737 Scan Flow

May 10, 2018 | Author: Cuthbert Evan Tay | Category: Cockpit, Takeoff, Flap (Aeronautics), Aviation, Aerospace Engineering
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737 Scan Flow...

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FLIGHT CREW TRAINING DEPARTMENT

B 737 SOP SCAN SCAN FLOW MEMORY MEMORY TOOL Hi, Welc ome to tra tra ns nsit ition ion tra tra ining. ining.  To help the the tr transi ansition we have put together og ether a “st “sta rter pa c k” Ess Es se ntia ntia lly a tra tra ining ining guide g uide a nd some e xtra tra c ts re leva nt to to tra tra ining ining.. • • • •

B 737 SOP SCAN FLOW MEMORY TOOL QRH EXTRACT FCTP APPENDIX A FCTP APPENDIX B

 The memory memory too tooll is is ess essenti entia lly to b e used used for sc a n pra pra c tic e in the the briefi briefing ng room to help hand eye coordination i.e. where to look, what switches to move or what lights / configuration to observe and help memorize the flow. Works well if practiced as a team. One reads while the other performs the PF sc a n and PM sc sc an.  This his helps helps to enri enric h the ti time spe spent nt in the the FT FTD / SIM We tried tried it a few times times for for a c o uple of d a ys b efor efo re the firs first FT FTD and a nd it helped help ed a lot. lo t. Typica ypic a lly lly ta ta kes 4 to 5 p ra c tic tic e runs to be a b le to per pe rform a ll the sc sc a ns from from memory me mory subsequently ubseq uently one prac tic tic e in the the b riefing iefing room roo m before each session helps.  The content c ontent is limi limitted to the the ac tion lilines of the the proc proc edur ed ures es.. •

C erta erta in ac a c tions a re highlighted highlighted a s shown how n below be low

 This his indica indica tes “poin “p ointt of entry entry” in the overhea overhead d sc an. This his helps helps to memor memo rize ize subsequent ubseq uent step steps s b a sed on “p “point oint of entr e ntry”. y”. •

Certain critical actions are triggered based on other actions hence are paired using “►” symbol as indicated below.

A s this this is o nly a tra tra ining ining a id plea p leas se refer efe r to offi o ffic c ial doc d oc uments for all c orr orrec t appli ap plic c a tion of o f proc proc edur ed ures es.. Enjoy your training!

JUN 2014

PF

PM

B737 COCKPIT SOP SCAN FLOW MEMORY TOOL PRELIMINARY PREFLIGHT PROCEDURE IRS VOICE REC FLUID QUANTITY

OFF – NAV ON sim sw does not latch

OXY / HYD / ENG OIL

DOCUMENT CHECK AND VERIFY FLIGHT DECK  ACCESS SYS

CHECK

ELT SWITCH

GUARD CLOSED

PSEU LIGHT GPS,ILS,GLS LIGHTS SERVICE INTERPHONE ENG PANEL

EXTINGUISHED

GEAR LIGHTS

SET PREFLIGHT PF

This is a sw on the door frame not shown in the sim

EMERGENCY EQUIP GEARPINS

OXY PANEL

PARK BRAKE

GUARD CLOSED

CHECK

EXTINGUISHED OFF SET SET ILLUMINATED

FLT REC SWTICH GUARD CLOSED MACH AIRSPEED TEST WARNING STALL WARNING TEST EMER EVAC GUARD CLOSED not shown in the sim SWTICH CIRCUIT CHECK BREAKERS P6 MANUAL GEAR CLOSED  ACCESS DOOR CIRCUIT BREAKER CHECK CONTROL STAND CIRCUIT BREAKER CHECK P18 EXTERIOR INSPECTION I

I

 ATIS

OBTAIN

I

I

COCKPIT LTS

AS REQ SET

I

I

I

I

INITIALIZE

I

I

TEST

I

I

FMC  ACARS / ATSU DOOR ACCESS

 All entries except C.G. and C.G. and V speeds at this stage. Always enter ZFW and ZFW and not GW

PF

PM

B737 COCKPIT SOP SCAN FLOW MEMORY TOOL PRELIMINARY PREFLIGHT PROCEDURE IRS VOICE REC FLUID QUANTITY

OFF – NAV ON sim sw does not latch

OXY / HYD / ENG OIL

DOCUMENT CHECK AND VERIFY FLIGHT DECK  ACCESS SYS

CHECK

ELT SWITCH

GUARD CLOSED

PSEU LIGHT GPS,ILS,GLS LIGHTS SERVICE INTERPHONE ENG PANEL

EXTINGUISHED

GEAR LIGHTS

SET PREFLIGHT PF

This is a sw on the door frame not shown in the sim

EMERGENCY EQUIP GEARPINS

OXY PANEL

PARK BRAKE

GUARD CLOSED

CHECK

EXTINGUISHED OFF SET SET ILLUMINATED

FLT REC SWTICH GUARD CLOSED MACH AIRSPEED TEST WARNING STALL WARNING TEST EMER EVAC GUARD CLOSED not shown in the sim SWTICH CIRCUIT CHECK BREAKERS P6 MANUAL GEAR CLOSED  ACCESS DOOR CIRCUIT BREAKER CHECK CONTROL STAND CIRCUIT BREAKER CHECK P18 EXTERIOR INSPECTION I

I

 ATIS

OBTAIN

I

I

COCKPIT LTS

AS REQ SET

I

I

I

I

INITIALIZE

I

I

TEST

I

I

FMC  ACARS / ATSU DOOR ACCESS

 All entries except C.G. and C.G. and V speeds at this stage. Always enter ZFW and ZFW and not GW

PF PA LIGHTS EFIS PANEL MCP OXY MASK CLOCK NOSE WHEEL STRG / Ground proximity panel*seat

PM CHECK

EXTERIOR INSPECTION

TEST

PREFLIGHT PM

SET SET (ON SIDE FD 1st.) TEST CHECK / SET GUARD CLOSED

FMC

VERIFY

FLT CTRL PANEL

CHECK

NAV PANEL

SET

DISPLAYS PANEL

SET

FUEL PANEL

SET

specific

DISPLAY SELECT PANEL T/O COFIG LTS CABIN ALT LTS DISENGAGE LTS STAB OUT OF TRIM LT FLIGHT INSTRUMENTS & FMA ISFD SPEED BRAKE

SET EXTINGUISHED EXTINGUISHED TEST

EXTINGUISHED CHECK CHECK / SET DOWN DETENT

ELECTRICAL PANEL OVER HEAT / FIRE PANEL APU START EQUIP COOLING SWITCH LAVATORY SMOKE EMER EXIT LIGHT PASSENGER SIGNS WIPERS WINDOW HEAT

*Advice Ground &

TEST 1. 2. 3.

