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

INSTRUCTOR CORNER: MANUAL OF STANDARTSAND OPERATION OF AIRBUS A320

ENGLISH CLASSES

2014

PONTIFÍCIA UNIVERSIDADE CATÓLICA DE GOIÁS

GOIÂNIA

REINALDO MOREIRA DEL FIACO

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 Linhas Aéreas; Instructor Corner, Miscellaneous, Flight Patterns and Systems of the homepage Smartcockpit; and in base of CBT displayed during the Flight Simulator Classes 2012/2.

MASTERMINDProf. Msc. Rodrigo Braz Muniz

RESEARCHREINALDO MOREIRA DEL FIACO

INSTRUCTOR CORNER: MANUAL DE PADRONIZAÇÃO E OPERAÇÃO DE VOO SIMULADO

2014

GOIÂNIA

COPYRIGHT 2013TELESISTEMAS REINALDO DELFIACO

SUMMARY

PRELIMINARY COCKPIT PREPARATION.............................................................................4F M G S P R E PA R AT I O N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5BEFORE TAKE OFF & CLEAR FOR TAKE OFF.............................................................................7TA X I L I M I TA I O N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8T A K E O F F . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9AFTER TAKE OFF & CLIMB.............................................................................12D E S C E N T & A P P R O A C H... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12I L S L A N D I N G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 3LANDING & AFTER LANDING.............................................................................15PILOT INCAPACITATION... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15G O A R O U N D . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 6PARKING & SECURING ACFT.............................................................................17R E F E R E N C E . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 8

LIST OF IMAGES

IMAGE 1: A320 C O C K P I T.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4IMAGE 2: A320 PEDESTAL.... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4IMAGE 3: A320 OVERHEAD.............................................................................4IMAGE 4: FMGS FUEL PAGE.............................................................................5IMAGE 5: FMGS PERF. PAGE.............................................................................5IMAGE 6: FMGS KEYBOARD DATA.............................................................................5IMAGE 7: FMGS PERF. PAGE INIT.............................................................................5IMAGE 8: A F T E R S TA RT.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5IMAGE 9: I G N . S TA RT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6IMAGE 10: T.O. CONFIGURATION.............................................................................7IMAGE 11: BEFORE TAKEOFF CHECKLIST.............................................................................7IMAGE 12: TAXI INITIATION.............................................................................8IMAGE 13: LADING LIGHTS...... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8IMAGE 14: S i d e s t i c k . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9IMAGE 15: S t e e r i n g . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 IMAGE 16: Steering ECAM Action.............................................................................9IMAGE 17: Sidestick ECAM Action.............................................................................9IMAGE 18: Takeoff and Bank Angle.............................................................................10IMAGE 19: After Takeoff and Climb Phase.............................................................................10IMAGE 20: After Takeoff and Climb Phase.............................................................................11IMAGE 21: Active Apphoach Phase.............................................................................12IMAGE 22: Landing Configuration.............................................................................13IMAGE 23: Performance Page/Approach.............................................................................14IMAGE 24: Final Approach.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14IMAGE 25: Primary Flight Display.............................................................................16IMAGE 26: Go Around . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16IMAGE 27: Enable A LT N.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16

English Classes Instructor Corner

Airbus A320

Preliminary cockpit preparation - 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 and operation of acft as fill FMGS, configuration of Overhead, FCU (Flight Control Unit), ECAM and pedestal;

- The check of overhead must be from left to right and upward, following the details in the picture;

CMTEPFFirst Officer

The pedestal, overhead and checks of some safety items are responsability of PF, how should follow the AIRBUS A320 check-list with the airline;

1 ENG Masters.....Check offENG MODE SEL.....Check NormL/G lever.....Check Down

2 Wipers.....OFFBAT.....CHECK/AUTOEXT PWR.....ONAPU FIRE.....CHECK/TESTAPU.....START*COCKPIT LIGHTS.....AS RQST

3 Parking brake.....ONACCU/BRAKES PRESS.....CHECKALTN BRAKING.....CHECKFLAPS.....CHECK POSITION SPEED BRAKE LEVERS.....CHECK RET

