tile label lCDIODadisplayed. Botllllle l8bd and lllc data aeadnuiS w11ic11 are reaoowed fnD the BUD br lbe dedctur fuaaoa will be I I S,lllbob, $Ddl &$ tile padt loddcr, wtadl clo- 11om: a label. are bbntrd ~ lbe ckMala daD is uaawajjblk

•""d'f ...........

laa tile eveau lllat lbe WSC is earable 10 P"'ode dal:a 10 u MDL dloe word ~"ill BY appears and Oasbes oo lbal MDt ud also oo tile HUD -4 dloe alreacd MDI is clriYia& lbe BUD. This word iJ writteu iD vcrr ~ letters o--edayiu& the display wtUcll was lasl updated br the WSC. 'Ibis latter error fanaioe is~ vided br the ~IDI itsdL If a llastiq STANDBY (or a sc:talllbled display) appe:m. the condit- cau be mn-ected br cyding the powu on the alfcaed 1!-IDL MDI CONTROLS

1lne MDI dosplly cootrols are located 011 lbe face dille MDI (see Fapre4-9).11le appcrfoar-poerpa (0FF-t.1Gtrr-AIITO-OAY) ,...a is used 10 lllnl Oil and tm1 olf I'O""C'" 10 lllr MDL Wllealthe S001Id:l IS set 10 tile !'>1GHJ; AUTO. or DAY p wj1 Mw power IS tllt8Cd OL 11le symbol brii:Jttne«raJI&C is iotaeascd 10 pnMde f. . - ' r:an&e lwi&b•.....,. a.trOI wt.eD tile S'W1Idl as set 10 lbe DAY p wj1 • • and IS 1educed 10 restrict the rure olsymbol bripuocss 10 the ao-.r IK d the aonaal ranz.e wlleu the !Wildt is set 10 lbe H!Gtrr poac.,. The AUTO p>-e separate lq •4 iadicat-

ia& tile auJ'CIIl szate_ Aler1a

Akm are cfi>played ia .,. alert display area located .. tile loft:r risbt coma- Oil . . dilplay (CXDa&S 00 botll MI>Is. Alem resa.l:t fiDE • "The faimre d boU buses 10 a terminaL • Cer12iD Wlun:s ol ~ • Failure d prdl.ipt daD 10 RKX:eSSfully laid iDID the WSC or ED'TM• A biiJI& saorc foiJowina a wcapon release

cxcnmancl AlcrU ~ intrDded 10 noul'y the pilot 10 use the saatm display, scmor display, or CDU for fanaional fault iDf0011•tjoe oa a Rlbsysteco bulL 1}-pical mbSJSlCSII faikiRS 1:11!51 be rit S..ntdl

.-enical •doc:ily is displayed as a readout adjaceatt 10 1M 0 feet per minute tict mart. aod is aa:mate 10 ten feet per minute. The llliMn& pointer mends £rom lhe 0 feet per minute tict mart to iodic:aae tbe .-enical velocityAltitude Scale

The minim111D enronte altitude {MEA) S1ritdt allows 1M piloc 1D inbiJi1 the display oi the breal. and -2!XXI feet per minute points. The

7_

The altitude scale is a .-enical..-ing display ol altitude rdeaeooed 10 a pointer fixed at tbe middle ol the altitude indicator boL The scale has short tict marts at 100 Coot intervals. witb louger marts at 500 foot inter.als- Altitude is •ritten in five c:fi&its next to each ollhe 500 foot

Wbcn tbe MEA S1ritdt is 1* I, the MEA legend is bca:ed to iodic:ate bolh tbe breal:away X cue and tbe 'WOice olen me att inhtited [(tbe S1ritdt is jMessed 1ibCil bca:ed, !he ailaaft asc:eodsabo¥e tbe MEA, or a manual or auto aact dJange occurs, the bca: is l'eniOO'ed aod tbe breal1lice alcncue are enabled

apia [( tbe airaafl ,_SI mtc below tbe MEA wbCil 1M MEA S1ritdt is enabled, the Dashing breaknay X cue is displayed oo tbe RUD and VSD aod the 'WOice alert cue AUTIUDE (n:peated) ~bean:~ illlheb.eadset; BodtatStxatizacentil 1M reataw3y Ole is a lalge X which is displayed flashin& wlleoe>-er tbe barometric refereoce altitude is at 01" bdow tbe minimum mroate a!Lirode (MEA) for lhe current TO desaioarion point. The me can be inhili.ted by pressing lhe l\.fEA swildl atlhe 10p of tbe VSD.

WSC VSD PITCH LADDER DISPlAY

When sdt.bcr MDI is tnmed olf, or powtt to aD MDI IS mterrupted. The eovnc sdcc1 and beadIll& muter mtiSl be reset ~ tbe ~ bob OG 1J1e auxiliary~ panel

Present ill Ul'f attack ._se. The a eap·"'' llle HU0 is detected l n llle ~~ lbe HU0 use.lf. « 1M PIU, fails. tile Ollly display caplbilily remaining for llle Rt10 is !be manual • -eapoosddn-ety reticle, wtucb is sepen1e llle rea olllle HUO

rro..

dl AD! (-.!ticla dtsplajs llle suac aettiftc dala as !be HUO and VSO., TACAN liiiOdes):""HSfepro.1rJe$bealllq ~

aDd

n:s

4-23

-

TO 1F- 117A-1

daul). a!Umaer. ailspa4 ioodicuor, oerucaJ speed in-

clicalor, and anpe-d-tilld: joc1caror. M ULnPURPOSE DISPLAY INDICATOR BACIIDI display fOI'IUlS OG eilber MDL lberdore. aay ooe d l.be Mawti .,.. be .. I ted- llodo MDis - - liC!OGSf). wbida '111111 aid fa!!lt .... _ iD l.be eveat bocll !>IDis s:bcald !aiL . - '*bp is poUtidtd bJ lhcdectJ•NIM • lpnQI ADl wblchpraentsARRSat· Illude and flqbt diJeaor data roc l.be TACAN aDd U.S IDOdcs. 1be HSI • ilicll promplet:ioo ol the self test. the EDTM bas failed

Tbe aitaafl sboold 001 be no.-a unless the rond bas bceft insetted into the EDTIIfiU and a three-f)anda.o E"P"nded DataTransferModule lnitcdaoe Unit (EDTMIU).

Wben power is fusl applied to the aitaaft. an EDT· t.nu sdC-tcst is performed which takes approlimatety ~~SCCOI~ During the sdf-test. the EDT!IiiU FAlL ligJu illwninates. lf the FAIL light remains ao after completion ol the self-test. the unit bas failed. Erase Control

EXPANDED DATA TRANSFER MODULE (EDTM)

•

The EDTM is a uansportable avnpoter memo'ewithiD oae stCODd d tbe failure.

Alter a W-WSC (WSCI) recoofigutatioo the pilot sbonld; (l)verifythe displays. ixd!Jdiu& the COU. are ftmcriooiDg lJOllDaJiy; (2) if in an anadt mode. •--erify !bt UFCP rernains in the ianllll AnacL

dciu...,_

For a mrapkte ol the lRADS s,-.um, refer to the F-117A Utility Naomadar Weapoas Oelr¥uy M.anual (1'0 IF-IJ7A-34-l~

RADAR LOCATOR SYSTEM The Racilr loc::alar Sygem (JUS) IS DOC >UppOi ted ud 1SdisM4cd The RLS coat:rOI pax:~ (see Fogan: 4-19) IS id . eel to allow the U~ &A Airs to be mrxted lor ~ « dlpiO]ed lor KiCICU.

4-30

-

-eauce

RADAR CROSS- SECTION MONrTOR SYSTEM A radar a= ••• (R.CS) ~system IXOrides a >is:::3l iocli ••;. •• liiU the airaal:t is cvnrirl& ia r:adar-detcaable When the RCS MON SWIIdt. located on the mazer test paDd Oil the ldt Side pax:l (see Foptt 1-24) IS sdeaed 0~. doaQaes m the nda.ra= reaioo exposnre to radar oibsa \lli.UQII tbaJ advuseJy affect the COIIfi&utalioD are iDOIIl10red and amber cauUQII baJlls located on !be pate5lueld ~ enabled 10aiMse the pilot lbal racl:u clctCCIOJ f*cbability is iacrQsec1. 11tr camioo li&JitS mdude theantemmdowa (ANT DOWN) light. tk RLS aotnna doooR (lU.S OOWI'o') ~and t1oe door (LBID and RBID) Jipu. Wlll:ube RCS MON sw1lda io the OFF positioa. RCS Rllm•nrjnz ol tk ..aaCt COilfipratiaa is DOl iD dJeeL

a

c-"'"•

*"" •

RCS LOW OBSERVABLE RECORDER SYSTEM The radar a= mtioo (RCS) low observable reconler S)-stem records daJa f10111 the aVIOIIic system·s MUX bus Cor mmpariout the 225.0 to ?m!TIS llo.fih fre.

tid1

"""":J:

wortiD& chaond ooly. For ~r.~nsminq purposes, the goan1 c:baDnd {243.0 MHz) may be selected by placingthe M ANUAL- PRESET-GUARDswitdloo the allltroi pand 1D the GUARD pasitioiL This aorouunicaDy sb.ift.s the main rm:i• U and tmnsminer to the goanl dlanod.

Ther.ldaraltimeleriXllltrollncb. located oo the lower ldt le with sccun: QliDdlorriratioos KY-S8 cquip-

ALTITUDE SCALE

UHF ANTENNA SYSTEM

The altitude scale pnMdes markings from zero ID 30XI r~ with~- ioaements below J(O) r..,. and m-foot inaements £rom 1(0) 1D 30XI f~

1fbe UHF antenna S)'5ICDl ronsjqs oi twO rcuaaabll: antennas. upper and lower. Th~ upper antenna is located on tbe 10p oi the fiJseia&e behind aDd slightly right ol the air rdueling~e. and th~ Jowerant&!:rllla is located oo the bottom ol th~ fuselage bdtitld aDd left oi the IIOSieWbecl (see FJ8111e4-21). TheS)Stem pnwides automatic selcctioo oi the antenna ..-b.io:b is receiving the strongest suitable signaL In ~ tranSiltitting mode, the receiving antenna ..-b.io:b IHe•ioosly was selected automatically is used as the

LOW ALTITUDE WARNING UGHT

The red low altitude 'II'3J1Iing liglu is located at the 2 o'doct position oo the face oi the r.ldar altimeter, and cnmes oo as the altitude pointer clts "'"ts throogll the altitode indicated by the low altitode index arrow. RADAR Al.JlMETER .AUDIO WARNING SIGNAL CONTROl KNOB

Refer to lntetaXDIDtmic:ation S)'Stem, thissu:tion for information COIN> • ning the r.ldar altimeter warning signal allltroi t:odl.

UHF COMMUNICATION SYSTEM (AN/ ARC-164V) The UHF communication S)'SterD and associated aote&Da S)'Stem provide amplinlde-modulated twO-way radio commtmic:atioas with other airaaft or ground saatioas equipped ,.ilh similar UHF equip:Deru. The UHF radio is capable oi mainuining twO-way lineoi~t COfi!!I!Unicatioas~u a A01!!3i~ tan&'" oi 22ll nautical miles dq>enc!iUg oo the fre.

4-36

•

IDCIIL

lJ"'nqnitrin&

antenna. The UHF anrennas are cs·

toerlded and reuaaed by tbc UHF Antenna Enendl Rctr.la (ANT) switcb located on the antenna cootro1 panel oa the ri&Jlt c:oosoJe{see Fogare 4-22). The ao>toennas mDSI be Clleoded 1D tranSiltit Oil UHF; boorev· er. with tbe antennas r:eaacted UHF ~r.~mmis9nn maybe tm:iO-i" & 1 WXI SQUELCH S'll'itcb is prorided on !be UHF paad. Tk OFF posnioa dis3bla the-... rec:enu squddl fgnaic)n wbile the ON pnsu- proVIdes ..... sqtldcll npeminn

L

l'miet freqoeocy c:arcl - Chedt that llle desired C.equCDOies ~ beal preset-

b.

Mode sdcaor S'!O=tl - PRESEL

c.

Cbannd sdcaor sorildt - lam 10 clcs:ed d:la.:IDel

d.

Anrenna - EXTEND.

e.

Nwctioo selector $W1ldl - MADI « BOTIL

(.

TO:O.'E rpngnit pus!>butiOD - Prc:sL

ns

UHF MANUAl.. FREQUENCY SELECTORS

F'...e UHF manaal Cr..q:oency $deaor tacbl aft pn>wkd oa tlle alOUtOI paad for settift& lhc diciQJ iDdialOIS 10 ury ooc ol the available 1IDl ftequeac:ia. The IMXIe selector S'll'itcb must be in the MANUAL

UHF VOlUME CONTROL

1lle VOL mouol boob co llle UHF mouol puc:! >oialnc tuatioa ol a tone tn1IJSmit [UJliCtioo.

-.vm-ap before uusmiuinc1- Press micropllone swudl 10 ttansmJL Release miuopxm.e switdiiO rcoeive. 1b ua.osmit aDd reeciwe on a frequency 111M on the

NOT£ 1bae tnongurSSj!w is DOl inhjbiraf witb l.be aatencas reuaaed It is I'""'"'mc•(!ecl ~ !be tonc ...-itt!~ DOl be dqA essed .-ab

u•=nr rrtAJ1cd

•

preset dPnnd iDdcs ean1: IL

I>Jode selector switdl - MA.'IUAL.

i.

Manna! freq.r.o m 111ne . . sq-..u. Tbe"'ii CpalleD'e'"•--s..-e"•''""'

4-38

aJJd tbetdCli'C more jam-R:sis1attl as more segments are a:sa1 Tbe WOO iS catered intO cme or 1110re ol the SIX preset d>annds 20-15. Tbe taiS, 1mits, aJid ta>lhs dililS are used for the WO O "'*''"'"'t Tbe llmidttxUs aad Jboirsagd!IJs djpa ol dJmnd deter· the fturaeocy boppiDg rate.

WOO ENTRY

The WOO & pormaily entered bdCli'C Oiglu. but it is p sfoi,e 10 CDJc:r il iD !tipL For a new WOO ft'C. qucncy e:uuy. saan at cbnnd 20 aacl me the sa.e method as., aoteriag preset f•eq•< irs iD the noraw mode liSZI1& u.e fteqJC&} Dabs and~ PRESET butiOIL After enuy, a smglc or dodJk beep IDCIC IS bard iD tbe headset Jndocating that chaD• nd 20 IS e.DJCred IDID preset llleliiOCJ- Channds 19, L8. 17. 16. and l5are seleacd tD that order Cor prue.t ftequc:ncy enuy. After eacb amy. a SUJ81e beep iS beanhuotilaCtc:rcbannel l5enuywllelladoublebeq) ..JS beard Jllllbi:zlmt !hal tbe radio has ~cd all six WOO C1itne$-

-=

•

TO 1F- 117A-1 TOO TRANSMISSION

Otu tbe double-«Jnc bmst is 1tui>ed. at tbe condusioa cl tbe abo1libble 10Xl frcqueucXs. T1loe IDOde sdecuw switda IDUSI be ., lbc MAA'UAL pnAIMX!

A-3-2-T SWITCH

'Jk A-3-2-T swiu:ll bas 4 plljtjoos placarded A. 3, 2. aad 1: Whal A is seleclcd. the actroe mode ol the UHF radio IS aanatcd. V.'hut 3 « 2 arc sdeacd. manaal frequency sda:tion is avaiWlle pnMded the IDOde sdec:tOI' swUcb is in MANUAL The T position IS a WI!!!CI!•ary posi!ion which enables the radio wacc:cpc a aewTOO fer ap to I minute after selcaioiL. T1loe T po6ition is also !ISed dDtiJia the em.......,. star· tapollbe TOO dod:..-.. TOOlS- .,...ihhh froaa eaemal $DGta:S.

UHF SQUELCH SWITCH A ~MX! SQUELCH SW1tcb IS pooldcd OD the UHF panel. Tbe OFF p151tion disallles the main rcCltl\'er JqQdcb function. •i>ile the ON position proVIdes DOmlal squek:b opention.

UHF VOlUUE CONTROL Tbe VOL aJGuol tDilb oo the UHF CXJAUOl pend 'IOiamecocuol f« DC Jecarca:>diorecep-

UHF fP1"' Y!Idl- Sa to desim:l cbaftlld

~

,.

1b opaatt< ia ....-IIIIOde: L

Frequency - As desired

10

de·

'•a -{ucler .,.ue&dloa.-uoclelt.c:a.ld}--~-

- Lift

4- 4 1

TO tF-1 11A-t

L

Preset dlannd pusbbuuon (under aa:ess door) -Press

SECURE VOICE COMMUNICATIONS SYSTEM (KY-58) The ~·Uc:ecommunirn•ionssystem isasedwith lbe UHF a:mmunica1iaii'fnys{em W i*Oiide ta:a:ma! (plaill) aod cipber (coded) mmmunirnrions. Operalion rl the mmmunicnions system is ._.,a! .men the KY-Sl!CICider is noc installed. The KY- 58oontrol pa.ud (see Fopre 4-26) is located oo the right CXJDde. The system is powered from the lefl •••eruia! de bas lluoogll a KY-58 c:ira1it breaker located in the left elearicalload center (E bay).

KY-58 CONTROLS AND INDICATORS MODE SWITCH

rocary mode swilcb bas four-pncitjons (P-CLD-RV). The p p3Sitjoo enables plain IClll cpc:ralioo. aod the C positjoo enaNes cipber tell cperation. lD (load) positioo allows Y.lriables to be read into the selected memory tqisler. The RV (rttrive .arieble) positioa allows transmined variables to be ...,.;."ell aod placed in the selected memoo:y rqisler.

The

SWITCH VARIABLES DESIGNATOR

Preset p3Sitions of the S'c· ~ wllb lh~ mode swiu:Xs for 5df-tCSL 1:11 MON (,.,.nnria&)p.Ytiwlbe ~ lcbt ril bliakon and ell IO jpdje:atr tlpt 5 HsfuL..ae:w I 5l!l 5 are ~ made il tile Ul!OCk(s) sdectec1

TO 1F-117A-1

•

IFF CONTROL PANEL

I l

-

4 CIHlUT S1I110I 4 KIIC.A.TlCII S111ltH

]

-

• COD(

1

IIASID! snJI:1llll SW11tM

•

IAb-OOHIDII SlfltCJI

'

I'!IIIIJ1rn:A11CIH:H'OSfll(JI S1IYltH aiDE snJI:1llll SWI10£S

Jl

S1UCf S1I110I

;....--~-~ I

AGURE 4-·28

MODE 1 AND 3/A CODE SELECTOR SWITCHES

group is 'lrilhbeld wben tlle liP switch is in the OUT

Six Ill~ l)pe S'tritdtesand adjan'nl ~ are p:fade I switch is numbc•ed 0 thron&IJ 7,the other is nmnbered 0 t!uoup 3 oo each baJf d lhe drum. The Mode 31A s.'ilcbes are nlllllbcred 0 throa&IJ 7. Spring-Joaded cernerin: derents ~~ ambiguity d selection.

TEST UGHT

IDENTlFICATION-OF-POSmON SWITCH

-

The identif"JC21ion-d-posirioo (liP) switch a~~~trols ~taosmjssjon dliP pulse groups. Theswitch bas 111m: positions, MJC. Out and a spring-bded IDENT posilion- The liP timer is ene.gized for tbiny secODds 'li'lleJl the switch is momentarily bdd in the JD. El'o'T p oci••·~ and liP rq>1ies will be made if a Mode

position. The MIC pociti•ds inaahe

A green TEST tight d tlle ~test and tum-todim l)~ is pro.i:led 10 indicate sarisfaaory operation of the transponder for se!Hesu d !>fades J. 2, 31A and C. W'ttll lhe RAO-OUT-MOS switch in the OUT position and the masler switch in the NORM posi•ioo, the tight comes oa when a mode switch is plaa:d in the TEST positioo if tlle se!C-e pancm. Jlocatine oC the l.c:tiS ud IUU1S knobs

ptt&ed • case oC aH:IIamld iDtcrCerence ill IKTIR IIIOde. Ia case oC tempOI.& J s@lsllaos, •dociiJ ,_. aorics tec:p tile bc:aria& 2nd nmge jndjcariOiiS uack· ""'for ap 10 3 aad lS stu•ds, respean-ely. or an til the Slplll IS tUCqlrin:d. Tbe TACAN set p cMclcs rwo l}PCS oC self-test tDildc:s wt.idlpoodcs a COIIfi. deeoe test oC the SJ1lem. The iillltlaal self-test 1-'oe ISIDilllted by setting the mode switcb 10 TIR and de· preswiJ the n:sr pW>-bali.OD, thereby d>eclaq truSIIIittcr output JIO"'CC. tetti•cr opcrabCG. and prooidma a COHmo eN at•., and a 180" bea.nnJ swaal. lf the n:sr ipdjca•or is slill 08 at the CDd oC lbc: self-test ()'de:. a malluoaioD or failure bas OC· C1ln'ed. Tbe test slooetd thea be "'P""led m tbe REC IIIOde. If tile rm gdira!or IS iiOl oa at the a.~ ol the self-test ()'de:. the malf.....:u. is ill the UUSIIUI· tcr and tile~ iafOl'IIDlioa is 'r.l!id. IC the "1CST ..,..,.,or IS oa at the CDd oC the self-test qde • tbe REC mode. aD iafOl'IIDlioa tettiw;Jy 10 sbow that the lest '""'a tor IS operarioeaL A TACAN aznsz:riuc:r udloo- aeoenu fult has beat deteaetl if the TEST tipt iiiiJI8iDales at UlJ other tae tllall at tbc szan cl a sdf-tea period. Bear· iDa udloo- ctma....- iadjc;uioos Slll.l be preseul • 1lal tbc TEST ti&Jn is OIL SUCII iDClocaliDGS mold be c:itbet pattiaJJy usable oo- lOWly onaoouate and sbould be aoss-dtected, DSin& e--ery available means. The pilot~beprepared foctheposgbiilyclTACAN eqoil""''"" Wlure a1 tbeTESTiight iltcmiaates rex 110 readiy ~ rea50IL The selftal feature em be t•a · aed a"M"fiaady by rocauq eilber dP~ sdeaor oo- iiiOde sdenor bdJIO-MIIb pM••

raoe

-r

•

•

TO 1F-117A-1

TACAN OPERATION

a.

Antenna - EJCJ"Er-"D.

b.

TACAN lliOde !dectocCXIIluol- TIR.

self-test- llllteTESTiigbteadin&) • Gl1lDDd Sperd • Ground Ttact • Headin& (true & ~) • W"llld Vector • Alblode • Tome 10 Go (destmat. .) • FszW,.rrrt Toe U AnwaJ • •

•

DlstaDcr tO DeaJMt. .

•

Deslnd Ttact

=

The INS 1bc iptioo S)=sD aad p:ooidts lAc follow1::l& f awhes

•

AUGN li&lll will fla5h until a NAV IDOdt IS sdecltd The dapsed time alignmeftt, and tbc m~ aa:ancy ril vuy accordmJIO tbe 1)-pe o1 a~cnmem Stltatd

r..-

OESPIHUGHT

cro despin (DSPI'o') lipt -

Caauols p:iumy po-er 10 lhr INS

"f11e

Ptooidcumeacsfora~t~tdl. «by BIT mmated sllmclowll. tile light iadil:ates a fi->e =inute 1Jt0 despin seqoold be condutted USIIII

"""'AI =•iptiou cma

Displays -;ptioo cbra and S)"Sl- opera. lioaalsuuos

Stkcu opttatiODal modes Dap1:rJs aad ~BIT arutmrio•ion The CDU call also be astd 10 load and disptay desbJIOIDIS 111 llu! N-WSC. The HUD and 1M MDIJCMDI •n. or eater or deac r•maiMs Otberwlse. tbe upper 21 d labds 011 tbc:ae swilmes pcrwos. TK upper label (una jews are all d tbe alletD&Ie aaJOa I)Jie-

Tl:le purposed tbe IIIOde daDJe (MODE) function is 10 drect an N-WSC IIIOde c1w1te. 10 ooc:aide tbe I'Oil« support bane.y (RSB) interloc:t. and tbe nxor SUJlPOII I'O"U asvmbly (RSPA) interlock. at INS llU1HIL The IIIOde dwl&e fuattioa is ~ eaioo, and ai'W3)~ ;nUable as an oplioiL Wbeft tbe MODEl MARX SWli.Cb is p I, a dleclt IS -.le 10 detcrIDiDe rl tbe p .;r; •• d tbe ...;ptioo IIIOde SWli.Cb bas d:wl&ed -.e tbe lasl ~ d 1Aa SWddL H so,

•

TK 111tc:nctioll d tbe olbet - p11111 DWIIber oae ---.fOFSAIMI~r.o(~ lbeta•essetea""nMp•iMIDOde~ f!!W'!!CWwnlullber!lfftCtjnnsiSasfollows:ThcOFS AIM I and OFS AIM 2 swircbcs ~ 10 eaivate a poP'iM display for tbe OAP and 10 speciCy tbat tbe deo'aiJOQ/minimam eruocne altitude (El.EV/MEA) and bearin&/~ (BRGIRNGE) fuoa._ are rebtiYe 10 tbe OAP m.ber tbaD tbe desm•uoa spcrif"lCd by tbe BrTIOEST •illdow. Therelcn. aan-atica d tbe IaUer ' - hmajms docs - dre:Kuvatc tbe OF'S AIM laodOFSAIM2fn-ajcwsl'kle~aC­ fea Gilly tbe CDU ~ Sdectioe d offset 'M!••tslor IRADSated pwt-aaod HUDdisplay is • ••1•ist. d buwCLA tbc:ae swddoes and tbe Woctk olbet ........ swib:IL 0-

Brfii::-"'J{ swildl isp I sillmltiiMlO'ISI)' with tbe MODE/MARK, tbe RSB or RSPA dltedcd is._... ridden. and tbe IMU sequeDCiQa ~ Thc intcrlod:poceastber:yros,audslloulc!Oillybeooenidden iC .operwouJ r.eeessity diclates.

The matlt funrtion 011 tbe O>U IS iuopenti¥e. The MARX SWli.Cb is la::a!ed 011 tbe lcft and ai&JI1 MDiol CNOIL The aad: fuauica is desai>cd aDder MDU CMDI M1Ptica Fw• r; MtS lllis R'C"!!!I

Hold

The purposed tbe dal3 bold funrtion 1$10 stop aDd tbe cly1wDic dal3 in tbe nwa dlsJUy area simlllta1.-s!y at tbe time d funrtion aciM.1.ioa. DMA HOLD IS aa alte!ate acUoe 5W1lda, and is availabk capt w1leu tbe ~ ~­ acmal ~-fa!IJb!!lislle n.aee. and alii!D!tr calitnt.. faca; ... are ac:IM. UpoG p:essiq tbe DATA HOLD swittD wbeu it is iuran-e, tbe data bold (~ " aaiv:ned and aD dylwuoc data displaj$ cease updatJn&. The daUI bold f~ IS-atrd by llfC$$in& tbe DATA HOLD swildl apm wbea data bold IS aaive.

Pwpole:

1l:l drea a dwl&e in tbe poutioo d tbe INS~swueb..

Anillbibly: INS mocle owiuil ill any pou•Jon ea:rpc OFF. AlJXL or A1JX 2. L ISS 80de S'll"ildl - Set 10 desired INS 80de L MODE strirebli&f!t COllie$ OR. 2. MODE srrild>lish• - Press L The INS mode odeacd ill Step I • m drect. b. MODE ~t ps olJ. lnctemenl, Decrement fUle1lons The~ d tbe iuacw:al

hmaJoa is 10

dloaJI&e tbedesiaarjnp refetrcd 10 •

Pw pose:

Swps aD data ddplajcd 011 tbe cou e:rcqJI ATF RNGE and Ali CAL

A~

INS IIIOde S'tl'1ldl ill any po9'iM ea:rpc OFF. AUXI. or AUX 2.

1b stop displayed data: DATA HOLD switeb - Press

I.

L

Data dispU)-ed on CDU is Popped

1b deaal\~e: 2.

DATA HOLD S'IO'ildl - Press

4-56

tbe O>U 11111iu display area 10 tbe DCXt . - : ill tbe prdloaftt data seqa "l1lc dta ement ( • ) fll:IICID ellaJ>&cs tbat dest-•0' 10 tbe p• li•tt des 1D ~ d&tL TKalllllberintbeBITIOESTwi.towindieares 'll1lieb desiuat,. is refetrcd tol8 tbe CDU maia display area. and is incremented or dm UDUUed accordin&IY.Theoe oin&Je aaioo...'\tebeoare ..uable wbeu lhe BrTIDEST window isdispb)'lJII dc:snuabOa daJa. md tbe ke)boanl is DOC in tbe data eatty mode. Upon CX>Dtiaaocs pressiD8 d tbe mcremau or dmUll - Press a. "lbe C)'de ends around, and destina:lioo point 99 is di:splaj ed in the BITIDEST window. b. Beating bias is displajed in the CDU upper main display window.

[I] OJ Purpose:

window.

c. Raqe bias is displayed in the CDU ioorer main display window.

Displays the destination point latitude and lnngimde, or elevation and min>mtiiD emaone altirade. in the CDU upper and ~ower mau. display wiDdows by dtan&i~ the desinatiOII point nufTber in the BITIDEST window.

A•-ailability: !An...QNG, ELEVIMEA.'TRJUlTG. or DTGIETA swin:bligbt oo. and the BITIDESTtrindow isdispla~a>desli­ nalioo number. 1. !An...Q!'IG , ELEV/MEA.. TRK/ITG, or DTGIEL\switdilight - Press

10 increase the desliaalioo point namba: 2. Inaement sY>;tdt - Press and bolr1 as tcquiled. a. "lbe desliaalioo pointlllllllbtt iocreme:Dts at rwo aJWlts per S is in !be AlJfO NAV, MAN NAV, or DR ~AV positioo.