FUEL PUMP START SW GEN ON BUS

NORM VERIFY GUARD CLOSED SET PARK ON

REV THR LEVER

DOWN

FWD THR LEVER

CLOSED

WING ANTI ICE

OFF

FLAP LEVER

SET

ENG ANTI ICE

OFF

PARK BRAKE ENG START LEVERS STAB TRIM CUT OUT SW RTP / NAV / ACP

SET

HYDRAULIC PANEL

SET

CUTOFF

AIR CON PANEL

SET

NORMAL

CAB PRESS PANEL

SET

LIGHTING PANEL IGNITION SELECT SWITCH ENG START SWITCH LIGHTING PANEL

SET

SEAT / RUDDER

SET ADJUST

PROBE HEAT

SET

AUTO

L/R  AUTO SET

MCP

SET

EFIS PANEL

SET

OXY MASK CLOCK DISPLAY SELECT PANEL

TEST CHECK / SET SET

PF

PM T/O COFIG LTS

EXTINGUISHED

CABIN ALT LTS

EXTINGUISHED

DISENGAGE LTS FLIGHT INSTRUMENTS & FMA BRAKE TEMP LT NOSE WHEEL STRG / Ground proximity panel*seat

TEST CHECK EXTINGUISHED GUARD CLOSED

specific

L / G PANEL

CHECK

 AUTO BRAKE

RTO

 A/SKID INOP LT ENG DISPLAY PANEL ENG INSTRUMENT SEC ENG IND CARGO FIRE PANEL RTP / NAV / ACP

►STANDARD

EXTINGUISHED SET CHECK SET CHECK SET

 ADF

SET

Wx RADAR

SET

TRANSPONDER STAB TRIM OVERRIDE SW SEAT / RUDDER

SET GUARD CLOSED ADJUST ►

T/O BRIEF (FOLLOWED BY F/O SECTOR BRIEF IF REQ BY CAPT)

DEPARTURE BRIEF PERFORM BARO/ALT/HDG CALL

X CHECK “ PREFLIGHT CHECKLIST”

BARO/ALT/HDG

X CHECK

BEFORE START PROCEDURE LOAD SHEET TAKE OFF DATA

VERIFY COMPUTE

LOAD SHEET TAKEOFFDATA

ENTER PERF DATA IN CDU

X CHECK

CDU

CDU

TAKEOFF REF

VERIFY COMPUTE LEGS

N1 BUGS

CHECK

N1 BUGS

CHECK

IAS BUGS

SET/ VERIFY

IAS BUGS

SET / VERIFY

MCP

A/THR – ARM SET – V2  ARM L NAV / V NAV HDG / ALT

FLIGHT DECK DOOR

CLOSED

PF TAKE OFF BRIEFING

PM COMPLETE

* config/ Rwy cond/ v speeds/ TAKEOFF BRIEFING thrust limit /over wt

 ATC CLEARENCE  ATC CLEARENCE

VERIFY OBTAIN

REVIEW PAX WELCOME PA BY CAPT CABIN CREW REPORT “ALL DOORS ARMED ”

WINDOWS

CLOSED & LOCKED

WINDOWS EXTERIOR DOORS GROUND CLEARENCE ►FUEL

(ENSURE STEERING PINS INSTALLED)

PANEL

SET

HYD PANEL  AILERON TRIM

SET VERIFY 0 not required to

RUDDER TRIM

VERIFY 0



STAB TRIM

CALL

SET ►

trim to the limits. not required to trim to the limits.

“ BEFOR START CHECKLIST TO THE LINE” PUSH BACK CLEARENCE  ANTI COLL

CALL

COCKPIT TO GRND

CLOSED & LOCKED CLOSED ► OBTAIN*

OBTAIN ON

“ CHK LIST BELOW THE LINE” PUSHBACK PROCEDURE CONFIRM ALL GRD CHECKS COMPLETE (ENSURE STEERING PINS INSTALLED)

COCKPIT TO GRND

CLEARED PUSHBACK BRAKE RELEASE  AT_

ELAPSED TIME

ON

ENGINE START PROCEDURE WHEN CLEARED TO START BY GROUND SEC ENG IND ► AIR  AIR CON PACK VERIFY

► ANNOUNCE

WHEN START VALVE OPEN LIGHT ON

START NO X ENG

PACK SW

ENG START SW

CHRONO ON VERIFY N2 RPM N1 +VE & N2 ~ 25%*



SET SET ► GRD

PF ENG START LVR

PM IDLE

CHECK EGT IN10 SEC

CHRONO ON

MONITOR FUEL FLOW  AT 56% N2 ENG START SW

ENSURE AUTO

START VALVE OPEN LIGHT OFF CHRONO

OFF

“STARTER CUT OUT”

ANNOUNCE

 AFTER ENG STABLE START OTHER ENG

2 MIN 10 SEC

BEFORE TAXI PROCEDURE ENG START LEVER  ANNOUNCE COCKPIT TO GROUND Observe PM work

VERIFY ► ANNOUNCE

MFD SYS display FLIGHT CONTROL

CONFIRM IDLE “ENGINE’S STABILIZED” ► “CLEAR DISCONNECT”



GEN 1 & 2

PROBE HEAT

ON

WING ANTI ICE

AS REQ

ENG ANTI ICE

AS REQ

PACK SW

AUTO

ISOL VALVE SW

AUTO

 APU BLEED SW

OFF

 APU SW

OFF

GROUND CLEAR► “FLAPXX” PUSH CHECK

FLAP LEVER CONFIRM ON GAUGE<  ANNOUNCE LOWER DISPLAY TRANPONDER

RECALL

ON

CHECK

SET AS REQ FLAP”XX” BLANK AS REQ

RECALL

CHECK CHECK all gauges CHECK all gauges FWD INSTR PANEL FWD INSTR PANEL and lights are and lights are normal normal GROUND WAVE OFF GROUND WAVE OFF VERIFY CHANGES TO TAXI BRIEF IF UPDATE CHANGES TO TAXI BRIEF IF REQ REQ “ BEFORE TAXI CALL CHECK LIST” BEFORE TAKEOFF PROCEDURE

~30% break away thrust.

