Instructor's Corner Airbus A 320 Puc Go - Voo Simulado e Inglês Técnico Reinaldo Del Fiaco

PONTIFÍCIA UNIVERSIDADE CATÓLICA DE GOIÁS

REINALDO MOREIRA MOREI RA DEL FIACO

INSTRUCTOR CORNER: MANUAL OF STANDARTS AND OPERATION O PERATION OF O F AIRB AIRBUS US A320 A320 ENGLISH CLASSES

GOIÂNIA 2014

MASTERMIND Prof. Msc. Rodrigo Braz Muniz RESEARCH REINALDO MOREIRA MOR EIRA DEL FIACO

INSTRUCTOR CORNER: CORN ER: MANUAL DE PADRONIZAÇÃO PADRONIZAÇÃO E OPERAÇÃO DE VOO SIMULADO

GOIÂNIA 2014 The following Instructor Corner refers the operation and standarts of AIRBUS A320, being prepared based in manuals FCOM e AFM of AIRBUS INDUSTRIE; MEL and QRH of AIR ASIA; SOP of TAM TAM Linhas Aéreas; Instructor Corner, Corner, Miscellaneous, Flight Patterns and Systems Systems of the homepage Smartcockpit; and in base of CBT displayed during the Flight Simulator Classes 2012/2. TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

SUMMARY PRELIMINARY COCKPIT PREPARATION.............................................................................4 F M G S P R E P A R A T I O N . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. .. . . . . 5 BEFORE TAKE OFF & CLEAR FOR TAKE OFF.............................................................................7 T A X I L I M I T A I O N . . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . .. .. . . . . . . 8 TAKE OF F.............................................................................9 AFTER TAKE OFF & CLIMB.............................................................................12 D E S C E N T & A P P R O A C H . . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . .. .. 1 2 ILS LANDING.............................................................................13 LANDING & AFTER LANDING.............................................................................15 PILOT INCAPACITATION............................... ..............................................15 G O A R O U N D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . 1 6 PARK IN G & SEC URI NG ACF T........ ............... ............... ............... .............. ............... ............... ............... ............... ............... ..........17 ..17 REFERENCE.............................................................................18

LIST OF IMAGES IMAGE IMAG E 1: IMAG IM AGE E 2: IMAGE IMA GE 3: IMAGE IMA GE 4: IMAGE IMA GE 5: IMAGE 6: IMAGE 7: IMAG IM AGE E 8: I M A G E 9: IMAGE 10 10:: IMAG IM AGE E 11: IMAGE IMA GE 12 12:: IMAG IM AGE E 13: I M A GE 14: I M AG E 15: IMAGE IMA GE 16 16:: IMAGE 17 17:: IMAGE 18: IMAGE IMA GE 19: IMAGE IMA GE 20: IMAGE 21 21:: IMAGE 22 22:: IMAGE 23: IMA IM AGE 24: IMAGE 25 25:: I M A G E 26: IMAG IM AGE E 27:

A320 CO CK PI T.. T..................................................... ................................................... ........................4 .......... ..............4 A320 PE DE STAL............................................... ............. .................4 A320 OV ER HE AD .............. .............. .............. .............. .............. .......4 FM GS FUEL PAGE..................................... PAGE................................................................. ........................................5 ............5 FM GS PE RF. PAGE.................... PAGE.................................... ................................ ............................... .........................5 ..........5 FMG S KEYB OAR D DATA.. DATA........... ................. ................. ................. ................. ................. ................. ................. ...............5 .......5 FM GS PE RF. PAGE IN IT.......................... IT...................................................................... ...................................................5 .......5 AF TE R START............. ........... .......... ........... ........... .......... ..........5 IG N. START............. .......... .......... ........... .......... .......... ........... ..6 T.O. CON FI GUR ATI ON.............................................................. ON.............................................................................7 ...............7 BEFO BE FORE RE TAKEO TAKEOFF FF CHE CHECK CKLI LIST.............. ST.................................... ............................................ .........................................7 ...................7 TAXI INI TI ATI ON...... .................................. .................................. ...8 LAD IN G LI GHT S...................... S....................................... .................................. .................................. .....................8 ....8 Side stic k...... ....... ....... ....... ........ ....... ....... ....... ........ ....... ......9 Ste eri ng.. .... ..... .... ..... .... ..... ..... ..... .... ..... .... ..... ..... ..... .... ..... .9 Steering ECA M Action................................... Action................................................... ................................ ..........................9 ..........9 Sidesti ck EC AM Action... ........................ ....................... ........................ ...9 Takeoff and Bank Angle. .......... ........... .......... ........... ........... .......... ........... ..10 After Takeoff Takeoff and Climb Phase................................................. Phase..................................................................... ............................10 ........10 After Takeoff Takeoff and Climb Phase.......................................................... Phase.............................................................................1 ...................11 1 Active Apphoach Phase................................................. ............................12 Landin g Config uratio n......... ............ ............ ............ ............ ............ ........13 Performance Perform ance Page/Ap Page/Approach... proach... .......................... .......................... ......................1 4 Final Appro ach................................................ .............................14 Primary Flight Display................... Display................... ...................... ...................... ..............16 Go Around... ......................... ......................... ........................1 6 Enabl e ALTN. ........ ........ ........ ........ ........ ........ ........ ........ ........ ....16

English Classes  Instructor Corner Airbus A320

Preliminary cockpit preparation

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- The Captain and the First Officer are responsable by yours respectives areas in the glareshield and yours position sides in the cockpit;  - However the PF (Pilot Fly) is the responsable to prepair the primordials instrument of navigation navigatio n and operation of acft as fill FMG FMGS, S, configuration of Overhead, Overhead, FCU F CU (Flight Control Unit), ECAM and pedestal;  - The check of overhead must be from left to right and upward, following the details in the  picture;  - In pedestal the check must be be downward keepong observing from left to right; - The numbers in the side show the sequence of check to be follow  by PF during the Preliminary Cockpit Preparation;  - The CAPT. should check the QHR - QUICK REFE RENCE HANDBOO HAN DBOOK K and obtain obtain the navigation chapter in the correct sequence of use.

CMTE PF First Officer 

IMAGE 1: A320 COCKPIT (AVSOFT, 2009).