10 change !be CII1TCill TO destinalioo point 1.. l.J'ULONuCJl'E!:EVME:Aswioclxti!lbtwPtcss -

4-57

--

TO 1F- 117A-1

2.

lna:analt (IX dca"ement) S'Orildl - Press

a. Increment 1¥ decnmcllt lhe current BIT/ DEST point tmtillhedesired"TO dcstinarion point appears in lhe BIT/DEST wiaxlow. 3.

Pwpose:

1X CHNG Stritdlliglll - Press

a. TK CHNG

soritd!Ji&lu alllleS oo

BIT- Indicates BIT deteaioo ol a catetpry 01. 02. or Q3 INS fault.

•

INl.K - Used simullaJw:oosty wi1b MODE S'Orildl10b)pass lhc RSPA interloci: relay and 10 apply powet" to the

IDOillel>-

w:ily.

IEUIIMU.

A-vaiJabi!ity= BIT- INS rnc.de swiutcb:Jl..':in~a")C'!J~pnsupn51t - IlL_ _ _ _ __ !" M i l l

c:a::epc OFF. AUX l, 1¥ AUX 2. c. Airaaft counecbaJJ:tes 10lhe selected dc$tination point.

NOTE

INl.K - INS mode swiu:b in STBY positioa.

If lhe BITIINLK swilct.liztu comes oo w1len lhe INS llliOde Stritrfl is in SIBY: L INS rnc.de swUct. - GND 1¥ AUfO ALIGN To b)-pass the RSPA interloct rday: 2. MODEandBITIINUStritrfles-Presssimulta-

owusty. a. 1'Vwer is applied to lhc JEUJIMU_

II a ttadt cbaJI&e oc:a>n during a levd o.lolt attack. lhe wzet ~ 10 lhe new ro destination point.

NOTE

BJPISSing lhe RSPA intedoct relay sl>oold be done oaly UDder coocfitjnns ol SC>'ttC: oper.nioaal cocsuain~ Under normal conditions, when lhe llflLK light is on. maintenance ac:lioo is tequilcd Sensor Update

The Built-in-'lesl {uruiuu bas lhree categories ol BIT warnings. Calcpy Q3 indicateS failures relatiYe 10 S)'Siem data uansfers and P'" •s"nt Calcpy 02 indicates failnres ...nidi could degJadesyStem operation bot not reqaire S)'Siem shutdown- CalcpyOI indicates failures which are batdware in DatUre and if persistent, and will cause lhe S)'Siem to antOOtariatlly reoert to lhc DR moc!e. Wbcn a BIT failure is detected.lhcBITIINI..K lightaxDesoaand lhecatq:c> ryisdisplayed in lhc BITIDEST window.lf !hefailure is tranSirru in nattJtC. pressinz lhe BITIINI..K S'Orildl may restore IIJO(tiia) operatinn If a Catcpy 02 falloa:ws and pressing lhc BITIII'>'LK S'Orildl does DOl restore IIJO(tiia) operatioa. degJaded perl~ can be expected (see Ftg!UC 4-39).

=

-

II lhe BITIINLK and MODE S'Orildlesare. pressed simultaneOUSly. lhe Rota.- SuppM I'I:Jwer Assembly {RSPA) interloct is 011eniddcn and lhe ~ru powaed up.

The~ apda:te

fanaioo oa lhe CDU is inopera-

li\'C.

Vilsual Update Tlbe Yisual apda:te £1IIK%iuu allows lhe pilol10 oorrea the INS pnsitinn to lhe airaaft present pnsitioo. « a pc c• iousl) entaed pnsitinn axreaion. Visual update uses lhe pnsitinn lhe point spcc:ified by the windowiOQ!Jcnlate the a.itaaft present posirion COl teaiocL The fanaioo is mutnally exdowi1b ury olher cfupl:ay. and is available when a naviption mode is seleacd

temO\'C couro sn'C

or

cou

VISII3.l apda:te is aan-atect w11en lhc pilot pr-esses the V1S UPOT swilcb when directly on::r lhe destination point. The VIS UPO"C BRGJRNGE. ENTR. and CLR swildilights ~on. lhe CDU upper main displaywindowdispla)s tnaDletic be:ariog (to the neanst dqtee), and lhe CDU lower ma.incfupl:ay window displays pound range (to lhc neanst fooc}. 10 the current desrination point. The pilot press the LATILONG swUct. to display the bearing and range

ro

may

TO 1F- 117A- 1

•

as alaiJI~ bias 10 tbc ocaR:Stll1Uidt'cdlll ol a IU111te. Azl altialde bias is - calrwA•ed by the .-Jap»terrwrirw

11>e rwo-dizz _, '"lli!i•• di!fereroce cube accqlled &lid used 10 bias tbc aitttaf'l iDcnial posnioa by presllllC tbc ENTR swiu:h. n.is SUire$ tbc poQUOG cliff~ ill de9in3tino 99. &lid tuniS oa the P-P s•nldWPL 11>e update is rqeaed by prc5SIII& lbc CLR S'Wtld>. « 881 other CDU display fWIClJOCI exc:epc LATILOS G, BRGIRNGE. 0< Al.TIIlM E.. 11us

b. P-P swjvtaligbt CX1DCS OIL 1b reuiD llle bias: S. CLR sorildiJigln - Press a. lbe CDU upper aJld lowu maio ddpby..;.. dows go blaaL b. Bias is reWned. "Jb(X)ftUt INS p osj•i•• IOaitttaf'IS present poUtioo· 1.

ca-.the-CDU-~

Tbe .--1 ap2ltt fiDII:Uoa is also used 10 ie80'!ip>• piC$ olL c. Display blanls --=:ntarily. d. ltbolh emries are within hmits. entered \'3.1aes are displayed e.. It eilbtt enuy is DO( 'Wllhm lmUis. c:mrent vaiiiCS remain ~gel!. BRG RNGE soritdltiJI't - Press a. BRG RNGE S'ftd!lieb• aoes olL

•

Of'S AIN I or Of'S AIM 2 ~---------------.,....,..,.,., -Press

~

Errout• "IIIII Ide

Tile pu.rpose o/the devationfminjmwa cnroa:te altitude (ELEVIMEA) funaioo is 10 dlsplly the dcvation olacte9ina•ion point spcriCoedby the BITIDEST .-~ow. or oae ol ils assoasted OAP$. and the associated miaim.- cmoo:ne allinde.. 1'be swircb is alterIDle 8Clioa. aad •mmlly adasiv'e wi&b ...,. Olhcr

•

data displa} ,.....,.. Tile ~...mimvm e»roete altdl:Jde ftmaioo is ~the t..c1 boezd is !IGC . , the dala a:uyCIDde.. Upoa pi & the ELEVI MEA SW1ld> wbeD a•dable. lhe devatoumjnjmnrn CII.RlUtc alblade fancrinn is made aam:. l.liJ Oilier dala dlsplly ftlOCiion is ~ted aod lhc:n, if the c:ootdmatesareava.ilable, lllede>-a'-andminimum CIU'OUte alutode ollhc cte9ina•ion spenfoec! by l.be BITIDESTwtiidow, or ilS8S!!DCilted OAP asselcaed by the Of'S AIM 1 and Of'S AIM 2 S'l'1ldaes. are displlllyed ., the main display. It these dala are DGC ...U. able, 111e maia display isNaetrd The damaa/llliciaava caroo:te .,,;.'ode f••• '"" isdeac:trva.tcd &Ad 1be: -a cliilpay blanked either by pi • & lhe ELEV/ MEA SW'ID wbca ~ emoute aJti. tude is acU¥e. or apoa ac:tMlioD ol aDOtbtt display f•JDC'fioe The d~ and IDm!IDam CDrOCtc aJti. tude ol a deslination « an OAP .a, be entered or IIIOC!itled by pressia& lhe ENllt swudl ..,i lile the dewalioalminimum eruoute ftlOC!ion is aaM:. enu~ring the devation aad minimum en.route alutode, aDd Pft5SI'I& lhe e."JR switd> aptiL

••dallk

1b clloaltce the '-ria& « ~ V2lues: l. ENllt OOsd>tipt - Press

4,.

a. ENTR swm:taJi&ht oo. b. Cl.R ~t a.es OIL Enter bc:aria& via tqboard (000 lhnt 359) a. Entered bearin& appean"' upper main dis-

Platpose:

pby.

S.

---6.

Eater ~ via tqboard (OOCXm tl&ru 999999) a. Eatered raJ1Ce appears Ill lower maiD display. E.l' ciated wilh tile dcstmation plint iadtc::ned in Lhe BITIOEST trilodow.

Availlbiliry:

u.-s moc1e SW11cb "" urr position """"""

L

OFF. AUX L or AUX 2. OFS Ani I or OFS AL'-1 2 swu.cblcltt - Press L

2.

OFS AIM S1liildlleht U.CS OL

urr LONG sncb'i&b' - Press a. L.a!pt OFF, AUX L or AUX 2.

CDU lower main display ,."indow.

L

HDG MGVR switdiligbt -Press

2. P-P switdlli8Jlt - Press --------------~a.--p-P~~~~~~~~~o~~------------------A•~HPG~~M~G~VR~~wu~~cb~l~~htU•~c~cs~~~------------

b.

~Yigatioo error aacJ time from start o1 oe--

b.

quax::ing an: tCSDOtklcity >'eCUI£. This switch is altttnate aaion and mutually est::lusi'i'e with other data display fuunjoos It is ...ailable if the keyboald is 110t in the data eutty mode. Upon pressing the w N switch ..-ben available. the ftmaioo is made IICin'e. any oilier display funcliOo is ~-ated. and the currc:ot wind vdoc:ily vec:toc is displayed in the CDU main displays. The upptt window displays the diteaion from wbir:b wind is mrni~ referenced to magnetic 1IOl'th. and the lower window displa)s the vdocily in bats. The funaioo is de3I::IMled and the CDU main display blanked by pressing the WN switch wl>li!ability: INS mode switdl in arty positjoo ea::qx OFF; AlJX J. or AlJX 2.

2.

thiS cr ~n"iooic c:omponaus., See ~tioa

DR NAVIGATlON M ODE

•

Vdoc:ily.-eaor rep!• d by

u.e W symbol

On lbC' MDls: • INS alert

OntheCDU: MODEIM.ARK Stritd!IJ&IIt mmcs

Alcn System in Seaioc l

OIL

II

cocs eli ,.-ben tbc: mode swum IS sec 10 DR NAV.

INS NAVIGATION MODES

u.e

modes. sdc:ctliiJk lhrllGP CDU. ate P"' ideeS. 1bese modes are AD•MN•r (AUTO). Maaual (MA'Q. aDd De.! Rrctoe-. (DR). ""-"!: training.

3.

The DR NAV mocie could be sckaed cl'lltin& uy aoraaltAioioc ..mioa as aequutd, ca::ept c:aii1IOil slloald be aaased ~ low altitrde

4..

!!l!!!!je • I

0

time is DOt available to aJia11 the INS.

AUXIUARY MO DES

1llc CDU pO'Iides for the sdeaioe ol twO aumioJy -.ada..~~ 2. Drr 'D'Xks •rr mrc! tao

. rene,.... prrsm-od

4-72

.ooes.

E:I>ThLf'rdbcluduaiadadedt:sz;.uonpoiDts..U tode. &:ICI a taoo-digjl seqocooe namber for each. order m wtucb the ailaaft should Oy oou the pclinK I'Ositoon 00 is the ground alii:D positiocl. &:ICI mntains the coonlmates used dunn!: pound aJ.iln.mcnL By use ol tbe CDU. tbe pilot may modJJy any ol the data for tbe deS'ination poiDtS loeded frnm the EU1M or aaid poatts 11 than the nmawn tlcsnmrjnp points were dc{"_.t lt is DOC D I A '"f that the points dr:f,..,bJ' tbeETlTM"""' 0( by lheJllln< t;M ~ secutn'e a:q e '*""',.'!1 s. ~. • autt:m.tic

rewu-

_...

•

TO 1F-117A-1

..:qa • ill& desu ibtd below. &he !it:>l lih'l Toed deainatilw ..,....,..nteftd allieS seqoooeius bad< to destin:a(jon 00. 1K piol cuy ase &he mark fllll!ClOI 10 add destin:atilw points ill flilbL The Expo......., Data Transfer Module (EIYIM) . . vide$ !he followiaJ .......-. systtill .,.,.t>olity: Naviption Alip mt l'lliat 00 [)csjjnMilw l'oillts (DPs) 01 tluoup 93 • Mad: IW>ts 94, 9S, 96. 97, and 98

SlereB. • Olf.scl Ailll

99~ (OAPs) oi up to rwo for eacb deciuatioo and ...t poim roc a ...,;. mum oi 188 OAPs ~

1K pilot ray ose &he tract~ fwx:tiw 10sdec::l asry desinatjon pllllll. eu:qlt tllo5e 'lrilh sequeaa: oumbcn from 941hroeP 98, at any time ill any steer· Ullmode, tbou&Jt it is noc ac:IUa1ly relevant 10 lh~ maDual h~ TACAN, and lLS modes. DestiJia. tm points wil1l ""!llf!IICO numbcn from 94 lhnl 98 are MARK poiDu, and c:u be 5Cicd'"' by use oi &he tract ~ f\mctjcws as TO deam•ino poiDB iD asry steeriD& mode .sepl CXIOilK 11M stl'flinl

w-.

~ ~ 15 sdeacd ""!ueuciu& 10 Jlle _., m deairntine PQID1 CIClC'IIa oa!J.wb!:D 1M pilot aR$ &he tract~ fVIICtioa C. &he OJU 1D sdcaaacwTO~poiDt.ud~alc..& &he last CiOalpCilCd pODIId tract IS piO'fided Ill> til thCft.

A manual uad: clwt&e pet(ormed afler a weapoa re·

lease is !ollow'ed by an autoseqUCDCe at ATF plus m-e

_..

NOTE

u an m s ·a cd DP or OAP is w' nect &he desinatiQD ilwaba dospMjed Oil lbc HUDec l-ID I is pre(rredby aa X. and a \'lllid DP (pre&ed by a D). oc OAP (pcdixed by :Ill A }. IDliSI be sekaed 10 &Cl awrta stccrios ud IRADS poiDlJDS incfirn!jons

DESTlHATJOH STEE.RIHG MODE

1K dccai•pi'!Mient of the INS. the HSI displa~only the v.slues input by the!»lot.

f1iBht path geomunes Cor the destiuation steering

-

modeue presented in F"og.n 4-33. Airaaft Aoa:npies the position sbolm 'tl'ben desination steering is entered SiDc:e the di:stance from the aircraft latitude aDd longitude 10 the current destination, P(t-1), is less than the turning radius of the airaa!t, il coruioneson wurse uniiJ il can make a dim:t tum 10 Oyovet the poinL The!. becaase aatoSeqomcillg is DOl in effea ill this example. the aircraft wot.innes on the great cin:le course il was 011 wllea il flew over the poinL Airaa!i B, OCCUJl)in& the position sbolm whal destination steering mode is entered. is already 011 the p-eat c:irde route from the pre¥ioos destiualion. P(t-1), 10 the curmu destinarim P(i). The initial turning mane-a-u is thetdOtt omitted. The ailaaft .,..pr:oc:eedukl , _

OOPOQil~

SliB POUIIS

- - ~ CIQI5( WlrH

OiOSS liACIC POSmCII lllROi llltO »ttl AU10 SlllWICIIiG - - - PIIDI OEYIAJICII l!fai'W£iY CXUCS! - - -

IDEAl CAPfUU CDJt5:E l1R'I CUilFi - - - llll'i:IC lAD IUS

0

~11lW

F1GURE-4-a3-

4-75

TO 1F- 117A- 1 •retape t11e creat circk CDUr1le 10 t11e CW1'CIII m c!c:p-IIQII poiut en-tile OIOe pi E; hill it ill tile~ fbcJ1t da1a. aad lheD 10 .aiaWII tba1 CliiUde. ne curran TO c!cainarion point is llldocalcd by !be number 11J11C:111D1 mtbe TO •illdow ol the COU, and it is also shown OCI a0 displays.

1be stett~~~~ iDdic:ators ~ oe !be bead-up display (HUD). -.atical sitcatioe display (VSD) aad bor-~~~ Sllaatioa di!play (HSO). auJIKIItiaz basic I!Jcllt cbspl:l~s. Coarse liloe stecrilt& isiavalid IOdesti- 0 0 (al-c]51be alip elll poiln). illOipllaatl poizlts 94 ~ 98. and ill cases nc..e !be prdJigbt dala IS !llilldeqa:Ue 10 mppon !be mode. Wbea !be liiOde IS found 10 be im3lid, steeriftl ddaults 10 !be -euiol mode. aad the CRS UNE swUd~Ji&bt ,oes oa. IU1 examp~e o1 c1a1a 1.11at IS mac1equa1e 10 support DJUne liDest=lnz isu Adjal • 1•1 poirol deslina&ioas 'lrilb idcnric:al a>onlmatcs. Wbea ..,.,...., line steeN~S is aD10nWically • 'ea:d for uy ol these ...-.s.lbe . . . . . . . loold •• t frooa llle oae prec:o:doila 11. and lheD -illtaJOI.bat coune by using the fit&bt aJiltrois IOIW"Il t.be aitaaft fliiU or left as indicated by !be steuioc bar. Doin& thiS tecps t.be velocI'J ol t.be HUD, aad the aucr.aft pitdl rderCDCie symbol ol the VSD and ADI centered oe 111e balllt steetlll& bar. AlteruxM:Iy, the pilot can use tbe autopilot 10 steer tbe airaaCl t.broocJa the illtctttptiue and coune r:ramtenonee by ea1awa the aavip- - - - itioe II!Oid .OOC.IA tlaiscase. !be anl'll""' :

TO 01'

0

I

r\

0

\ \ >Lc&llD~tus\

\

\

•

\

\.

- - !!lEAl. COJiiS£ WITI! Cl!lSS tiACl( 1'(61Ttell -~~~~ zoo - - - t:lEAl aB:O'O'!llY COIR5£ RR PI-I J.0e PI ..... . . ~ llEIMitY COlliSl All ? All) P I 1 0 11D aJillll I<

+IGURE :&:-3-t

4-n

TO 1F- 117A-1

Airaaft D tepcesents the case wbere the airaaft is

l!eacfin& away from the seleaed cow:se line steering

Tbe purpose oi this mode is 10 prO¥ide bank &IJ8}e aeering jncljratnrs 10 the pikx. and at the piloc's option. steeriJlgordeB10 the amopilol. IOdirecl the airctaft 10ac:llieoe and maintaiD the great circle route 10 the current TO deS!ination point with a specn....t approac:b CXJW:Se. The current TO destination point is jndjr;!ted by the nltlllber appearing in the TO window ol the CDU, and is also sbowll oa all displays. The steeriJ:Ia inc:licators appear 011 the bead-up display (HUD) and the vertic2J situation display (VSD) aug-

•

marse, and the ctisu!W'P from the cowse is equal 10 or less than UlS times the tum Jadius. If the iohlaJ beading and the selected c:ourse difrereDOJ: is greater than l!iD", the airaafi IUmS llO" 10 the ri8hl and thell 'l0"10 the leftiO assume the seleaed CX)OlSe. If the iohlaJ headin&isequal 10or less than 180"dilfereat from the selected marse, the airaafi turns 180° 10 the left. and thea mates a final90" right tum at the rom rwfigs ro zswme abe crlef'1rd Cl:llal.es the selected aJUJSe oo a beading 90"10 the IXCC::..zatioa is iideftticalto lhe comsr sdea steerift& mode with respca 10 tbe apptuadt and iruercqK ol !be desired radiaL Tbe only difference is tbat tbe steering commands are based on TACA.'I data r:uber than inertial data. Capwre ~ is automatically progtammed as a function ol comsr erroc and deviation. A higb cmssuad: erroc me n"SUiring from bigb groundspeed. Jarxe intc:n::ept angle. sbort distance from tbe TACAN statioa, or anycooabi•iltioa ol tbese £aaon, mzy cause initiation ol capture~ before tbecounedeviatioa indicatOrS leon~ tbeirfully ddleaed positions. This minimizes lbe po«PPi'Y ol aa initial o-asboot ollbe radiaL Appcuacb to and intereqw ollbe sdeaed radial is ooitbout rq;ud to tbe TACA'I station location. The is esrao. lisbed in tbe most expeditioos manner. •hetber or 1101 tbe result is 10 bead 10 or away from tbe TACA'I

station.

The TACAN steering mode mzy be U5ed with the auUlpilol eogaged; howe>a:, commanded bank angles riJ DOC exceed 30°. The noniption bold rea~ ol tbe auwpilol is mmpattie with tbe TACAN st~ mode- Sd c :tion ol TCN oa tbe UFC pand with NAV engaaed does DOC ~gage lbe autopilol or altimdeiMacb bold.

lfTACAN data bemmes ill.alid, aU TACAN P"""iiar displa)s are ..-~ after lhree > ...s, induding tbchagj amjpgbm,lttbeau10pi!cxiseopl""andc__ __ mcpled in NAV bold, that Sllbmocle riJ drop oat and lhe AlP ROLL DO rd.......,. light riJ flash. When tbe Cligbt director senses tbat tbe aimaft is in lbe a10e ol COllfusioa SUlJOUJlding lbe sdlaced by mmmands 10 maintaiD tbe aircraft's heading.. This ovastatioa woc:lition is terminated by c:apcnre ol tbe outbound radial The bank steering bar oo lbe ADI is driveu tbe same as those oo tbe BUD and VSD with a IL'edJaniral flag pnl'YidiDg aa invalidity indicatioa instead ol symbol blanking The HSl and HSD comsr deviation indica· tors ftmaions exactly tbe same. l:iowC\'CI', tbe piklt must set tbeprupeccow:se usillg tbe BSI cow:se knob in order 10 oblain a prupec preseotation.

ILS STEERING MODE

Tbe JLSst~mode isseleaedbypres:singtheJLS switthligbt on tbe UFC p;utel. JLS LOC is automatically displa)~ in lhe prese1ea bar in lbe upper right wmer ol tbe HSD. This mode PfO''ides bank and piu:b srefflng wmmands 10 tbe pilot 10 ~ manual intc:n::ept and uacting ci lhe JLS Jocalim" and gtir'es'ope It also provides bank Wlllrnands 10 tbe autopilo< to suppott amomatic Jocali= steering. Bank and pitcb steering ban appear oo tbe HUD and VSD at c:apcnre (see Frgure 4-38). Locali= rourse and glideslope de¥iation aredicaiiQI 11M: distan« betweca the po51tions ill nautical miles up 10 99.99 nautical ides. ud the lhJtd 1tnc sbowU1J 11M: dill'crcnce in altitude ill rea up to99.999 fce1. A -sip is dispbjed if the new altilude is below lhe Jllft;ow: one. A + sian Uldicates lllc new allllude IS p-eatcr llwllhe old altitude. The thtee cl&mensional diflereox:c is entered as a 111- dimension bias bJ pre:ssmg the ENrR swucb on the MOL T1us causes the bias to be Rored in dc:sltnauon pOUlt numbcr99. tbe posnion difJCJCIICCS dilpb)ed 011 tbe MOl to be I"C1JIOO-ed and tq:tbald by lllc OME ud TAS readouts. the Present IUit.- (PP) r~ on the cou to be aaMI.e d to display the oewiy biased auaaft JXIII10I. tbe semor apdstc flltiCiion to be cleac:tiYaled. ud tbe MDE s.~ Slritcb to be

g.........,

After ps. 'llhictl is beiDa lidded to tbc pare ioeniaJ 1•+•••\ are dispb)ed oalbc COU bJ iuuewenti!lg destinalJilll point aamber 99 ilno tbc BITIOEST wiadow. Tbc:sc twO • • 1 ents and lbc abirude to 'If ; CDI of this bias ClD be zeroed, IIIIlS c:ausq tbc N-WSC to OUiplll pare iDcnial data. by pressin& tbc CDU VIS UPDT swiacb a.! lhc:a 11M: cou ENlR switcb.

Slew bias isc:anocelled wilh aut~>-rew:m ,.i>cn a sensor update is entered. The altil:ode bias resutti!lg from an altitude c:almtc function is internc:tive ,.;111 lhe altitude bias resulun& from a semor update fnN'linn Syuem alutode IS biased by the resuta of wllicbever oflhcse tf!O rUftCo t-.s was pedormed las., llut t.be ooneaion values are aJ&etni: adcfitioas to tbc past am~alall\-e bias. ENTER AJNCT10N

1'k emer (E'o"llt) sorilcb is~ ~e oalbc 1l' aad HSO displajs. It is tiRd only in 'XM'J""C'witll tiM: semor cpdate ftmainD to aa:qx lllc ~ lated WOI!!Qiill"S

a.EAR FUNCnON 'The clear (Q.R) swilcb is always a+Wil:lblc: 011 lbc 11' aad HSO displajs.lt is tiSed only in coojUDCtioa W11ll tbe semor t:pd;tte fuoaiw to .qea lbc c:a!c:ulaled COOI'!Wuates

SENSOR UPDATE PROCEDURES Semor npdau:s shonld be pedomled mffricntly in ad-oanOeally iD adv.ulce of aUUJSeqllellCt· ic diteaioa and speed SIOred in the N- WSC. The wind values are those calallated by the N-WSC during inertial navigation mode by a:llllpOiin& inertially derM:d aUaaft velocity with air mass velocity based oo ADC ptOO'ided Uspeed. wt1ess the pikll utilizes the CDU 10 enter wiad •'alues. l"iio< entered nlues bon~ priority...ucalculated nines. In this dead n:d:ooing (DR) mode. the N- WSC prooioXs ils best estimate ol aD the poa.ramews i1 normaDyprooioXs 10 the other suiJos)-stcms on the bus. Normal S)'Sle:ID fuDc-

=

sic:Jns wjJI he gpjnpjped 'brwt&h swne rtc,,,,.,tjnn in stability andloo- lii:D1l3cy will occur. The IDOSI

•

•

TO 1F- 117A- 1

SEQUENCING BfT FAULT CONDfTIONS BIT OIT NO. I

2 3

s

81TF14U

0

NO. I I

•s

.s .s

3Nf50~ GIM!!Al~

•

I

$2

8AYTSIY TEST fNI.

50 56 56

53

II

"

12 f3

' •• IS ' ''

.. Ill

17

Ill 20

21 22

I I I I I

s

eo

~II IIOC UICIEIMlUAGE

AOTOR OVERTUF

1

GYRO YAO.UIISAO

215

1

\'JC.. IUW t01 < IOWA

27 211 2ll 30 31 l2 33

1

'I{J.C.~ii'Z oo the intemJIDIDonication (ICS)conuol panel- 1'be BCN switdl mllSl be in the polleck>ut position iD order to enable mart.er beaaJo idcntif>er audio.

WEAPONS DEUVERY SYSTEM For detailed information dn"e:IJ Manuals) Cor detailed desaiptioos ol anad modes and prooedans. j

j " " " ' " '. . . . . .

STORES INVENTORY

See !be F-117A Utility Flqb! !>b.oml C!pssjfoc:d Supplcmall (rO IF-117A-1-l) fcc a liR ol stores !be F-ll7A amaJ't is capable ol ~

AVIONJCS SUBSYSTEMS ON-BOARD TESTING Oo-boanl t=ing ol ' - CICIIIIIeaed 8VIiXliCS subsystems is •• i""l~isbl;c:l !ISiJI& JIIOtiDal fbcbt funaww; and tesl fmw Same tesl (goa. . . a.re available fcc liSe only on llle zroand wllile Others also a.re a-Uable for liSe iD DigbL 1'lle teSl func:uons are: Slams dispby and alerts (Jround and in

lDFT MODE 1'lle Jolt iiiOde is prc,.;ded Cor amomatic ddi\'ef)' of .....o=--~~- U'betsr nuelcarwe:lpOIISOI"fonna l "'IDfii:DU. - - -

•i-

•

lliglu). Maintenance display and alerts (Jround and in fli&lu).

•

S)Slee>

,...,.,mess 1es1 (pocmd).

• NIAC prdlipl ttSl (pocmd). AOC iniria•ed bllilt-m tesl ~ IRADS baill_.,. leSlS (poaDd ud ., Oiglu). 00 bai!t-ill test (poaDd and Ill u.Jit). Fault is•>~iou ...rona~ tetO!dial 011 EIJIM (8rooJid UK! iD flicbt for pll5l ~ pux:essing).

•

~Rusnt•cu~~~OWNmm~~·----------------

' 4-95

TO 1F-117A- 1

Use ol normal lligln functions and test fUDCtions for opemional readiness~ and OIHioard £ault c:leteaioft is included in this seaioiL Ftgure 4-41 shows major Sllbs)'SUIDS tested.

WSC STATUS DISPLAY AND ALERTS The I:ISD swus display and alens (see F~!~= 4-42) are av.Uiable 10 pooide lhe pilot wilb eertain

sobsystem: • fimctijiftjil fiiilt U l l - (iiSaUJ dliriJJi prefligbt 0£ in lligln). • Fault ncdjca!jm • Faolt isolation informarim for maintenance piii]JCISeS usin& the maint .......... display.