~26% keeps it rolling.  At idle thrust A/C stops

TAXI CLEARENCE

OBTAIN

LIGHTS

AS REQ

PF IF CHANGES TO T/O CONDITIONS Wx RADAR TERRAIN DISPLAY

PM REVISE BRIEF SET AS REQ

REVISED BRIEF

VERIFY

Wx RADAR

SET

TERRAIN DISPLAY

AS REQ

CABIN REPORT

OBTAIN

“ BEFORE TAKE OFF CHECKLIST TO THE LINE”

CALL

BEFORE ENTERING RWY ENSURE RWY IDENT,RWY / APP CLEAR WHEN CLEARED TO ENTER RUNWAY  A/T, V2, LNAV, VNAV

CONFIRM ARMED ON FMA

any power interruption causes all of the above to trip

STROBE / LIGHTS

ON / AS REQ

TCAS CABIN  ANNOUNCEMENT

TA / RA COMLPETE

“ CHECK LIST BELOW THE LINE”

CALL

WHEN CLEARED TO TAKE OFF FOR TRAINING PF HAS CONTROL OF THRUST LEVERS.  ANNOUNCE THRUST LEVER Smoothly advance to park TLA at the 4 posn on the N1 gauge

WHEN STABILIZED When both engines are at 40%

“TAKEOFF”

START

CHRONO

40% N1

PUSH TO/GA SW VERIFY CORRECT T/O THRUST IS SET

FOR ALL FLIGHT PHASES  ANNOUNCE FMA’ S “ E.g. N1 TOGA”

 ADJUST THRUST AS NEEDED.(before 60kts) CALL “THRUST BY 60 KTS SET”

CHECKED CONTROL COLUMN LIGHT FWD PRESS VERIFY 80KTS & CALL “THROTTLE HOLD”

MONITOR AND CALL OUT ANY  ABNORMALITIES CALL 80KTS

CHECKED Note; All FMA call outs are VERIFY V1 not listed in this Document  AUTOCALL

OR CALL V1

VERIFY V1  AT VR CALL

ROTATE

ROTATE 15º

“+VE RATE” VERYFY ON ALT &CALL“GEAR UP”

SELECT L/G UP

>400 RA CALL FOR ROLL MODE

SELECT OR VERIFY ROLL MODE

PF

PM VERIFY VNAV ENGAGED

 AUTOPILOT MAY BE ENGAGED ANY TIME ABOVE 400 FT* if in-trim  AT THRUST RED HT VERIFY CLMB THR SET(FMA changes) VERIFY ON FLAP SCHEDULE

ACC HT CALL FLAPS

RETRACT FLAPS

ON SCHEDULE*

confirm on gauge / light for every action on flap lever. VERIFY FLAPS UP ON GAUGE AND NO LIGHTS ► SET / CHECK ► AIR CON / BLEED

“ AFTER T/O CHK LIST”

CALL

 AUTO BRAKE

OFF

LAND GEAR LEVER

OFF

Note: Actions to be completed before check list is called

CLIMB AND CRUISE PROCEDURE SEATBELTS > 10,000

AS REQ LIGHTS OFF

“PASSING TRANS ALT” “SET STD”

“X CHECKED”

“SET STD” PASSING FL 200

“CHECKED”

MONITOR PASSING FL300

“CHECKED”

MONITOR PASSING FL400

“PASSING FL—“ “TWO ZERO ZERO” ICING / FUEL /PRESS “THREE ZERO ZERO” ICING / FUEL/PRESS FOUR ZERO ZERO

“THOUSAND FT TO LEVEL OFF” “CHECKED” PASSENGER PA

COMPLETE BEFORE DES

Use of the jepp brief strip sequence to s et up In the same order: freq, crs, minimums, land alt etc Choose landing flap Vref speed and Auto brake setting

 ATIS LANDING DIST

RECALL FWD INSTR PANEL

CHECK CHECK all gauges and lights are normal

OBTAIN DES / ALT CHECK

CTR TANK

MANAGE

LAND ALT

CHECK

RECALL FWD INSTR PANEL  AUTO BRAKE

CHECK CHECK all gauges and lights are normal SET AS REQ

PF FMC / VREF

PM VERIFY

FMC / VREF

SET

RAD NAV FREQ /CRS / MINIMUMS SET*(course set individually)  APPR BRIEF  ARRIVAL  ANOUNCEMENT CALL

INITIATE COMPLETE “ DES CHK LIST” SET AS  APPROPRIATE USE AS REQ

RADAR  ANTI ICE TCAS

SET AS REQ CHECKED

PASSING FL300

CHECKED

PASSING FL 200

“THREE ZERO ZERO” “TWO ZERO ZERO”

CHECKED

PASSING FL150

“ONE FIVE ZERO”

SEAT BELTS/LTS*

ON (15,000 AFE)

 APPROACH PROCEDURES COMPLETE APPR PROC BEFORE IAF OR START OF RADAR VECTORS TO THE FINAL  APPR COURSE OR THE START OF VISUAL APPR. “TRANSITION LEVEL” QNH SET ------