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The pedestal, overhead and checks of some safety items are responsability responsabi lity of P F, how should follow the AIRB US A320 check-list with the airline;

ENG Masters.....Check off  ENG MODE SEL.....Check Norm L/G lever.....Check Down

IMAGE 2: A320 PEDESTAL (AVSOFT, 2009).

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Wipers.....OFF BAT.....CHECK/AUTO EXT PWR.....ON APU FIRE.....CHECK/TEST APU.....START *COCKPIT LIGHTS.....AS RQST

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Parking brake.....ON ACCU/BRAKES PRESS.....CHECK  ALTN AL TN BRAKIN BRAKING.. G.....CHECK  ...CHECK  FLAPS.....CHECK POSITION SPEED BRAKE LEVERS.....CHECK RET

TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

IMAGE 3: A320 OVERHEAD (AVSOFT, 2009).

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PROBE/WDW HET.. HET.....AUTO ...AUTO APU BLEED....ON AIR COND PANEL.....SET ELEC PANEL.....CHECK  VENT PANEL

 Airbus A320 RECALL L ..........……………… ..........……………………….... ……….......PRESS ...PRESS 5 *ECAM RECAL

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6 EMER EQPT ........………....CHECK  C/B panels ............……..….CHECK  *EXT.W *EXT .WALKA ALKAROUND ROUND ...PERFORM

*ECAM OXY PRES S/HYD QTY/ENG OIL QTY...CHECK  QTY...CHECK 

Continuing the Cockpit Preparation Check-list we have Take off Briefing and FM FMGS GS Preparation. Take off briefing: - Consulting the Metar, TAF, TAF, NOTAM, MEL, M EL, CDL, C DL, Use the anti-ice, radar meteorological; meteorolog ical; - Briefing Briefing the cartas de pátio (caso esteja disponíve disponívell no AD de partida) partida),, ADC e SID; - Estar ciente das condições de motor, motor, manutenção da ACFT e da taxa de DE G; 

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2 BLOCK

TOW

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FMGS  preparation in INT Page, seguindo em ordem as LSKs

LW EXTRA/TIME

- The DEG (degradation) rate of fuselage is between 0.1 and 10.0, 0.1 is considered a new airplane and 10.0 to an aircraft out of conditions to flight. - The The INIT INI T B and and PERF PER F PAGE must be fill after the Operational Weight and Fuel Weight be confirmed.

IMAGE 4: FMGS FUEL PAGE (AVSOFT, 2009).

F/PLN - Adjust the RWY and the  SID; - Check in FMA the altitude target (blue);

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5

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ENGINE FAILURE - Before V1: CAPT stop the A/C F/O monitors DECEL e REV; - After V1: Continue TK off. 

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PERF T/O

The i nput dadas fulfilled in PERF Page are put inserted in FMA FM A and in ECAM;

IMAGE 5: FMGS PERF. PAGE (AVSOFT, 2009).

FMG S Preparation FMGS Preparation - The correct ordem to input navigation datas in FMGS is:  N a v i g a t i o n D AT A a n d a f t e r Performance DATA, each one witch yours function following the navigation key in the FMGS painel; - As in a Normal Check-list, the PF should keep the right ordem to fill navigation datas, and this order is described on the image. 

IMAGE 6: FMGS KEYBOARD DATA (AVSOFT, 2009).

3 In some flight simulator simulator functions like SEC F-PLA F-PLAN N A or B can be validated, if the AIRAC’s Frequency are wrong compared to that used by the simulator, simul ator, the frequency can be adjusted in RAD NA N AV, and can be check in VOR page, fix, ILS or other in F-PLA F-PLAN, N, if you you prefer the frequency frequency can be adjusted in DIR DI R page during the flight. TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

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IMAGE 7: FMGS PERF. PAGE INIT (AVSOFT, 2009).

 Airbus A320

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Before Start

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During Before Start Operation, have a sequence of checks and procedures to do, the procedure must be standart, following with caution and fulfilling fulfill ing the check list by the PF and PNF, PN F, in this topic we will see the check-list in a diferrent view, detailing the procedure to each pilot. The Before Star Check-list is divided in Before Start and Automatic Engine Star Sequence.

PF

PNF

1 Before Star 

LOADSHEET……………..………………….CHECK  COCKP IT DOOR………..… DOOR………..………… ……………… ……….CLOSED .CLOSED

PF

2 Automatic Engine Star Sequence ENG MODE SEL....... SEL............. .......IGN/START .IGN/START BLEED PRESSURE…...…CHECK  ANNOUNCE…...”STARTING ENGINE 2” MASTER SW 2….......…….ON 2….......…….ON

TAKEOFF DATA..…ENTER/REVI DATA..…ENTER/REVI SE

TAKEOFF DA DATA. TA....…XCHECK  ...…XCHECK  SEAT BELTS……………… BELTS…………………………… ……………….ADJ ….ADJ UST MCDU……...PERF TO  

MCDU……….F-PLN EXT PWR……..OFF

BEFOR E START down to the line..…PERFORM line..…PERFORM Confirm any take off limi-

ANNOUN CE….”BEFORE START C/L down to the line COMP LET ED”

tation;

START VALVE VALVE OP ENS  N2 INCRE IN CRE ASE ASES S IGNITER  FUEL FLOW EGT  N1 OIL PRESS START VALVE VALVE CL OSE • 50% N2 CFM • 43% N2 IAE - ENG IDLE PARAMETERS...CHECK NORMAL - ANNOUNCE..........”STARTING ANNOUNCE..........”STARTING ENG INE 1” - REPEAT START START SEQUEN CE FOR EN G 1...

Ask for external power disconection

After Before Before Start procedure proceduress the PF must ask to PNF the read of Before Start Check-list, the PNF will ask item by item with their PF answer, an swer, if something be out of standart the check-list must be redone. The same has to happen after engine start, and the PF will ask to PN F to reed the AFTER AFTE R Start Checklist. Checklist. 

AFTER STAR START T

PF

PNF

ENG MODE SEL..........…NORM End of START sequence : Signal for PN F actions

IMAGE 9: IGN. START (AVSOFT, 2009). 2009).

1. GND S PLRS………… PLRS……………ARM …ARM 2. RUD TRIM………RESET 3. FLAPS….....………SET 4. PITC H TRI M……… M……………. ……..SET .SET ENG ANTI ICE…… ICE………AS …AS RQRD WING ANTI ICE……..AS RQRD 6. APU MASTER SW………OFF Overhead and  Pedestal

APU BLEED…........ BLEED…............. ......….OFF .….OFF ECAM STA STATUS………CHECK  TUS………CHECK  ECAM DOOR PAGE….CHECK  ANNOUNCE..........…”CLEAR TO DISCONNECT” TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

IMAG E 8: AFTER START (AVSOFT, 2009).