4 PROBE/WDW HET.....AUTOAPU BLEED....ONAIR COND PANEL.....SETELEC PANEL.....CHECKVENT PANEL


- In pedestal the check must be downward keepong observing from left to right; - The numbers in the side showthe sequence of check to be follow by PF during the Preliminary Cockpit Preparation; - The CAPT. should check the QHR - QUICK REFERENCE HANDBOOK and obtain thenavigation chapter in the correctsequence of use.

IMAGE 1: A320 COCKPIT (AVSOFT, 2009).

IMAGE 2: A320 PEDESTAL (AVSOFT, 2009).

IMAGE 3: A320 OVERHEAD (AVSOFT, 2009).

PERF T/O

T h e i n p u t d a d a s fulfilled in PERF Page are put inserted in FMA and in ECAM;

Airbus A320

5 6*ECAM RECALL ..........……………………….......PRESS*ECAM OXY PRESS/HYD QTY/ENG OIL QTY...CHECK

EMER EQPT ........………....CHECKC/B panels ............……..….CHECK*EXT.WALKAROUND ...PERFORM

Continuing the Cockpit Preparation Check-list we have Take off Briefing and FMGS Preparation. Take off briefing:

- Consulting the Metar, TAF, NOTAM, MEL, CDL, Use the anti-ice, radar meteorological; - Briefing the cartas de pátio (caso esteja disponível no AD de partida), ADC e SID; - Estar ciente das condições de motor, manutenção da ACFT e da taxa de DEG;

BLOCK

TOW

LW

EXTRA/TIME

2 FMGS preparation in INT Page, seguindo em ordem as LSKs

1

3

F/PLN - Adjust the RWY and the SID;- Check in FMA the altitude

target (blue);

ENGINE FAILURE- Before V1: CAPT

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

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5

FMGS Preparation- The correct ordem to input navigation datas in FMGS is: N a v i g a t i o n D ATA a n d a f t e r Performance DATA, each one witch yours funct ion fol lowing 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.

In some flight simulator functions like SEC F-PLAN A or B can be validated, if the AIRAC’s Frequency are wrong compared to that used by the simulator, the frequency can be adjusted in RAD NAV, and can be check in VOR page, fix, ILS or other in F-PLAN, if you prefer the frequency can be adjusted in DIR page during the flight.

- 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 INIT B and PERF PAGE must be fill after the Operational Weight and Fue l Weight be confirmed.

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

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

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

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

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2

Airbus A320

Before Start During Before Start Operation, have a sequence of checks and procedures to do, the procedure must be standart, following with caution and fulfilling the check list by the PF and PNF, 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 LOADSHEET……………..………………….CHECK

COCKPIT DOOR………..………………….CLOSED

TAKEOFF DATA..…ENTER/REVISE

TAKEOFF DATA....…XCHECK

SEAT BELTS……………………………….ADJUST

MCDU……...PERF TO

MCDU……….F-PLN

EXT PWR……..OFF

BEFORE START down to the line..…PERFORM

Confirm any take off limi- ANNOUNCE….”BEFORE START C/Ltation; down to the line COMPLETED”

Ask for external power dis-conection

1 Before Star

PF2 Automatic Engine Star Sequence

ENG MODE SEL..............IGN/STARTBLEED PRESSURE…...…CHECKANNOUNCE…...”STARTING ENGINE 2”

MASTER SW 2….......…….ON

START VALVE OPENSN2 INCREASESIGNITERFUEL FLOWEGTN1OIL PRESSSTART VALVE CLOSE• 50% N2 CFM• 43% N2 IAE

- ENG IDLE PARAMETERS...CHECK NORMAL- ANNOUNCE..........”STARTING ENGINE 1”- REPEAT START SEQUENCE FOR ENG 1...