QNH SET ------

TERRAIN DISPLAY AS REQ UPDATE APPR  AS NEEDED BRIEF UPDATE RNP AS NEEDED

PASSING 10,000  AFE

PASSING ALT-----

LIGHTS ON

CHECK AND VERIFY NAV FREQ & IDENT / CRS / MINIMUMS DISPLAY SELECTION AS REQ FOR TYPES OF APPR :ILS, LOC, IAN, LNAV/VNAV,VOR, “ APPROACH CHK CALL LIST” “CHECKED”

PASSING 5000

“FIVE THOUSAND”

Before commencing approach approx 12~15 nm to t ouchdown “CABIN CREW TO  ANNOUNCE YOUR LANDING STATIONS” PASSING 2500’ VERIFY RA VERIFY RA INDICATION AND “RA ALIVE” INDICATION AND “RA ALIVE” CALL CALL WHEN REQUIRED TO CONFIGURE ON FLAP CALL FLAPS EXTEND FLAPS ON SCHEDULE SCHEDULE CHECK GAUGE & LTS* AT EACH SELECTION. ILS APPROACH

PF

PM WHEN CLEARED TO INCPT

Use LNAV / HDG SEL VERIFY TUNED & IDENT VERIFY POINTERS ARE SHOWN  ARM

APPR ON* only if planning SECOND AP  Auto land Note: All FPT sessions are AUTOLAND but FFS sessions are with single AP except LVO “LOCALIZER CALL  ALIVE” VERIFY LOC CAPTURE “GLIDE SLOPE SET RWY TRK CALL  ALIVE” SEL L/G DOWN & CALL “L/G DOWN FLAP 15” VERIFY* FLAP 15 SPEED BRAKE ARM / CHECK LTS G/S CAPTURE

SET VREF ON MCP FLAPS—(landing flaps) MISSED APP ALT

CALL SET

SET

FLAPS---

 AT OM / FAF VERIFY CROSSING ALT CALL HT DIFF CALL

CALL

CALL

CALL

__FT LOW / HIGH.

“ LANDING CHECKKLIST”  AT 1000’ AUTOCALL* “CHECKED OR GO“STABILIZED OR CALL  AROUND FLAPS xx” GO-AROUND”  AUTO CALL OUTS AT 500’ AND 200’ RESPOND “CHECKED” FOR AUTOLAND VERIFY AFDS STATUS AT 500’ AGL. 100 ABOVE “APPROACING “CHECKED” MINIMUMS CALL MINIMUMS” LATEST BY MINIMUMS DISENGAGE A/P & A /THR (single channel appr) “CONTINUE” OR  AT MINIMUMS CALL “MINIMUMS” “GO-AROUND” GO AROUND AND MISSED APROACH PROCEDURE

 AT THE SAME TIME

1.PUSH TO/GA SW 2.MOVE THR/LVR FWD 3.CALL “FLAP15”

POSITION THE FLAP LVR TO 15

MONITOR FLAP RET

VERIFY ROTATION TO GO AROUND ATTITUDE VERIFY THRUST INCREASE.  ADJUST THRUST

 AS NEEDED*shouldn’t be at the cost of gear retraction

“+VE RATE” VERIFY ON ALT & CALL

“GEAR UP”

SELECT L/G UP

PF

PM VERIFY

IF AIRSPEED IN  AMBER BAND (Anytime below maneuver speed)

MISSED APPR ALT SET

LIMIT BANK ANGLE TO 15º  ABOVE 400’

CALL

HDG SEL / LNAV

SET / ENGAGE

HDG / LNAV

MONITOR MISSED APPROACH PATH LANDING ROLL PROCEDURE THRUST LEVERS VERIFY

CLOSE SPEED BRAKE LEVER UP

CALL

VERIFY CORRECT AUTOBRAKE OPERATION MOVE TO RELEASE WHEN BOTH REV REVERSE THRUST INTERLOCK.APPLY GREEN CALL  AS REQ IF NOT, CALL AS  APPROPRIATE CALL CALL BY 60KTS WHEN ENG AT REV IDLE BEFORE TAXI SPEED CALL IF AUTOLAND THRUST

SLOWLY REDUCE REV TO BE IDLE BY TAXI SPEED REV THRUST LVR FULL DOWN(STOW) USE MANUAL BRAKE / DISARM  AUTOBRAKE. “MANUAL BRAKES” DISENGAGE A/P BEFORE TURNING. IDLE / TAXI THRUST

SPEED BRK UP OR SPEED BRK NOT UP “REVERSERS NORMAL” “NO REVERSERS ENG NO –“ OR “NO REVERSERS” “AUTO BRAKE DISARM” “60KTS”

“900 MTS TO GO” “300 MTS TO GO”

CHRONO

ON for 3min cooling

 AFTER LANDING PROCEDURE WHEN CLEAR OF ACTIVE RWY  ACKNOWLEDGE AND CONFIRM TAXY INSTRUCTION ► MOVE OR VERIFY SPEED BRAKE ►SPEED BRAKE VERIFY DOWN► LEVER DOWN LEVER ► APU MAY BE STARTED AS REQ* TO BE  AVAILABLE BEFORE ENTERING GATE. PROBE HEAT SW AUTO  AS REQ / STROBE EXTERIOR LTS OFF WX RADAR OFF WX RADAR OFF

PF

PM  AUTO BRAKE SEL SW FLAPS

OFF UP

TRANSPONDER STBY / AS REQ TAXI INTO GATE BY CREW IN CAPT SEAT UNTIL SETTING PARK BRAKE AND VERIFY PARK BRAKE LIGHT ► “CABIN CREW DISARM SLIDES” ► ANNOUNCE ► ►ELEC ►ENG

START LEVERS

PWR

CUTOFF ►FASTEN

ESTABLISH GROUND CONTACT

WHEN CHOCKS IN PLACE FD SW

BELT SW

OFF

FUEL PUMPS

OFF

PARK BRK RELEASE CAB/ UTIL SW OFF

OFF

 ANTI COLL LT

IFE SEAT PWR SW

AS REQ AS REQ

WING ANTI ICE

OFF

ENG ANTI ICE

OFF

HYD PANEL RECIRCULATION FAN  AIR CON PACK SW

SET  AS REQ

ISOLATION VALVE

OPEN

AUTO

ENG BLEED

ON

 APU BLEED*

ON

EXTERIOR LT FD SW TRANSPONDER  APU CALL

SET►

AS REQ OFF STBY AS NEEDED

“ SHUTDOWN CHECKLIST” SECURE PROCEDURE

CALL

“ SECURE CHECKLIST”

IRS

OFF

EMER EXIT LTS

OFF

WINDOW HEAT

OFF

PACK SW

OFF

Training Notes: •

CABIN ALTITUDE WARNING exercise is seat specific.