 Airbus 320 After the PF check the doors and announce the plane can be desconnected in gate or finger, the PF and the PNF continue the follow the After Start Check-list, figure beside, but before antes observe in ECAM the conditions of engine, ground spoilers, warning tie belts and smoke, parking break and TCAS, after 2 (two) minutes should appear in the same windows in ECAM MEMO the following topics as in the figura bellow, and after this check, the the PNF P NF has obtain free push back and the CAPT. assume the acft taxi until the take of line.

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PF

PN F

 NW ST RG D ISC M EMO....... ........CHE CK  PUSHBACK/START CLEARANCE…….   ….OBTAIN WINDOWS and DO ORS………... ORS……….......... ............... ........ CHECK CLOSED WINDOWS…………..…CHECK 

THR LEVER S……. S……...... .........… ....….IDLE .IDLE BEACON………………..……ON PARKING BRAKE ACCU PR ESS…....... ESS…......... ..   …...CHECK 

PARKI NG BRAKE…........ BRAKE….........….ON .….ON ORDER…...................................................... .”BEF ORE START C/L below the line” GROUND CREW COMMUNICATION…   ESTABLISH

When PARKIN PARKIN G BRAK E is ON:  brake pressure is shown PARK BRK MEMO is displayed

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If the acft moves despite of   PARKING BRK ON,  immediately release PARKI NG BR K handle to to restore pedals braking. ANNOUNCE.............…… .....‘‘BEFORE START C/L   COMPLETE”

Before Take Take OFF O FF & Clear for Take Take OFF O FF

IMAG E 10: T.O. CONFI GURATION (AVSOFT, 2009).

The AIRBU S’ philosophy philosophy of of flight consists in dark cookpit to indicate that no failures in operation, new commands and inputs & outputs are represented in form of light warmings in FMA, EC AM or inparts of overhead, as in the picture above after the pilot press the TO PB and no one blue sing must appear in ECAM.

(The Before Take OF OFF F and Clear for Take OF OFF F CheckChecklist are based from SOP - Standard Operating Procedure of TAM Linhas Aéreas). Aéreas).

- Do the Cleared for Take Take Off Check-list to receive the authorization auth orization to join in runway; runway ; - If chance the runway in use during the taxi, the CM2 should recalculate the weights limiting of take of performance values, entering this value in FMGS, checking the items described in Runway Change Check-list. Check-list. Should be check and analyzed by both (CM1 and CM2):  - FMGS: F-PLN F-P LN Page: Runway, SI SID D their, Constraints of speed and altitude; RADN RA DNA AV Page: Navigation Aid Frequency; PERF PER F Page: Runway Runway,, Speeds, (TO SHI SHIFT FT if applicable applicable), ), Flaps/THS and Flex TO Temp.

PF

PNF

SEL............ ....... AS RQR D APP PA PATH CLE AR OF TRA FFIC.. MODE SEL.......   ..CHECK  The ignition is necessary in case of rain and/or wet runway. EXT LIGH TS...... TS........... ...........SET ......SET STROBE LIGHT ..........ON  NOS E SW ................TO  Note: Is is need the ACFT hold in the runway waiting the clearence to take of, RWY TURNOFF SW....... ON lights should extanded to OFF position LAND SW .....................ON and extanded to ON after obtain the PACK 1+2.................. AS RQRD clearence to start take of. The Strobe Light BRAKE FANS........CHECK OFF and the LANDING LIGHTS should be CABI N CREW.. CREW........ ........... .......ADVI ..ADVI SE CLEA RED FOR TAKEOF F C/L .. .... CALL

- During the taxi the wind speed must  be ob se rv ed co mp mpar ar in g th e ai airc rc ra ft limitation;  - If have delay during taxi the First Office should recalculate the fuel and check the news informations informations in FMC. F MC.

turn on when cross the wait line to runway. “Crew, ready for takeoff”

CLEARED FOR TAKEOFF C/L..   ..........READ

IMAGE 11: BEFORE TAKEOFF CHECKLIST (AVSOFT (AVSOFT,, 2009). TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

 Airbus 320 After the Cleared for Take OF OFF F operational rotine will done, the PF P F will ask for read the Cleared for f or Take Take Off Check-list, when done, the ACFT should join in RWY and start the running to take of, after execute the Before TAKE TAKE OFF procedure.

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 Taxi Initiation

The straight taxi in A320 must must be until 30 kt and in turne must be in 10 kt, and with dirty or wet taxiway the taxi speed is the half of speeds above. The The turn is made until 180°, the taxiway must have at least 75 ft side lenght.

PF When Taxi clearance obtained:  NOSE  NOS E LIG HT..….. HT..…............. .................…T ......…TAXI AXI PARKING BRAKE..……............OFF THRUST LEVERS….... LEVERS…........AS ....AS RQRD

7  A320

NORMAL CHECKLIST  

04-JAN-2010

CLEARED FOR TAKEOFF CABIN CREW..............ADVISED ENG MODE MO DE SEL........AS SEL........AS RQRD PACK ACKS...... S............ ............ ........... ......AS .AS RQRD BRAKE BRA KE FAN... FAN......... ........... .......OFF ..OFF RADAR &TERRAIN ON ND..ON

During the taxi must be review the takeoff briefings and ckecked headings and couses to after takeoff, as well as warnings for crew, tire  pressure  pres sure and brak brakes es temp temperat erature, ure, and our respectives temperatures which must be constantly Before Taxiing:  NW ST RG D ISC.......….C HEC HECK K monitored. In the hold point, the fuel not displayed on right flow and operating minima should ECAM MEMO  be reviwed.