Other similar information is JIIO¥idcd by the: • CDU for the J:NS. • Sensor display for the IRADS. • Annunciator pand for the ADC and eertain

WSC MAIHTCHANCE DISPLAY The mainte..ance display (see F~gtU"e 4-44) is a _ . lion olthe swusdisplay for ase by mainteoaoce perSOGDd- ll is selected by~ the MAJ\'T n.itdt at the top olthe status display. All sobsystems, terminals and bus falllts, iC any, are sbowD reganlless ol !heir fail:nre status. ID addition. the runaiooal fault informalioo is eyaoed by LRU, SRU and!O£ Other

!ault informa•jnn This fault infor:matioo presents failure swus ...ards from sobsystems. The display • eptescntsfailuresb)' nWIIDCISO lhroUgD 9iiid I A tbrougJI F, and llllllfaiJ:nres by c:lou. Mainteoance pc:nonndusea writteupiocedwe IOinterpret theinformarim wbidl is apc!ated ev-ect from Sllbs)-stem funaiorml failures as mo., in F~!~= 4-43. The swus display is apc!ated every second

-

ALERTS

4-96

•

TO 1F- 117A-1

•

AVIONICS SUBSYSTEII TESTS AND FAUUS OPE'RATIONAL ON-80ARO FAUll" DETEC'T10N

READINESS ~

SUBSYSTEM

wscs

.

0tlSEha110i I 01 normal displays onMDIS (1) Abs&....e 01 WSCS an SlaluC

Aa:st*lg STANDBY oo bolh l.tDis. alelt 00

t.l

BIT SWIICfl on COU II INS on arranaaiDr panel

11011i!1J!ed

Observe hi! cou.

AOC

•

Nole: (1)

j

lorUldlon)

~ ...

et*ies oortl!dl)! Absa ICe OI INS on SlaiUS display

I a llaS*1g STANDBY camel De • · -ed by noanal means. ensue llel 11!1 systems are lUlled an. h!n RESET lie~

4-97

TO 1F-11 7A- 1

•

WSC STATUS DISPLAY

aso wsa wsc:z aso (Jfl

IllS 1(1;

CiliUI IlLS lac

-

11'5

•W•x •m PS llll • X Ill' PS IIU

I'U W\ X lUG! PS 1111 M5C UUII lllllll

.... -........

,.

- .. nr;-

•• ,..... ,. ,.

IUPI~

IS'

SIIS

SPI

srz

IIAI

.,

IUC C.I

'Sle

ltSO

.... .... .... AI II

SIIP'I2

or

AI

.s

CAD CAIZ

VIII

"f iGURE .._.2

"*'

Alens resDh en.:

•

4-98

rcure

Failure ol prd1ciU data 10 sucassl'ully toed UIIO tile

E.D1M.

2ll!i

SMI

w

Bl

..

~_,

WSC BASIC TEST DISPLAY

ne wsc basic 1es1 display (see r~ 4-45) is DOC ·~ dvriD& lDpL It is selected by prasill& tile TEST swiadl wbca'"" MDI is in tile VSD rom.t, ud a esllbles tile IUS, r.'l.AC. WSC. and SMS s-a~ 10 permit tile sd •••• ol tbese u:su. "The swilcbes are aloCOPte aaiaa type, w!Uch pcmrit• the tests 10 be iailiated aud a bar 10 appear UODDd tile $WIIdl *"00)W wbca fim pttw>i. Wbalpc:wxJ q:aiB. tbe boot is rcawed. tile test ,....-..,,ed, ud tbe dilpby is~.:d.

"lbe basic lCSl dispby sboaid DOC be 1: I :I : :ted after 5d ·~anSRT(Rl.S.NJAC. WSC,orSMS}aadbef«r tile sdrt1ed leSl is bared.

All ol tbc • • • 1-

itcd.

Stanin& F.GT aDd oil pressure limits are presented in F>gnres 5-2 aDd 5-3. Rt:fc:r to ScaioG II few Ratting proa:duccs.

The Ratting l.imits aDd ignitioa cxcitc:rduty cycles are as follows: • Ma-rjmnm time to Jjgbt-«1" is 20 second< Ma-rimum time from fu:sl indication ol an rpm to Idle is 7S sec()! ds F.m ssan oi lhc day may em::eed limit by 30 seu""1s. M:ainte· naJIIle aaioa required if cqioe rqJC:alcdly • •• ceds liiJl4 Minimum time bcno'CCD ssans is 30 second< :aftc:r core rpm bas readled :wo. • Ignition cxcitc:r duty qde; 2 minuteS on. 3 minutes olf. 2 minutes on, 23 minutes oil {gromld «air SWtio&).

AIRCRAFT CAPABIUTlES AFTER START (ON GROUND) See F~ 5-U for a prescsu:atioo oi the airaa!t capebililyas a frmaion oiapptOted uscaod Sen-ice Bulletin incorporatioo.

See FJgUIC: 5-4 few idle core speed liiJl4

AIR TURBINE STARTER (ATS) ENGINE START

ENGINE UMITATlONS

I

()pmUinJ limitations

few the F*-GF.-FlD2 m-

&ints are presented in F~ZJUCS 5-1 tbroogb 5-4.

The D:G SfART n-itch can be engaged few n>'O minutes during engine sran rqardlcss oC. air source. A rooldowD timed 10 miontes is recommended sbcn lht duty cycle is ccadlcd.

5- 1

-

TO 1F-117A-1

ENGINE UMrTATlONS CHART Oil PRESSURE

EGT

·c

PSI

GROUND STEADY STATE

-

-

START

INOICAllOH l!l

>81512! &l]

-

IDLE

> 700::; 815 ID

Blllilll!ZI

-

~70 NOioiiHAL

40:100 NOMINAL

FUGHT >700:$&15 m

-

-

START

IDLE

-

M•XIMIIM

106

INOICAllOH Bl

>81sm

rnm

-

68T072

55-102 NONIHAL

810:820 NONIHAL

102

!I!

IZIISJ

GROUND OR FUGHT

m "T"tw.- a~.""*"' enQk>e ..... EGT '*"Po- 200·c. 1z:

IEGTc:aAcni!Qt'fcam~SOI\.abortS~M.

_,-.

p• ' ••ceiOc:hedMg EGT-.. lif'rOis (See fV.n~

llo ROIL c:aAcn IIQt'f cam1S 01\. ,._., lh't:J!Ie IOtBlg oil

-..~

II!Qt'f remai'ls on. stu

When ...,...ali111 bar a • lie Oil U.l'n!slu'e CaLCian 1.Vfn • ...,...., and hJ-..... slaadysaata lmi, oil pressue !hiii....,IOnormal YM.e ....,cne -a!lerCOiii(AaliiQ - · CltiUalse studoM'i enQk>e, Tl'e'8 are ro lmilts 011 rurblr o d idle time ro.- •-arioos ;m. tial Cud tempe:ru:ures. lnilial fad ~mllSl be obcained from mainteuaaoe persomld. "L'd:. F-U7A-2-'lQJG, Po:ouplant Orpniz;ariMal Mail>renaooe Job Guide. THE WAXIYIU SPEED U111T FOR THIS COHAGURA"TION IS 4SSICI:ASID !ll MACK.

-·p N

SPEED IS '140 ICCAS

I&AlQUIU AI.Til\£lE IS 3S,OCO F££T

WIXINUN AIRSI dD FOR THE FUR/DLiR SYSTEM IS 525 KCASIIlSO MAOi NO. WAXINIIN All&'tB) FOR FUGHTS WITHOUT A TAII..HOOK CXJIIER IS 500 KCASIO 90 MACH NO. NAXJNI IN All&'tB)WITM RCS ENHAHCSRS INSTAU.ED IS 500 KCASIIlSO MAOi NO.

F1GU1iiE s-6 ABORT FUGHT ENVELOPE

Foe 7 (AOA) and F~ S-8 (load fador).

o ....•iud - 15 tnocs NOTE

Altra)5 pe:rfOilD a CXIDUOIIabiJily cllect at sale altitude todetennine mfuimum allowable speed 1D be used OD the fiDal appoacb and Iandin&-

5-8

PROHIBITE.D MANEUVERS a. Rnuse bratiDg (braking 'lrilh bacb;ud mo-

WARNING

I

Aircraft may depatt al 1aJge negative angles oC atlact asgxiued wilb negative g roanetm:riog.

TO 1F-117A-1

•

ANGLE OF ATTACK UMITS DATA BASIS: FLIGHT TEST RESUI.JS

......

.. 0

"'0

•

" 0

5.. 0

~ 0 :z

. c 0

!C !::! 0

:z

IIACH NO.

•------~

FlGUR£5-7

S-9

TO 1F-117A-1

ALLOWABLE LOAD FACTOR CLEAN CONAGURATION SYMMETRICAL FUGHT

•

'

. "' I

c 0

::;

~

~ 0

c

g 0

-~

AIJISPU.O - KCAS

NOTE: 1. 1l£ Al1DWAI!l.E LCIAO FACTORS RlA THE WEAI'ON BAY DOOR OPEN OR OPEJV.WIG ME 1liE SAME foS THE ClEAN COHAGlJR.\llON 2. RlA AOUING I'Ul10UTS THE MUMN LCIAO FACTOfiiS8CI'll. OF 1l£ ~ Ullll. THE I.CIWER UIIT LCIAO FACTOR IS -1.0 G. 3. 1l£ PIUJT laJST MONTOR Sl1Q( llotPUTS SINCE FUJ. AFT OR FUJ. RlAWARl Sl1Q( CAN exceD THESE POSmYE OR KEGATIIIE UIIJTS.

FIGURE 5-8

5-10

I

TO 1 F-117A-1

•

MINIMUM AIRSPEED TO INITIATE RECOVERY FROM PITCH GLUIUP DATA BASIS: FUGKT TEST

Non: lnitiai!CSI pbn - appnm:d above 60° pittb angle

A0U. 1110• NID 1'\Al. TO RECOIIER

•

50

..

co«<

".. •

•,.

a::

:::>

0

~ 30

"cz

,.z

.. c u

...

X

0

!::!

'

iL:zo

NOTE

OBSaM: NEGATI'IE AHGl£ ~ AJ'TAO( lAiiTS AT AU. TillES

10

0

120

140

150

1110

200

220

RECOVERY INrT1AnOH SPEED - KCAS

•

AGURE5-9

5-11

TO 1F- 117A- 1

MANEUVER UMITATIONS ROLL UMITATIOHS IZl ID WTngU!I•a•BilliiQt-:hMVS 1800b.ffi TOTAl ROll. ANGLE

loiAH8JVER

SPEED LESS lliAH 200 ICTS OR GEAR DOWN

Ill

SPEED AT OR ABOVE 200 ICTSNID GEAR UP

FUI slide mls

90"

360" laWY nu;a be at "'~ 1*11• l)l 1-gt..

FUI slide mls on

90"

360" ............ lca::tla::lcr atet*yis80%cl lhelca::tla::lcr CJt:iOU'>ed 11om

lheAOA~

(UI aft SliC:fl)

f0n5-8. FUI pedal n.a:lc* mls

90"

FUI pedal n.a:lc* mlson lheAOACfUI aft SliC:fl)

90"

90" 90" Maldnun load tac:oor at anDy~ cllhe load tac:oor cA:irail i8d 11om

fOn$-3. NOTE:

.-:n W1gl >

m

Fa wing U!l •a•BilliiiQ

IZl

FUI slide m1s COI•obill8d-. aitlng ac 4\XlSiiiQ Ul pedal...,._.,. ara p a - .

!Jl

o.-.-nall slide tails COli obi! i8d.., -.g ....-_pedal rolls ara pan

@

~UI-SIIdt360" mlsarepcl• Mj

1800 b.. haW stidc ac pedal mls ~ 7

I

ROWNG PUUOllTS

WARNING

Refer 10 F~ 5-8 for ~ puJJoot load l'aao.-

I

lii:Dit$.

PrTcti ATlTTUDE UMITATION Refer 10 F"~gUtt >-9 for minimum airspeed to initiate from pitdl DJalleU\US. Refer 10 TO 1F-ll7A-l-1 for weapon clelioaypilch •trirode limits.

'"""ClJ

SIDESLIP UMITATION

Full pedal sideslips~ permined. lntentioaal sideslips abo¥e .fill KCAS are prohtitcd. Refer 10 TO 1F-117A-l-1 for aeapoa ddi>ery sideslip limits.

Wrth single c:bannd operation, automatic 1ozic is disabled and amnplo« swttdl q;c and tigbt q;c can be satisfied (swttdl ri1 ~and AlP NO REF 1i81n ril eninguisll) willloot the autcpilol faneriming After tbeauwpilol isselcaedoa, the pilol sbott1d ascertain that theauropUot is, in faa. funajnnin8 propedy prior 10 ClliiUIICIIC:in8 weapoa system operatica. Fnquall aoss cbecb sbott1d be aaxJmz plisMd 10 eruutt the auwpilol remains endiseng;!Be

Pled

SYSTEM UMITATIONS AUTOPILOT UMJTS - SIHGLE OR DUAL ctiANNEL

-

The auwpilol can be used at a.ay point 'OI'i1IWI the a.t.JooGI!Ie~ea•dnpes ~will eaga~ an!p1

for air refudinJ: or altiiUiks below 200 feet AGL

5-12

ElPU U MfTS

EPU operatioa is limited to U minutes to pre>'ellt tempenmres in em::ss ol 4QO•F. The J2 =iaete~=ded-w'-crirical ===• EPU oil

t;enC1 conditions.

- 1

TO 1F-117A-1

•

nRE

uuns

MMn GeM

nres

opm 10 approximately six inches or less. The maximum tDi speed for this• QO•Ii• ••• is60 tmou induding wiDd or gusiS.

1be maximum groaod speed rating u the maio gear lites is 216 tnols.

Hose Gear nre The maximum groaod speed rating u the IIOI5e gear tire is 220 tnols. BRAKE

uuns

1be brake capacity for a rejeaed takeoti (RI'O) is 62,000,1XX) fi-lblbratelbe maximum illi1ial bnl:D:Ig speed is JRSI'III:ed iD Fr&are s-10 and nrit:s .nil gross wft&bl. amhim• u•mper;nutt, altitode, and wiDd. 1be speeds are brased oo a dly. bard rwrway ,.;u, zero slope and wilb001 drag chute~

DRAG CHUTE UUJTS

1be maximum ainpecd fee drag chute deploj ouocnt is 'Z15 KCAS. The DOse pr sboald be oa the ground and l.be aira"aft aligned with the rwnray before the drag dune isdeploye

'I'D

....,. ....,.

-

-

FIGURE 5-12: (Sheet 7 ol 8)

------------------------------' 5-24

TO 1F- 117A- 1

AIRCRAFT CAPABIUTlES 5aMCE BUUETlNS ~TED FOR CAPABaJTY

.

.

~

CAPABaJTY

A.JGHT TESTED

ATTITUlE yaa: Al.EilTS (SIB H-30221 ID Cl!

YES

-4WIJ'

YES

(SIB~

l!l

INTEIWtlloW' UGKT

INSTAU.AnOH

CS.'IN-DS:Il

YES

a;

Iff MODE • e

Hull lateral Stitt oc ~ inputs can be used individually at speeds abcwe 200 knots roc roll a1111ro1 while maintaining aft srict. See Section rolllimitalion$. Full ~ sideslips .nth fun aft Stitt at spems below 200 knots can require faU opposite roll stili: to maintain 'lriDgs leod. Full sbc:t rolls wnh aidialg 01" faU ~·sin& pedal inpnts have not been

run

v roc

fon

teSied.

LOAD FACTOR UMmNG EJz:msions to a large neptive AOA can result in an unconr.rolbble pitcb-dovo-n d!araaeriqr If mcb a "' Joan departure oc:c:us. teahety is highly unlikely. (Refer 10 OperaUng timltatioos,~~

6- 2

•

TO 1F-117A-1 mum attainath roll rate varies from app:Olinaately 110"/sec at low speeds 10 about J.SO"Isec at speeds abo>'£ 300 KCAS. These roll mesare redocedat bigb AO/Its or load facton because ol tbe FCS pitchlroll llli= priorities.

The~ limit load factors are positi\'C 6

&'sand neptioe 2 g's for gross wci&hts below 41.(XX) poonds; bwever, the Fl.CC will allow the pilot 10 attain 7 g's abo>'£ SOO KCAS at low altitudes. In this simatica. the ~ load kods are ore positive than -3• AOA. (Refer to Openlin& 1 imitatjons, SeaioD V.)

I

WARNING

·

tbe piJot mUSI initiate ,.........,., from bigb pildl anUocle, low airspeed conditions so that the minimum speed dllrin& the real~"· ery does 1101 fall below a minimum safe speed

The airspeed 10 initiate •l!roOj ainpeeds. For pittb angles up 10 45°, apply ma:Dmum ~and initiate a~ wings 1£\'d pusboics. For pitc:b anitades abowe 45°. unload 10 reduce AOA below 10°, roll tbe aira:a!t 1110" (0< as required 10 in>'cstcd}and pull tbe DOSe below the boriz.oo. Compl..,ioa ol tbe ~·can be made after tbe oose is below the bOOznn and tbe airspeed is ill-

-u

- gabote

6-3

TO 1F- 117A -1

WARNING

I

EXTREME FO RWARD e.G

m.

(Payload forward tr.mSftt tanks full. wings and aft tl311Sftt tanks empy)

•

This condition requires the devoos to be almo5t full u:p to mamtaill 9.5" ADA iD 1 & llighl. lbetd"ore if Based oa fli&ht sifnnlarjoo, ~-e ADA a oormai landing apptoach is made, '"el)' littlt pitdr depannre is possible iD this speed and reoonuo1 is mWa!Jit for llariD& the airaafl. This probCD-a.roond. mDSl !Nl!!jtor the oqative ADA limil$as Sn!T,Y.,1 CODtrol JIO'I'U" is availablt if the apptoach _ _ _ ___,s= bow,_,u,_,in Ffltllre..,=.== S..::.!7.:.. · - - - - - - - - --iiss-"mar ...... k~ mazinuua at 1" ADA. IIJo.djfficv!ti" are CIXOIIIItCR:d at speeds ato.-e 200 KCAS in the ~ ooofipia1ioa.

EXTREME AFT C.G.

(NopiJ!oed. forward tr.mSferaank empcy, 'lfrin&sand a:ft tr.mSfer W1k fuD).

TRIM CHANGES SiDce then are DO !laps or speed lxakes. the onlyCDDfigumion c:banges wbich will affect trim are enp JlO'I'U c:banges, gear raraaion or eueusioo. and openillg orc:losin&ola single baydoor. I'Uwttc:banges baTr a miDor dlca oa pilcb trim wbile the DlOlion ol the gear or sin&Jt door ba>-e a small dlea oa yaw trim. "The pooou dfeas are no«iceable only at low speeds ..ru. the gear down wbere all iJx:rase iD power set· tiDp will cawe a~ nose up trim cbauge.

Because the siD&Je 11015e gar door is binged on the ldi side ol the ailaaft ceruetline, nose gear door openiag and nose gear 01ensioa caases some miDor air flow dislortion. This n=lts iDa nose left side~ ol appu ojnwely oae degree wbicb can be retrimmed. as desired, br the piJoL Com-ersdy, gar retnaion and subseqaeot door dosure n=lts in a ~ nose IW>t side slip wbicb can be similady rer-rimmect ()peninJ ol a single bay door bas dleets similar to gear 01ension.

FUEL TRANSFER FAIWRES CAUSING EXTREME C.G. VARIATIONS

-

.l'k...lollowin-&-..drarantrisrics..&Dd based 011 fliglu simulation results.

ctjvnuicms

are

This condition doesll"t pr-eseru aJrf suioas problems as loag as the laoding apptoach is made with a maDmum ol7" ADA. Do DOtatr.empt to "bold thtairaaft oiJ". 10uchdown with a maximum oi9.S0 ADA. Do IXJl make aJI"f rapid ~ maneti¥erS at speeds below 300 tnocs. OFF CENTER e.G.

(Full store iD ooe bay with full wing fuel 011 same side with opposite wing and fuselage tanks empty). Full roll trim will DOl a1Jow ha.nds-l!arion (PIO) may oo;:ur, "'V'"ially during tatroff, « during Jrl&b tbrusl, qb AOA situations. Automatic yaw trim is pO¥ided to motrol and slloold auuxmtically trim lbe yawaxis10lesstha.D u•otsideslipin l51020R• ••ois foiJowin&an ~ Cailone 'lrilh lbe gear up. The au· tomatic yaw trim is c!eaaiYated if the pilot applies more than 20 poomds ol rudder pedal or if lbe lilidiiig gear iS eueiidlld

sKies!.,

roroe.

Engine failure at low AOA auise macitims results in a small sideslip aa,le alXI a very mild roii!DW:Uds lbe dead enpe wbicb is easily allll:rollable with lat· era! stict inpmsonly. The auuymric yaw trim will te· dace the sideslip angle to no more than u• in a few secoods aJX!lbe pilot CUI use the maDual yaw trim to redace lbe sjc!es!ip 10zero if desired. If the autopilot isenpged at the time ol Cllgine failore, it has CIJOUgb roll authority 10 maintain roll matrol but a 3• 10 s• bank aa,~e be be ttqaixed 10 maintain bc:ading. EnJjne Cailnresatltigller AOA (Col- at taUoll) cause laiF sideslip angles("'' 109• ) alXI a more rapid roll towards lbe dead eo&inc.. The recommeoded pilot tec:bniqne is 10 raise lbe !aDding gear as soon as pass;.. ble. bank s• into the good engineaJX!mna:n•rnteon maintaining the AOA less than 10• 'll1lile the aUaaft .,.,. lm!tes 10 the best sift&le eo&ine rate ol climb speed. Gear tdlaaioo actn'ates lbe automatic yaw trim whicb smoothly iedDCCS lbe sideslip toooatt\s zero. If lbe pilot aggrcssi•dy tries to matrol Pdeslip 'lrilh ~· rudder pedal iopn:s.. the a!Jiomatic yaw trim isc:leactivated,a roll/yaw PIO may result. and the pilot will be fort:ed 10 di>-ert attentioa from the more aitic:al ainpeed and AOA controL The autopilot may be used after the pilot bas sratNim! the aircraft and the best single engine me ol climb has been attained. AI lower speeds, the ant0pi1ot does - bave enoagb authority 10 maintain adequate motrol

--~-----------------------------6-5

TO 1F-tt7A-t

•

DIVE RECOVERY CHART

0

4

a

t2

15

--------------~· 6-6

TO 1F-117A-1

•

airaafl with the mmray.1bis lc:IMX&) is~

CROSSWIND LANDING BcaiiSIC ollbc FCS ckaip. !be uaaft bas a suoa& y10 wealhcr-iaiO !be willd after IOO:IdldowL s-uJator raa.lts Sllow llw ..0 ts peuc:r lllall LS t.Ks. !be airaa!t c:u IGme !be rem_, oa ~~~c apw-.ad side ..a~c:s awc:ai~ l1ldckr aad diffcrmlial be, 1962. Coaeaioas for oon smndatd tanperalure «'XJJ!ti!jnas !me been included ~posSible- A fuel flow~Iaaor bas - been added 10 either lbe estimated oc fli&Ju laldala-

MOPS VS FUGHT MANUAL PLANNING MDPS pcediaed Cud ma&e will be wilhiD No ollbe vaJaes i:Ddicated by tbis llizju manna! wbidJ iucot ...... rates lbe mast n:ooent fli&Ju lest daJa_ NO"re Where missioa fuel may be a ailicaJ Iaaor, MOPS Cud pmli are based oo FJi&ht 1tsl resalts.. Switcbooerpoint:sfrom El..Ecrto PNEU IIIOOe are sbawD ill F~gU~e Al-3.

•

TRUEMACHNO. VSCAUBRATED AIRSPEED F~ AI~ mows lbe rd:uioosbip bel• een true Mach nUlllber, JliC:SSWc altitude, and calb:atcd air-

speed~

KCAS CONVERSION TO KEAS 1!be aJmusioa from KCAS 10 KEAS is preseoted iD F>gare Al-S- Tbe ainpecd CXIIDpi"CSSiJil oorrcctioo ( ~ V} can be cbtained from tbis 6gu.re and applied 10 KCAS for detemlinalion ol KEAS..

FREE AIR TEMPERATURE VARIATION WITH ALTTTUDE Free air tempenuure vanuion with aJtimde is presented iD Flp.I'C Al-6 for lbe U.S. S>anc!ard Almospberc 1962. MIL-STD-2lOA Allar Day, and MD._STD-2JOA Tropic Day.

TRUE MACH NO. - KTAS CONVERSION Tbe wn•usiou from True Madl No. 10 IITAS is presented iD FigUre Al- 7 forambinu temperai11rtS from -60°C 10 + 60°C.

STANDARD ATMOSPHERE TABLE Tbe U.S. Sl3ndard Atmmpbere - 1962 is presc:nted ill FJgUie Al-3 and is lbe basis for calcnlating pcrformanc:e iD tbis appc • ,;.

STANDARD UNITS CONVERSION CHART

ne Sl31ldatd nnns aJmusioa chan. Jll'eSCDled u.

FJgUie Al-9, JliOtidcs a means for di:cca coaou sious ol 1empera111re from degiees Centigrade 10 degiees F.a.brenbeil,.and ol dittal!N' and speeJ from feet. nanDc:al miles. feet per second and feet per minute to metric cqaivalents ol meters, h1cwnCfas, meters per second and meters per minute. r:espec:tively.

• A1-2

TO 1F-117A-1

RJEL AND RJEL DENSITY Tile performance • Ail p • "'' A is besed oa airaafi faded_. JP~, Tile asr al JP-8 f11d has a nec~Ci­ bk dlca oa aarcnft pc:rfor-..c:e lased apoa JP-4

..., JP-8 cnUsc perf~~ raults al Fbf;bt~ JP-Sfuelaooldlilne the-~ bk dlca oa ainnft pctf~

Fvd deasilr ;s presented roc JP-4, JP-S. ..., JP-8 fads iD F'l""! AJ-10 as a functjoo a1 fuel tecDpel'llmre. Use JP-4 fud dcmiay for NATO F-40 aod IET B hods. a:se JP-S fuel density b NATO 1'-44 foci. md use JP-8 fad deasily for NATO F-34, NATO F-lS, md IET A-I fads.

• A1-3

TO 1F-117A- 1

•

AIRSPEED AND ALTITUDE CAUBRATION STAIIDBY' StS aM GEAR UP IIOOEl.: •• • •• •• • p;.1f7A DA1"A BASIS: •• • FUGHT TEST DATE: ••••• • ••• 1 MARCH 1 -

s z

:.:: I

z

0

...a:~ a: 0 0

>



Cl> Cl>

5

"' a:

CL

KCAS

•

AGURE At - 3

At -7

TO 1F-117A-1

TRUE MACH NUMBER VS CAUBRATED AIRSPEED TWO 9IGUIES AT loiAlCIMIIII POWER GEAR UP - CG 0 u.o'lo MAC AU. TEIII'EJIATURES C1.71111ACH ItO.

PRESSURE ALlTTlJOE -1000 FT

a: w

CD

::E

;:)

z

:r u c ::E

KCAS

A1-8

•

TO 1F-117A-1

TRUE MACH NUMBER YS CAUBRATED AIRSPEED

PRESSURE Al.l'TTUDE -1000 FT

KCAS

-L~~---------------------------flG~1~1~2~~---------------------------A1-9

TO 1F-117A-1

•

KCAS CONVERSION TO KEAS

1CEAS

s

KCAS -AV

2S 20

20

15

!!! 0 z

X

l

>



FUEL TEMPERAWRE -~

A1-16

•

•

TO 1F-117A-1

APPENDIX A PART 2 - ENGINE DATA

TABLE OF CONTENTS PAGE TAKEOFF RPM CHECK ••.••••••.•........ .• - .••.•••••.••.••.•...... •.••• ..••..•.•..•.•••• A2-2

UST OF ILLUSI'RATIONS FlGURE PAGE NomiDal Fan RPM Scbedule ••.•••••.•••••••••• _••.•.•.•.••.••.••••••• A2-l . • . • . • . • • • • . . • . . A2-3 Minimum A U c ... '!:::>

"' i

::>

~J . ~ I~

•

t

=

zo

~

.... ... ....

~i oo

1..0

~

a:

0

t20

10

tao 70

ADO OJ X HEAOWIMD COIAPOMEJfT TO ABORT SPEED. SUBTRACT U X TAILWIMD COIAPOMENt.

AGURE/U--7 /U--13

-

TO 1F-117A-1

NORMAL PERFORMANCE OR MINIMUM DISTANCE TAKEOFF ABORT SPEED BRAKE ENERGY

-FS------

C2) f-..aE-f'1 D2 fUU GRADE: - -- 6--4 fVB. DEJISITY: •• U UIIUS GAL

_ , _ , •••••••• F-1T7A Do\TA IIASts:: ••• fUGHT TEST Do\Te ----- - -- - 1110¥1-

•

IIIWCf £II£IIGY UJoiiT -

a x 10" n -t..a. I)/I/////, Do\IIGOI

:IDlE

CAU110II 101tE

~ OI'EIIA~

:IDlE

---10

0

CXJ'! CU&I

-~

FlGUREA34

A3-14

______ ----:_.

TO 1f -117A-1

•

NORMAL PERFORMANCE OR MINIMUM DI STANCE TAKEOFf ABORT SPEED BRAKE ENERGY _...ES: ...... CZ1 FlO I GE FID2 RIEL GAAilE: ••• ~ RIB.~ • U UWS CAL

tt00E1.: •••••••• f.117A DATA tiASIS: ••• RJGiKT TEST DATe ••••••••• t -~-

-20 -to o to 20 AIR TDII'OIATURE - "C

_,. I

I

- 20

0 -

I

I

20 .., .., • TEIIPOIATUJIE • •f

I

I

1110

120

DI£JIGY UttrTUXtail R-lll. IIIW(£

l//////l/1 DAIICOER ZDitE

CAII1lOif ZDWE

5

.. •'"' '

0

-IIAL ....!::'

100

i

z

OPDIAllHG ZDitE

•

.,"'c

f1GUREA3-9 A3-15

TO 1F-117A-1

MAXIMUM WET RUNWAY BRAKE APPUCAnON SPEED ~SPUIII

~ 0

F-1f7A fUGHT TEST

QOJQWEJI:

o o o 0

1

fUEl.~

00000000

llo\TA BASIS: llo\TE: 0

0

0

0

0

0

0

0000

fUB. GAADE:

ocr ,_

.