Its “throttle hold” and not “thrust hold” ( FCTM )



In the previous fleet there was a requirement to call out “30 speed resting Climb Nav Blue one FD two…..” as part of instrument cross check This is NOT required in the current fleet, as Boeing procedures are designed differently and hence PFD and ND needs to be checked as described in SOP



For All NPAs as part of the procedure FAF altitude shall be set (even though the system capability may exist ) this is for standardization purpose so that irrespective of the type of guidance selected ( IAN , VNAV , V/S) the procedure ensures FAF alt is always set.



Similarly on VNAV approaches: Approaching FAF speed intervention shall be used to open the speed window. This again standardizes that; the speed window on MCP shall be open on final approach.

FLIGHT CREW TRAINING PROGRAM B-737

FCTP APPENDIX A SilkAir specific Approach types to be trained during Boeing Conversion training: Session title

Approach Type

Approach technique

FTD 7

RNAV GPS

LNAV / VNAV

FTD 9

VOR

LNAV / VNAV

FFS 2

RNAV GPS

IAN

FFS 3

VOR

V/S

FFS 4

LOC

LNAV / VNAV

FFS 5

LOC

V/S

FFS 6

VOR

LNAV / VNAV

FFS 6

NDB

V/S

FFS 6

RNAV GPS

LNAV / VNAV

FFS 8

VOR

V/S

In addition to the sessions above the training program includes ILS approaches, visual and circling approaches which are indicated in the lesson plans.

Rev 00 OCT 2013

FLIGHT CREW TRAINING PROGRAM B-737

FCTP APPENDIX B Table of di fferences:

Items SilkAir B737NG

BTC Simulator

1

Taxi tiller on both Captain and First officer side

Taxi tiller on Captain side only

The pilot in the right hand seat will practice taxiing during  Aircraft training and line consolidation flights with Instructor pilots

2

Engine start switch position decal is GND-AUTO-CONT-FLT

Engine start switch position decal is GND-OFFCONT-FLT

Ignition is available in AUTO posn. No change to procedure

3

Probe heat position decal  AUTO-ON

Probe heat position decal OFF-ON

PROBE Heating is available in auto posn No change to procedure

4

No Head Up Display (HUD)

Head Up Display (HUD)

Not used for training

5

No Class 3 EFB

No Class 3 EFB

Not used for training

6

No Auxiliary Fuel Tanks

No Auxiliary Fuel Tanks

Not used for training

7

Evac command Panel installed

No Evac command Panel

Instructor to brief crew that SilkAir aircraft are installed with EVAC command sw to be used after the Evacuation announcement

8

Printer installed on the  AFT electronic panel

Printer installed on the AFT electronic panel

Location of Transponder, trimmer etc are moved as a result of this. Crew shall familiarize during  Aircraft training and line consolidation flights

Rev 00 OCT 2013

Comment

B 737 SIMULATOR TRAINING

• •





 This is a task sharing tool.  This does not replac e official Boeing doc uments. Refer to FCTM 5.67-5.78, FC OM and Q RH  To be used a s a training aid for simulator prac tic e only. Manual raw d ata flying is enc ouraged during training to a c hieve proficienc y in: Scanning  Trimming handling   

• •

Referenc e WT of 65T used. Referenc e RWY : KMWH 32R

PF

PM SIM TRAINING GUIDE VISUAL CIRCUIT KMWH RWY 32R ROTATE + VE RATE

“L/G UP” 400 FT “HDG SEL”

SET RWY HDG 1000 FT

“ SET 180 KTS, FLAP 5 ” 180 kts is a good ref speed to cover all weights and minimizes heads down time. Once on downwind reduce to F5 speed “SET DW HDG, AFTER T/O CHECKS”

SET 180KTS SELECT / VERIFY F5, PERFORM AFTER T/O PROC SET DW HDG & PERFORM AFTER T/O CHKS

 ARR Page: RW 32R RW EXT 3 nm LEGS Page: REMOVE DISCONTINUTY DIR TO RX -32,INTC CRS 324 >   EXECUTE FIX Page: RW32   Insert: / 2.3 circle (to indicate circling area)   Insert: 234/ (to indicate ABM point)   Insert 054/ ( for FO circuit)  APP Page: Select VREF30/40  AUTO BRAKE SET* DO NOT SET FOR TOUCH & GO DOWN WIND • •

• • •



• •



“DES & APP CHKS”

“COMPLETED”

 A/P A/T & F/D OFF* anytime on down wind. (ref wt:65T: 6º ~ 60%)  ABEAM “CHK TIME”

3sec/100f t= 45 sec ± w.c. “10 sec to go”

“GEAR DN FLAP 15, SET RWY HDG” SEL GEAR&FLAP, SET HDG &SPD  ARM SPEED BRAKES* “TIME UP” DO NOT ARM FOR TOUCH&GO COMMENCE TURN 20º~25º Initially Shallow ROD to Allow Speed Reduction to F15 BASE LEG SEL FLAP CYCLE FD AND PERFORM LDG CHKS TARGET TO BE 3NM AT 900~1000 FT

“FLAP 30 / 40 LDG CHKS”