PNF

TAXI C LEARAN CE..... CE.........OBT ....OBTAIN AIN ELAPSED TIME ........…AS RQRD

ANNOUN CE….. CE…..‘‘‘BRAKE CHECK’’ BRAKE PRESSURE..... CHECK ZERO

BRAKE PEDAL…..............…PRESS FLT CT L……......... L…….................... ...........…CHEC …CHEC K 

ANNOUNC....”PRESSURE ZERO” FLT CTL….......................…CHECK 

 ATC CLEARAN CLE ARAN CE…….......CO CE…….......CONFI NFIRM RM

FCU ALT….............…...CHECK  If ATC ATC requests to maintain runway heading or in case of a radar vector procedure : HDG……..............................SET

TERR ON ND……............. ND……...............AS ..AS RQRD 1. RADAR / PWS……........ON PWS……........ON / AUTO 2. ATC…............................………..SET 3. AUTOBRAK E………. E………...... .......... .......…MAX ..…MAX 4. T/O CONFIG…….................PRESS

FLIGHT INSTRUMENTS…....CHECK 

5. T/O T/O MEMO….….CHECK NO BLU E

T/O BRIEFING…....CONFIRM IMAGE 12: TAXI TAXI INIT IATION (AVSOFT, 2009).

PF

PNF

150°C……. APPROACH PATH CLEAR OF BRAKE T EMP BELO W 150°C…….   CHECK  TRAFFIC.…CHECK 

CABIN CREW…… CREW…….ADVISE .ADVISE EXTERIOR LIGHTS…… LIGHTS……..SET ..SET SLIDING TABLE……...STOW

BRAKE FANS………OFF TAKE OFF/LINE UP CLEARANCE…   OBTAIN

By joining track and CMTE CMT E Copilot should check the magnetic heading of the runway, and advertising Checked.  Note: In the PS PSS S simulators Brake & FANS and RADAR TERRAIN not work. 

ENGINE MODE SEL....AS RQRD TCAS…..TA or TA/RA PACKS 1 + 2…….AS RQRD SLIDING TABLE…..STOW

TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

IMAGE 13: LANDING LIGHTS (A (AVSOFT, VSOFT, 2009). 2009).

 Airbus 320

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During the TAXI some controls checks shall be done in the sidestick and in steering; - In sidestick: The check is to move sidestick to up and to down, and to right and left side, folowing the movings in ECAM and saying: FUL FULL L UP UP,, FUL FULL L DOW DOWN, N, NEU NEUTRAL, TRAL, FULL LEFT, FULL RIGHT AND NEUTRAL; - In stering: press the botton in the middle, and move to right and left side, following the moves in ECAM and saying FULL LEFT, FULL RIGHT & NEUTRAL.

IMAGE 15: Steering (AVSOFT, 2009).

IMAG E 14: Sidestick (AVSOFT, 2009).

In the taxi, can have some changes in data configuration configura tion inputed inputed in FMCDU, FMCDU , a cross-check cross-check is necessary between FMCDU and Navigation Instruments, Instrume nts, EFI S and FCU, and and stand by instruments. 

Take Off  Of f 

After enter with the aircraft in the runway, the Captain can ‘‘scan flow’’ the equipments, buttons, windows, from left to right side, from up to down, cheking if the others buttons and check-list itens, to a safety take off and standart. The main itens sho uld  be said aloud.

IMAGE 17: Sidestick ECAM Action (AVSOFT, 2009). 2009).

The commander must keep on hand in the Steering Steer ing Tiller since the beginning of the maneuver until stabilization of engines to 1.05 EPR or 50% N1 in order to avoid a  possible loss of control due to engine power asymmetry in the initial stage of the takeoff . The commander will be responsible for adjusting the  power for takeoff and must  After aligning the aircraft on runway PF remain with the hand levers should check the runway heading on the compass and the FMA F MA as letter. In case to the V1. of runway on the other side of the After stabilization of the headboard has ILS, appeared in the FMA engines and the actual start of yaw bar that indicated the central alignment of the runway that aircraft the takeoff roll, PF (CM1 should follow.

and CM2) use the Sidestick as described in FCTM. It is also recommended to avoid potential problems of directional control during durin g alignment, the engines are brought to the initial power settin g ONL ON LY AFTER THE AIRCRAFT ALIGNMENT WITH THE AXIS OF THE ROAD. During takeoff until the FL 100 to be a care situation estremo after takeoff pilots should TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

 .    )    9    0    0    2  ,    T    F    O    S    V    A    (   n   o    i    t   c    A    M    A    C    E   g   n    i   r   e   e    t    S   :    6    1    E    G    A    M    I

 Airbus 320

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remain HEAD HE AD DOW D OWN, N, observing the indications of the instruments, in the race for takeoff eg pop should observe the speeds like 80 and KT 100 kt what are the speeds speeds of IES CHEC CHECK K POWER PO WER CHEC C HECK K and after those speeds should observe the arrival of the aircraft a ircraft in its goal of V1, VR and a nd V2 + 10 for the ascent of the  plane and cleaning. c leaning. In addition a ddition to the th e indication of the speeds spe eds of the motors on the th e ECAM EC AM instruments must be observed and measured to check the MI NUM NUMUS US when the minimum power power required to TKO FF. In navigational instruments a cross-check, cross-c heck, and reported aloud by two pilots should be done. - If the plane is light, and in case of dirty or wet runway can take off with the APU ON; - During takeoff up to 80 kts must use the steering after must be corrected with the pedals in case of ILS on the other bedside PF can observe the alignment of the aircraft in yaw roll in indicating direction and heading in the FMA;

- In the operations and the standards of the Cmte and the first official training, both should have high awareness of operational aircraft,  being ready for any malfunction and  perform the procedures as stated in the briefing takeoff; - An example of takeoff briefing for

IMAG E 18: Takeoff and Bank Angle (AVSOFT, (AVSOFT, 2009).

 bedside 32 SB SBGO: GO: 'We will make a standard bedside 32 takeoff flap with conf ... our wind 07 to 140 kt, our velocities are V1 V2 ... ... ... VR, rising up to the authorized level .. ., our speed cleaning of aircraft is ... in any case of abnormality should said loud and clear, minimum or maximum operating  paa r a m e t e r s e x c e e d e d i n e n g i n e s o r  p obstacles on the track will abort our takeoff  below 100 kt above 100 kt with fire in motorcycles, windshield and operational

The message retraction lever toga or MCT / FLEX TO appears on the FMA in its first quadrant of the trust level and FMGS the page should be changed to TKOFF CLI MB according to next figure>>>>> TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

IMAGE 19: After Takeoff Takeoff and Climb Phase (AVSOFT, 2009).