0

o oo

Cl) ~DIZ

0

~

0

0

o o

•

U UIIUII GAL

GROSS WT - 1 - Ul

-

-

-to

• 10 a • Alii TOIPERATUIIE - "'C

0

a

•

111

eo

•

too

"

• 1:111

AIR T£MP£AA1UIIE - • F

-----------------------------AG~1o------------------------~==~~ A.S-16

•

TO 1F-117A-1

NORMAL PERFORMANCE OR MINIMUM DISTAHCE TAKEOFF MAXIMUM ABORT SPEED

NO-

ftTRU-AY

11000.: • • • • • • • P-t 17A DUA U$1$: • • • fUGHT TEST OAl'E: • • • • • • • • • t OCT till'

-20

0

20 ... 10 100 AIR Tflfi'OU.TVM - • F

B1G1NES: •••••••••• (:l) , _ GE F1 02

RIB. GRADE: • • • • • • • .IN fVB. DBIS!Te .••••• U lA/US GAL

120

i•

.... ::>

.. .. -.....=. :

0

::>

0

:

i

ic

• A3-17

TO 1F-117A-1

NORMAL PERFORMANCE OR MINIMUM DISTANCE TAKEOFF MAXIMUM ABORT SPEED BAK- 9 BARRIER IIIOOEl: ...........1 f7A DATA BASIS: •••• fUGHT TEST

DAre •.•.•••••• n IIOY 1 -

-20

0

20 40 .. 100 AIR TEMPEIIATUR£ - . ,

t20

AVAD • • f RUNWAY fR()M 8RAICE llnLUE TO BARfiiEII - 1 - n

110

-

1110

1711 110

110

150 110

1711

,.

110

110

/

/

/}

110

150

/

\

ADOU X IIEADWINDCOMPOHENT TO~ SPEED. SUIITIIACT U X TAILMKD COMrOIIDIT. W£T IIUWW.lY

DRY IIUWWAY

----------~nmE~n ----------------------~--~ 43-11

•

TO 1F-117A -1

•

NORMAL PERFORMANCE OR MINIMUM DISTANCE TAKEOFF MAXIMUM ABORT SPEED BAK-1 2ER OR BAK-14 BARRIER C2l f404-GE.f'1 D2

IIOOEl; •••••••• F-117A

EHGIIl£S: • • • • • • • • • • •

O.TA IIASIS: ••• fUGKT TEST O.TE: ••••••••• II -~-

J'U£1. GRADE: • • • • • • • • -

J'U£L DEMSrrt! • • • • • • 6.5 UIIUS CAL

-20 - 10 0 10 20 ~ AIR TEIU'SUTURE - "C

-

I

-20

0

20 .0 150 ., AIR TEIU'SUTUR£ - •F

100

t20 AV• • • AI F RUNWA-Y FROIIBAAJCE REI..EAS£ TO BARRIER - 1000 FT

Z20

2.0 210 180

200

1!10

200 1711

110 180

170 ISO lfiO

/

/

/l

/

150

1.0

\

•

1&0

ISO

140

I

WJO atUTE

WITl1

140

W/10

atUTE at\IT£

WET RUNWAY

WITl1 atUTE

ADO U X IILADWUID COiolf'OKf'ln TO~ SP£ED. SUBTRACT U X TAILwtlCD COioli'OHBfT.

OII'YRUKWAT

FiGURE JCS= IS

A.l-19

TO 1F- 117A-1

NORMAL PERFORMANCE OR MINIMUM DISTANCE TAKEOFF MAXIMUM ABORT SPEED BAK-13 BARRIER DIGIIIES: __ ........... CZ) P'IOI ~02 fUEL GRADe •••••••••• JN fU£1. llEJISITY. •••••••• U L8IUS GAL

MOOE1.: •••••••• F-117A DATA BASI$; •••• FLIGHT TfST DATE: •••••••••• 1 - 1 -

~

~

-a

•

~o

o

a

10

~

AIR TEIIPERATURE -•c 20

~

•

•

~

100

•

~

1a

AIR TBIP'ERA"TUU. - • f

liD

2211

..

.

0

0

;

::> :Z:IIO

""'c

"c

.. 517e ..

..

~uo

~1111

:z:

·/}

/

110

:z:

c

- -......- - i / /

zoo

i

1f0

110 110

150

150

I\

ADOUlllf.E.ADWIIfDCIOIU'OeiBn

FIGURE c

.. GROSS WEICHT - 1000 La

•

RC''RE.-.M--11

A4-20

TO 1F- 117A-1

•

CUMB PERFORIIANCE loiOOEL;

F-117A

o.\TA BASIS: RJCHT TEST o.\TE: 1 WAR t988

m FINAL AU. -

1ooct-Ft.-

TWO eiGINESAT W-'"'MN ~ GEAR DOWN - CG@ Q.O% WAC STD o.\Y .. 2D"C

$

10

HTW. GAOSS WI.@ SL

l5--l-20--l

saMCE 25

32000lB.

C211NG

29400 Ft.

TME TO ID - loiiN.

1.0

.2.2

3.S

5..3

1.7

23.3

RJEl USED TO ID - lB.

2*

5\3

770

106S

1516

2993

DISTANCE TO ill - N.Y.

4.5

\0.2

16.6

25.3

41.3

108.2

23.8

NT\Al GAOSS WI.@ SL

31iDDDlB.

2liiiiiO FL

l.2

u

4.3

6.8

\3,0

m - ta

296

817

9.a

1350

21n

3360

DISTANCE TO ID - N.Y.

5..3

12.3

20.A

32A

62.1

112A

l1IIE TO Jl - 1o1M.

RJB..IJSB) TO

INmAl GAOSS WI.@ SL

2'5110FL

~lB.

l1ME TO [D - WIN.

1.4

3.2

5..3

8.9

FUEL USED TO 1D - lB.

352

7 44

1159

Tn;e

DISTANCE TO ID - N.Y.

6.A

25.3

~

,.....

HTW.GAOSSWL@SL

u

6.7

12.7

422

1J(J1

1A62

ZC40

DISTANCE TO ID - H.J&.

7:1

"\U

32..2

6\..1

z.o

u

m - ta

513

DISTANCE TO ID - H.J&.

9.3

ZUI

1131

1910

ol()\2

:2Z.9

42..5

105.2

RJEliJSB) TO

1!1 - LB.

DISTANCE TO Jl - N.Y.

-

-

62

\2.3

faT

,~

21>31

11.8

29.5

59-4

113.5

a.• 4352 12&.3

29.6 5152

142.2

191110FL

52000 LB. 2.5

3685

2DIS40FL

&.1

INfT1Al GAOSS WI.@ SL

1VE TO 1D - WIN..

--

p.e apc:ratia& and wnh tbc p r up is 5bowD in FlgUI'CS AS-19 tbJ1I AS--23. MaximUIIl Powu lilies (one eap) are pn> WJed for SWidard day &empetatDie clevabaiiS ol - 20"c. + lO"c. O"c.IIDd -JO"C. if• , . . Ullormarine

•

LONG RANG£ CRUIS£

f..oal.....,eau;r informa•WM! forme CD~iac.apaa~­

SPECIAC RANGE - TWO ENGINES GEAR UP Sperifc fal1le (nanticll miles per um pounds ol fuel) vs MD wilh a .,.,....lc ol KCAS i1 s1ooom in FipRs AS-1 llara AS-16 roc altjtnclc:s r.- seale'l'd 10 lS,IIlO [eeL 1lle Clll'a --~foe llle qx:ratx.aJ ~ ol ,._ ~ at cadi alrirnde and aJttt tbc speed ruce a•ailallk. 1be IIID:im,. eadurance (loiter) and loll& range auise speeds are iDchoded for each altirude. ldalimum Powu lilies mm.n! dlyde\~ol + 20"C. ~ lO"c. O"C.and -lO"C are abo P'"'ided.

ro.

iq ud willl tbc p r ap is '"'""'a da:d iD F~g~~re A5--2A. The h " \ I pocedme IS IOta llle opentinc eoopoc at Ma:ciaaaw Powu ud ud allow llle arptme 10 ame-dimb 10 llle alrirnde md speed sdiM!olc sbowu..

SPEClAC RANGE - TWO ENGINESGEAR DOWN Spcci6t , . . information roc rwo es~p.es wnh the c,ear doom is precmu•l in F~ AS-26 tbJ1I AS-31. Tbe mror-tioo is presented lllld used as .-c•iously h !for 111c rwo eoop.c- scar ap~ip!ali • Loll& ruce O"'li5e is -ldll mFcurc AS-32. LOHG RANGE CRUISE

NOTE Rder 10 Sectioa v for speed timnat._

lA:Io& ruce craise iDformMiDa for_,~ operlililll ud ..o lllcscar doom is ...._ "LtCd m F~g~~re AS-32. 1lle to • .ted poa:dw e is 10 x:t bocb • 4 · w s as Mamatml P'oM:r' ud a o:isc drrb at the altitade-.cd v'wdole sbowu..

ED.alpe:

DetermiDe 111e range avaiable at JO.OCO rea 011 a SWidard dly at Q.80 Madl ro. aa inilial weight o/40,000 pouals if 8JX) ~ ol fuel IS 10 be alltSIIIIDed. Eater F~ AS-11 at40,000 poamsmd O.S Mad! No. and n:ad speafic raQ&e as W namical miles per JIXXI powods ol fuel.. Reenter at O.S Mach No. '""" 32.000 poundl («l,,XX-IDXI) '""" read ~ cilic r-cc as 97.7 nau•ra' miles per U:XXI poalllds ol fad. The specific~ is 91.& allticaJ IDies per 1(0) pouals ol fud .., llle . . . .-aibbk ro. a:m poaadl ol fuel _ _ , is 734.4 aautocal miles ('!11.8" lDJlll~

v-

••CO#!

LONG RANGE CRUISE

laD& dJI&r auise ill!..-- ro. twO~ operatin& ud wnh tbc pr ap IS SWIIlll8rized m Fcure AS-17. The recommeacled pocedu.re IS 10 set bocb

•"i es at Maxim,. POwer and Cl'llisepected dlorill& ......, RaD&c Cn:tise at crmnnJ altilode for SWidatd day condit.OIS wUh two mcP- npemm& gar ap, with ODe eap:.e apcmiolz '""" Oile Cllpe ;,. • •U.C. &ear ap. Uti willl rwo ac e• operatia&. ccar doon, respeai.-dy. The CXJ(ji ,..,.,... Cl1lise Mad! No.lllld SWidard day 1ille Ainpeed are also sbowu.. Corrections for --mndml dly c:ooditioas arc o;opplird, if rcqail cx:l The fuel flows are cSetiw:d r.- doe U., ~ JiK5 sbowa 0. doe SptriCoc ~ dian:$. Fcurcs AS-1 JhtoaP AS-16 (twO I opcraria& pr up), Fogares AS-191hroop AS-Z3 (one eq;.,e opcnJio& one CQiillc ~ up), aDd Frpres AS-26 tbtoa&h AS-31 {two '"I&. oper-

c:r-c

s

ccar

atin&. ccar ""-">-

!•

----------------------------~·

TO 1F- 117A-1

•

SPECIF1C RANGE SEALEYEL

TWOBfGDlU - GEAIIUP CG.Gft iiAC

ew;urcs= •••••• C2') f •ot CL.,.1 D2

IIIOOE1; • • • • • • • F-1 17 A

QATA BASIS: • • •

RIB. GRADe ••• ,... RIB. OEIISfrl: •• U LIIIU$ GAL

AJGHT TEST

DAre • • • • • • • • • 1 IUY 1 -

~

~-

5a z ' »

..

ic

2

~ a ~ 'u *~DID.

•

0

o..so IIACH 110.

100

150

---

•

_.~====~====~--------------------~AS-1 ------------------------------AS-3

TO 1F- 117A-1

•

SPECI A C RAN GE SOOOPT lWO BIGUIES - GUll W

CGOu.n.IIUoC IIODEl: • • • • • • • • 1'-117A DAJA IIASIS: ••• fUGHTTUT DATE: • • • • • • • • • I IIAY 1-

100

\a 150

zoo

EJIGIIIES:: ••••• CZl f l OI GE-#1112 fU£1. GRADE • • fU£1. DBCSIT1'! • U UWS GAL

-

-

CUIII

-AGUR£~2------------------------------~

TO 1F-117A-1

•

SPECIAC RANGE

·-"

1WO BIGlllU- GEAR UP

coe-MAC

11100!1: • • • • • • • f-117A DolTA BASIS: • • • fUGHT TEST DolT!: • • • • • • • • • 1 IIAY

t-

£IFDIES: ...... C2) reo • GE~ m fUEL GRADE: ••• ~ fUEL oetSII t: •• U UlJ\1$ GAl

......".

'~

RANGE CRUI$E

ID

~

§SO

STDOAY

:; i

+20"

..." z

STDDolY +10"

I

r

z c

STDOAY

c

-10"

6

:'»

•

20

•

c

STDOAY

...2

100

c

ISO

200

-

.... 500

c

TO IF-117A-1

•

SPECIAC RANGE 1-fT 1WO EJIGillU - GUll UP CG.e.KIMAC

......,.,.,.. • • • • • C2) HOt GE ~1 02

IICXlE1: • • • • • • • • F- 117A DATA BASIS: • • • fUCHT TEST DATE: ••••••••• 1 IIAY 1 -

RIU. GRADe •• ~ RIU. DEIISI11t • U U/US GAL

• 5

1. 5a

.....

MAXIIIUII

ou

Ji

STDDAY

+20"

1 ..

c

STDDAY +10" c

..

2

STDDAY

•~-

- to· c

STDDAY

·~ ;;.··

•

..... tot

150

2SO

------------------ -f'IGI'FlE M4---------------------.,

TO 1F- 117A-1

SPECIFlC RANGE

-FT

TWO~-

G£AII UP

CC@~IIAC

loiOOE1: • • • • • • • F-117A DATA BASIS; • • • FUGKT TEST DATE: ••••••••• I IIIAY 1 -

IEJIGiliU; •••••• (2) ~ llQ fUEL GRADE: ••• .114 fUEL DEJISfn •• &.5 LII/US COAL

.. ...

.~ . · ·~­ RANGE CRUISE _

....

STDDAY

+10.

c

.,so

STDOAY

"a:cz

-1o· c

STDOAY

0

;;:

2.a • L

30

;:!::!

UJ :J,.IMD

20

100

•

o.so 150

RGURE~ -------------------------------

TO 1F-117A-1

•

SPECIAC RANGE 2:5000f1r TWO £1IGIIIES - GEAR UP

c:GO-IIAC £JIGIII£S: FVB. GRADE: •• FVB. DEII$ITY.: •

IIIIOOEI.; • • • • • • • • F-117A DAtA BASIS: • • • RlGHT TEST DATE: • • • • • • • • • 1 IIAY 1 -

- - - - --.,001

--·~

10

10

~ ,711 ...i

.

~

'

STODAY + 211' c

-

z

' 60 u

..!l ~ c

.

...•2so «<

fll

~

STODAY +10' c

m~~ c

-10'

'

~fQ

::;

~liD.

.

' ' 3D

100

CIAO

IUD

150

o.so

Cl.lll IUCH 110. ~

ICCAS

Cl.1ll

-

CLIO

CLIO

-

•

TO 1F-117A-1

•

SPECIAC RANGE

-"

TWO~-QARUP

CGOaJI'J.IIAC IIODEl= •••••••• f-117A

EJIC"..DI£$· •••••• (2) -~·*IDZ

OA.TA BASIS: ••• FUGKT TEST

RIB. GRADE: • • Jl4

RIB. DENSIT'e • L5 U11US GAL

DATe ••••••••• 1 IIIAY 1 -

110

100

e .... §

10

::; i

z

..•

TO

0

iZ

z

STD DAY

+20.

c

"'&:0

..•.. Q

eo

-1o· c

"!50

.

.

'

...,

R ~or":

30 11.30

o.AO

o.so

uo MACH NO.

•

c

STD DAY +10. c STD DAY STD DAY

100

1:10

20D

250 ICCA.$

.flGURE-AS-1

CI.10

GAO

o.IO

TO 1f -117A-1

•

SPECIAC RANGE 1WO fJIC~"GENII UP

reecs cc:e-MAC

D'C"""" ...... Cl) --GE-1'1112 fVEL GRADE: ••• JN fVEL IJEII$Ift; •• 6..5 1.111\J$ GAL

111000.: ••••••• F-117A DATA IIASIS: • • • fUGHT TEST DATI:: ••••••••• 1 IIAY 1 -

110

100

-

10

~

§

10

~

...i ~

z

..•

.,.

STDDAY

~

~

It

g

..•iil •

.. , •. c

STDDAY STDDAY

- so· c

~~

so

.....

o.AO

t50

AS-10

~

+21'C

STDDAY

2'00

TO 1F-117A-1

•

SPECIAC RANGE -I'T

1'1110 OICOIIIES - GEAR UP OG. C1ft MAC

£Wi!MFS: •••••• C2) ~.f'1 02 RIB. GRADe ••• ~ RIB. DEIISlT'e • L5 LB/US GAL

* - 1 : ....... F-1174 Oo\TA IIASI$c ••• fUGHT TEST Oo\TE: • • • • • • • • • 1 IUY 1 -

110

100

5

'..

10

...i z

STDOo\Y

•20"

70

,:;~

ic c

- 10" c

~

~

10

•

•

. , •. c

STDOo\Y STDOo\Y

2

2 •

c

$TDOo\Y

100

a.30

CIAO

15e

&.50

-

...,

ue

- - NO.

Z5D

ICCAS

tJRE-A>

LIO

.,...,

-

TO 1F-117A-1

•

SPECIFIC RANGE -FT

1WO ENGUIES- GEM UP CG 0 4S.O'S fMC

_,,1:12

~£" •.•... p) _ PUO. GRADE: ... ....... 1'VB. ~ • U IA'US GAL

F-117A DATA BASil: • • • fUCHT TEST DollE: • • • • • • • • • 1 MAT -

IIOClEl; • • • • • • •

ue

.,, LOIIG IIAIIGE CIIUIR

~ ~

=taiiio- • 100

10

~

I:;

.. ..

...

10

i

STDDo\Y

~

711

0

z

-te·c

2

~

•

+to· c

STDDo\Y STD Do\J'

~

... 2

•a·c

STD Do\J'

10

~ '

50

~

...,

30 Q.30

IIAO

&.50

CI.JO

...,

...,

IIACIIIIO..

100

150

2:50

200

JCAS

AGUREAS-10

AS-12

•

TO 1F-117A-1

-"

SPECIAC RANGE 1 W O - - GEAR UP CG.OY.IUIC

IIODEl; • • • • • • •

EliGIIfD;: •••••• ~ ,__-#IOZ

f-liTA

RIELGRADe ••. .IN fUEL~ •• U UIIIJ$ GAL

DATA BASIS: • • • fUGHT TUT DATE! • . • • • • . • • 1 IIAY 1 -

110

CJI()$$ wt. -

1000 1.11

100

110

~

I

5s z

.00

..

•

"

..•

.

•20"

c

STDDAY +10° c STDDAY STDDIIY

0

z cc

STDDAY

-1·· c

7'0

0

-.. 2

MAXJII!JM POWEJI 10

so

o..so

150

•

RG~~tl------------------------------A.5-13

TO 11'-1174- 1

•

SPECIF1C RANGE ,_fT

TWO fWA•U - CUlt UP

c:cea.RMAC

~ •••••••• F-117A

EliQUCES: ...... CZ1 ftOt CE F1 D2

DATA IIASCS: •••• fUGHT TfST DATe •••••••••• I MAY 1 -

fVB. GRADe ••• fVB. DEJISI1"e • L5 UINS GAL

110

100

!!

§

:;

•

AU.

TDAI'SIATURES

i

z

.."

5c

g 2 •

..

70

If:

. so

..

,

Cl..tiO

l$0

-

~-----~·

TO 1F-117A-1

•

SPECIFlC RANGE

-"

TWO EIIGUI£S - GEAR UP CG·~IIAC

- = 0 0 000000

DATA BASIS:

Doll"E:

o o o

o o o o o o o o o

-D: o

f-117A RJGHT TEST I IIAY 1 -

o o oo o

RIB. GRADe FUU. DEJISlTY;

0

0

o

Ql ~IDZ -

6.5 L81US CAL

110

100

10

•.. I

ALL TDIP£JIATUAfS 10

5a

...;.+~

~~

z

.

70

ic &

~

2 • ~

10

50

,. o..30

....

o..so

GAO

IIACM 110.

•

100

1511

all IICA$

AGUAE~

Q.10

....

-

....

A5-15

TO 1F- 117A-1

•

SPECIR C RANGE

-"

TWO a.GPES - CEAII UP

mea.n.IUC

£WP'"D: • - • • • • CZl f.otOI.-Gf.#1 az

_ , •••••••• f-117& DoU.t. IIIASd: •••• FLIGHT TEST

fUEl. Ga.t.DE: ••• .114 fUEl. OEMS!re • L5 UIIUS GAL

oare .......... 1 au.Y • -

lit

••XJMJM

to

~

I:;

to

i

z

•

i ~ 2. • c

to

,...,. Ito

-

&.50

....

15D

210 ICCAS

-AS-14

AS-16

Ull

IIUioCM .a. Z5D

GAO

CUIO

-

•

TO 1F- 117A-1

SPECIF1C RANGE -fT lWO ~- GE.AII UP

oc e a.n.IIAC

BIGIIIES: •••••• C2l ~~ DZ RIB. GRADE: ••• J,... RIB. DBISI'I"t •• U IA'US QAl

IIOOEl: • • • • • • • F-117A Qo\TA BASIS: • • • fUGHT TI!ST Qo\Tf: • • • • • • • • • I IIAY 1 110

IIAJCIIIUII

110

!l

§

10

:;

- tt>~

i

z

.. ..2"' -..

~

1'0

0

z

c

2

10

50

30

030

o..so

OAO

.... IIAQIIIQ.

•

110

ISO

200 ~~CAS

.flGURE-M-15

&.70

....

...

TO 1F-117A-1

•

SPECIRC RANGE

-FT

TWOBIGIIIES -GEAR UP OGO~IlAC

EIIGINES: • • • • • (2) ~40ie.fl D2 FUB. GRADE: • • Jl4 fUEL DBISrrt: • 1.5 LIIIU$ GAL

IIOOB: . • . • • • • • 1'-117... DATA BASIS: • • • fUGHT TEST DATE: ••••••••• 1 llAY 1 -

no

LOHG RANGE CRUISE

GIIOSS WT- 1000 LIB rT

.

.

.. .

'. '-1 ......

IIIAXJIIUM ENDURANCE -i H""" 100

5

§

::;

i

z

.."

· ~

10

~

l

z

c c

ALL Ta&PEJIATURfS

•

10

~

..•... 0

10

o..so

0..110

I

150

200

I

zso

300

~--~--~· A5-18

TO 1F- 117A- 1

LONG RANGE CRUISE SUMMARY TM> BIGIIIES AT IIAXIIIIUIII POWER GEAR UP- CC 0 - MAC o.m IIAQIIlO.

BIGIIIES: •••••• (Z) H04-GE-f'ID2 fUEl. GRADe • .. JP-4 fUEl. DEIISIT"e •• U UIIU$ GAL

IIODEl: ••••••• F-117A DATA IIAS&S: • • • FUGHT TEST DATE: ••••••••• 1 MAY 1 -

....

ID 0 0 0

~

~

100

z l

Ill

0

z

-c a:

10

0

iL

0 Ill

..,... co ...... !;iC O l

--c co ~-<

t:

60

• 2

0

co

0 0 0

I

Ill

a

36 (II

~

-c 0

!:i -c a:

Ill

:00:

32

:::>

1/) 1/)

Ill

...a: 2S

•

GROSS WEIGHT -1000 lB --AGUR~

AS-111

TO 1F-117A-1

•

FUEL FlOW FOR LONG RANGE CRUISE - CONSTANT ALTITUDE TWO ENGINES OPERATING • GEAR UP CG 0 4l.O'Irt .w;- STAHIWI> tw' PRESSURE AU.- FT. 30000l8. MACH NO. ICTAS

$.L

1CXXIO

5000 ..9)

A

15000

.62

25000

81 .a3 2090

FF/EHGIHE

3011 2S70

325 2lii90

..53 340 24W

34000l8. MACH NO. ICTAS

A 3Z1

FF/9IIGfNE

3100

.53 3C3 2!170

.56 3511 2750

.51 339 3-420

3511 32:20

.52 346 315110

5I 311 3450

3270

3100

2950

.55

..59 383 3870

.63 000 3450

.A 42115 3330

J3 4-41 3200

.61 395

.li5 4 12 3610

J'O 41 3570

..15 OliO 30Ql

35otO

.71

.76

..,

413 31160

444

461

3730

3&10

31!000l8. MACH NO.

KTAS FF/ENGIN£

KTAS

FF~

2450 R

MACH NO. FF~

50000l8. MACH NO. KTAS

fFIBiQo1E 52500l8. MACH NO. ICTAS FF/ENGINE

363 311110 .56 312 0000

38110

.sa

.61

3110

399 4050

4300

a

Zl!IO

.az

.fi6

.71 C29

216110

2JC70

23110

312

.60 000

.£1 .,3

2!170

211110

2670

.sz

.,.

431

-

395

-LB.

KTAS

382

3110

.sa

.55

ca:JOO LB. MACH NO.

LJO

sn

-

J'O

30000

.72 4216 2IIJD

.77 452 2350

402 2820

:r•

.77 "55 2560

J7 062 211211

.82 413 2940

.10

.13

C79

4&9

3270

3210

..,

-

41111 3700

11

MACH NO.

0.50

QB)

().]0

11..110

6 KTASf10"C

6.0

7.2

8.4

9.6

;- HOTCW'

· CXllDDAY INCREASE FUEl. F1.J:1W :nl. PER 10"C A80IIE STAHIWI> OAY TEMP. DECREASE RJa F1.J:1W :nl. PER 10"C IIB..OW STANDARD DAY TEMP. •

DATA ARE FOR Q.99...,..... N NN/1000 LB.

•

DATA Bot.SIS: FUGHTTEST REStAJS

RGUA£ AS-11

• AS-20

TO 1F-1 17A-1

•

SPECIFIC RANGE SEA LeiS. 011£ EJIGUIE IJIOf'EIIATIYE GEAR UP - CG ct - I I A C

IIOOEl; ••••••• F-117A DATA BASit: • . • fUGHT TEST DAre ••••••••• IIIAY 1 -

fJIGII(U; •••••• (:!) -...caE.f'1D2 FUEL GIIA.IlE: ••• .114 FUEL DEKSITY; •• 6.5 LII/\IS GAL

• li l" ll lll

LONG RANGE CRUISE

·.~

J;:

50

'~' IY

..i c

"'~ 2... • 20 UliiJT DID. AOA

10

100

•

150

AS-21

TO 1F-117A-1

•

SPECIAC RANGE

-"

01C£ EJIGilfL IHOf':VIA'ItYE GEAR UP c:o•~IIIAC

_ , _ , ••••••••

f.W.H r.u= . C2) fiOt CZ-#102 PUB. GRADE: • • 1'-4 PUB. IIEJiSi I t; • U LIIIVS GAL

~1tJA

u

DATA IIASIS: • • • AJGHT TUT DATE: ••••••••• 1 MAr 1 -

100

150

200

-

ICCAS.

••

-

• AS-22

TO 1F-117A-1

•

S PECIF1 C RANGE 1-fT ONE D'G'IIE GoEAII UP CC.a.KIIAC

-TI'I£

IIOOEl; •••••••

F-1f7A

EJIGIIIES• •••••• P) HCMGE-#'1 DZ FUa GRADE: ••• J~ RIEL IIEJI:SfT't •• U 1.11/U$ GAL

DATA ISASIS: • • • RJGHT lUT DATE: ••••••••• 1 MAY 1 -

7'0

· 111:1> MT

•

.. 50

"ccz

..

2

..