Typical A/C posit ion as seen on ND RX-32

Downwind Abeam Point

Base Leg Turni ng Final

CIRCLING APPROACH REFERENCE: FCOM SP 4.4 & 4.5 QRH MAN 2.8 FCTM 5.67-5.72 PF

PM VOR RWY 14L CIRCLE TO LAND RWY 32R THIS APPR FLOWN USING V/S MODES OF AFDS  ARRIVAL Page:   VOR14L LEGS Page: CLEAR ALL DISCONTINUITY MODFY 4000 A TO 4000 AT EPH DO NOT MODIFY ANY PIONTS BETWEEN EPH AND RWY FIX Page: • INSERT RW32R •  Insert: / 2.3 circle (to indicate circling area) Insert: 234/ (to indicate ABM point) Insert 054/ (for FO circuit)  APP Pag e: Select VREF30/40 • ENSURE LATEST BY 4NM b efor e FAF (EPH) •

• • •



  

   

AIRCRAFT IS AT F5 SPEED PITCH MODE: IS IN ALT HLD WITH V/S ARMED ROLL MODE: USE LNAV OR VOR/LOC ENSURE LATEST BY 2NM TO FAF

MCP SET MDA1800 (cannot set 1740) CALL“GEAR DOWN F15” SET F 15 SPEED ARM SPEED BRAKE  APPROX 0.2NM FAF

SEL GEAR AND FLAPS

SET V/S AS REQ 100 FT ABOVE MDA PRE SEL HDG 190º / 99º (CAPT/FO)

LOOK OUT FOR VISUAL CONTACT  AT MINIMUMS

VERIFY ALT HOLD VISUAL CONTACT PUSH HDG SEL ,SET MISSED APP ALT FLY TO THE EDGE OF THE CIRCLE STAY WITHIN CIRCLING AREA  ABEA M “TIME CHECK”

start turn “F30/40 LDG CHKS”

3sec/100f t= 18 sec Stay within circling area “TIME UP” SEL FLAP CYCLE FD AND PERFORM LDG CHKS

 AP & A/TH OFF  AIM FOR THE INNER EDGE OF RUNWAY WINGS LEVEL BY 300FT

Typical A/C posit ion as seen on ND

Downwi nd Abeam Point

Base Leg Turni ng Final

PF

PM

ENGINE FAILURE (NO DAMAGE) AFTER V1 (FCTM EXTRACT 8.9)  ANNOUNCE “ ENGINE FAIL” CANCEL CAUTION / BELL “ +VE RATE” “ GEAR UP” SILENTLY ASSESS FAILURE/ DAMAGE 400 FT “ HDG SEL” SELECT RWY HDG  ANNOUNCE “ENGINE No -- FAIL NO DAMAGE" “ CHECKED”  ABOVE 1000FT  A/C SPEED ABOVE ENSURE COMMAND SPEED IS “UP” RETRACT FLAP AS REQ “FLAP--” SELECT N1 PAGE ON FMC CALL FOR SUBSEQUENT FLAP RETRACTION AS REQ UNTIL “ FLAP UP” FLAPS UP NO LIGHTS SET ALTITUDE IF REQUIRED AND “ LEVEL CHANGE” LEVEL CHANGE “MCT” SEL CON ON N1 PAGE “ENGINE FAILURE NON NORMAL READ AND DO CHECKLIST AS GIVEN CHECKLIST” BELOW  AUTO THROTTLE “ DISENGAGE” “ DISENGAGED” “ THRUST LEVER NO --“ PLACE HAND ON THE FAILED LEVER AND  ANNOUNCE “ COFIRM NO—?“ VERIFY AND ANNOUNCE “ CONFIRM, CLOSE” SLOWLY MOVE THRUST LEVERS TO CLOSE AND ANNOUNCE “ CLOSE” “ START LEVER NO—CONFIRM CUT OFF?” “ CONFIRM” “ CUTOFF” ON COMPLETING THE REST OF THE ITEMS  ANNOUNCE ”ENGINE FAILURE CHECKLIST COMPLETED” “AFTER TAKE OFF CHECKLIST” PERFORM AFTER TAKEOFF CHECKS DECISION MAKING

PF

PM

ENGINE FIRE AFTER V1 (FCTM EXTRACT 8.9)  ANNOUNCE “ FIRE” CANCEL CAUTION / BELL “ +VE RATE” “ GEAR UP” SILENTLY ASSESS FAILURE/ DAMAGE 400 FT “ HDG SEL” SELECT RWY HDG DISCONNECT A/THR ANNOUNCE “ENGINE No −− FAIL " HOLD FAILED THR LVR & ANNOUNCE “ THRUST LEVER No—CONFIRM?” IF CORRECT ANNOUNCE “ CONFIRM” SLOWLY MOVE TO CLOSE AND  ANNOUNCE “ CLOSE” ONCE THRUST LEVERS ARE CLOSED PLACE HAND ON THE FAILED START LEVER AND ANNOUNCE “ START LEVER No—CONFIRM?” WHILE MAINTAINING A/C CONTROL ENSURE CORRECT START LEVER AND  ANNOUNCE “ CONFIRM” MOVE START LEVER TO CUT OFF AND  ANNOUNCE “ CUTOFF” PLACE HAND ON THE FIRE SWITCH AND  ANNOUNCE “ FIRE SWITCH NO—CONFIRM?” ENSURE CORRECT FIRE SWITCH AND  ANNOUNCE “ CONFIRM” PULL AND ROTATE TO STOP HOLD FOR 1 SEC ONCE BOTTLE DISCHARGE LIGHT ILLUMINATED CHECK TIME 30 SEC  ABOVE 1000FT  A/C SPEED ABOVE LOOK OUT FOR TIMING, IF FIRE SW STILL ILLUMINATED ROTATE TO THE OTHER STOP HOLD 1 SEC ENSURE COMMAND SPEED IS “UP” RETRACT FLAP AS REQ “FLAP--” SELECT N1 PAGE ON FMC CALL FOR SUBSEQUENT FLAP RETRACTION AS REQ UNTIL “ FLAP UP” FLAPS UP NO LIGHTS SET ALTITUDE IF REQUIRED AND “ LEVEL CHANGE” LEVEL CHANGE “MCT” SEL CON ON N1 PAGE PERFORM AND ANNOUNCE “ENGINE FIRE NON NORMAL CHECKLIST” “ENGINE FIRE NON NORMAL CHECKLIST COMPLETE” “AFTER TAKE OFF CHECKLIST” PERFORM AFTER TAKEOFF CHECKS DECISION MAKING