 Airbus 320 - After the authorization of descent should be selected on FCU, FC U, T / D descent must be made with 50 ft of reason with the ramp-down; - During the descent should be monitored and given letters of descent with those those at the base date of FM CDU; - The frequency of the VOR / DME radios should be  placed in orbit in case of direct removal; - The weather data should should be adjusted in FMCD F MCDU U pages of PERF and F-PLN; - In case of change of lane changes needed to be made in FMCDU and conferred on EFIS, in case of not landing a  precision V-DE -DEV V and VAP APP P should be calculated by the PN PNF. F. - The descent may be made in various parts depending on the attitudes authorized by ATC, ATC, since the procedures proced ures cabin is divided into four parts, preparation of descent - as described on the previous page - procedures for descent desce nt / descent (sidebar), downhill FL F L 100 and after the descent phase or end. - The order of the procedures described in sop TAM, are outlined in the figure below; In case of decrease in the mountainous region NAV displays should be firing on the TERRAIN ON ND P N F a n d P F i n R A D A R  

B E F O R E T H E  A P P R O A C H c h e c k l i s t should be done when overcome TA and pursue orders as in the table below.

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PF

PNF

ENG ANTI ICE.......AS RQRD

CSTR P/B ............. ............... .. AS RQRD

CSTR P/B ............AS ............AS RQ RD

ANNOUNCE….. CHECKED”

     ’      ’

DESCENT..................INITIATE MCDU....................... F-PLN ANNOUNC E ...... ............. ..............FMA .......FMA  NPA APPR US E.......... PR OG

 Note: The engine anti-ice anti-ice MCDU preferabl preferably.. y..... ... PROG / must be ON during all PERF DESC DESCENT.............. MONI TOR  DESCENT.............. SPD B RK........ RK.............. ........AS ..AS RQR D RADAR TILT. TILT........ ........... .... ADJUST

 Não se usa o AUTO BRE AK MAX para pouso, o LOW é usado para pouso em RWYs extensas e MED para pistas curtas.

ground and flight operations when icing conditions exist or are anticipared. During climb, cruise or descent and ice temperature is below - 40° C S AT the engine anti-ice must be ON.

BEFORE APPROACH BRIEFING..............CONFIRMED RWY C OND......... OND.............. .......DRY/WET ..DRY/WET IAL MISSED APPR.......REVIEW V. BUG S...... S........... .......... ..........SET(B .....SET(B OTH) SEAT BELTS............................ON BARO/MDA/DH........SET(BOTH) ENG M ODE S EL ..... ........ ....AS .AS RQ RD AUTOBRAKE..............AS RQRD

- Before reading Before the Approach checklist approach briefing should be done, the PF should notify their intention to pop that will have to remain attentive to the instructions, should take into account weather conditions, review the type of aircraft, technical status , RTA,  NO  N O TA TAM M ap ro nt os am on g others, comment on the computation landing card, then present the cards to be used and specify the  procedures to be performed, continue reading and comment FMGS lateral and vertical navigation using the

cards and the ND in PL AN / CSTR C STR function to display display the altitude altitude and speed constraints, as well as the projected path, MSA, significant elevations. Also review the procedure and the sequence to be followed in case of rush, highlighting the items that mark the steady approxi-mation.

TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

IMAG E 20: Active Apphoach Phase (AVSOFT, 2009).

 Airbus 320

10

uncertainty also our takeoff ta keoff is aborted, above V1 proceed with takeoff and in case of fail ure will continue as flight emergency plan in case ca se of failure of the commands command s will be with me and asked if you help h elp me with  phony check list and, (if the first officer is PF he should speak in case of crash commands are real and if requested will help you a check list and telephony).



After Take Off & Climb

- After the rise of the aircraft and its cleanliness must be cum-ply with with the AFTER AFTE R TO / CLIMB CHECK LIST as described in the figure below checklist TAM; - Inside the terminal and in the critical phases of the flight the pilots were to remain head down, after leaving the TMA, the PNF should fill the fixed navigation and PF constantl constantly y review the route to be flown; - When crossing FL290 check the altimeters to enter RVSM airspace.

 AFTE  AF TER R T.O./C T.O./CLI LIMB MB

- At any stage of the flight, the PNF will announce "ONE THOUS TH OUSAND AND TO GO" before passing passing 1000ft altitude or authorized FL (ALT's that were selected in LDG GEA GEAR...... R........... .......... .......UP ..UP FLAPS.....................RETRACTED FCU), respond to what the PF "CHECKED".

PACKS....................ON MEMO..................REVIEW BARO REF..............SET(BOTH) 

Descent & Approach

- The preparation of descent must be made with 80 or 15 minutes of of the MN T / D (TOP OF DESC D ESCENT); ENT); - During descent descent PF should remain HEAD HEA D DOWN, DO WN, and pop should try to stay with the conditions of the aircraft and do the calculations for navigation, landing and fill LANDING DATE. - Pop tb should shou ld seek data from f rom ATI ATIS S and ATC ATC units. un its.

PF

PNF

LDG ELEV AUTO on CRUISE   page…..........................CHECK 

LANDIN G DATA .......….OBTAIN .......….OBTAIN

FMGS……………...PREPARE

DESCENT CLEARANCE ......…OBTAIN

FMGS ......…..………...CHECK 

............………....AS RQRD APPR BRIEFING...... PERFORM ANTI I CE ............………....AS

AUTO BRAKE….…AS RQRD When new ATC ATC clearance : F L 80 FCU ALT……SET and MANAGE SPEEDBRAKES .…....AS RQRD RADAR TILT…………ADJUST TERR ON ND ……..AS RQRD MCDU ……….…… ……….……………….F-PLN ………….F-PLN DESCENT CLEARANCE...........OBTAIN

- At start of the descent pilots must observe the arrival of the aircraft in the T / D plus the speed of the pink dot V-DEV,  both the PF PFD. D. IMAGE 21: Landing Configuration (AVSOFT, 2009).

TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

 Airbus 320 

12

ILS Landing

It is mandatory for safe operations that pilots perform the approach of stabilizer-Lizada and standardiz ed way. Is understood to be stabilized approach with the aircraft on final approach fully configured for landing at 1,000 FT AGL when in IMC and 500 FT AGL when in VMC, VM C, noting: - In Vapp Vapp and stabilized with the engines at the correct correc t power; Ramp-being Ramp-be ing in the G / S and LOC L OC axis (BM I); - In FAF / OM, configured confi gured with the FLAP FL AP landing and Final C / L complete; -VASI -V ASIS S Or PAPI (CM V) or visual ramp aligned with the axis of the runway; Thus, at 1,000 feet AGL IMC and VMC 500 feet AGL, the following should be performed performed Callout:

PNF

PF

“APROXIMAÇÃ O ESTABILIZA DA” “ CHECKED ” Qualquer anuncio de desvio observado abaixo de 1.000 pés AGL IMC e 500 pés AGL VMC deverá ser anunciado o Callout: PNF PF “APROXIMAÇÃO “APROXIMAÇÃO NÃO ESTABILI ZADA” “GO AROUND FLAPS”

AIRBUS INDUSTRIE recommends that the approach of the A320 is divided into three phases, Initial APP, Interm. APP and APP Final, these phases should be used in all types of landing licensed to operate the aircraft. - The A320 A320 is licensed for operation of I LS CA C AT III B; - In APP VOR / DME DM E NOT ACCURACY ACCUR ACY must follow in order BIRD changing the FC U HDG HD G & V / S TRK & FPV F PV mode and pursued APP as IAC; IA C; - In visual landing procedures must be followed as mentioned in Flight Patterns of aircraft, pilots must have a high degree of conhe cement of Flight Patterns; - In the two AP decides to be triggered in the event of loss of the other system is active to continue APP; - The auto-landing should be done with CONF FULL FLAP and observed the functioning of ALS and other services identification of AD for l anding;

PF  APPR

LOC LO C G/S

When they are captured the APPR PB should be fired. When When over overfly flyin ing g the the DECEL DECEL poin pointt , APPR phas phase e

PERF APPR

D IMAGE 22: Performance Page/Approach (AVSOFT, 2009).

- During the landing or takeoff is alert should pop the table of wind and operational constraints of the aircraft in case of auto-landing operational speeds change, VIDE VID E QRH QR H always ifif in doubt. doubt.

Winds - Maximum KT The following are the maximum demonstrated crosswind with flight controls in normal and direct law (with or without the yaw damper) Crosswind - Takeoff

29

Crosswind - Landing

33

Crosswind with Gusts

38

Tailwind - Take off and Landing

10

PNF

Initial approach NAV ACCURACY MONITOR ENG MODE SEL ..... .......... .......... .......... .......... .......... ........AS ...AS RQD ENG MODE SEL ..... .......... .......... .......... .......... .......... ........AS ...AS RQD 10 NM to IAF ORDER………..... ORD ER………..... “ACT IVATE APPR PHAS E” APPR PHASE................................. PHAS E.......................................ACT ......ACT IVE CONFIRM/ANNOUNCE………”APPR PHASE POSITIO NING ..... .......... .......... .......... .......... .......... ........ ... MONITOR  ACTI VATED” VATED” SPEED D OWN……………………....MON ITOR RADAR T ILT ....................................... A AD DJUST When cleared for I LS approach  APPR P/B ................................................. ................................................. ARM BOTH AP ............................................. E EN NGAGE FMA ..... .......... .......... .......... .......... .......... .......... .......... .......... ......AN .AN NOUNCE FMA ..... .......... .......... .......... .......... .......... .......... .......... .......... .......“CHECKED” ..“CHECKED” At green dot and below VFE ORDER ..... .......... .......... .......... .......... .......... .......... .......... ..........“FLAPS .....“FLAPS 1” Announce Announce ..... .......... .......... .......... ......... .... “SPEED CHECKED” FLAP S ..............................................SELEC ..............................................SELEC T 1 CONFIRM/ANNOUNCE ……………” ……………”FLAPS FLAPS 1” LOC CAPTU RE ................................. MO M O N ITO R  ANNO UNCE UNC E ..........................................“LOC ..........................................“LOC ” FMA ..... .......... .......... .......... .......... .......... .......... .......... .......... .......“CHECKED” ..“CHECKED” GLIDE SLOPE CAPTU RE ............... MO MON ITOR  ANNO UNCE UNC E ............................................“G ............................................“G S ” FMA ..... .......... .......... .......... .......... .......... .......... .......... .......... .......“CHECKED” ..“CHECKED” ORDER ..... .......... ..... “SET GO AROUND ALTITUDE” GO AROUND ALT......... ALT.............. ........... ........... .......... .......... ........SET ...SET TUDE xxx SET”  ANNO UNCE .. “GO AROUND ALTITUDE

TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

 Airbus 320

13

When FLAPS 2 ORDER ..... .......... .......... .......... .......... .......... .......... ....... “GEAR DOWN” L/G..... L/G.......... .......... .......... .......... .......... .......... ......... .... SELECT DOWN GRND GRN D SPLRS SPLR S ..........................................ARM ..........................................ARM EXT LIGHTS.............................................SET Nose Sw TAXI & Rwy Turn Off Sw ON Em condições IMC Noturno somente ligar as NOSE lights após atingir VMC CONFIRM / ANNOUNCE ......“ ......“GEAR GEAR DOWN” Checar pressão residual no triple indicator. When L/G down and below VFE ORDER ..... .......... .......... .......... .......... .......... .......... .......... ..........“FLAPS .....“FLAPS 3” ANNOUNC E ..... .......... .......... ....... “SPEED CHECKED” FLAP S ...........................................SELE ...........................................SELECT CT 3 CONFIRM / ANNOUNCE……….”FLAPS 3”

Appears below 2000 ft RA

1000 ft In IFR

Appears at 800 ft RA

GO AROUND 500 ft In ft In VFR

GO AROUND

IMAGE 23: Final Approach (AVSOFT, 2009).

If the FM A pseudo DESCEL Waypoint is displayed must activate the APPR PHASE appear in magenta D self-activation is v  possible, when it is blank v D Before 3 miles from the IAF first flap should be lowered. If the APPR requires

a reduced speed for a restriction of the letter flap must first be lowered to ensure the secu-rity of flight of the aircraft, the APPR will be con-firmed with two flap down and checking the check on ECAM, as in the figure. In the event of removal VOR orbits or APPR chrono-meter to check the time  procedure should be fired.