2 •

•'to

1110

•

150

-

TO 1F-117A-1

•

SPECIRC RANGE

-'11\'E

1-P'f ONE BiGUIE GEAR UP'

oc:;ea.n.MAC

f.NCiiiUlES; • • • • • CZ) f'tOt ~..fl1 D2 RIB. GRADE: • • JP.4 PVO. DEIISii"e • U LiiiVI GAL

MODEl: . • • • • • • • F-117A OATA BASIS: • • • RJC0HT TEST DATE: • • • • • • • • • 1 MAY 1 -

•

to

I.DGIW~

•

;+

~~, fm~

5

§

10

::!:±:l

:::;

~

AY

~~~~

i

z

." I

z

•

c a:

0 &:

0

..."'

•

jF

~

so

150

•

TO 1F-117A- 1

SPECIFIC RANGE

-"

ONE -INOI'EAA11VE GEAR UP - CG. G..O'JL llAC

~ ••••••• f-1f7A DoiTAIIASlS: ••• RJGKTTEST DATe • • • • • • • • • 1 IIAIICII I -

5

I:;

cw;wF$· •••••• CZ) flOe GE~1 D2

fUB. GRADE: ••• ~ fUB. LtiiSiit: •• U LAW GAL

10

i

z

.. 0

z

c c

g ...•2

AS-25

TO 1F- 117A- 1

•

LONG RANGE CRUISE SUMMARY OIEBfGUIE-lM.. GEAR Ul'- CG • G.K MAC

AU. TEIIPSIATURES o.7a MACH 1110. DICMES: • • ••• CZ) ~112 fUEL CIIADe • • .... rue. - n . u 1.11/U$ GAL

IIOilEl: • • • . . • • • f.1 17A DATA BASIS: • • • fUGHT TUT O.O.TE: • • • • • • • • • 1 IIIAIIQI 1 -

-..., z ..

•

i

l

0

z

• 2

•

-

t:: 0

g

l

Ill

20

0

§

10

Cl>

fl)

Ill

...a: 0

GROSS WEJGHT -1000 LB

fi6YAEt\5 M

-

- - -...............-~~·

TO 1F-117A-1

FUEL FlOW FOR LONG RANGE CRUISE - CONSTANT ALTTTUDE ONE ENGINE INClf'ERAlNE -GEAR UP CG · -MAC - STANDARD DAY

-

PR£SSURE

LL

ALI. - FT.

30000lB.

A3 211-t

MACH NO. KTAS

Ff/EHGM'IE 34000lB. MACH NO. KTAS

FFIEHGINE

~

.¥1 299 4730

A5 299 5420

322 53!10

.so

....

311000lB. MACH NO.

52 :s:sT 5850

314

KTAS FF/B'GHE

fi02I)

42000lB. MACH NO. KTAS

FF/EHGIN£

FF/EHGM'IE MACH NO. KTAS

FFJENGINE 52500lB. MACH NO.

MACH NO.

dKTASnO"C

.57 7:i1

5170

5121)

.55

.58

35t

368

5760

5721)

.sa 3611 6440

52 343 1250

.55 363 1'030

380

.53 351 76150

374

.eo 7121)

.sa

77«1

.sa

379 8030

0.40

o.so

QSO

u

1.0

7.2

INCREASE FUB. A.OW ~PER 1D"CABICNE STAHDAAO DAY TEMP. oe DAY- NO WIND

GIIOSSwt.

Pllf$SUIIE AU1l\IDE -

- LB.

Full Fblr Mn/IOOOI.b. :mlOO

40000

48000

s

10

15

20

4160 14.4

4 130 1 4.5

4080 14.7

4 130 14.$

4 180 14.3

219

219

219

219

219

0.3£2 5.1

o.397 5.1

OAS7 5.1

QA31

Fullfblr Mn/IOOOI.b.

4710

4&1)

12.9

KCAS -No. NJA

232 D.351 5.1

232 • Q.3IS.C 5.1

46'50 12.9

4720

12..7

232 0.421 5.1

232 0.462 5.1

Fullfblr Mn/1000lb. KCAS IMchNo.

5190 11.6 247

5220 11.5 247

5250

5$10

Q373

112 247 0.490

N)A

5.0

OMIT 5.0

11.4 247 0.4-1) iD

tile JateaiJ seaioaolllli5 Apt o\ 1 fO< CIOD'TENJ'S PAGE UST OF ~ONS ............. •..................................................

~I

INll{OOlJCTI()N • • • • • • • • . . • • • • • • • . . • • • • • • • • • • • • • • • • • • • • . • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • ~3 ~ ............................................ .,. . .-.-.. ...................__..........

..~3

FUEL COSSUMP110N . • • . . • • . . . . • . . • . • • • . • . • . • • • . • • • • • • . • • • . • • • • • • • . • • • • • • . . . • . . . . . . . . . . TIME, FUEL USED. AND DISTANCE FROM BR.AICE RELEASE TO aJMB SPEED . . . • . . . . . FUELJETJlSON ......................................................................... FORMAT11NG SPEEDS AND AlnTUDES .................. ...... ................ ........ LEVEL RJGHT ACCEl..ER.A110N PERFORMANCE • . • • • . • • • . • • • . • . • • . • • • . • • • • • . . • . . . . . • . LEVEL RJGKT DECEI..ERATION PERFORMM'CE • . • • • • • • • . • • • . • . • • . • . • . • . . . . • . • . . . • . • . Sl1STAINED 1URN CAPABll.IJ'Y .. . .. . • .. .. . .. .. • . .. . .. . . .. .. .. • . .. • .. .. • • .. • • . . . .. .. .. .. MAXIMUM LEVEl.. RJGKT SPEED • • . • • . . • • • . . • . . • • . . . . • . . . . . • . . • . • . • • • • • • • • • • • • • • . . • • • . DIVERSIOS RANGE SUMMARY TABLES .. .. • .. • • .. .. .. • . .. • . .. .. • .. .. • • • .. .. .. . .. . . .. ..

~3

~3 ~3

~3 ~3 ~3

A9-4 A9-4 A9-4

USf OF ILUJSTRATIONS

TITLE

FIGURE

TOLD Cant ....................................................... ~I (Sbecll of 2) TOLD Cant~ ........................................... ~I (Sbecl2 of 2) Normal ~'l)tedl· Tae from Brake Rdcasuo Oilllb Speed ......................... ~2 (Sbecl I of 3) Fad Um:t fJOm Brake Rdease 10 canl is&"'""'"'br lbe M.islioa l'lanocrs asia& lbe MJssioD Dala Plo · 1 S,SU.. (MOPS). lbe top of tloe TOU> canl bas spaces for pt. Joe entries for llle folloorm& rtems as sbowrt ill !be TOU> card ilbtlieoialioes . 0. ID.itial al.t itude - 30,00) ft. E. Diswx:e 10 dcstinatinn 250 NMi Detcrminedhusioo taJ>1C infonna•inn forDnusioo Range SUTD1113T)'1llble for rwo ~ opemi:ng. no piJioad e inopc:rati>-e, cacb with gear up and with JA)too.ds o{

lmcremaua.l Cud remaining (4200 lb. - «XXX lb.)

200NMJ

200 lb. (appta - lA DISTANCE - N. WL EUJ'SEDTIIoiE -MIN.

EUJ'SEDTlME - MIN.

.aaoo R.Jausa>

- lA

DISTANCE - N. WL EUJ'SEDTlME - MIN.

RIEl. usa> - lA DISTANCE - N. WL

GR. WT. -lA

ElAPSED TIME - MIN.

3:11100

36000

p 2

+

~ ~

~

FUEL usa>

- lA

FUEL US&> - lA DISTANCE - N. WL

2.0

1.5

30

a.o

Z2

2.3 C90

4.0 190 31.0

2.5 57S l7.0

• •6 1000

u.s

~.0

5.0

300

350

400

C50

en

~

0.5'

Q.63

11.12

o.ao

o.a.

G.3 ISO 1.0

0.5 105 2.0

o.a

1.1

u

150

220 1.B

3111

2.4 510 l7.2

0 0 0

0.4 65 2.0

131

0 0 0

0.5 7S

3..0

.aaoo

ElAPSED l1UE - MIN. RJEL usa> - lA DISTANCE - N. WL

0 0 0

Q.6 130

52llOO

ElAPSED RJEL usa> - lA DISTANCE- N. WL

0 0 0

CUI 170 3.7

nNe--.

12 250 11.5

t2..5

3.3 7&1 a-5

lZ2

DISTANCE - N. WL

- lA

t75 4.0

5.0

~

21.5

a.o

0.5 100

FUEL usa>

~

a.o

Z2 5111 18.0

3..0 670 19.5

0 0 0

EUJ'SEDTIIoiE - - . ~

s.o

~.5

EUJ'SEDTIIoiE - - FUEl. usa> - lA DISTANCE - N. WL

DISTANCE - N. lolL

52llOO

12

u 330

3.3

3.S

• AEf'ER TO SECIIOH S RlA 4 0 EW IJYIUmONS.

....

5.0

o.s

13.0

1110 39.0

2..8 &DO 21.5

1..3

2.0

180

211)

U)

5.0

7.8

1• .5

1.1

1.6

2.3

2DO

sao

3.A 720

7.0

320 9..0

17.D

25.0

1.3 235 7.5

1.B 380 11.0

2J

175 5.0

5110 19.5

4.1 1111 30..0

1.0 215 5.5

1.5 27S 1.5

C50 12.5

1.3 27'S

u 31!10

6.0

9.5

Q.6

s.o

0.7 150 4.0

o..t

Z2

2.5 550 14.B

3.3 690 21.5

·-

5.0 1050 ~

u

aoo 25.0 •

AGURE-A9-G~ 2 of2) -------------.....;~

All-1 1

TO 1F- 117A-1

LEVEl. FUGtfT ACCELERATION

.

- L8. 32000

GEAR UP. C.G. @ - LB. DISTANCE - N. loll

36000

FUR usa> - LB. DISTANCE - N. loll

0 0 0

(1.5

40000

B.APSallWE- t.IIN. RIEL USED - LB. DISTANCE - N. loll

0 0 0

Cl6 90 3.2

ELAPSB>TIME -WIN. LB. DISTANCE- N. loll

0 0 0 0 0 0

0.9 t22

B.APSalTIME- WIN.

0

•

~

•

~

0 0

~

.uooo RIEL USED -

"'

B.APSalTIME - t.IIN. ~

RIEL USED - LB. DISTANCE- N. lolL ELAPSa> TIME -WIN.

52)00

FUEL USED - LB. DISTANCE - N. .._

KCAS GR. WI.

MACH

-LB.

NO.

32000

36000

~

40000

0

~

(/)

44000

~

52)00

•

ELAPSB>TIME -WIN. RJEl. USED - LB. DISTANCE- N. 14 ELAPSa> TIME - WIN. RJEl. usa> - LB. DISTANCE - N. 14

B.APS8l TIME -WIN. RJEl. usa> - LB. DISTAHCE - N. 14 B.APSalllME -NIH.. RJEl. usa> - LB. DISTANCE- N. 14 ELAPSB>nME- MIN. RJEl. usa> - LB. DISTANCE - N. MI. ELAPSa>TIME -WIN. RIEL usa> - LB. DISTAHCE - N. 14

69 2.4

17.4 4.6

2.6

3.8 615 26.3

4.0

4.8

625 25.2

778 33..0

2.5

3..6

343

617

5.8 893

11.8

51A 1&.7

l5.8

35.8

1040 46.D

2:SO

300

350

400

42,4

0.4"

G.55

Q.S5

G.7S

OJ!5

o.so

0 0 0 0 0 0 0 0 0 0 0 0

0.4 58

1.D

12.4 2.1 351 1A.6

22 369 15.9

D.5

12 192 7.6 1.5 231 9.1

1.8

2.0

0.8 tal 4.5

0 0 0 liDO

0 0 0 0 0 0

73 2.5

0.7 95 3..3

0.9

5.4

295

1St 6.8

1.8 285

2.6 4Z2

112

172

1.6 238

2.3

3.2

358

12

- f-

6.9

2.6 444 19.D

3.2 536 22.9

3..9

u

14.0

1.90 6.6

22 329 12.0

469

519 21.4 4.1 661

1&.1

26..9

2.5 359

3.7

4.7

5.9

7.1

539

710

1160

1:2.2

19.4

:!13..8

r¥11 37.1

129 4.5 1.3

3.1

• REFER TO SECT10N 5 FOR AIASI UD UMITATIONS. -flGURE-A9>-e~et

k f 2)

658 28.0

5.0 834 35.2

47.8

TO 1F-117A-1

LEVEL FUGHT ACCELERATION loiOOEl;

F-117A

-LB.

33JOO

36000

0

•

l:? +

40000

~

0

e

..000

"'

48000

52IXlO

200

250

300

350

400

4\9

0.44

D.S5

Q.65

0.75

Q.8S

Q.89

B.APSEDnNE- MIN. FUEL USED - LB. DISTANCE- N. lolL

0 0 0

0.4 2.0

4.5

B.APSEDnNE- MIN. AJEl USED - LB. DISTAHCE- N. lolL

0 0 0

Q5

1.0 160

KCAS 1-MN:H NO.

33JOO

p & +

40000

~

0

e

"'

48000

52IXlO

-

12

2.1

190 8.0

330

2.3 430

14.0

17.0

2.6

400

2.9 480

5..0

u; 240 10.0

0 0 0

0.7 95 2.0

12 190 s..5

B.APSeD T1N.E -MIN. FUEl. USED - LB. OISTANCE - N. lolL

0 0 0

0-8

1..5 235 6.0

11.0 2.A 380 11..5

EI.APSEDTlN.E- MIN. FUEL USED - LB. DISTANCE - N. lolL

0 0 0

1.4 190 ..0

2.2 320

490

8.0

1..0

B.APSeD 11J.IE - MIN. FUEL USED - LB. DISTANCE - N. loll

0 0

2.3 370

0

\21)

2.0

3.1

211.0

3.7 500

4..3 720 31.0

22.0

4.5

3.6 580 25.0

s.o

740 24.0

990 32.0

3.6

4.8 760

6.0

990 12.0

19.0

200

250

300

350

400

409

NO.

Q.44

D.S5

Q.65

Q.7S

Q.85

0-87

0 0 0 0 0 0 0 0 0

0.4

Q..8

1.4

55

130

4213

25

5..0

220 8J

2.3 370 16.0

EI.APSEDTIUE - MIN. RJEl USED - LB. DISTAHCE - N. lolL FUEL USED - LB. DISTANCE - N. lolL

Q5

85

1.0 160

1.7 210

2.8 450 211.0

EI.APSED11J.IE -MIN. RJEl USED - LB. DISTANCE - N. lolL FUEL USED - LB. DISTANCE - N. WI.

B.APSEDTIME - MIN. FUEL USED - LB. DISTANCE - N. lolL B.APSEDTIUE -MIN. FUEL USED - LB. DISTANCE - N. lolL

0 0 0 0 0 0 0 0 0

3.0

6.5

11.0

Q.6

12

110

200

2.0 330

3.5

8.0

13.5

Q..8

1..6 250

130 4.5 1.3 220 &5 2.6

390 13.5

9.()

2.3 370 13.0

2.6

410 16.0

2.6

19.0 3.1 510 24.0

3.4

3.9

540 2..0 4.3

630 29.0

61915

820

30.0

'ST.O

s.o

3.4 550

21.5

4.0 610 21.0

• REFER TO samoH 5 FOR AikSF€ED UNITAllONS-

FIGURE U4t(Sheet 2 of 2)

A9-22

1&5 3.1 440 19.0

NAQi

B.APSEDTIUE - MIN.

..000

80 2.0

Q.7

115

B.APSeD TIME -MIN. F\JEl. USED - LB. DISTANCE - N. lolL

EI.APSEDllWE- ~ 36000

so

1.9 300

KCAS Gil wr: -LB.

FUEl. GRADE: JP~ FUEL DENSnY: &5 L8/US GAL

C.G.@ 4S..O% WAC A1JTT\JOE: 20,000 FT.

DATE: 1 JUlY 1968

GR;W'I:

ENGINES: C21F404-GE-f'1D2

1WO EHGINESAT NAXI"' IJol POWER GEAAUP •

OATABASIS: RJGHTTEST

•

•

TO 1F-117A-1

LEVEL FUGHT ACCELERATION lWO ENGIIESAT M&JQM N POWER

MOOEI.: F-1l7A

GEAR UP.

DATA BASIS: FUGKT TEST DAre 1 .llAY 191111

C.G.043-KWAC AlJTT\Jile: 25,000 FL

GRWL -LB.

32000

311000

s> •

~

250

300

350

38S

NO:'

OM

OJ50

0.72

Q.83

B.APSEDllloiE - YIN.. FUEL USED - LB. DISTANCE - N. lolL

0 0 0

0..8

12 1A6

2.0 242

OJIO 2.8 351

7~

t2.S

19.7

B.APSEDDE -YIN. FUEL USED - LB. DISTANCE- N. lolL

0 0 0

o..t

u

2.5

lUi

309 16.3

3.5 455 2A.9

B.APSEDDE- YIN. FUB.. USED - LB. DISTANCE - N. .._

1.3 lC3

41000

B.APSED T1loiE -MIN. FUEL USED - LB. DISTANCE - N. lolL

48000

B.APSEDllME - MIN. FUEL USED - LB. DISTANCE - N. WI.

0 0 0

52llOO

B.APSEDDE - MIN. FUB.. USED - LB. DISTANCE - N. lolL

?( 0

200

0 0 0 0 0 0

40000

~

KCAS

32000

311000

?(

40000

0

e I

99 4Ji

&.I

22

tf1

3.A

4.7

4"12

6110

2.3 2I6IS 13.2

ns

6.1

~.0

zct

3..6

5J)

41:3

599

1150

11.7

20.A

31.0

46.11

3.9

~

436 2D..7

679 3:1.6

200

250

300

350

38S

OA

o.eo

o.n

Q.83

OJIO

B.APSEDDE -YIN. FUB.. USED - LB. DISTANCE- N. lolL

0 0 0

0..8

74

l3 155

3.5

7:1

2.0 25S 13.3

m

B.APSEDllME -MIN. FUB.. USED - LB. DISTANCE - N.loll.

0 0 0

Q.9

...

t.7

1CR

202 10.0

17.0

3..6 480 25.9

B.APSED TIUE -MIN. FUB.. USED - LB. DISTANCE - N. MI.

0 0 0 0 0 0 0 0 0

1.3 1$2 7.0

m

2.3

3.4 -433

63Z

KC.AS

GRWL -LB.

n

3.A

MACH NO.

440011

B.APSEDllME -MIN. FUEL USED - LB. DISTANCE- N. MI.

ceooo

B.APSED TIUE -loiiH.. RJIEl USED - LB. DISTANCE - N. lolL

52llOO

B.APSEDTWE- YIN. FUEL USED - LB. DISTANCE- N. lolL

z.6 325

20.5

u

13.1

zz..•

6.1

900 41.9

22 21152

3.15

5J)

Q5

680

1Z.1

zt2

32.2

u

2.8

$1.0

5JI

~

n1

Z1.4

3AJi

• REFER TO SECTION 5 FOR AlkSP£ED UWITAllONS.

fiGURE"U-9 (Sheet 1 Of"2~r---------------

TO 1F-117A-1

LEVEL FUGHT ACCELERAnON UQOEI.;

F-117A

1WO ENGINES AT MAlON! IN POWER GEAAUP

DATA BASIS: RJGHT TEST DA~

ENGINES: 12)F-404-GE-F1 02 FUEL GRADE: JP-4

•

C.G.@~MAC

1 JUlY 1988

•

FUEL DENSITY: 65l.SIUS GAl

Al.JTTU)E: 25,GlOO Fl:

KCAS

21)0

2SO

3llO

350

385

-;o:"

0. - lB.

1.3

2...4

150

300

DISTANCE - N. MI.

0 0 0

7.0

14.0

ElAPSEDTIME - MIN. AJEl. usa> - lB. DISTANCE - N. MI.

0 0 0

2.3

3..8

44000

2S)

12.5

500 23.0

48000

ElAPSED TINE -MIN. AJEL lJSS) - lB. DISTANCE - N. MI.

0 0 0

•.1 480 22.5

52000

ElAPSED TIME- WIN. FUEl. usa> - LB. DISTANCE - N. MI.

I":'"t8_.. 32000

36000 0

~TIUE-MIN.

-

40000

0 0

44000

•0

FUEL USSl - lB. DISTANCE- N. .._

+ ~

FUEL USSl - lB. DISTANCE- N. .._ ~TIME-WIN.

IG

FUEL USSl - lB. DISTANCE - N. .._ ~TIUE-MIN.

48000

52000

FUEl.USSl - lB. DISTANCE- N. .._

GR.wt:

MAO!

-lB.

NO.

36000 0

•~

40000

+ ~

0

e

CD

295

5.1

~TIME- WIN. FUEl. lJSS) - lB. DISTANCE - N. MI.

KCAS

32000

1.3

B.APSEDllME - MIN. AJEl. lJSS) - lB.

5.0

REFER TO secTlOH 5 FOR MG clD UNITAllONS.

3.1 500 25.5

•

HGORE .U::V\'Sflee('2 of'21~------~---------....;;;...

• ._24

TO 1F-117A-1

LEVEL FUGHT ACCELERATION lWO ENGINES AT WAXM., POWEll

WOilEI.: F- 117A

GEAR~·

OATABASZS: FUGHTTEST DATE: 1 JUlY 1988

C.G. 0 C10'Ir. WAC

.AI.:TTT\JOE: 30,000 FT.

GR.wt -LB.

p ~

•

?( 0

~

KCAS

2llO

2:50

300

347

I-MACH NO.

QS4

Q.B1

0.79

o.so

12

32000

ElAPSED DE- WIN. FUEl. USED - LB. DISTANCE - N. .._

0 0 0

110 7.0

2.4 ZZ4 \5.1

425 30.1

38100

ElAPSED DE-..._ FUEl. USED - LB. OISTNtCE - N. ....

0 0 0

2.1 \17 11..11

3.1 350 2:U

6.4 650 CSD

40000

B..APSEDlWE- WIN. RJB. USED - LB. DISTN«:E - N. .._

0 0 0

5..t 5211 3:2.9

KCAS

2llO

2:50

300

347

IIACH NO.

-

-

-

4.2

ElAPSED TIME-....._ RJEL USED - LB. DISTANCE - N. .._

48000

8..APSEDTIME - WIN. RIEL USED - LB. DISTANCE - N. loll

5l!llOO

RJEL USED - LB. OISTN«:E- N. .._

EI..APSEDTIME - WIN.

GR.wt -LB. 32000

38100

QS4

0.6&

o.J!I

o.so

EI..APSEDTIME- ..._ RJEL USED - LB. DISTN«:E- N. .._

0 0 0

12 115

2.4 Zll5 \5.1

U7 312

B..APSEDTIME- ..._

0 0 0

3.1 366 242

6.6 686 Q.8

RJEL USED - LB. OISTNtCE - N. ...

B..APSEDTIME -MIN. USED - LB. ?( 40000 RJEL DISTANCE - N. .._ 0

~

•

-

ElAPSED TINE -NIH. RJEL USED - LB. DISTANCE - H. loll

48000

8..APSED TIME -WIN. RJEL USED - LB. OISTNtCE - N. ...

5l!llOO

B..APSEDTIME -MIN. RJEL USED - LB. OISTNtCE - N. ...

0 0 0

7.3 2.1

191 \2.5

0

6.0 5115 34.3

• REFER TO SECT10N 5 f()A lo.i&'EED UMITATIONS. flGURE as-te (SiaZI 1

at2}---------------.. A9-25

-

TO 1F-117A-1

LEVEL FUGHT ACCELERATION TWO ENGINES AT loWCIM JN POWEJl

NOOEl.: F-117A

GEARUP

DATA BASIS: FUGHT TEST DATE: I JUlY 191!8

C.G.@ 43-.K NAC AI.JT1UDE: 30,000 FT.

ICCAS

2llD

250

D)

3&7

(1.5'

Q.67

11.1'8

o.so

B.APSED'TIYE--RJEl. USED - LB. DISTANCE - N.. I&

0 0 0

12 110

2.5 240

.., 4.5

&D

16.0

34.0

B.APSEDllNE --RJEl. USED - LB. DISTANCE - N.. I&

0 0 0

2.1 2llD 13.0

390 25.5

2llD

250

D)

3&7

(1.5'

Q.67

Q.7t

o.so

B.APSEDTINE - YN. RJEl. USED - LB. DISTANCE - N.. I&

0 0 0

1.3 120

2.5 255

7..S

16.5

4.7 525 36.0

B.APSEDTioiE --FUEl. USED - LB. DISTANCE - N.. I&

0 0 0

2.2 215

oiC)()

14.0

tt.O

GRwt:

YACH

- LB.

NO.

321000

3fiOOO 0

~

«1000

~ ~

B.APSEDllME - - RJEl. USED - LB. lliSINICE - N.. ...

40000

B.APSEDTIIE - loiN. RJEl.lJSB) - LB. lliSINICE - N.. ...

..000

B.APSEDTlME--RJEl. USED - LB. DISTANCE - N.. I&

...

.

EHGIHES:

C2)F404~-F1012

•

RJEl. GRADE! JP~ RJEl. DENSrTY: 6.5 UIIUS GAL

~

-

u

B.APSED T1ME - loiN.

521100

RJEl.lJSB) - LB. DISTANCE - N.. I&

ICCAS GRwt

YACH

-LB.

NO.

321)00

3fiOOO

p

..

1TIIoiE -

450

2llO

1.1 35 11.2

39

o.a:s

Q.90

1.9 40 11.3

om

0..90

1.8

1.9 42 11..$

40

11 2.5

5.2

7..$

9..$

112

G.36 0 0 0

0.45

().Sol

Q.63

Q.4

Q.S t7 4.0

12 25

0.72 1.5 33

o..ao 1.7

0.89 1.8

41

6.0

a.o

$1

11.0

Q.33

Q.41 Q.4

Q.50

0-58

Q.7

1.1

f7

24 5..$

Cl.ll6 1.4 31

t.5 0.74 1.6 311

7.1

&.7

G.S2 1.7 41 10.3

0.61 12.

11.&11

Q.76

Q.83

o.a:s

29

40

3.1

4.8

&.4

35 7.6

1.6 42

1.6

l6

053 0.9 ZJ

$1..4

11.6

0 0 0

G.30 0 0 0

10 Z2

•

2.D

:!.1

Q.3ll

0.45

•

Q.B

cu

1.6

u

u

u

0..90

1.8 44 11.3

Q.8S

u

45 12.D

~

REFER TO SECIIOH 5 ~AIRSPEED UliiiTAllONS.

~·._11 --------------------------------At-Z7

TO 1F-117A-1

•

SUSTAINED TURN CAPABIUTY TWO EJIGDI£S AT I&.UIIIIUM POWEll GEAR UP- CG C1K ~

e

I-I-

IIIIXE1.: •••••••• F-117A CIA~ IIASIS: •••• I'UGHT TEST DAre ••••••••••

e:••ts- ···--- CZ)fiOI

~102

fUEl. GIIACE: ... ..... RJO. DIEJISITY; • U UIIUS GAL

u

. • I

~

:I

:u

:•c

.... 0

z

::>

~ z

:t.D

Ul

..,

GAO$$ wr. -

50

tOO l8$

~

•::> •

•

TO 1F- 117A-1

•

SUSTAINED TURN CAPABIUTY TWO

or.•..-s &T

M

GENt UP - CG

·YD'l'lll POWER

e C;U"J' MAC

EIIGIIIES: • • • • • • (2) , _ ~· 02

IIOOB; • • • • • • • • F-1171• DATA BASIS: ••• RJCHTTUT DATE: ••••••••• 1110¥ 1 -

fVV. GRADe ••

~

FUEl. DEIISI'rt • U

IA'US GAL

... ..• •

~

.. 3

u

cc. c 0

z

0::

...

::>

Ul

ez :• ::>

•

...

30

..

10

~S~ - IOOUIS

... .••.

. ~

3

~

:1.0

az a:

~

Q

"' z Ul

•

UIUCH-1.7

u

u

311

40

50

~s~ - 1oo1.11S

,.

~

•::> •

TO 1F-117A-1

•

MAXIMUM LEVEL FUGHT SPEED 1WO BIG''ES AT MAICDtUII POWDI GLUIUP OG·~MAC

f.ll7 A ruGHT TOT DATE: ••••••••• I MAM:H 1 -

IIIOOEl; • • • • • • • • DATA IIASI$: • • •

EW"-s: . . . . .

P'IGdFIE .,_.., (SIIWt I Of 2)

At- 30

CZ) F~l m

fUEl. GAAile • • .114 fUEl. DtXSJ It • U Lll/\l$ GAL

•

TO 1F- 117A-1

•

MAXIMUM LEVEL FUGHT SPEED TWO flCQII

n

AT IUliiMUII rowER GLARUP

c:oe-MAC

EiiCidlES: •••••• p) ,_-G2>#1 DZ

IIOOB: • • • • • • • F-117A

RIB. GRADE: ••• ~ RIB. DEXSnT; •• L5 ~GAL

DATA IIASJS: • • • fUGHT TEST DATe • • • • • • • • • 1 IIUJICtl 1 -

STD DA'I'

+ 10· C

•

~

::>

~zo

.. ~ c

::>

•• 10 .. ::

•

•

--~--------------------------AGUA£~13~~~------------------------At-31

-

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE TWO ENGINES - GEAR UP

M00EL: F- 1t7A DATA BASS FliGHT TEST

BfGINES: C21F404- ID Oplnun Al. OIAie. O!*nLm Al. 0 1C1 On Ocusa

344 55J CI.S2

3III1 59.7

4211 1!2..7

65.2

0.167

o.n

~ ~

OJ9

Q.83

35

35

315

35

35

• 340 KCAS .0.71 Mach No.., MD1rrun-. 8000 Lb. cl Fuel. 0... - Cllrrt>..,loQI>dmum ~. CUll! Mach No.

• Wll1

men....,

At-32

-

I

14000 31700

FIG ORE U:::l C (&4ft 1 Vi 3)

1&000 301100

•

•

TO 1F-117A- 1

DIVERSION !RANGE SUMMARY TABLE lWO ENGINES- GEAR UP 2500l.8. ~ - CG.@~ MAC STANDARD DAY- NO WIND

loiOOEL: F-1l7A DATA BASIS: F1..IGHT TEST DATE: 1 MAY 1se8

ENGINES (2)F--.aE-F102 FUB. GllADE: JP-..

FUB. DEHSITI': 6.5 LBIUS GAL

PROCa>UM

RANGE AHD TilliE TO 1500 LB. FUEIL R9IAIHING AT SU L£VE1. $.L

5

10

15

20

2S

30

35

S1 9.S O.C9

62 \1.4

87

100 16.7 o.li6

113