FFS 9 FC32 & RNAV Qualifi cation DAY SESSIONS Preflight quick start up by Instructor 1. Reject Takeoff: Engine Fail just before V1 2. Take off reposition FL350. High level stall clean configuration Auto pilot on 3. Over Speed: Auto pilot, Auto thrust off, Maintain CRZ thrust. Pitch down to 10º nose down overspeed MMO. Recover by reducing thrust and applying speedbrake 4. Rapid depressurization uncontrollable. Emergency descent 5. Base turn Stall with Gear down & F15 while vectors for ILS approach. 6. ILS approach Manual Go around on instruments 7. Reposition for No Flaps No Slats landing from 10 miles 8. Reposition No Flaps Landing from 10 miles 9. Takeoff One Engine Fire between V1&V2 10. Fire drill 11. Single Engine ILS Approach and Landing NIGHT SESSIONS 1. 2. 3. 4. 5.

Takeoff Engine Fail Between V1&V2 climb to circuit Visual circuit Single Engine Manual Flight Single Engine Visual Approach Manual Flight Single Engine G/A Manual Flight Single Engine ILS Approach &Landing

RNAV Qualification: 1. RNAV Approach from Intermediate fix Go around due Unable RNP message. 2. RNAV Approach from 10 miles Go around due No contact at Minima 3. RNAV Approach and Landing

FLIGHT CREW TRAINING PROGRAM B-737

FFS 9

FLIGHT CREW TRAINING PROGRAM

FFS 10

LOW VISIBILITY TRAINING

Objective: To ensure crew attains the required level of proficiency for CAT II approaches and low visibility taxi and take-off operations SilkAir B737 Aircrafts are equipped with a Fail-Operational Aut o land system.

Reference:   FCOM



o

Systems description Automatic flight Warning systems  

  FCTM



Approach and Missed approach OPS MANUAL VOL A Chapter 8 o All Weather Operations o





Sessi on data: WSSS RWY 02L / 20C; Winds: 110/05kts; Vis: varied according to the exercise. Temp / Dew: 25º / 25º; QNH: 1010 Hpa. GW: 65000 kg; Fuel: 10500kg; ZFW: 54500kg; Reserve: 4500kg; CI: 35; CG: 18%

>

FLIGHT CREW TRAINING PROGRAM B-737

CAPTAINS RHS T  Objective: To ensure crew attains the required level of proficiency for Right Hand Seat Operations.

Training Programs: For Line Captains: During the conversion training will carry out Right Hand Circuit without any failures. During the Base check will carry out one Right Hand Circuit without any failures and be Certified to fly as PM in the CM2 position

For LIP/IP: During the conversion training will carry out Right Hand Circuit with a V1 Cut, Single Engine Approach and Go‐Around, Single Engine Landing (A/THR and AP off) During the Base check will carry out Right Hand Circuit with a V1 Cut, Single Engine Approach and Go‐ Around, Single Engine Landing (A/THR and AP off) and be certified to fly as PF/PM in the CM2 position

FLIGHT CREW TRAINING PROGRAM

Low Visibility Training for pilots shall be categorized as follows PF in LHS ( Part A,B &C ) Captains PM in RHS ( Part D ) First Officers

PM in RHS ( Part A, B & C ) PF in LHS ( Part A & B )

Command trainees PM in LHS ( Part D ) PF in RHS ( Part A,B & C) Instructors(IP/LIP) PM in RHS ( Part D )

PART A - L OW VIS TAXI VIS

PHASE OF FLIGHT

INSTRUCTOR FACILITATION

100m

TAXI to Takeoff TAXI to Gate (at end of training session)

Provide guidance on procedures and precautions with regard to surface movement and safe taxi technique

PART B – LOW VIS TAKEOFFS VIS

PHASE OF FLIGHT

INSTRUCTOR FACILITATION

Between 400m 125m

TAKEOFF  – in reducing VIS

Set TOW 65 tons  Adjust RVR 400m reducing to 125m

125m

TAKEOFF  – Reject Takeoff (Low speed)

Engine failure at 60kt (RTO before V1)

125m

TAKEOFF  – Reject Takeoff (Hi Speed)

Engine failure at V1 minus 10kt (RTO before V1)

125m

TAKEOFF  – Engine Fail

Engine failure between V1 & V2

125m

TAKEOFF  – PF incapacitation  – PM takes over

PF subtle incapacitation above 100kts before V1

FLIGHT CREW TRAINING PROGRAM

PART C — CAT II APPROACHES, LANDINGS & GO-AROUNDS VIS

PHASE OF FLIGHT

INSTRUCTOR FACILITATION *

RVR 300m

Intro to LOW VIS Approaches  APPROACH (CAT II)  – 2 APs & ATHR DEMO  – Complete CAT II Briefing Checklist

Commence exercise from intercept HDG To LOC > 2500’ Freeze at 350’, 200’, 100’ & touchdown.  At each freeze POS; demonstrate the visual cues at each VIS selection & how seating position affects visibility.

300m

Complete an uninterrupted  AUTOLAND until exiting runway

 After DEMO REPOS 2000ft on final

300m

APPROACH (CAT II)  – ENGINE FAIL  – Continue with AUTOLAND

 Autopilot, CAT II, ILS approach Engine Failure Flaps 30 approach  AUTOLAND and ROLLOUT capable

300m

APPROACH ( CAT II )  – ENGINE FAIL  – Missed Approach procedure

ENGINE FAILURE (at 500 feet)

300m

APPROACH (CAT II)  – Missed Approach procedure

300m

APPROACH (CAT II)  – Missed Approach procedure

RUDDER DC FAIL (LAND 2 annunciation) continue Approach. At minimums NO CONTACT” Exercise complete SOURCE OFF (NO AUTOLAND annunciation - fail operational)

300m

APPROACH (CAT II)  – Missed Approach procedure.