After Before Start procedures the PF must ask to PNF the read of Before Start Check-list, the PNF will ask item by item with their PF answer, 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 PNF to reed the AFTER Start Checklist.

PF PNF AFTER START

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

APU BLEED…..............….OFFECAM STATUS………CHECKECAM DOOR PAGE….CHECKANNOUNCE..........…”CLEAR TO DISCONNECT”

1. GND SPLRS……………ARM2. RUD TRIM………RESET3. FLAPS….....………SET4. PITCH TRIM……………..SETENG ANTI ICE………AS RQRDWING ANTI ICE……..AS RQRD6. APU MASTER SW………OFF

Overhead and Pedestal

PF

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COPYRIGHT 2013TELESISTEMAS REINALDO DELFIACOIMAGE 8: AFTER START (AVSOFT, 2009).

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

Airbus 320

PF PNF 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 PNF has obtain free push back and the CAPT. assume the acft taxi until the take of line.

NW STRG DISC MEMO...............CHECK

WINDOWS and DOORS……….................. CHECK CLOSED

THR LEVERS……..........….IDLE

PARKING BRAKE ACCU PRESS…......... …...CHECK

PARKING BRAKE….........….ON

ORDER…...................................................... .”BEFORE START C/L below the line”

GROUND CREW COMMUNICATION… ESTABLISH

PUSHBACK/START CLEARANCE……. ….OBTAIN

WINDOWS…………..…CHECK

BEACON………………..……ON

If the acft moves despite of PARKING BRK ON, immediately release PARKING BRK handle torestore pedals braking.

ANNOUNCE.............…….....‘‘BEFORE START C/L COMPLETE”When PARKING BRAKE is ON:

brake pressure is shownPARK BRK MEMO is displayed

Before Take OFF & Clear for Take OFF

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

- Do the Cleared for Take Off Check-list to receive the authorization to join in 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. Should be check and analyzed by both (CM1 and CM2):

- FMGS: F-PLN Page: Runway, SID their, Constraints of speed and altitude; RADNAV Page: Navigation Aid Frequency; PERF Page: Runway, Speeds, (TO SHIFT if applicable), Flaps/THS and Flex TO Temp.

PF PNFAPP PATH CLEAR OF TRAFFIC.. ..CHECK

CLEARED FOR TAKEOFF C/L .. .... CALL

MODE SEL............. AS RQRDThe ignition is necessary in case of rain and/or wet runway.EXT LIGHTS.................SETSTROBE LIGHT ..........ONNOSE SW ................TORWY TURNOFF SW....... ONLAND SW .....................ONPACK 1+2.................. AS RQRDBRAKE FANS........CHECK OFFCABIN CREW...............ADVISE“Crew, ready for takeoff”

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

Note: Is is need the ACFT hold in the runway waiting the clearence to take of, lights should extanded to OFF position and extanded to ON after obtain the clearence to start take of. The Strobe Light and the LANDING LIGHTS should be turn on when cross the wait line to runway.

- During the taxi the wind speed must be observed comparing the aircraft limitation;

- If have delay during taxi the First Office should recalculate the fuel and check the news informations in FMC.

The AIRBUS’ philosophy 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, ECAM 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.

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IMAGE 10: T.O. CONFIGURATION (AVSOFT, 2009).

IMAGE 11: BEFORE TAKEOFF CHECKLIST (AVSOFT, 2009).

Airbus 320

A320 NORMAL CHECKLIST 04-JAN-2010

CLEARED FOR TAKEOFF

CABIN CREW..............ADVISEDENG MODE SEL........AS RQRDPACKS........................AS RQRDBRAKE FAN................OFFRADAR &TERRAIN ON ND..ON

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

The straight taxi in A320 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 turn is made until 180°, the taxiway must have at least 75 ft side lenght.