1,$..0 OS1

18.2

125 19.S

2Q5

Q.53

74 13.2 o.57

0.72

0.78

o..83

t27 23.4

1C8

171

220 34.3

36.4

2&1 37.4

38.6

D.50

Q.53

29,() Q58

1!15 31.7

2.U

26.3

Q.62

Q£1

0.72

Q.8()

o.&C

35

35

35

35

35

3S

3S

3S

Oplimun A.L - 1000 R.

205 30.3

218 31.7

230 331.

2 10 Oplim.m A.L OUise. Oplimun A.L Descend On Ocone

tUii.

221

49-.3

s:u

37S

41.3 O.S1

260 45.4

335

Min. Mach No.

055

o.59

(1.63

56.7 0.69

30

30

30

30

380

392 54.1

41S 56.7

FUEL

lUll.

2500

.

L8.

Min. Mach No.

lUll. Min. Mach No.

4000 L8.

lUll. Min. Mach No.

6000 L8.

26S

273

279

37.3 o.83

38.2

38.6

o.83

o.&C

414 59.7

0.73

443 60.1 0-81

-

30

30

30

426 58.1 0-81

436

59.3

443 60.1

0-81

Q.81

30

----

0-81

Q.81

.....

324 58.6

370

420

473

5ZT

579

616

63.9

68.9

78,()

81.9

Q.52

056

0-60

73.7 O.li5

0.70

0.75

81.7 Q.82

30

30

30

30

30

30

30

IUii.

552

564 75.8

576 77.1

587

599

609

616

78.4

79J

Q.81

Q.81

Q.81

Q.81

80.9 Q.82

81.7

Mach No.

74.4 0-81

Q.82

-

kle-Desai No.

43.4

290 47.1

o.ao

53.7 o.JO

391!1 56.1

56.6

Q.!i6

'SO 50.1 ORi

0.7$

0.12

o.sc.na en Oouse

30

30

30

30

30

30

30

0p1imum AIL - 1000 R.

372

3S4 52.1 0.12

395 53..4 0.12

4IJ1 51.7 0.12

417

55..1

424 56.6

0.12

0.12

511 74.o

77.0 0.12

......

lolacll No.

LB.

o.so

10

PROCEDURE

ZI.I

N.MI.

4000

so

1.1

5

....

N.MI.

......

8000

LB.

N.MI.

......

124

14S

22.3

25.1

().!It

311)

364

Q.81

424

0\aa.,..AIL

CMse • od en Ctuae

Qlr!t)t:)~AIL

[Moe

od On o:use

0\Ase a Hlal AIL

Clft*>t:)~AIL

49..&

so.a

lolacll No.

Q.81

Q.81

311

362

4\0

Win. Wadi No.

55JI

61.0

().53

o.57

65.1 0..61

410 70.3 O.li6

o.n

557 77.5 0.77

......

30

30

30

30

30

30

30

Oplimum AIL - 1000 R.

524 89.9 0.12

536

541

5110

72.S

n.a

581 7U

77.0

0.12

0.12

0.12

571 75.1 0.12

581

71.3

0.12

0.12

CllrO., ()pWru:n AIL OUse • ()pWru:n AIL Dasoend On Oouse

kle~o.c.a

u;

9.7

T - - Win.

4()

219

7

115 23

115

a 340 ICCAS -0.7lloolad'l No.._.,..,-_ • WiriiiDil ..... 1000 ~ cl Fuel. Oulle -

10000 31300

Cllrt>-....,....... ,_.0.12 Mach No. 12000 30 ID O!:Jwru'n Ak. 0

rclenOcuse

0\.aa"**IIM. O..O.d en Ocu'se Qplnun AI. -

1000 A.

Clnt> ID O!:Jwru'n AI.

o.-. Os>*Yun AI. o

d en Or:uw

nne - un

Full - Lb. DilL - N.ML

a-:1 en 30000 Lb. Z..O Full w.g.!*,IS 5000 Lb. Pay"*' Mach No. stuM> isNIIIO... Nachna. T"'"' Fuel. and ts a~ 1cr On c::an. Clnt>.., Cl!*Tun AlliiUI8and 1cr On Ctluw 0.:...10 ..... 0 PelioL cart> a 320 KCAS -G.78 MilCh No.. MaDn.m Poooer. W"ll1 """" ...... 1000 Lb. d Full a n i > - ........... Poooer. o.ao Nach No.:

o·

oue. -

121100 27900

sea

,. =

• At- 36

TO 1F--117A-1

DIVERSION RANGE SUMMARY TABLE TWO BIGtiES- GEAA UP

MODEL: F-117A

NO ~'Wl.OAD- CG @_40% IAAC lWO WEAPON BAY IXXlRS OPEN

DATABASIS: FUGHTTEST

DATE: 11o1AY 191!11

STANDARD DAY- NO WIND

RANGE AHO T1ME TO 1500 L.a. FUEL REMAINING AT~ LEVEL

-

RIEL

25

2B

17.&

192 31-3

0\Ase allnilial .u_ Deoce don Ooo.ne

0..65

202 31..6 OJi9

28

2B

2B

Opirrun AL - 1000 FL

29.5

191 30.5 QB9

202 31..6 OJi9

0\Ase. Opdrrun .u_

OJi9

198 31.3 OJi9

374

451 10.2 0..68

69..8

0-58

414 68.0 0-62

28

28

2B

2B

10

15

1\9

137 25.9 0-51

155 ZIS

CIA"

23S 0-47

o..ss

29-6 0..60

2B

2B

28

28

N_UL

156 25_7

0..68

165 ZID 0..68

175 211.3 0..68

184

loin. Nacf>ND.

263 54-1

297 51S

0-ND.

4000

5.L 103 21-7

PROC::aJURE HlW_ ALI

- 1000 FL

L.a.

N_UL

Min. Nad'IND.

8000 L.B..

•

• •

0-72 Opcilrun AL - 1000 FL

.&10

ClintiiO Opirrun .u_

69..8

0\Ase. Oplirrun .u_

0-72

Descend on Ooo.ne

108

5.8 l33

22

29

6.5 1... OpiirTun AI.

Zll.

0 \ a • OpoluftAIL 0 • id on eo-n.

OJi9

o.-. •

413 61.1

.._AIL

Dasca id on

eon.

CL6i

fi0..9 Cl.li5

o.n

2S

2S

2S

OpiirTun AIL - tOOO R.

4()6

413

o.n

sa.s

60.0

610..8

61.1

0.71

0.71

0.71

0.72

arrt>., Op.nun AIL 0 \ a • ()pinunAIL ['a& • id on OourM

Idle PcMW o.oetl

1.2

2..5

u

250~

s.o

30 5

59

II1 17

114

140

Time - 1o1ft. FUll - lb.

24

30

CooL - N.ML

illad'IND. 8000l&

.....

N.ML

D.71

illad'IND.

Goer Up

•

1711

D.5D

w.:t>Na.

•

ZJI.

163 2&.1 Cl.83

N.ML

•

2S

146 25.2 CL5I

4000l&

•

130

NIIAL AU. - 1000 fT.

20

2:15 D.St

N.ML 1M\. illad'IND.

•

15 -

10

PROCEDURE

3S1

390

-

It

6.1

a..d on 30000 lb. z..o Fuol 'l'lloiCt'. 5000 lb. ~· ecf ....,... Na. .,.._, .~r.-a~ Ouisa Mach no. nr., Full, rd 0 J C8 ~tor On 0ourM c:»'lC> _, ()pnunAIIiLide rd tor On 0:..... 0Wow I lOS.. ~0 llliOI L c:a'lt>·300~ ~Mach

lb.............,,__

-,.,......., 8000 lb. d Fuet a.- - arrc .....

.,....,..,_lb. .,....,AL-A.

8000

10000

23600

227a)

Maximum-. o.n

12000 .21700

FIGURE AJ-16 (ShHI 2 of 2)

A!l-31

Uach No.:

tam 19800

17500

1!1200

•

•

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE NOOEl: F-1 t7A OATABASIS: R.IGHTTEST

ONE ENGINE INOPERATIVE

GEAR UP NO PJI.Yl.OAO - CG 0 ~WAC STANDARD DllY - NO WH>

DATE: 1 WAY 1 -

R.UIGE N1D T1IIE TO 1 !00 La. fUR MMMIIIIQ AT-SEA t.EVU..-

25011 LB.

!i

10

N.Jooll.

56

w.:nNo.

11.5 0.45

fil 13.1 0.49

71 14.6

16.2

11..53

Q.56

4000 LB.

N.M.

liiXXI

LB.

11000 LB.

......

15

•

....

l57

177

l9S

w.:nNo.

139 2a.1

30.2

32..2

34..1

QA

050

11..53

Q.S7

.... w.:nNo.

24

Z1'5 SUI

305

332

ol9..3 O.C7

54.7

56.7

Q.51

Q..5'

o.se 460 78.0

N.M.

N.Jooll.

......

353

390

4:29

69.5

72.6

76..0

w.:nNo. o..a

ldle-o.>enl 250KCAS

0..'-'>

o.sz

o..ss

0.81)

1.5 18 6

3..1

4A

36

51

,.

RJEl. DEHSnV: 6.5LB/USGAI.

PROCEIMJIE

$.L

RIEL

ENGINES: (2)~-F1D2 RJEl. GRADE= JP-4

IMITW. AU. - 1000

OU.alr*IIIAL

0oacrct on ec....

OU:se•--

~onec.n.

au.·-a.-·--

~onec....

~onec.n.

20

a-

r.,._....._

fual-lb. Oist. - N.M.

• -on 30000 lb. lao fual-.;ta. No~ • - N o . - · - ()Use lolach No. • n-ne. Full. a'lCI 0 tar On ec.n. ~ 10Sea . . _ o••

•

n

1e111o •

FIGURE AS-17 (Shut 1 of 3)

.._3,

TO 1F-117A-1

DIVERSION RANG£ SUMMARY TABLE MOOEI.: F- tt7A DATA BASIS: FliGHT TEST DATE 1 MAY t9ll8

ONE EHGINE~llYE GEAAUP • 2500 LB. PAYLOAD - CG 0 ~MAC STAH!lARDDAY - NO WINO

R.UIGE AIID Tlllf TO 1500 1.4. FUEL ROIAIIG.IG AT SEA lEVEl

REL 2500 LB.

4000 LB.

lUlL

Win. Mach No. N.Ni. WilL Mach No.

&000 LB.

N.Y. Win. Mach No.

8000

lUll. WilL IMchNo.

LB.

$

10

5' 1Q.I

CIS 12..3

76

Ill

14JI

15.4 1).51

OM

o.so

135 2!II..C

152 211.3 D.S1

1n

181

311..5 ().$4

31.!1 Cl.5l

2&6 49J

294 $1.6

SZ.!I

0..52

Q.56

0.511

240 D.AI

SC2

4115..2

o.so kill.,_ o.:.rr 2S01CCAS Gear~

1$

().$4

~

:rn

413

6&.2

n.s

Q.53

0.57

1.5 18 6

3.1 36 14

•

~

$.L

O.A7

9IGINES C2'JF.a4-GE- FlD2 FUa. GRADE: JP-4 FUa. CIEMSI1"t. S.SI..B/USGAL

Stl

1111TW. AU. - tODD Fl.

OUi&e allrillial Aa. o.:.-.::1 Cl'l o:u. 0\jse ... . . - Aa.

Oescen:l Cl'l o:u. ()Usa allrillial Aa.

0

ld Cl'l Oouw

--

OuiSl8"' Aa. Oo6c» ld Cl'l Oouw

....

rome-Win.

-

51 20

Fuel-lb. OisL- N..Ni.

• Based Cl'l30000 lb. z.o Fuel Welg"a pU 2500 Lb.~

• Mach No. stoon 1& Hill O...lolacb No.

r....._ Full. a"ld o

ulrc:ldod tcrOn ac..w o.:.rr 10 s. .__ o

1 ..,. •

FIGURE AS-17 (ShNt 2 of 3)

------------------------------~·

•

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE ONE 9IGINE lfOPBlATIVE G&.RUP 5aXILB. PAYlOAD - CG @~ MAC

N0DEJ.; F-117A

OATABASIS: R.IGHTTEST DATE: l MAY \988

ENGINES: (:!'lF~-F1D2 AJEL GRADE: .JP-4 AJEL llENSI'r¥. 6.5 LfiiUS GAL

STANDARD DAY - NO WIND

.

RANGE AND TillE TO 15001LA. FUEL n =.. • ~• FUEL

2500

.

LB.

4000 LB. IDlO

LB.

8000 LB.

$.L

5

10

15

73 13.3

83 14.6

IUii Mft. Mach No.

53 10.1

63 11.7

0.~

052

o.ss

G.liO

IUii Mft. Mach No.

131

147 26.7

104

-

24.7 O.A.9

28.8

052

232 U4 Q.50

257

28Z

45.9 053

48.5 ().57

331 61.3

S65 64.3

67.1

o.54

Q.S8

15 1B 6

3.1 36

IUii Mft. Mach No.

IUii Mft. Mach No.

O.S1

Idle~ Desaot

250KCAS -Up

o.ss

396

u

-

-

INmAL AU. - l 000 FT.

0\ise atlnilial M Deoscand on Ocuse 0\ise atlnilial M Desaod on Ocuse 0\ise at Wlial M Deoscand on Ocuse

cn.a.e at Wlial M o on Ocuse

De& •

4.4 51

20

TII1W- Mft. Fual-lb. Dist. - N.Mi.

• Based on 30000 lb. Zero Fual ~ 1*JS 5aXIlb. F'a)'load.

• Mach N o . -is lrillial OI.Ose Mach No. • T....... FUel, a-Id Cis C8 h::U:Ied tcr On 0cuse Desao liD Sea ........ ll&slillil!b •

FIGURE A9-17 (Sheet 3 of 3)

•

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE M00B.: F-1 t7A 04TABASIS: FUGHTTEST 04TE:1NAY19118

ONE ENGINE IINOf'IERATlYE - GEAR UP NO l'l'.'lt.OAO- CG 0 ~ ~

ENGINES: ~F~-F102 RIEL GRADE: JP_.

ONE WEAE'OH BAY DOOR OPEN STA/olliAAOOAY- NO WINO

RIEL OENSm': 6.5 L8iUS GAL

RAHGE AND TINE TO 1500 lB. RJEL RB 1-IG AT SEA I.£YB.. RJEL

.000 lB.

1000 lB.

...... .... ...... ......

YachNo.

YachNo.

de 1'\:Mw 0..::.. 2501

6

12

......

N.ML 1000

5

......

lob:tiNo. de~ Desc:erl

322

•

- " " 30000 lb. z.ro Ft.oll Wei11'11*8 50DO lb. ~ Mactt N o . - i s - OUse lo&acn No.

•

T..... ,.., and Dislance rculed tar On Q:uw

•

cn.. • cn.. •

FIGURE AS-18 (sa-t 2

or 2)

..-Aa.

Time- NO\. Ft.oll - lb. 01111.- N.ML

32

o.:.n IDSea I.JMII C

..-Aa.

eiiOi •

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE M00a.: F-1 f7A OATA BASIS: FUGHT TEST OATE: 1 NAY 1988

ONE ENGINE INOPERAT1YE - GEAR UP NO PAYLOAD - OGO ~MAC TWO WEAPON BA.Y DOORS oPEN STANDARD DAY - NO WIN>

~~-F1D2

AJB. GRADE: JP-4 FUEL DENSm': 6.5 L.8IUS GAL

PACXBUI£

RNfGE /IHD TilliE TO \500 l& FUEL RFl' Q•IG KT SEA LEVa.

SL

5

lO

NJa

107 24JI

119 25.0

130 215.1

W8chNQ.

0.41

QA5

CI.AI

.....

28!1 51.6 0.44

29l 59.6 0.48

60.5

FUEL

.....

QlO

l&

NJa 8000 l&

....

w.cnNa.

-~ 2501CCAS Gear~

• •

\..1

13 5

•

INI11AL AU. - 1000 FT.

O...•t*'IIM. o ldonC::O....

313 (1.51

O...•hliiiiM. o ldonC.:U..

2.2 21& lO

FUll - lb. Dill.- NJa

r.,._...._

-0'130000 lb. :z.o full~ No Payltad W8ch NQ. .,._, 15 ...... 0\-. Mid> NQ.

• r..,., Fual....., OCoz :ce incLidld tor en Qusa eesc.na 10 Sea . . - o r ldlio•

FIGURE A9-11J (ShHt 1 of 2)

--------------------~--------~·

•

TO 1F- 117A-1

. DIVERSION RANGE SUMMARY TABLE MOOB.: F-1f7A DATA BASIS: RJCiniET DATE: 1 WAY 19118

OM: ENGINE INOf'ERATlYE- GEAR UP 5000 1.8. FY.Y\.0.\0 - OG ~ C3..0'I' 1o1AC

TWO WEN'ON BAY DOORS OPEN STA.NDARD DAY- NO WI'C>

PROCEDURE

IWfGE AHIJ TINE TO \5001.8. FUEL RaUoiNINO AT SEA LEVB..

-

FUEL

1.8.

11000 1.8.

.... ....

N.MI. Ma:hNo. N.MI.

Ma:hNo.

ldllo- Oosara

SJ..

5

119 2D.tl OM

:t1.5

OA6

OU.•-M. ld en C::CU..

0..41

o-

51.3 O..S1

0

12 14 5

Z5DKCAS GaarUp

•

108

- -

5QJI

INITIAL. AU - 1000 Ft;

OU.•-M. • den C::CU.. ~-

....

Full- Lb. DilL- N~

•

a-:1 en 30000 Lb. z..o Fuol w.g.I)IUI; 5000 Lb. ~

•

- N o . SI'IOM'I is~ 0\llse Ma:h No.

•

lime, fwl. and llistan:a h:Ldad tor On Q)urse Oosara ID Sea ~ Oee:ii i8lb •

AGURE A._ til (SMa 2 ol2)

At-45/(A~ BUnk)

TO tF- 117A-t

•

APPENDIX B PERFORMANCE DATA RCS ENHANCERS INSTAl I ED

TABLE O.F CONTENTS PAGE Rder to Appaw'ix A

PART I

IJIITRODUCT10N

o .... o o o .. o o o •

PART 1

ENGIJio''E DATA o o o

o • o o o o o o o o o o o • o • o o o o o o o o o o o o o o o. o o o o o o o

PART 3

TAKEOFF PERFORMANCE

o o o o •

PART 4

CU."'fB PERFOJBIASCE o o o

o o o o • o o. o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o • o

114-1

PART 5

CRUlSE PERFORMANCE

o o o o o o. o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o

85-1

PART'

ENDURANCE

PART 7

D~'T

PART I

APPROACH A.'"D IA.'"DING P ERFORMANCE

PART'

MISSION PIA.."il''L~G

o o o o o o o o o o o o o o o o o .

PERFORMANCE

o • o o •

o. o o o o

o • o o o o o o o o o o o o o o o o o o o .. o o

o o o o o o o o o o o o o o o .. o o o o • o o o

Rder te Aweodix A

Refer t• Appmdix A

o o o o o o o o o o o. o o o o o o o o o o o o o o o o o o o o o o o o o o

86-1

o o o o o o o o o o o o o o o o o o o o o o o o o. o o o o o o o o o o o o

87- 1

o o o o. o o o o o •• o

Rder to Appmclix A

o o o. o o o o o. o o •••• o o o o o o o o o o •• o o o o o o o. o o o o o o

B-t /(8 - 2

~I

BIM*I

TO 1F-1 t7A- 1

•

APPENDIX B PART 4 - CUMB PE.R FORMANCE RCS ENHANCERS INS'T:AI I ED

TABLE OF CONTENTS

mu:

PAGE

list o( lllu:sl:rlUiaDs . • . . • • • • . • • • • • • • • • • • . . • .•• - . • • • . • • • • . • • . . • . • • . . . • • • • • • • . • • . • • • . . • . . • • . • • • 84-1 - - - - - -lllln I • • • • .. • • • • • • • • • • • • • • .. • • • • .. .. .. .. .. .. .. • 840imb Speed Sdla!Dles................... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84-2 Climb l'Pd'Y"Nnce - Two Enginrs, Gear Up . ... . ... . .... . ..... . .... . ... ....... . ...... . .. .. ... 84-2 l'Pdornwx:e Ceolinp . .. . ...... .. .. .. . . ... .... . .. . . .. . . ... ...... . ............... . . . ......... 84-2 Siqk EoFe Climb- Gar Up . . . . . . . . . . . • • . . • • . • . . • . . • • • . . . . . • . . . • . . • . • . . . • . . • . . . . . . . • . . • • . 84-2 Two Engine Climb- Gear Doom • • • • . . • . • • • • • • • . • • • • • • • • . • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • 84-2

UST OF ILLUSTRATIONS

FlGURE

PAGE

Climb Speed Scf>ed!des................... . . . . .. . . . . . . . . . . . . . . . . . .. . . . . • .. . . . . . Refer to Appmdix A Climb Paform•nce= Two EagiDes, Gear Up STD DAY - IO"C ••.• . •.•••.•••.•••••...........•..• . .. . •. . ............ 84-1 ••••••••• 84-3 STD DAY ••••••••.•.•.•••..• . .••••••••• . •••••••••••.•.••••••••••••• • • 84-2 ..•.••.•• 84-4 STD DAY + lO"C •.•...•••.•••......• - .........•.••..• . ••.•••.•••.• . .• 84-3 • ••.••.•• 84-S STD DAY + 20"C ••••• • •••••••.•••••••.• . •• . •• .•.. . . •..••.•••••••••••• 84-4 ••••••••. ~ l'Pdorm• nce Ceolings ...... . ................ . ....... .. ................. 84-S . . ... .... 84-7 ()oe Engine\

Gear Up

STD DAY - IO"C . . . ....•...•...•...• •• . •••• . •.••.•.....•..... . . . . •.. .. 84-6 . . ....... ~ STD DAY • • • • • • • • • • • • • • • • • • • • • • • • • • • • • . • • . . • • • . • • • • • • • • . • • • • • • • • • • • • • 84-7 •.••••••• 84-9 STD DAY + lO"C .•••.••••.•.....••........ . ..•........••..•..•.••..•. 114-8 •.•••••• 84-10 STD DAY + 20"C .•... ••.. . •..•• . ••••••.••..•.••.• • ••••••••••.•••..••• 84-9 .... .. . . 84-U l'Pdormance (;eolin&S RJC - 100 FPM . • • . . • . • . . • . . • .. • . • . • • . • • • • . .. 84-10 •••••••. 84-12 RJC FPM . •• .. •.•..• . • • ••• . .• • •.•.••.•• 84-U •••••••• 84-0 RJC - ~ FPM • •• •• • • • .• • . ••• . •. . ....... •. •• 84-12 •••••••• 84-1. Two Engines, Gear Down STD DAY -IO"C ..•.•....... .. ... . .... . ... . .. . . . ....•......•.•..•..•• 84-0 •. •.•... 84-lS STD DAY ••••••••••••••..••.•••.••.••.•..•.• .• ..•.••.•••.•••••••.••• 84-14 •. •. . •• • 84-16 STD DAY + lO"C .•..•• ... ...... . ...•• . .....•.•..•.••.•••.••.......•. 84-lS .. •. •••• 84-11 STD DAY + 20"C •••••••..••..•••••••• . ••. . •• . •.••.••.••••••••.••.••• 84-16 .. •••••• 84-18 l'Pdormance Ceolmgs . • • • . . . . . . . . . . • .. • . . • . .. .. . . . . . • . . • • • . • • . . . • . . . . . 84-17 ... ..... 84-19

m

• 84-1

TO 1F- 117A - 1

INTRODUCTION

PERFORMANCE CEJUNGS

This pan olthe a''P"'""" TO !D - L8.

15!1

325

506

719

970

12311

1921

2134

DISTANCE TO !D - N..lol.

3.0

7.0

12A

2DJI

33.6

51.1

1011.6

129.6

N1W..GROSS wt.@SL.

33350 FT.

40000l.B.

TINE TO !D - MIH.

0.6

t.3

2.3

3..6

5.7

u

RJEl. usa> TO 1D - L8.

179

:sr

574

820

1123

1495

DISTANCE TO ID - N..lol.

3.A

7.9

1A..1

23.9

39..3

63.7

NlW..GROSS wt.@SL.

4A()()()l.B.

lWETO !D- ...,_

0.7

1.S

2.6

u

RJEl. usa> TO Ill - lB.

201

4\3

&II

DISTANCE TO !D - N.lll

3.11

u

16.0

N1W.. GROSS [email protected]

6.7

11.1

935

1306

1896

'Z1.4

46.3

115.4

1.7

u

4.1

7.9

RJEl. USED TO ID - L8.

224

468

731

1066

1536

!D - N.lll

4.3

tO.D

18.1

31.4

55.5

o.a

1..9

m - t.a

250

518

!D - N..lol.

4.1

112

RJEL usm TO

DISTANCE TO

3.3

20.5

2323 131..1

1&2 2519 132.9

2S690F't.

o.a

TINE TO (I; - - .

-

48000L8.

N1W.. GROSSwt.@SL.

14.0

314&DF't.

TINE TO ID - NIH.

DISTANCE TO

-

-

--

-

52lJOO lB. 5.5

9.7

1220

1847

362

68.4

-

----

1&.5

2733 135.6

27990F't.

1L7 2932 136.9

TO 1F-117A-1

•

CUMB PERFORMANCE NODEI · F-117A Oo\TA BASIS: FUGHTTEST

TWO ENGINES AT MAXIMI .. POWER

GEAR LF - CG 0 TO

T1loiE TO

35

1.5

m - MIN.

D&STANCETO

3D

321100 LB.

NT1AL GAOSSwt Os.L TIYE TO

25

(L1

RIEL usa> TO D&STANCETO

20

-

-

-

-

20.2

3101 \53.3 211360 FT.

SIOOO LB. I.I

2...

~MAC Sft) DAY

RCS IENHAIICEJIS INSTAU.ED

m FINAL AU:. -

10011 n

SEJIYIC€ 5

10

NTW. GROSS wt@ S.L

2D

2..0

u

1.5

19.1

FUEL USED TO

!D - lB.

272

586

992

1828

u

22J

42.9

w:r

e S.L

ClUING

20970R

..c.

NTW.. GROSS wt

25

32000lB.

TlliiE TO 1D -

DISTANCE TO ID - N..l&.

-

-

3lillOO lB.

25.11 2303

132.3

111Z50FL

-

:u

IIJ)

11.9

-

FUEL USED TO l!l - lB.

341

7fr1

1366

-

--

2503

DISTANCE TO ID - lUlL

11.5

29.3

&0.1

-

--

131.3

l1ME TO

m - WIN.

INITIAL GROSS WI:@ S.L

.aooGlB.

llME TO 1JJ - MIN.

u

L1

19.3

FUEL USED TO 1JJ - lB.

438

10211

2160

DISTANCE TO ID - N..l&.

l43

319••

98.5

NTW. GROSS W't@ S.L

m - -.

11.1

-

FUEL USED TO (!; - lB.

5112

W5

-

DISTANCE TO ffi - N..l&.

19.1

56.1

NTW.. GROSS wt@ S.L

-

25..0

-

6.0

19.3

FUEL USED TO ill - lB.

829

2421

DISTANCE TO ID - N..l&.

21..2

95.1

INmAl. GROSS W't@ S.L

9.9

FUEl USED TO ID - lB.

1356

DISTANCE TO ID - N..l&.

46.3

-

21669

\21.2 l3730R

-

-

-

-

-

2lLS

3021 135.1

12DOOR

10 m - LB. nwE 10

1!1150FI:

99.2

-

-

-

113lill

-

502.4

• C1JMB SPEED SCHEDUl.E: 210 KCAS - O.SO WAOi NO.

FIG1.IR£ 84-t ~-~~----------84-11

TO tF- 117A- t

•

PERFORIIANCE CEJUNGS ONE DIGDIE AT IUIXIMWII POWER ONE ENGINE INOHJIATIYE GUll UP - CG 0 MAC 210 KCAS - o...50 IIA.Ct4 NO. RCS EJIHAMCStS IIISTAI.UD

43.0"

ENGIII£S: (Z) ~..., 02

111100EL: F- 117 A DATA IIASIS: FUGHT TEST DAre 1 IIAII 1-

FUEL GR DE: ·~ 1

fUEL DEXSI'TY. 6.5 Ull\l$ GAL

AGUREB4-t0

84-t2

--------------~·

TO 1F-117A-1

•

PERFORMANCE CEIUNGS ONE~

AT "'!'MN POWER Q E - M C !MTM

QE.UI . .

-CO. -IIM:

V.ICCAS - LM IIACM IK1. IICS El'WIM.I'UMICEI'I$4 -.TAI.LB)

11100£1.: F-117A DATA BASIS: RJGHJ nsT DATE: 1 M.UI 1. .

DIGJIIES: (21 ~--- D2 FUEL GRADE:..,_. FUEL~ 1.5

UII\JS GAL

!

i

•

F1GUR£ 84-11

84-13

TO 1F- 117A-1

PERFORMANCE CElUNGS

•

OlliE BIG1IIE AT ••x-• POWBt OlE ~ INC UltTW'E GEAII UP· CC e lilAC ltCAS - L50 IUal 110. RCS BIUW: 4 ...-JAU.fD

m

lt00£1.: f-117A DATA BASIS: fUGHT TEST DAT£!1 MARl-

FlGURE 84-12

--------------~·

•

TO 1F-117A- 1

CUMB PERFORMANCE MODEL: F-l17A ~TA BASIS: FLIGHT TEST DATE: 1 1o1AR 1988