LOC or G/S indicators flashing

PART D — PM TRNG FOR CAPTAIN (RHS), INSTRUCTOR (RHS) & CMD TRAINEES (LHS) VIS

PHASE OF FLIGHT

INSTRUCTOR FACILITATION *

300m

APPROACH (CAT II)  – 2 APs & ATHR  – Missed Approach procedure

Loss of visual reference below 50’

300m

Complete an uninterrupted  AUTOLAND until exiting runway

REPOS 12nm final

FLIGHT CREW TRAINING PROGRAM

CAT II APPROACH PREPARATION In addition to the normal approach preparation Start APU. The Commander should include the following for CAT II operations:

1.  Ai rc raf t: Review Auto flight limitations DDL / MEL / Technical log Aircraft STS review QRH required equipment list 2.  Ai rport : Check that the airport is in the list of approved CAT II airports Verify LVO in force Verify status of airfield facilities: ILS, Approach lights Verify RVR reported is adequate for the approach Verify braking action if reported is not poor. 3. Weather: Verify reported winds are within limits Verify no wind shear reported 4. Crew: Verify crew qualifications. Set seat position for correct eye level reference. Review PF / PM responsibilities and additional callouts. Set DH or RA if available in FMC. Review Runway turn-offs and expected taxi route Review additional ATC calls

FLIGHT CREW TRAINING PROGRAM

 AUTOL AND CAT II CA LL OUTS The Radio Altimeter (RA) shall be used for all call-outs, when conducting approaches in Low Visibility. The following call-outs are required in addition to standard call- outs CONDITION

CALLOUTS (PM)

RESPONSE (PF)

500ft AAL

LAND 2 / LAND 3 / NO AUTOLAND

CHECK / GO AROUND

50ft RA

FLARE / NO FLARE

If no ‘FLARE’, carry out a go-around.

30ft RA

RETARD / NO RETARD

If no ‘RETARD’, move thrust levers to idle.

 At Touchdown

ROLLOUT / NO ROLLOUT

If no ‘ROLLOUT’, disengage the autopilot and take over the directional control.

T The Commander is looking out during CAT II approaches, the callouts “visual” or “no contact” on reaching DH are replaced by “Landing” or “Go-Around” by the Commander.

LIST OF APPROVED AIRPORTS FOR LVO COUNTRY SINGAPORE

 APPROVED AIRPORTS CHANGI INTL DH100 / RVR 300M

Note: Refer INTAM for updated list

FLIGHT CREW TRAINING PROGRAM

REQUIRED EQUIPMENT FOR CAT II

EQUIPMENT REQUIRED

CAT II

 Autopilot

2

 Autopilot Disconnect Switch

2

 Autopilot Disengaged Warning System (Aural)

1

 APP Switch

1

TO/GA Switch

1

Low Range Radio Altimeter and Display

2

Decision Height (DH) Display (RA)

2

Windshield Wiper

2

ILS Receiver and Display

2

Flight Mode Annunciator

2

 ADIRU in NAV Mode

2

Hydraulic System

2

PFD

2

FLIGHT CREW TRAINING PROGRAM B-737

FLIGHT CREW TRAINING PROGRAM B-737

RNP APCH CREW BRIEFING TOOL In addition to the normal descent and arrival briefing, the PF/PM should complete the following RNP APCH operations checklist review. Please note that RNP APCH operation is variously referred to in Jeppesen charts as: • RNAV (GNSS) Approach, • GPS Approach, • RNAV (RNP) Approach • RNAV Approach Note 1: All the above terms are collectively known as RNP APCH in ICAO terminology. Note 2: SilkAir is not authorized to conduct RNP AR (Authorization Required). Note 3: SilkAir is approved to conduct RNP APCH with APV BaroVNAV down to LNAV / VNAV minima. RNP APCH CREW BRIEFING TOOL RNP APCH Approach checklist: (To be reviewed by both PF and PM) 1.

RNP APCH QUALIFICATION ........................COMPLETED

2.

AIRCRAFT STATUS ......................................... REVIEWED

3.

APPROACH CHART......................................... REVIEWED

4.

APPROACH PROC IN FMC ............................. REVIEWED

Check that RNP APCH procedure in FMC agrees with the published chart procedure. Crew are not allowed to modify any part of the RNP APCH procedure drawn from the FMS database. ATC “direct-to” clearances can be accepted up to the Intermediate Fix (IF) provided the track change at the IF does not exceed 45º 5.

SYSTEM REQUIREMENT ................................

6.

MINIMAS* ........................................................... SET

7.

MISSED APPROACH PROCEDURES .............

8.

ATC CLEARANCE FOR RNP APCH ..........................OBTAINED

10.

APPROACH RNP VALUE (0.3) ........

11.

REVIEWED REVIEWED CHECK DISPLAYED

For missed approach procedures based on conventional aids (VOR, NDB) – ensure that the

appropriate ground aids required are operational and tuned. *Note:

For approaches down to LNAV minima, set published MDA + 50ft. For approaches down to

LNAV / VNAV minima, set published DA.

FLIGHT CREW TRAINING PROGRAM B-737

REQUIRED EQUIPMENT FOR RNAV 1 / 2 AND RNP APCH PROCEDURES

Equipment

FMC CDU  ADIRU GPS Receiver VOR & DME FD PFD ND Navigation Database Flight Plan on ND  AP  A/THR GPWS / TAWS

Procedure RNAV 1 / 2 RNP APCH 1 2 1 2 1 1 1 2 1 (if required for 1 (if required for FM FM update and/or update and/or if if required for the required for the procedure) procedure) 1 2 1 2 2 2

Must be updated

Must be updated

Must be displayed on both 1 0 0

Must be displayed on both 1 1 1*

Note: 1. AP must be used during both the procedures. 2. RNP APCH is permitted only at WGS 84 compliant airports. 3. * GPWS / TAWS must be operative when in IMC or night conditions.

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