PF PNF During the APPR situations When FLAPS 3 and below VFE o n t h e R W Y s h o u l d b e ORDER ..... .......... .......... .......... .......... .......... ........“FLAPS ...“FLAPS FULL” ANNOUNC E ..... .......... .......... ....... “SPEED CHECKED” observed and spoken during FLAPS ..... ........... ........... .......... .......... .......... .........SELECT ....SELECT FULL CONFIRM / ANNOUNCE ... ......“FLAPS ...“FLAPS FULL” t h e c h e c k i l i s t B e f o r e VAPP ....................................................CHE ....................................................CHE CK WING A ICE .......................................... .......................................... OFF Approach, in case of rain SLIDING TABLE ..... .......... .......... .......... .......... .......... .......... .......STOW ..STOW SLIDING TABLE............ TABLE................. .......... .......... ..........STOW .....STOW FINAL C/L.............. C/L......... ........... ........... .......... .......... .......... ........... ........ .. CALL should be informed and RWY CABIN CREW............ CREW.................. ........... .......... .......... ....... ADVISE COND, CON D, WET, then the engine “Tripulação, pouso autorizado”  FINAL C/L............................................READ should be in S TART mode and Passing the Outer Marker the APU should be connected  ANNO UNCE UNC E …”PASSING PASSING (FIX NAME)…xxx NAME)…xxx FT” in the same way during a  ANNO UNCE UNC E ............................... ............................... “CHE CKED” UNC E ANY FMAmodification FLT PARAMETERS ..... .......... .......... .......... ..........CHEC .....CHEC K takeofff the APU and the ENG takeof E NG  ANNO UNCE  Announce any deviation in excess of: mode should also be attached. V/S 1000 ft/min In case of LOW Visibility IAS speed target  +  + 10/ –5 ILS 1 dot up/down should observe proce-ments Max deviation allowed: described in Flight Patterm 500 ft AGL……1 dot  LOC  LOC / GS Low Visibility Approach Cir300 ft AGL……0.5 dot  LOC  LOC / 1 dot GS Pitch attitude...2.5 degrees nose down cling. (319/320)……..10 degrees nose up During a crash or the pilot (321)…………..7.5 degrees nose up BANK………… 7 degrees decide to seek a new speed POSITION/FLT PATH...........................CHECK VAPP case in the FMCDU BANK 7° PERF PAGE DING-LAN is not working, the pilot should add the + VLS CONF in 10kt FLAP 3 or VLS + 5 in CONF FULL Speed Target VAPP - 5kt FLAP, during the final the +10 kt +10° FMCDU is locked, then the pilot Vapp PITCH & SINK RATE should continue its VAPP in SPD GLIDE 1 dot -2.5° 1000 ft/min Vapp selected mode, in case of doubt the PNF should consult consult the QRH. With Wit h the LOC and GLID G LIDE E interLOC 1 dot ceptados the Cross Check of AMF should be checked.  1 0

 1 0

10

10

10

10

10

IMAGE 24: Primary Flight Display (AVSOFT, 2009). TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

 Airbus 320 

15

 Landing & After Landing

Between 50 ft and 30 ft FLAR E Between mode is active, the auto-trim will work for a low pitch and with the command of the PF, and the mes-mo right now will command the elevator with the intent to touch the thousand mark the corre-sponding RWY (if auto-landing the PA will remain on even bring in the reverse idle position). Interestingly, the pattern of 4 ° pitch applied for PF in the landing procedure,

At touchdown

REV .......... .................... ................... ................... ................... ................... ............ MAX  ANNOU NCE...... ................ ....... “GND SPLR S”  ANNOU NCE...... .......“R EVERS ERS G REEN” BRAKES.......................... BRAKES................................... ................. ........ AS RQRD ANNOUNCE……………… ANNOUNCE……………………...”DECEL” ……...”DECEL” At 70 kt

 ANNOU NCE...... ................ ................ .... “70KT” REV .......... .................... ................... ................... ................... ................... ...........IDLE . Em condições normais a eficiência do REV. abaixo de 70Kt é mínima além da possibilidade de causar danos ao motor. Após o callout   de 70 kt, o piloto deve trazer as manetes para a posição IDLE REV da maneira correta, evitando acelerar a aeronave novamente. Before 20 kt

 AUTO BRK .............. ................ .. DISE NGAG E ANNOU NCE..... ................ .. “AUTO BRK O FF”

causing a fall in the path of - 1 °, avoiding Tail Strike, the announcement of RETARD the aircraft will  be 20 ft on the radio altimeter. alti meter. After you tap the PF should bring to the MAX reverse position from the touchdown giving birth to CALLs CAL Ls OUTs. O UTs. (see (see table opposite) To achieve 70 kts should bring to the reverse idle and 20 kt before the auto-break will be disabled and announced by the co-pilot at that time the brake will be commanded by Commander announcing 'I have controls'. CM1 CM2 After landing, on GRND SPLRS ..... .......... .......... .......... .......... .......... .......... ....... DISARM APU Maste Masterr SW…………………… SW……………………………… ……………..ON …..ON NOSE NOS E LT SW.................................................TAXI SW.................................................TAXI entering the courtyard, LAND LIGHTS…………………………… LIGHTS…………………………….AS .AS R QRD observe the following (Desligar após confirmação do CM1) b rake RWY TURNOF F SW……………………..AS SW……………………..AS RQRD  procedure: Select brake STROBE LT AUTO.......................Ao livrar a RWY fans ON at least 5 minutes PWS………………………………………………OFF after the temperature check RADAR……………………………………OFF/STBY ENG MODE sel……………………………….NORM or When The Brakes Hot FLAPS……………………………………..RETRACT Ecam Warning Warning displays. d isplays. (If SAT ≥ 30°C, maintain CONF 1+F) The Cm2 starts starts AFTER AFTE R TCAS MODE sel...................................ABV/STBY BRAKES TEMP……………………………...CHECK LANDING CHECKLIST  APU Start SW…………………………………….ON  ANTI-ICE………………...........................AS  ANTI -ICE………………...........................AS RQRD RQR D must be done in silent GLARESHIE LD…………………… LD………………………….FD/LS …….FD/LS OF F mode after Cm1 disarm the  ANNO UNCE……………………..“AFTER UNC E……………………..“AFTER L ANDI NG spoiler lever, meeting the C/L COMPLETED” duties under scan flow and  Anunciar somente após após confirmação de APU  AVAIL  AVAIL / APU Inop. checklist.

± 45 º de alinhamento com o gate solicitar Desligar Desligar a TAXI LIGHT (e RWY TO LIGHT). “LIGHTS OFF”. 