lWO ENGINES AT a.&AlCJMtJN POWER GEAR !DOWN - CG ~ oi3..K MAC

sro

DAY -1o•c

ENGINES: (21F~-F1D2 RJEL GRADE: JP-4 RIEL DENSITY: 6.5 LBIUSCAL

TO BE SUPPLIED

•

AGURE 84-13

84-15

TO 1F-117A-1

•

CUMB PE.R FORMANCE YOIJe.; F- 117A

TWO ENGINES AT MAXNUM POWER

OATABASIS: AJGHTlEST

GEAR DOWN - CG@ 43..0% MAC

STn DAY

DATE: 1 WAR 19118

ENGINES: W404-GE-Flll2 FUEL GfW:lE: JP-4 FUEL OCr& I 't: 6.S lB/US GAL

SERVICE (!) AM.llAU.- 1000 Ft.

5

10

15

20

25

28820Fl:

321l00l.B.

INfTW. GROSS wt@ s.L

cauHG

TIME TO (!) - MIN.

8.0

1.7

2.8

4.6

&.3

20..8

FUEL lJSa) TO (!) - LB.

211

.:m

669

951

1399

2613

DISTANCE TO (!) - N.Nl

3..3

7.S

13.D

212

37.8

93..9

INfTW. GROSS wt @ s.L

26250Fl:

36000l.B.

TIME TO (!) - MIN.

Q.9

2.D

3.4

5.9

13..3

21.0

FUEL USED TO (!) - LB.

Zae:t-.iDc the ~ a'f2ilabk al 30,00) feet oa a SIMIIatd day a1 0..80 Mado few ao I8JliaJ poss weipa of~ poiiiK!5 if UXl poa.is of fud IS to be COI>a.c4. Eater Fipre BS-7 al ~ pomds aDd ~bdl No. aa:t mid spedic ruce as liiJl nanrical per pomds of Rceatc:r u Macll No. ud 32.000 pocmds (~ - 8IXXl) &Jid mid spe: cifJC ran&e as 91D namical m.iles per tim poaDds of

o..s

..a.:s

1cm

raet.

o..s

Cod. 1be ~specific IU&e is SS.5 nautical miles per tOOl pouDds of Cud and the ran&e ..mlabk ror I'OXlpouDds of Cod ••••so eel is 708..0 Datltical miles (SUX~

lOHG RAHGE CRUISE

L.o.c ruce cr1lise mrormauoa 'lrilh llle &ear ap is wodiaF'~BS-9. lloert" led~ crediDtt IS 10 set bolA • Ul M - - l'tJoftr aad

l..oac ru&e cr1lise iDfOO!I!Itioll few oae c:ap.e opeo~iD& &Jid 'W1th \be &ECAEASe FUEL A.DN ~ P9110"C BELOWSTAHDARD DAY TENP.

AGUREB5-16

115-18

•

TO 1F- 117A- 1

•

SPECIAC RANG£

twO----fUT

CO.-MAC

IICS EMUIC E 4 MtaU.ED

ENGINES: (2) F404-G£-f'1 D2 FUEL GRA0e: JP_. FUEL DEIISITY: 6.5 UIIUS GAL

WODU; F-117A

DATA~ FUGHT TEST

DATE: 1 IIAY 11118

--·-ICCioL

MOt'!,: ........ .-eD wrnt

.. .•. •

"

~~

.STDDAY

' + 2II'C STDDAY + IO"C

f

STDDAY

~

~

STD DAY - IO"'C .:::

0 IIAOf 110.

I I II I I I I I I I I II I I I I I " -

-

200

250 IICAS

-

II I I -

AGURE 85-11

85-20

I I II I I -

•

TO 1F-117A-1

'

SIPECIAC RANGE -FEET 1WO - E S ·GEAR DOWII CG·~IUC

RCS BIIIIIHC S INSW.LSl

EHGIN~~..f'1D2

IIOOEI.; F-117A

FUEl. G • JP_. FUEl. DEHS!n 6.5 LIIIUS GAL

DATA BASIS: FUGHT TEST DATE: 1 MAY 1988

IIOTE:

••xrw• SPEED wrnt GEAI'I DOWNS- KCU

UlNG RANGE CRUISE

DAY • 20•

e

_...

-

LMI'IID.

•

11.50 IIACtl NO.

IIIII I

I I

I

I

I

I

AGURE 85-19

85-21

TO 1F- 117A- 1

•

SPEClFIC RANGE

-RET

TWO- ·-

c:o•-IIUCDOWII

IICS OIN'IICUI& ~

MOO£L; F-117A DATA~ RJGHTTEST DATE; 1111AY 11181

---

..,....

OIIOSS WOGHT

--La

~

I •

-

·,

ENDIIIR' ItiiCE "": ,L. ) I

•

~

z

STDIMT +»"C

-

....,. IICI.

,.

... I

tse

I

-

...

cuo

- - IIACM NO.

••

I

I

I I I I

I

I

ICCAS

AGURE 85-20

85-22

I

I

I

~

I • I sse

...

...._

_

•

TO 1F-117A-1

SPEctAC RANGE -RET .,_-. -

co e-uc:11011!11

IICS £IIHAIIICOIS ~

MOOIEL: F-117A DATA BASIS: FUCHT T£ST DATE:1 MAY 1 -

ICJT'I: ......... Sf£ED wmt GEM DOII!IIIS- JCCU

__._.

-WDGHT

STD DAY • 20• C

~

STD MY + 10" C STDMY STDMY - IO"C

I •

j

z

I

•

1• I

I

'

I

'

I

I

I •

I

I '

I

I

...... Vft · -

RGUREBS-21

BS-23

TO 1F-117A-1

•

SPECIAC RANGE 2511118FUT

TWO-·CIUADOWN

CGO-IUC - - . - IIII"W.I.ID

DIGI~1'404-GE-f102

1100£1; F-117A DATA BASIS: fUGKT TEST DATE! 1 MAY 1 -

*'1'E!

FUEL

• J/11-4 FUEL OEIISIT'e 1.5 ~.a/US GAL

••xw•

SPEED .,.,. GEAIIDCIWII a -ICCU

.. • I -z •

ALL TL&C AT\MEI

i

I•c ...G2

r•

40

,. ~

• ""':

•

...

....

..

I

I

I

a:&S

AGURE 85-22

BS-24

....

LSe IUCIIIID.

I

VII

I 250

•

•

TO 1F-117A-1

LONG RANGE CRUISE SUMMARY TWO EIIGIJCIES AT IIAXI1Wiil POWER GEAR DOWN - OG 0 41.0'S MAC ACS EIIHAl!ICERS IHSJAU.ED

T10 BE SUPPLIED

•

AGUREB5-23

85-25

TO 1F-117A-1

FUEL FLOW FOR LONG RANGE CRUISE- CONSTANT ALTITUDE I4()0A • F-117A

DATA IWiZS:: R.IGHT TEST DATE: 1 YAY 191111 PR£SSUII£ AU. - R

AWllNO. KTAS

Ff/EHGINE

ENG&NES: C2l F404-GIE-F1D2

OG 0 C3om1. .....C - STAHDAAD DAY

AJe1. GRADE! Jl'~ AJe1. ~ 6.5l8o\JSGAI.

ACS eow«::SSS INSTAU..ED

SIOO

s.L

30000L8.

lWO ENGINES OI'EFIAnNG- GEAR DOWN

-

10000

1SIOO

20000

25000 .52 3l3

.39

_.43--

.46

256

'ZTZ

286

3&50

3:W)

32SO

.48 29S 33110

.39

.Al

256 «Xll

2llil

.A5 21!15 3150

.II1 1S1

3~

3620

36l50

:!IT

;au 3650

•

3160

34QOOL8.

a.w:HNO. ICTAS

Ffte«31HE

38000lB.

~

a.w:HNO.

.Al

.A3

ICTAS

2A

Ff/EHGifE

4&00

283 4290

.47 2!17

C\80

43100lB.

a.w:HNO. ICTAS

Ff/EHGIHE

O!IOOOLB. a.w:HNO. ICTAS

Ff/ENGINE

.A2

21!0 410

....

a.w:HNO. Ff/ENGINE

.A7 303

All 308

4610

5180

3 15 5090

-~ 299 5130

312 5610

3211 5630 .52 334 &a2D

..

-

.52 321 4070

.51

317

~10

.so

290 5300

50000 LB. ICTAS

.A5 2!15 c780

.A9

3111

.51

.52 3216 Sl20

.5\

52500L8. ~NO.

.46

.c9

KTAS

30&

Ff/ENGINE

&a2D

315 5900

UCCT10NS:

a.w:HNO.

0.40

Q.50

Q.liiO

6 KTAS/lO"C

c JI

6.0

7.2

+HOT DAY - COlD DAY

~ AJEl A.OW 211. PB1 to·c ABOVE STANtW'lD OAYTBIP. oecREASE AJEl A.0W 211. PBI 10"C BEl..OW STAHDAAD DAY TBtP.

• B$-26

TO 1F- 117A- 1

APPENDIXB PART 6 - ENDURANCE RCS ENHANCERS INSTAl I ED TABLE OF CONT'El\'TS

PAGE l...is:l oi JJJusua.tioas --------------------------.-------------- ------ ------------ ----- -- -------- 116-1 ID.ueclactilJB ...........................................................-. ............................. ~ •• - .._-··-··--······· ~z_ Maximum EDdurance •• --.-- .• --.-- .•• --- •• -- ·--- --------------- •• --.-- •• -••••• ---- ••• -- ••.•• 116-2

LIST OF lLWSTR>\TIONS

FIGURE

PAGE

Two Engines- Gear Up •.• ----.-- .. -- •... ------------------- ........ -- ... 116-1 .•. --.-- .. 116-3 One Engine- Gear Up-- .. --- ...... -- ••..• -- .. -- .... -- ....... __ .. -------. 116-2 __________ 86-4 Two Enpaes- Gear OoorD -- ------- --- .•..• --.--- •• -. ------ -- .-- ----- ----- 86-3 - --------- 116-S

86--1

TO 1F-117A-1

INTRODUCT10N

a.w- '" mctaim pbnninz informa. muia- cacluraJice_

This pan d tk ! . - («

DATA BASIS

The petfOI"'UUICe illf(I(1Jialioa COI>taiooed ;, this pan d the 4V K•• IS tJesa1 Oft flicJu leSt data.

MAXIMUM ENDURANCE Mlxim11111 endunnce in ~crms d minuu:s per liOl poa8ds a1 roc:~ ascd f« _, egpvs, sear up. is..ancd iD F".pre 86-L ficurcs 86-2 and 86-3 are f« oae ~ pr ap ud twa mgirr, sear dowD. reo speaively. 1\J.apc:a p.-ftipll. doe &CASudllDAfcrJUD. eedwa.... -'11111latrirtwte F« pilot-.

um KCAS aDd ...!!S""nt AOA YalDes rt'eaed &Dd are listed • tbe tables co 4\*tar .-te tk attcal speeds and AOAs f« &a:CiillWA Clll -PRESSIIBL

-

RIEL

ALJTTUDE

TillE

- A.

- MilL

-LB.

OIST. - IUIIL

SL

0

0

0

50110

1.5

33

10

10IXIO

3.0

65

\9

150110

4.4

98

28

20000

5..9

134

36

25000

7.5

165

42

30000

9.1

21)(

50

35000

1Q.6

244

58

Descllnd at 250 I DAY

'

11"0 BE SUPPUED

•

AGURE87-3

B7- 5/(87181ank)

TO 1F- 117A-1

•

APPENOIXB PART 9- MISSION PLANNING RCS ENHANCERS INSTAl I ED

TABLE OF CONTENTS PAGE

TITLE

List of IDustntinns .................... .. ................................................... 89-I Inuod•K%in• .............................. ................................................. 89-3 TOlD Ca.nl ............................................................. ... Rder 10 Af'lomdix A Fad Coo•Gililj•ic"' ............................................. . ............. RderiO App"wtir A Ttme, Fad Used, and DislaDce From Brake Rdea:se 10 Climb Speed .••.•..••.•.•. RderiO App'•wtir A Fad J ettisoa . . . • • . • • . • • • . • • • . • • • • • . . • . . . • . . . • . • . • . . . • .. • . . • . . . . . . .. . . .. . • • . . Rder 10 Appenctir A Formattio& Speeds and Alrimdes •••.......•...•.• . • . ..• . .•..•.......•..••..••. Rder10 App ,.,;, A Level f1i&ht A'C:i {.6T- -10. O' C) .•...•••.•....•........•.•...... B9-1 (Sbcet I af2) •.••. 89-4 5.(0) Ft.

JD,f.CXJ FL

15.(0)Ft.

•

20.003Ft. 25.(0)FL

{.6T- +10, +20'C) ••••• ••.•.••...... . • . .. •• . .• {.6T- -10. o·q ...................... .. ... ..... (.6T = +10. +20'C) .•.... . .•. •. •••..•.• .•..•.• . (.6T =-10,0'C) ...... •.. . •••..••......•..•••.•. {.6T = +10, +20' C) .. ••.••....•••••••.•.•..•.•• {6T- -IO,O' C) .....•..••••••••••............• . {.6T - + 10, ~ 20' C) ••••••.•.•.•........ . .... . .. {.6T- -IO.O'C) .••.•••.••••..•.......•....•.... (6T- +10, +20'C) ••..••.........•... . •..•.... (6T- -JO,O'C) .....•.•••.•••.••.••..... . .. . ... {6T - + 10, ... 20' C) • • • • • • • . • . • • • . . • . . . . • . . . . . . .

89-I{Sbcet2of2) 89-2 (Sheet I af2) 89-2(Sbeel2af2) 89-3(Sbcetlaf2) B9-3(Sbcet2af2) B9-4{Sheet laf2) 89-4 {Sbeft 2 af2) B9-S{Sbeft laf2) 89-S(Sbeet2af2) B9-6(Sbeet laf2) 89-6 (Sheet 2 af2)

•.••• 89-~ •.•.• 89-6 ..... 89-7 ..... B9-3 ..... 119-9 ••.• 89-10 .•.• 89-U .•.• 89-12 ...• 89-13 ••.. 89-14 •••• B9-1S

89-1

TO t F- t17A- t

TITLE 30.1XX1 Ft.

UST OF ILWSTRADONS (Continued} FlGURE

PAGE

(OT • -10, O"C) •.....•••.•..•.••••••••••••••••• B9-7 (SIIeel1 ol2) ...• 89-16 (oT- +10. ..-20"C) ••.•..•..........••• •. •.•... B9-7(SIIeel2ol2) ..•• 89-17 Lc-n::l ~ Dccderatioa fPr£ MFii«e .. • • • • • • • • . . • . . .. .. .. • .. .. .. .. • 89-8 ................. B9-IJ SnsamM Tao Capebil«r OT•(-to.O"C) ••••.•••••.•••.••.•••••.•.••..•••.•.••••••••••.•. 119--9(Sbeet loll) •. .. 89-19 OT•(+10. +20"C) .•••••.•••..•..•.•........•.....•••..••....•. 119--9(Sbeet2ol2) •... 89-20 M njmnm Lc-n::1 f'licbt Speed t.T•(-10. O"C) ....•.......•..•....•••••.•..•..•••••••••••.••• 89-10 (SIIeell ol2) .... 89-21 t.T-( +10. + 20"C) • • . • • • . . • . . . • . • • • • . . • • • • • • . . . • • . . . . . . . . . . • . • 89-10 {SIIcel 2 ol 2) •..• B9-22 Da•u:sicaa R.atce Se=eary 1:ables 1Wo E.pes- Gear Up No hj"""" .. . .. . . . .. . .. . . . . . . . . . . .. . . . . . .. . .. . . . . .. . . .. . . . B9-ll (Sioea I olJ) .... B9-Zl 2jOO lb. 1'17"""" . . . . . . . . . . . . • . . . . . . . . . . . . . . . . . • . • . • . . . . • . . . . B9-ll (SIIeel 2 ol 3) •... B9-2A 511Xllb. 1'17"""" ..•.... ... .......•....... . -... ..•....•...... B9-ll {SIIeel3 olJ) .... B9-2S One Ellp.e laopera!M - Gear Up No l'a)ic*' ••••••••••• ....••..•••••••••..•..••••.•• ••.••••• 89-12 (Sbeet I ol3) •••• 89-26 2jOO lb. h)"""' . .. . .. . . .. .. . .. . • . . . .. . . .. .. • .. . • . . . . • . • .. .. 89-12 (SIIeel 2 ol3) .... 89-27 511Xllb. f'aJ"""" . .. . .. .. .. • .. . .. . .. . . . . .. .. . . .. .. . . . . . . . . . . . 89-12 {Sbeel3 ol3) .... 89-211

•

• Bll- 2

TO 1F- 117A- 1

DIVERSION RANGE SUMMARY TABLES

INTRODUCTlON Tllis pan d the IPP"'wfft CXII>taim addi•ioua! infcwmalioo {01" mjssiDn planning All daia is based 011

fli&ht Test results. LEVEL FUGHT ACCEl..ERATlON PERFORMANCE Two ~ le\'d ffi2ju ........._rion pedormaroe at Maximum Alwer. par vp, and for a 13111Cd ICrllpelratures is presented in F.gme B9-1 thru B9-7.

LEVEL FUGHT DECELERATlON PERFORMANCE Two enpue le\'d fligbt decderarion performance at idle power, par up is jnStnted in F~ ~ f« a saandanl thj. Tempennues and C.G. dleas are nqlip>le.

F~ B9-ll and B9-l2 prOTide. in tabulated fonD, tbl; ""''C available and lime rcquiRd (Sialldazd day. oo wind) 10 reacb a Sea l..-:1 desjnatjon for 2m, «XXX, (,00), aDd 111m lb.. d Cud rmaining at the in.iliarion d diTIWE - MIN. FUEL USB> - LB.

36000

ElAPSa>TIWE- loiN. FUEL USB> - LB.

40000

ElAPSa> TINE -loiiN. FUEL USB> - LB.

D1ST~-N.UL

•0

~

+

D1ST~-N.UL

~

0

~

ElAPSS)Tit.IE - loiiN.

44000

48000

52000

FUEL USB> - LB. DISTANCE- N. UL ElAPSa>TlNE -loiiN. FUEL USB> - LB. DISTANCE - N. Ul

•

0 0

...en

48000

52llOO

•

soo

50S

11.30

0.41

Q.50

Q.5ll

O.li6

Q.74

Q.8Z

D.83

0 0 0

02

o_.

(1.6

0.7

1.1 295

().3

l.D

65

121)

160 2.5 0.7 180

220 4.0

0 0 0 0 0 0

lOIS 12 G.5

0 0 0 0 0 0

0.4

(1.6

82

180

2.2

3.8

5.7 1.1

eo

G.5

2.0

3.0

7.1

16J)

730 22.0

1.3 3315

2.6 650

8.0

21.0

soo

1.0

2.0

3.0

().3

(1.6

Q.9

1.1

2.9

3.6

110

150 2.5

1.5

225

270

380

700

&40

22.0

27.0

Q.9

12

9.8 1.7

240

300 &2

430 12.0

810 215.0

1.4

2.0 480

8JO

1.5

G.5

0.8

115 2.7

180 4.0

4.0

265 5.9

6J)

360 &2

11.6

800 215.0

3.2

3.7 27.0 4.0

1.7

2.3

430

5al

3.0

6.5

9.0

13.5

960 30.0

250

300

350

400

450

489

11.30

0.41

Q.50

Q.5ll

O.li6

Q.74

o.80

02 511

G.5

0.7 145 4.0 0.7 175 4.5

ElAPSa>TlNE - loiiN. FUEL USB> - LB. DISTAA'CE - N. Ul

0 0 0 0 0 0 0 0 0 0 0 0

ElAPSa>TIWE- loiiN. AJEl USB> - LB.

0 0 0 180

3.5

240 5.D

1.3

MACH

NO. MIN.

AJEl USB> - LB. ElAPSa> TINE -MIN. FUa USB> - LB. ElAPSa>TIWE - MIN.

44000

450

330

g 40000 FUEL USB> - LB. + DISTANCE - N. Ul ~

400

l.D

DISTANCE - N. UL 0

350

250 42

DISTANCE - N. .._ 36000

300

0.6

ElAPSS) T1WE -

32000

250

145

ElAPSa>TIME - MIN. FUEL USB> - LB. DISTANCE - N. UL

KCAS

GR.WL -LB.

180

MACH

DIST~-N.&.L

0

wnH ENHANCERS

1.2 (1.3

!IS 2.2

1.5

G.5 110 2.5

().3

(1.6

65

135 3.0

55

1.8

Q.9 2llO

5.D

Q.9

12

2.6

210 5.5

320

621)

9.0 1.6

22.0

Q.9

250

345

12

10.0 1.8

660 24.0

280

~

750

7.5 1.4

11.5

27.0

2.0

3.6

330 8.0

480

870 28.D

2.3 550

6J)

(1.3

Q.7

1.0

80 2.2

160 3.5

225

0 0

G.5 105

0.8

12

1.6

185

270

DISTANCE - N. .._

0

2.3

4.0

6.5

385 9.5

ElAPSa>TIUE - MIN. FUEL USB> - LB.

0 0 0

0.6

1.0

1.4

1.9

2.8

130

225

320

445

640

2.5

4.8

7.0

1G.5

17.0

OIST~-N.&.L

6J)

12.5

14.0

3.1

3.2

42 1000 34.0

REFER TO SECTlON 5 FOft M lSI ElD UMITATlONS. RGURE 89--2 (Sheet 2 of 2)

89-7

TO 1f -117A- 1

LEVEL FUGHT ACCELERATION MOOEL: F-117A DATA Bo\SZS: RJGHTTEST DA~ S FEB 19811

!TIWE - YIN.. RJel.. USED - LB.

0 0 0 0 0

DISTANCE - H. 14

0

8..AJ'SEDTIWE- IIIK RJB. USED - LB.

0 0 0

lliSTAHCE - N. ...

~1.0

0

DISTANCE- N. MI.

DISTANCE- H. 14

S.A 720

0 0 0 0 0

2.6 3£5 15.0

B..AJ'SEDlDE--AJEL USED - LB.

31.11

~

4.3

REFER TO sa:noN 5 F - Ul. OIS'£I.Na: - N. loll

0 0 0

1.4 135

290

9.0

19.0

36000

B..APSS>TINE - MIN. FUB. usa> - Ul. DISTANCE - N. NL

0 0 0

2.S 260 15-a

4.6 470 31.0

40000

B..APSS>TINE - MIN. AJa usa> - Ul. DISTANCE - N. lolL

0 0 0

44000

B..APSS>TIYE - MIN. FUEL usa> - Ul.

DISTANCE - N. loll

0 0 0

48000

B..APSS>TIYE -MIN. FUEL USED - Ul. DISTANCE - N. loll

0 0 0

52000

FUEL usa>

B..APSS>TNE- MIN. - Ul. DISTANCE - N. loll

0 0 0

KCAS

GR.wt -UI.

NO.

32000

0

•2

+

?( 0 0

t;

KCAS

2ID

250

300

().54

0.67

(1.19

B..APSS>TWIIE- MIN. - Ul. DISTANCE - N. loll

0 0 0

1.4

2.B

t35

285

8JS

19.0

B..APSS>TIYE - MIN. - Ul. OISTNiCE - N. ML

0 0 0

2.S 260 15.9

4.6 470 30.8

B..APSS>nNE- WIN.

0 0 0

- UI. 32000

36000

FUEL usa>

40000

FUEL USED - Ul. DISTANCE- N. loll

0

ta +

~

0

~

FUEL usa>

~

B..APSS>TIIoiE - MIN. AJEL USED - Ul.

DISTANCE - N. loll B..APSS>TlWE- WIN.

48000

FUEL USED - Ul. DISTANCE - N. loll

52000

FUEL usa>

B..APSS>TIYE- MIN. - Ul.

DISTANCE - N. loll

RJB.. OENSilY: 6.5LBI\IS GAL

2.B

MACH NO.

GR.wt

•

RJB.. GRADE: JP-4

C.G. @ 43.0% MAC Al.JTTUDE: 30,000 FT. WITH EMf»>CERS

MAO-I

ENGINES: (21F404-GE-F1D2

0 0 0 0 0 0 0 0 0

• REFER TO SEC1lOH 5 FOR AlkSPEED '--lATIONS.

AGURE 89-7 (Sheet 2 of 2)

89-17

TO 1F- 117A- 1

LEVEL FUGHT DECELERATION loiODEl: F-\17.0.

TWO ENGINES AT IDlE POWER

EHGih'ES: C21F~D2

GEAR UP ,ZERO WIND C.G. 0 43.0%, MAC STAHDARO DAY

RJEL GRADE: JP-4 RJEL DENSITY: 6.51.B/US~

DATA BASIS: A..IGHTTEST DATE: 2 FEB 1988

All. GROSS WEIGHTS RCS~INSTAU..ED

PRESSURE

200

250

300

IL54 0 0 0

D.6T

Q.19

11.3 1S

12

3.7

2J6 7:1

0.49 0 0 0

OB)

0.72

G.83

WIN.. AJEL USED - LB. DISTANCE - N.ML

11.3

1.0

1.5

w.c:HNO-

0.44

KCAS

AUTTVDE

w.c:HNO30,000

n:

ElAPSE) TIME -

WIN..

FUEL USED - LB. DISTANCE - 1UA. w.c:HNO-

25.000

n:

20.000 FJ_

ElAPSE) TIME -

ElAPSE) TIME -

MIN. FUEl. USED - LB. DISTANCE - N.ML

w.cH 15..000

n:

N()_ ElAPSE) nNE -

WIN.

RJEL USED - LB. DISTANCE - N.ML MACH NO.

10.000

n:

WIN. AJEL USED - LB. DISTANCE - N.ML ElAPSE) TIME -

w.c:HNO. 5,000

n:

ElAPSE) TIME -

WIN..

RJEL USED - LB.

DISTANCE - lUlL MACH NOSEA l.EYB..

ElAPSE) TINE -

WIN.

FUEl. USED - LB. DISTANCE - 1UA.

400

450

500

550

UMIT MACH

o..so 1.6 34

10.7

o..so 1.7

13

24

32

6.7

33 9.3

0.55 0.5 12

().65

o.75

D.B5

1.0

l.4

1.6

30

3..0

21 5JI

1.7

36 10.5

o.-o

0.50

0.59

Q69

1:118

0.87

0 0 0

0.4

0.8

1.5

1:1

10

t9 4.5

12 'Z1 7.0

34

a.o

38

39

1l.ll

\1.5

D.36

0.45 0.4 9

0.54

0.63

0.72

0.80

D.7 17

1.1

l.4

1.8

3.8

25 5JI

31 7.5

1.6 36 9.D

D.33 0 0 0

0.4 1 D.4

0.50

0.511

Cl.66

1.0

12

10

0.7 17

22

1.6

3.5

D.30 0 0 0

D.38

11.3

0 0 0

0 0 0

22

36

1D.9

o..so 1.8 38

112

o..so 1.8

o..so

0.89 1-7

1.7

39

39

11.3

11.5

D.74 1.4

D.82

0.88

1.&

1.7

33 8.5

36

39

5.5

28 0.8

9.5

10.1

D.45

0.53

D.01

D.68

0:16

0.83

0.8

1J)

1.3

1.4

1.5

1.6

8

D.4 15

21

32

34

1.5

2.8

2J6 5.5

&6

7.5

37 1.5

1.8

REFER TO SSCTlON 5 FOR All & &D UNITAllONS..

flGUJU: 89-1

8 9-18

350

4.1)

o.as 38

TO 1F-117A-1

SUSTAINED TURN CAPABIUTY

t-

TWO EJIGIN'ES AY WAXlloiUII POWER

IIOOE1: F-117A DATA BASI$ : FUGHT TEST DATE: 21 IIA8CH

GEAR UP

CG @ 43.0% IIAC

RCS ENHANCERS INSTAU.ED 5.0

..

!

.·

i

I II

tS

• :II ' ...

11.11

...

Ul

GIICISS WEIGHT - 1 - l B

II.AaiiiO.

I'

Ill

II

--FT

I

STOOAY

I

•z

- - AlJTTUOE

. -·

i I

LIO

...

... ,

jo

Ul

50 GROSS WEIGHT - 1-lB

RGURE 8'9-9 (Sheet 1 of 2)

89-19

TO 1F-117A-1

•

SUSTAINED TURN CAPABILITY TWO EHGUIES AT MAXIMUM POWER

GEAAUI' CG@ 43.0% MAC

IIIIODn: ~1 f7A O.TA BASIS: FUGHT TEST

RCS EHHANCERS INSTAl I ED

o.re 21 IIARCH • -

'no o ~~

...

" ".._,

u

t .'4

0

ti'T

~;: ~

I

~

· IS

~

.....

•

uo

D.l'IJ

...

~ ~

....

30

•

~ WDaHT-

..

1000!.JI

,. 0

•

u~

pMS!!JN AUTTUDE- &L..

i

I'T

!

I

i

•

..

u GROSS WDaHT - 1000U

.... --..u------FIGURE 89-9 (Sheft 2 of 2)

81-20

•

•

TO 1F-117A-1

MAXIMUM LEVEL FUGHT SPEED TWO ENGDIES AT IIIAXIIIUM POW£11 liiODEl; F-1 T7A

DATA BASIS: RJGifT TEST DATe %1 IIAIICH 1 -

..

GEAR UP 43..11% MAC

oo e

RCS ENHANCERS INSTAU£0

AGURE 89-10 (Sheet 1 of 2)

89-21

TO 1F-117A-1

•

MAXIMUM l.EVEL FUGHT SPEED IIOCEl:F-117A DATA IIASIS: RJCKT TEST

DATE: 21 IIAIICH 1 -

TWO lHGJKES AT IIIAXJIIUII POWEJt GEAR UP CG 0 43.0% lilAC

RCS ENHAHCERS lNSTAU.£D

t

I I

I

I

•••-·•·•••···o·• •FIGUR£ Bi-10 (Sbeel2 Of 2)

89-22

•

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE N00B.: F-ll7A DATA BAS1St FUGHTTEST DATE: I WAY 1 -

TWO ENGINES- GEAR UP NO f'lllt\.OAO - OG 0 43.0% Mote STANDARD DAY - No WIND RCS EHHAMC£RS IHSTALLED

PIIOCUIUIIE

RANGE AND liiiE TO ISOO .... FUEl.IIUIAINJNG AT SEA J.PJ'E1. FUEL 2500 LA