PF PNF

TAXI CLEARANCE.........OBTAIN

ELAPSED TIME ........…AS RQRD

BRAKE PRESSURE.....CHECK ZERO

ANNOUNC....”PRESSURE ZERO”

FLT CTL….......................…CHECK

Before Taxiing:NW STRG DISC.......….CHECK not displayed on right ECAM MEMO

When Taxi clearance obtained:

NOSE LIGHT..…...................…TAXI

PARKING BRAKE..……............OFF

THRUST LEVERS…........AS RQRD

ANNOUNCE…..‘‘BRAKE CHECK’’

BRAKE PEDAL…..............…PRESS

FLT CTL……....................…CHECK

ATC CLEARANCE…….......CONFIRM

TERR ON ND……...............AS RQRD

1. RADAR / PWS……........ON / AUTO

2. ATC…............................………..SET

3. AUTOBRAKE……….............…MAX

4. T/O CONFIG…….................PRESS

5. T/O MEMO….….CHECK NO BLUE

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 and brakes temperature, and our respectives temperatures w h i c h m u s t b e c o n s t a n t l y monitored. In the hold point, the fuel flow and operating minima should be reviwed.

FCU ALT….............…...CHECK

If ATC requests to maintain run-way heading or incase of a radar vector procedure :

HDG……..............................SET

FLIGHT INSTRUMENTS…....CHECK

T/O BRIEFING…....CONFIRM

By joining track and CMTE Copilot should check the magnetic heading of the runway, and advertising Checked.

Note: In the PSS simulators Brake & FANS and RADAR TERRAIN not work.

PF PNFBRAKE TEMP BELOW 150°C……. CHECK

BRAKE FANS………OFF

TAKE OFF/LINE UP CLEARANCE… OBTAIN

ENGINE MODE SEL....AS RQRD

TCAS…..TA or TA/RA

PACKS 1 + 2…….AS RQRD

SLIDING TABLE…..STOW

APPROACH PATH CLEAR OF TRAFFIC.…CHECK

CABIN CREW…….ADVISE

EXTERIOR LIGHTS……..SET

SLIDING TABLE……...STOW

Taxi Initiation

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IMAGE 12: TAXI INITIATION (AVSOFT, 2009).

IMAGE 13: LANDING LIGHTS (AVSOFT, 2009).

Airbus 320

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: FULL UP, FULL DOWN, NEUTRAL, 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.

In the taxi, can have some changes in data configuration inputed in FMCDU, a cross-check is necessary between FMCDU and Navigation Instruments, EFIS and FCU, and stand by instruments.

Take Off

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 should be said aloud.

and CM2) use the Sidestick as described in FCTM. It is also recommended to avoid potential problems of directional control during alignment, the engines are brought to the initial power setting ONLY 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

The commander must keep on hand in the Steering 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 remain with the hand levers to the V1. After stabilization of the engines and the actual start of the takeoff roll, PF (CM1

After aligning the aircraft on runway PF should check the runway heading on the compass and the FMA as letter. In case of runway on the other side of the headboard has ILS, appeared in the FMA yaw bar that indicated the central alignment of the runway that aircraft should follow.

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IMAGE 14: Sidestick (AVSOFT, 2009).

IMAGE 15: Steering (AVSOFT, 2009).

IMA

GE

16:

Ste

erin

g E

CA

M A

ctio

n (

AV

SO

FT

, 200

9).

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

Airbus 320

remain HEAD DOWN, 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 of IES CHECK POWER CHECK and after those speeds should observe the arrival of the aircraft in its goal of V1, VR and V2 + 10 for the ascent of the plane and cleaning. In addition to the indication of the speeds of the motors on the ECAM instruments must be observed and measured to check the MINUMUS when the minimum power required to TKOFF. In navigational instruments a cross-check, and reported aloud by two pilots should be done.