 Pilot Incapacitation

The incapacitation of one of the pilots is a situation that requires special attention because it can present itself in many different ways and possibly occur without the presence of a previous notice. The techniques most commonly used to recognize advance one disability are: -Monitorar And Cross-check instruments; If a crew member does not feel good, the other driver should be notified immediately immediately;; -Monitorar The behavior of another member of the crew, noting deviations from standardization, callouts and incoherent to the flight phase actions. To characterize the disability, the remaining crew must: -Declarar Emergency to ATC ("MAYDAY MAYDAYMAYDAY-"); -take All measures to ensure that incapaci-tation of the other driver does not cause interference in command of the aircraft; -Solicitar The help of a doctor who may be on board; -Checking If there are any extra pilot on board; -Pousar As soon as possible after considering all the factors involved; -Solicitar Medical assistance after landing; TELESISTEMAS REINALDO DELFIACO COPYRIGHT 2013

-ao Approaching Approaching for landing, anticipating anticipating the APP ROA ROACH CH PREPA-RA PRE PA-RATIO TION N and reading the checklists; checklists; -Solicitar If possible radar vectoring or a longer approach, due to the increased workload in the cockpit; -Efetuar Landing on the seat currently used; -If Commander is incapacitated, the co-pilot must coordi-nate with the presence of the company maintenance team to tow the aircraft or even to meet on the trail. For this, you must inform the control tower that after landing the aircraft remains on the runway. The APU should  be on and after confirming confirming APU AV AVAIL engines should should be cut. The co-pilot should not taxiing the aircraft.

 Airbus 320

14

At MDA + 100  ANNO UNCE……“ONE UNCE ……“ONE H UNDR ED ABOVE” ABOV E” FCU SE LECTOR V S/FPA…………… S/FPA……………….PUSH ….PUSH FMA Announce…….” VERTICAL SPEED ZERO” FMA…………………………………“CHECKED” At VDP ou MAPT (o que ocorrer primeiro)  ANNO UNCE.....”MINIMUM, UNCE.....”MINIMUM, VENTO XXX”

 ANNO UNCE UNC E ......... “CONTIN “CON TINUE UE or GA FL APS” IF CONTINUE  AP DISCON DI SCON NECT.............................”AP NECT.............................”AP OF F” POSITION/FLTPA POSITION/FLTPATH... TH...... ...... ....CHECK/ADJUST .CHECK/ADJUST Quando interceptar a rampa visual. ORDER ..... .......... .......... .......... .......... .......... .......... .......... .......... ....... “FD OFF” FD.............. FD................... .......... .......... .......... .......... .......... .......... ....... .. SET OFF ..... .......... .......... .......... .......... .......... .......... .......... .......... .......... .......... .......“TRK/FPA” ..“TRK/FPA” TRK/FPA ..... .......... .......... .......... .......... .......... .......... .......... ......... .... PRESS ..... .......... .......... .......... .......... .......... .......... .......... ....... “INSERT RWY TRK” MAG RWY TRK.............. TRK................... .......... .......... ....... .. INSERT At 200 FT AGL  ANNO UNCE ... “CONTIN “CO NTIN UE” or “GA/FLA “GA/ FLAPS” PS”

INFORMAR O COMPONENTE DO VENTO.

FINAL CABIN CREW..............ADVISED A/THR.................. A/THR............. ..........SPEE .....SPEE D /OFF ECAM MEMO ...LDG NO BLUE MIS SED AP PR ALT..... ALT......... .... FL SET  



LG DOWN SIGNS ON

 

SPLRS ARM FLAPS SET

 GO  G O Around Around

During BRIEFING approach is required that pilots who verifi-points of the ROUTE MISSED APPROACH are exactly the ones provided in the letters of ship-gation. Missed approach  p r o c e d u r e : - W h e n s e l e c t i n g  paraTOGA  paraTO GA levers with FL FLAP AP lever leve r at least position 1 the "GA TRK" mode  becomes active and the aircraft will maintain the "TRK" the time of selection performed until another way HDG HD G / NAV NAV is selected;

3.THRUST REDUCTION/ACCELERATION ALTITUDE

1.GO AROU 1.GO AROUND ND INITIATION

2.LATERAL GUIDANCE

PF PNF THRUST LEVERS ...... ......... ...... ...... ...... ...... ...... ...... ...... .....TOGA ..TOGA  ANN OUN CE ........... “GO ARO UND – FLA PS” FLAPS .......... ............... .......... .......... ....... RETRA CTONE STEP R O TAT IO N ...................................... PE P E RFORM FMA ........................................ ............................................A ....A NNO UNC E  ANN OUN CE .....................“PO .....................“PO SIT IVE C LIM B” “MAN TOGA/SRS/GA TRK/ATHR BLUE”  ANN OUN CE………………………“CH ECK ED” ORDER ......... .............. .......... .......... .......... .......... .......... .........“GEAR ....“GEAR UP” L/G LEVER…………………..……SELECT LEVER…………………..……SELECT UP GRND SPLRS ......... .............. .......... .......... .......... .......... ......DISAR .DISAR M RWY TO / TAXI LT................................... OFF  ANN OUN CE ............“GEA R UP – F LAP S XX” FCU HDG/TRK-SELECTOR….ORDER HDG/TRK-SELECTOR….ORDER PUSHOR PULL (NAV OR HDG) NAV or HDG……..…SELECT ORDERE D FMA………………………………. FMA………………………………... ANNOUN CE FMA………………………..…….…CHECKED At GA thrust reduction altitude THRUST LEVER S .......... ............... .......... .......... .......... .......... ..........CL .....CL At GA acceleration altitude SPEED............. SPEED.................. .......... .......... .......... .......... .......... ....... .. MONITOR FLAPS .......... ...............RETRACT .....RETRACT ON SCHED ULE

5.DIVERSION 4.HOLD

(missed (misse d appro approach) ach)

IMAGE 25: Go Around (AVSOFT, 2009).

- Pressing the FCU HDG / TRK the SELECTOR (NAV) mode becomes active, the aircraft aircraft will follow the F-PLN F-PL N  programmed into FM FMGS; GS; - In a selected rise due to restrictions in the IAC must be pressed the elevation knob and use the F PA mode if you climb gradient required; - The PNF should go to the DIR on MCDU and put in DIRECT TO the VOR to hold; - To carry on the ALTN AD, gun in CLIMB PHASE.   ENABLE