N.Ni. Win. _,No.

.....

NJoiL

lla::toNQ. GIO LA

s.L..

5

10

15

20

25

30

35

51 9.9

62 11.7

73 114

115 15.1

111 1&2

l23 19.8 0.14

133 20.3 O.S1

Q.Q'

o..so

Q.55

Q.58

911 16.7 OJI'

126 243 0.46

146 21.1 Q51

1E8

192 32.2

217

241

262

2!1.1 Q56

SoU

311.7

311.7

'ZT7 311.11

Q.IO

Q.8S

0.71

0.15

Q.l2

35

35

35

35

35

~M-IOOOR.

212 38..4 G.l1

'ZT7 311.11 11.82

OU.aOplrrunM l'e ld On Clcu'8e

62.2 0-83

o--.d on O:usa ~M-1000R.

o..as

35

35

35

N.IIA.

21)8

2t9

253

25t

34.6

36..0

lla::toNo.

31.9 O.SI

230 33.3

242

30.6 G.l1

O.S1

Q.81

O.S1

31A G.l1

22-4 C2.9 0.49

251 46.8

293 50.5

o.s3

35

35

N.Ni.

393

Win.

.as 55.a

572

-No.

54.5 11.82

11.82

Q.l2

108. Win.

321 80.1

366 liS..a

7Q.5

.....

N.Ni. Win.

-No.

6000 LA

...,No.

332

372

57.&

4 10 110.3

Q.57

~.0 Q.S2

OJiiS

0.72

441 62.9 0.76

35

35

35

35

35

35

439 59..9

.ug 612 D.82

456 62.1 D.82

62.2 0-83

416

415

51.5 0..12

..

11.82

1'5.0

522 79.5

0,63

.42]

572

613

QSI

82.8 0.13

85.6 0.11

462

462

---

o..so

Q54

o.sa

30

30

30

30

30

30

30

5153

575 80.7

'5115 82..0

596 83.4

6CI6 k7

Q.77

0.11

613 8S.6 0.11

--

,...

1n

9..3 210 48

1D.6 239 57

lOCI)

LA

IHiliAL AU. - I 000 Ft.

N.IIA. Win.

78.0

564 79.4

loladlNQ.

Q.77

Q.77

o.n

1.6 311 7

S2 75

.... -Dascanl Z50KCAS O.OUp

,.

o.n u

6.3

110 22

30

7.3

39

-

ou. ........ D

ld on Clcu'8e

au. a - M

D

ld on Clcu'8e

ClirTOIO~M

au. .........

ClirTO 10 Cl!*'rUn Al.

~. Cl!*'rUn Al.

l'e •ld On O:usa

au. a - M D

ICI on Clcu'8e

~M - IOOOR. ClirTOIO~Al.

au.. Oplmum Al. l'e •ld On Ocuse

Full -

~-Win.

Lb.

DilL- N.Ml

• a..d on 3CDlO Lb. Zsm FuoJ waq-c. No Pay"*~, ACS EJ •• cas hs:dBd. lla::to No. st"OM'I i s - OIJse lla::to No. • 11me. r..I,.-ICID caftidodlarOnOcuseCiint>IOOplinunAaJdaardlarOnc::rur.O.:.W

.,s....-o . .,...

• ClirTOa 340~11aeh No.. Maldnun ~ • .......... lOCI) lb. c1 Fual. 0\Ma -

CJia'C)--....,-. 0.11211aeh No.

'

1-Full-

Lb. hiii.IAL-R.

lOCI)

33100

t2000 31100

16000 29300

I

FIGURE 89-11 (Sheet 1 ot 3}

89-23

TO 1F-117A-1

DIVERSION RANGE SUMMARY TABLE W0DB..; F-117A DATABASIS: A.JGHTlEST DATE: 11o1AY 1988

lWO ENGINES- GEAR UP 2500 Ul. PAYlOAD - CG,@ ~MAC

ENGINES: C2)~-F102 RJEl. GRADE: JP_.

STANDARD DAY - INO WIND.

RJEl. OENSnV: 6..51..8/US GAL

•

RCS ENHANCERS INSTAUSl RANGE AND nM£ TO 1500 Ul. FUEL REIIAINING AT SEA LEVEL

30

35

108

o.n

\19 1&.9

128 19J

OUiseai-AI.

0.75

Q.82

()aso •d on cane

2111 33.0

233 M.9

251 3&.6

Q.1iiT

0.12

o.n

264 36.9

315

35

3S

315

3S

Oplinun AI. - 1000 A.

231

33.3

2w ld en Cco.ne

Q.58

1.5 18

3.1 36

51

Tora-Mn. Full-lb.

6

"

20

OisL- N.MI.

la:t>No.

G.AII

G.53

N.MI.

.....

3 17

64.7

Mach No.

~-· o.so

308 62.2

a--~

o..so

m

o.Ase....... M ~cno:use

OUise•nliiiM

...

['a& •ld en

eas.:lcn30000lb-Z.OFull~!*aSCIOOU.. ~'a)?

• Mach N o . - .. t*lll 0\.iisa Madl No.

• rma.. Fuel. ano c

a

0~--AI. ld en C:::O:U.

-------

l46

2fil!l 46.1. o.56

..-.-o.sc.r. ZSDICCAS •

5

hclJdad tlr o.. aour.

c:::o:u.

'RC$61&"*"''

7

toe:e'., S..Leooal O&sD - . . .

FIGURE 89-12 (SMft 3 of 3)

Bi-21

ENGINES: CZ)F.e()4-GE-F1D2 FUEL GRADE: Jl>-4 RJEl.~ &5LB/USGAL

•

•

TO 1F-117A-1

I

GLOSSARY

-A- AlA AlP AIR AfT AC(ac)

Air-tO-air

ACESD

Ad.-ancal ++1M I j4 ejrnjno seal Annamt:l!t cnotrol paad. Air data WCUfCiltt

ACP

ADC

Atnopi1ot Air n::fuc:tio& All1othrollJe ~ameat

ADF ADI

Alncaalic dileaiou finder

AfY\1

~

Altimdc cJireaor indjralt)£

AERP

A.iraew C)'etic variation Miaopboot Military Main laDclin& p r Mooit« Memooy point tradlin&

MUX

Mnltipkx

MD..

NAV

Naviption

NCC

~tioa control oomputer

NlAC NLG NORM N-WSC NWS Nl N2

OC1P OFS ORIDE OVRT OVI"EMP

PAL PASS PCM

PDU PlO

P1U PLA PNEU PNl...

~tioa

mrerface aDd awopilo« computer

Nose landiJ!& p r

lobmal Naviption -Weapon S)~eM

TACAN

1ktic:aJ air oa•-iptioa 1b be dettm!m..l

TBD "'TBS

•

-

-'!b-be'SI•J\ICd

•

•

TO 1F-117A-1

TACAN T""'P""'tnre

TCN TEMP

TK

Tradl:

roo

Trme ol do«-q>elliug Trme ol release

TOR

•

TOr

Total

TRK

1iad: Thpeze

TRPZ 1TG

Tunerogo

UNLKD

Up frmt ts AnnnnQatcY Panel

Annunciator Pand Warning. Cautioa. and Advisory l...igbts lncfiratiop Antc:ona Cnrtuol Panel Antc:ona Locatiolls Antc:ona Sysaems AnlellDa S)-stem. UHF Anti-Collision Lig}l!S Anti-Collision I.igbts Switcb A.rllhG-Suil-SJ=m_

3-45. 3-46" 4-lS" 4-34" 4-33 4-36 1~1

I~ I

J,-21

1-2'

Am.i-iceJDcice Panel ~SJstcms AntHtid Fdure AntHtid Sysacm AOAJ.imils AOA Wamiog Sysacm App IM1il -ARM-4

-Fn (Ground) -Ftre '1\'amiQg Detection S)'Stem

1-24

-Ru!f'Ctnllfi'"Sit.~

1-~

Pa&e numbc:rs with asterisk (") denote illusuatioa lndex-3

-

TO 1F-11 7A-1 1-23 _, jejtacjops

~

-t.tode Seqacaa: l...i&bt ..OFF CaDtiao LicJu -Ptesmr&WI Air Swt S)SUIII (PASS) -Swt -SwtSwilcb APUIEPU Panel A.naamesn Coauol Panel (ACP) Arralilt& ('Diil) Hoot. System_ -Coauol a.oclllldicator -Hoot Down Licbt -nil Hoot. SW1ldtl.gbt An t1! •IS (.Abon/Dcparulre &d) An P IS (Appoem &d) Ali+Cj . . ~ ntJ1e AIDdtModes -l..e¥d w~ Dc:liYay Mode -Loft Mode Rdea5e Mode -stores lavatiOiy

-.u•oa'

A"*lftiNe Roll Rates AI-.bk Sded'P Anpes Allitode Oueaor lndlcaiOC'S Altitude HeadJn& Rderentt System (AHRS) Arulode IDdator. SWdJy Autnpib -AititudeJMacll Hold Swildt

..a.,act Sdca S'lrirdl -Coatrols a.ocllnc!yatrcs

-a.trol SlG o.uols -!)isc:ow.....,ed

upt

-Doa: FP' SWIIIC:II -Dual NoRd~ Licbts -Eitp&e StrUcb - f'nwt!OOS - IJuual En~ Aititode ADates - Lmuts -Naviptioo Hold Switdt -RdctU~~:Z Swudt -su.,le Cbannd LicJII -&ata a.oc1 V.'arain& J...i&hts

1-24

•

1-2S 2-6 1-23 1-24" 1-73, 1-7S·

1-68 1-69. 1-zs· 1-68, 1-2:1· 1-68, 1-2:1· l-6

3-39 Al- 2. Al- 14" 4-9S 4-9S 4-9S 4-9S 4-9S

fr3 fr3 1-al. 1-64". ·~ 1-68"

·~ 1-69" ·~ 1-68" 1-Sl

I-S4. I-SS• 1-S7. I-SS• 1-S4. 1-ss·. I-S7

1-.sa. 1-ss· 1-.sa. 1-ss· 1-.sa. 1-ss· 1-.sa. 1-ss·

1-s.. 1-ss· 4-24

1-56· ~12

1-S7. t-ss•

t-SS. t-ss· t- S9. 1-ss· l-SI 1- jO

-Warup AIXI:iliMy AC EJcctrical AJwtt System AtD.ib.ry ~ Paad (HSI) ...coonc Sdca KJIIlb -HQdiaa Sdca KJIIlb -HSI Sdea Switdt Alrcltary f'ooau Ullll (APU)

------~ -~~~~~~~ ~

lndex- 4

1-216

alllli>eu with asterist (") ~e illustratiao

F0-3"

·~ 1-67" ·~ 1-67" ·~ 1-67" 1~1-67"

•

1-23

------- ~-~ ----;;....

TO 1F-117 A-1

-Ftre Waming Ligbt - Fuel CmaiT S'll'iu:llljgl!t -Fuel Switcb -OFF Caulioo Ligbt -PASS ()pe!ation

1- 24. 1-24. 1- 23, 1-24.

-PASS~em

Avionics Air Hol Avionics Air Hol J...iaht A>'ioftics Orim, Fau Failure AriDnits Growllla..=S)'Siml A>'ioftics Ground ftJwu Swilcb A>'iollics Systems Inuodna;.,., A>'ioftics Sobsystcms Ott-8can:l Thsling

Bachp. Computer 8actup. Displays Bactup. lnerti3l Platform Barrier An'eslJI>eolt L.imi1s Basic HUD Display Basic VSD Display Battery Stan Cbeddisl -APU Start -Cleanup Chect -Qxi:pi!IDterior Cbed: -FCS Pbstslan BIT Chect - FCS Prc:swt BIT Cbect -HOI INS Computer Rdlocx - lmln:lmeal P.u>el

-LdlComole -Ldl EDgine Swt -Right Comde -Ri&hl EDgine Swt Bd-Reswt Switth - l'ower Switches Compotter Failun: (lnlligbt) Camplcte Loss of Either Hydralilic S)"Stetn Ccmale and Pand Lights ~Utility l...ights

-Lights S...Ucb -Fiood/StonD l...ights Switcb

-HUD/MOII...ight S-..itcb Insmunent UgbL-Saitch -Mapupt -SutHftsl:tument Ugbt Switch - Wamin& Lights Switcb Coatrol Display Ullil (COU) (INS)

- - - - - --

- AiigD Ligbt -Aiipmeot Mode - Dcspin Light -Dimmer Coatrol - lotedoc:t Light -Ke)tloanl - lamp Test and Bri&htness Coatrollesl Switch -Mode S..ncb FwiiCtioo --Navigati011 Mode -OIJMode --Stan-a }-26 ~s·

1-12 l-18, 6-1 :Z..ll AS-I

B.S.. I 1-35

2--23, l-2.4· 1-33 1-33, 1-34· f0-7• 1-23 1-23

>-36

Defoe~!

Deicer Coouols and lndarors Deplnart>-End Arn:stnlalt DesttmiBdore I """"'& Descent Pedormuce Desceor Pedormaacc: (RCS Fabanaon IAslallc:d)

1-Sl, 1-S2• 3-0 :Z..ll A7-1 87-1

Ora& Dtlte Coatrol

1-1 4-23 4-1, 4-3• 4-4,4-24 A9-2 1-$,1-ll'

-T--Hade

1-6}. fO-t •

~Backup ~ (HUD, MDI,

SD)

-ContrOl Stict f1:Dc:t.o;. micos Raat;e Smanwy "Oiblcs

Ora& Omte Deplojed iD fliPr Ora& Cllate u.uu Ora& C1lote ~ DaaJ Airspeed Faure DaaJ Bleed Nt Oua ~ DaaJ Comerter Failure DaaJ &poe FlaJDeout Deal R:S I..J&In DaaJ R:S Fail Lic'lt lndirarn DaaJ As *'' 1 • . . , . . Pa:uc:na Dual Genemor Failure Da:!l Lead Add Baucries DaaJ MDIIOIDIIHUD Failure (lafbabt)

- - - ECSS)stem- - - - -

lndex-8

•

}-)9

~13

I-$ }-35

}-36 }-26 }-16, }-17• 1-4 }-32 }-17

}-lS 1-33

}-38

•

•

TO 1F-117A-1

E01l.1 Data - Verify EGTUmits EGT Overu:mpctanuell.ow Thtusl Ugbts Ejeaion Ejrnjon l'roc:alutes Ejrnjon Seat -ACESD

-Banay lrw!irntor -Controls and Incfirators ------------~~~~ -Normal Ground Egress

-Performance -Safely De¥ices

-System -Sar>nal Kit Elearical -AC Amiliaiy FOoou System -AC Elearical S)"SUID ~troiPand

-DC Syslm> and 1\:Joou {)islri>nrino -OuaJ Com-ener Failure -Doal Generator Failure -Ooal Lead Acid Baueries

-Emeqa>cies -Extemal ~ s~ -Extemal Power S>= Cootmls and IDclicatars -Fault l.ndicuor Panel

-Generator Failwe

-!'Ower Distri>orinn (~U..-c Systems) -~Supply S)'!lem

-System Cootmls and lndS:ators Electconic l'loc:cssing Unit

1- 78, 1--81" 1-79 1-78, 1--81" 1-81" 1-78 3-10" 1-78, 1-80" 1-78, 1--81" 1-79

F0-7" 1- 33 1-34"

1- 33, F0-7" 3-216 3-25 1-33 3-25 1-34 1-34 1-35. 1-36· 3-2S 3-25 3-27"' 3-23" 1-33 1-33, J-34" 1- 10

Eu>aJ;Cllq

-Airoaft Enuy -Brake S)'Uem

3-45, 3-49" 1-32

1-n

-Canopy System 3-zr, 3-28" -Elecuic:al Power Distri>orinn 1-33 - Elecuical Syslem 3-4 ~round Egress 1-216 - 1-f)dtaulic Sv.ildl 1- 26 -H)'Ciraulic System -I anding Gear Eldemioo 3-40 1- 28. 1- 29' -Landing Gear Release Syslem 1-28 -Landing Gear Handle 3-8,3-41 -l.anding Gear Reuaaioo 1-74 ...Qsnal Lever 1-78 -0:1)-gen Supply 1- 25 -~Unit (EPU) -1'11o< l:mergeocy Enr.ldioo --- ~~ Page nlllllben ,.;u, asterist ( ") deDotc illusuarinn lndex-S

-

TO 1F-1 17A-1

-Pnx:edwes

Emer&cDdcs -Groome! Operation -lnfli&ht -LAndin&

-l»eoof EDdurance Eadurance (RCS Fnhana:rs lnsaalled)

3-1 3-4 :H 3-39 3-S A6-1 86-1

•

Fnpne Abn7,s-3' 1- 39 1-~

M-3 ~1

Al-2

Foe!

-Ain:ralt Syacm - Alternate -Both W"ma 'Wib Fail tu Transfer -lloo5t and Transfer l'llmps Inoperative (Grouad Opeatioo) -ContrOl Puc~

...cor-,._

-Croafecc! -Crossl'ecc! Coauols ..... lndic:ators -Crossl'cec! Lipt -Crossl'ecc! YaM ()pea [pdjcatm; -Crossl'ecc! ~ SwitdJ -Onoft SWlldl upts -DeG!y

-Damp RMc:s -Dulllp SW'IIdl

1-10 s-6 ~24 ~2$

M-3 1-14' 1-U 1-U

1-13 1-18' 1-12. 1-191-16, F0-1 ' Al-3, Al-16'

1-13 1-13, 1-14'

"':Dump~=-

''""' f'6oo¥

lndu-12

•

•

TO 1F-117A-1

l-22

-Emergeocics -Engine System -FecdS)~em

-Feed Sowee Switch -Flow foe J...oa& Range Cruise -Flow foe J...oa& Range Cruise (RCS FnMJlCNS lnslalled) - Forward Transfer 1&nks Fail to Transfer -tncficat« Li:&h• -Indicator Malfunaioo -I.Dert S)~em CQrllrol aDd lodicaJDG tmtata'M%'

-Jenisoo

1-3. ro-u· 1-11. ro-u• 1- 12, 1-14" AS-2

B>2 l-24 1-18

l-22 1-13 l-22 M-3

- J ettisoD (RCS Enha,..,.,. laslalled} -Leak -Limits

1!9-1

-~lij:biS

1-11

l-22 s-6 s-6

- Negative G timilalioos ~ Wong l3nk Fails to Transfer -Pressure f...i&IUs

l-24 1- 11 l-23 s-6 1-18. F0-11'

-PrimaJy

- f'r'esmrizatioo IDertiag aDd Venting S)'Siem -Quantity Indicator -Quantity ~ IJidicatioo -$)'Stem CoGtrols and lndicatols. MsellaDeoas -Sys~em Emcrgcocics -Unk Capacities -lll.nts Pressurization. lnertin& and Venting System - "R:mpcr.llure timilalioos -Transfer -Transfer Emeagcocics -Transfer Failutes Causing Extreme C.G. Variialioos Fueling Opentions -Normal

- Air

Fusefa&e Li:&hJS Switch

1-17. 1-IS'

l-23 1-22 l-22 1-11' 1-13, FO-Il"

>7 1-U

l-24,3-25 6-4 1- 14 1-14 1-14. 2-11 1-41

-GGain Sensing s,.-itctJes Failed 1o Gear J:>o,."' Posilioo Gain Sensing Switches Failed to Gear Up I'O!iruoo G-Suit S)'Slem

l-33 l-33

Geucnloc Failure Glide Dislanf% aDd Speed Schedule Glossary Go-Around Grid (Air Inlet) Ddciug S)'51em (Engjne) Groand Ocarua: GI'OUIId Fueling. Normal

l-2S l-18•

GI'OUIId Opcratioo Emcrgeucies "Gm!s~

1-21

Glo5saly - 1

2- 12 1- SZ 2- 23, 2-25" 1-14 l-4 l-Ie

lndex-13

-

TO 1F-117A-1

s-7 2-12

BaTe Q=d (HQ) System

-:; upo::.KY Ncu -Maluple WOO~ Quiet D) -Net NDOIIbc:r ..n.e-d-Diy (TOO)

------- ~R~--

-TODU• -WOOEauy

.•

-WOO 'lft:Dsftt ..v;ord-o(-Uoe-Diy (WOO) Ha'f't Quidt brio Coatrols -A-3-2-T SWlldl -Antem~~ Sdeaor Switda -f'aaci.DI Sc:k:Clor SW'IIdl --M1nual FR:queecy scwun --Mode Sdeaor -Preset Cbannd Sdeaor Switch

s-cb

-Sqaddl Switch -lbnc Transmit Switch - \\llutDe Control

Head-Up (HUO) Display HeacHJp (HUD) Display Bact:vp HIP ADA Reco~ Al1diD S•itdl - Weapon Al1diD S..-ildl Idle Core Speed Limits IFF Controls and lndicaton -lclc:rUi["IC3tiocH:If-Pbsition Switch - Master Sdeaor S..-ildl -Mode 1. 2. 3/A and C ContrOl Switches -Mode I and 3/A Code Sdeaor Swiu::bes

•

1-2 1-Sl l-SI 4-42. 4-44' 4-43 4-44 4-43 4-44 4-42 4-43 4-43 4-44

s-s· 4--45. 4--46' ~4--46·

4--45. 4--46' 4--45. 4--46' ~4--46·

-Mode 4 Code Selert S..-ildl ~'dode • Caution Ligltt -Mode 4 Controls and INfirntors

4-46· . 4-47 4-46• , 4-47

-Mode 4 ldentificatioo Switch -Mode 4 Oo-Out S'lritcb -Mode 4 Reply Ligbt

4-46•, 4-47 4-46•, 4-47 4-46· . 4-47

-RAD-OlJT-MON Switcb -Test Ugln IFF~ Opc:ratioo

- Modes I, 2 and 3/A IFF Nortto31{)poatiuu

~4--46·

4--45. 4--46' 4-46, 4--46' ~ ~

--+4

lndex-15

TO 1F-117A-1

-Modes 1. 2, 31A. and

.....a .....a

c

-Mode~

4-44 4-93 4-93 4-93 4-93 4-93

IFF ~CIIl (A."'IAPX-101)

u.s Cocii'Ok and IJidaiOR -FveqdiCftC)' Jnctjc:at()r Ftcqwy 1lmiD& Coctrol KDOb5 -~"ower CociJOI Swildl -~ Coctrol s-ud~ n.s PI octdw cs ~ed 10 1hoe NlA Coc•allioa

J....u.J ~ Sysaea (lNS) -Comrol Display UDII (CDU) -laenial MeaswtsiiCDI Uail (1MU) -lalcrface E1ec:tn:*s Uail (lEU) -Ke,tloeid JJIUtill Plalfona (IMUIIEU} Bac*ap bien Swiu:h, Fuel IDeriJSwftdiUaltts. Fuel lallipt Emo&Ca:w::it:l Jllfnm:l ~bOll ~CIIl (IRADS) ln1el Grid Ddcu Cocuols and lndicatcws -Deice Flui111.4ltt -Engine Inlet \VqJC1' S">tcb - WIPC" 1.4ltt 1llopaalNe System.siFUnc:hons. Altaaft {EmerJ I'Qor.u} INS (IDenial Nniption ~CIIl) -AalltmeialOI" Ualtt -Bailt-m 1tst -Bailt-m Testll:ntedod: SW11Ch -Comro1 Dlspl8y Umt (CDU)

--EDnt D:11a - Verify -Epa lo£mute Reltw ...fdme ~Ahp_.,c

INS~Modes

-AID:iiary Modes

-Coene tiDe Steeriq Mode -Coene Sdea St~ Mode -')esriaat ... St~ Mode -DR Mode -U.S Steeriola Mode -Mamral H tin& Stecn.. Mode -TACAN ~Mode -lbm S2oan cct -Paucm/Approaches

7-1

IDsuumcnts {flWlt) I.JucraJmnlunicnioo (ICS) Pand IAten:oammniraOOn S)'5tall (ANIAIC-25) IRADS Control Pand IRAOS Sensoc Display

KCAS Cou>usioa 10 KEAS Kqtloatd.CDU KY-ss Control Panel (Secure \tlic:e Communn•ion)

I

ancting

-Appoacb - Appicab and I anding Faformmce -Applcab and Lancfin& Faformance (RCS Enhancers I!!S1311ed) -Blown or Damaged Tuc(s)

-Ciwt Use -Criteria

4-44• 4-42

4-30" 4-29"

Al- 2 4-62, 4-54• 4-42, 4-4)•

2-12, 7-4 2.-12 AS-1 B-1 3-42 AS-2 ~3

~

2-13, 6-S

-Dual Ent;ioe Fla.meout Pauem

~17"

~39

-~

-Cy Eneasion --I

w

~4-96'

4-96 4-10' 3-34 4-9S 4-93, 4-9(•

1-10 1-39

•

•

TO 1F- 117A - 1

SDn'ivaJ Kit Sustained Tt1111 Cal"'!vlrty Sasuined Tum CaJX"'PPity (RCS Enba!M"e!'S ln:s:lalled) SJ$tem Umiw.ioas SJ$lems -AMAD - Anterul3 -Angle ol Auact. Warnin& (AOA) -Anti-G Sail -Anti-lcin&(Ddring -Arrcslin& Hoot -Avionics -Bleed Air 4:om.mnnQrjons, Navip~ aDd Avioaic:s -Ejectioo Seat -Eicaril:al -En\'ironmcnta!Conuoi(ECS) -Fxptnded Data Thmsfer -Fue~ (APU) -rue\\~ (ENGJ:NE)

--flighl Qxluol (FCS) -Fod -Hydraulic

-lFF -loertiaJ Naviplioo (INS) -lnfrared ~(IRADS) -Instrument 1 andinz (lLS) -IJlteralOimnnicujons (ICS)

-' anding Gear -Ligbling _Limitalioos -Nosewbed Steering (NWS)

-OJ;yJcn

•

1-79 A9-3

85-2 5-U 1-18 4-33

1-49, 1-51°

1- 21 I-SO 1~

4-1

1- 19 1-31 I~

1-78 1-33, F0-7"

1-44. ro-s·

4-25, 4-26" 1- 24 1-2 1-44

1-10. ~ ro-u· 1-216, F0-9" 4-44 4-S2 4-27 4-92 4-44 1-27 1-37

5-U 1-29 1-74 1-43

- Pitoc-Swic -Seaue ~ Coolrannicalioo (KY-S8) -Stores Management (S~IS) -TACAN ~igalioo -Weapons OdMty - Weapoas Ba)'lliape:ze

4-93 4-48 1-72,4-91 1-72, 1-75"

"Lt.CA-: Approadles uo.cAN QxltrOis and lnclicator5 -annd SdeaOB and lndicalOB -Mode Sdcclo.- Swildl -self-lest Pushbnuoo and Indication l..igbt -Volume Cootrol TACAN Ope:ralioo

4-49,4-SO" 4-49 4-49 4-SO 4-SO 4-51

..

--

~.,-~~ ~~ • OQit:SOtn...,..x"'aa

4-42

7-2

+48

lndex- 23

TO 1F-1 17A-1

13il Root (Ainstin& Hoot) S)'Stem

1ailbootiBanier Limil 1lilpipe I imirarinns 1»ealf 1»ealf aDd Oimb 1»ealf Odinition ol Teaas 1»ealf EmotpJCies 1»ealf Planning 1atecfi RPM Cbedt 1)xj

1lD:i Liabts

1~

s-u.s-w s-6

Al-l. 2-10 1-1

Al-3 3-S

Al-3 Al- 2

~-------------------- 2-10 1~

TOLD Card TOLD Card (RCS Eobancen IOSiaDed) llaroule Pand

llaroules TJreUmils

A9-3, A9-6"

89-3 1-9" 1-8. 1-9" 5-13

Tire(s). Dama&ed'BJoom. 1 •odin& 1ixal aJII!lnslantaneous HUD FidckJ{-Voew

3-42

4-S" 2-13 1-72

~Ianctiag

Trapeze System Trapeze System ContrOls Trim Chances "liue Mad> Vs Calinted Airspeed -nue Mad> Vs JCTAS Convenioo True Vs Indicated AOA Tll!bulence aDd Thundetslorms 1hrbuleoa:/GUSIS Dutin& Landing Tum aDd SJjp !Jxlicatoc Tum Capabolity Thm Capahlity (RCS EohaJ:Ioen Installed) Thming Radius aDd Ground Clearance

UHF Antenna SJ5tem UHF Comnmniouino S)'Slem (ANIAAC-164\f) UHF Control Pand UHF ContrOls -Antenna Sdeaor Switdl - F\mct.ioa Sdeaoc Swildl -Manual Frequency Sdeaoc - Mode .S eleacr Swildl -~Channel Seleaoc s.~

-Squdctl Swildl - Thne Uansmit Swildl -~ume Control UHF Opetatino UHF Opetatino ~Quiet) Unit:s Coaousino Chart Unsafe Altitode Waraiftgs -,Up F: wn Cooolftii-BI !I (ll:J'q. ~ nUlllbas 'lrith as1erist (")denote illDSU3Iino

lndex-24

•

1-7S" ~

Al-2 Al-2 Al-2 1~

2-12 1~

1-63" A9-3

89-3 2,.23,

z,..zs•

4-36 4-36 4-38" 4-36 4-JS", 4-31 4-31, 4-38" 4-31, 4-38' 4-31, 4-38' 4-36, 4-38' 4-31, 4-38" 4-31. 4-38' 4-31. 4-38" 4-31 4-40 A1-3 1-~ ll •

•

•

TO 1F-117A-1 1-57 1- 39

Up-Front Control Pand Alltopilol Cantrols Utility upus. C«tpit

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4-22 1-~

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4-96,4-96'

2-20 2-3 ~38

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2-14 2-8 2- 17 2-17

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TO 1F- 117A-1

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FOLDOUT ILLUSTRATIONS

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Blaook)

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TO 1F-117A-1

RIGHT CONSOLE

COCKPIT ARRANGEMENT (WSC AIRCRAFT)

RIGHT SIDE PANELS

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TO 1F- 117A- 1

ENVIRONMENTAL CONTROL SYSTEM

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