- 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

- 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 P F c a n o b s e r v e t h e alignment of the aircraft in yaw roll in indicating direction and heading in the FMA;

bedside 32 SBGO: '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, min imum or maximum opera t ing parameters exceeded in engines or 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 CLIMB according to next figure>>>>>

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

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

Airbus 320

- After the authorization of descent should be selected on FCU, 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 at the base date of FMCDU;

- The frequency of the VOR / DME radios should be placed in orbit in case of direct removal;

- The weather data should be adjusted in FMCDU 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-DEV and VAPP should be calculated by the PNF.

- The descent may be made in various parts depending on the attitudes authorized by ATC, since the procedures cabin is divided into four parts, preparation of descent - as described on the previous page - procedures for descent / descent (sidebar), downhill FL 100 and after the descent phase or end.

- The order of the procedures described in sop TAM, are outlined in the figure below;

PF PNFCSTR P/B ............... AS RQRD

ANNOUNCE….. CHECKED”

MCDU....................... F-PLN

NPA APPR USE.......... PROG

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

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

DESCENT..................INITIATE

ANNOUNCE ....................FMA

MCDU preferably..... PROG / PERF DESC

DESCENT.............. MONITORSPD BRK................AS RQRDRADAR TILT............ ADJUST

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

- Before reading Before the Approach check l i s t 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 s ta tus , RTA, NOTAM aprontos among others, comment on the computation landing card, then present the cards to be u s e d a n d s p e c i f y t h e procedures to be performed, c o n t i n u e r e a d i n g a n d comment FMGS lateral and vertical navigation using the

cards and the ND in PLAN / CSTR function to display the 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.

Note: The engine anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipared. During climb, cruise or descent and ice temperature is below - 40° C SAT the engine anti-ice must be ON.

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

BEFORE APPROACH

BRIEFING..............CONFIRMEDRWY COND................DRY/WETIAL MISSED APPR.......REVIEWV. BUGS.....................SET(BOTH)SEAT BELTS............................ONBARO/MDA/DH........SET(BOTH)ENG MODE SEL .........AS RQRDAUTOBRAKE..............AS RQRD

B E F O R E T H E A P P R O A C H check l i s t shou ld be done when overcome TA and pursue orders as in the table below.

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’’

IMAGE 20: Active Apphoach Phase (AVSOFT, 2009).

Airbus 320

uncertainty also our takeoff is aborted, above V1 proceed with takeoff and in case of failure will continue as flight emergency plan in case of failure of the commands will be with me and asked if you help 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 the AFTER 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 constantly review the route to be flown; - When crossing FL290 check the altimeters to enter RVSM airspace.

AFTER T.O./CLIMB

LDG GEAR..................UPFLAPS.....................RETRACTEDPACKS....................ONMEMO..................REVIEWBARO REF..............SET(BOTH)

- At any stage of the flight, the PNF will announce "ONE THOUSAND TO GO" before passing 1000ft altitude or authorized FL (ALT's that were selected in FCU), respond to what the PF "CHECKED".

Descent & Approach

- The preparation of descent must be made with 80 or 15 minutes of the MN T / D (TOP OF DESCENT); - During descent PF should remain HEAD DOWN, 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 seek data from ATIS and ATC units.

PF PNFLANDING DATA .......….OBTAIN

FMGS ......…..………...CHECK

DESCENT CLEARANCE ......…OBTAIN

ANTI ICE ............………....AS RQRD

MCDU ……….……………….F-PLN

DESCENT CLEARANCE...........OBTAIN

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

FMGS……………...PREPARE

APPR BRIEFING...... PERFORM

AUTO BRAKE….…AS RQRD

When new ATC clearance : FL 80FCU ALT……SET and MANAGE

SPEEDBRAKES .…....AS RQRD

RADAR TILT…………ADJUST

TERR ON ND ……..AS RQRD

- 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 PFD.

10


IMAGE 21: Landing Configuration (AVSOFT, 2009).

Airbus 320

ILS Landing

It is mandatory for safe operations that pilots perform the approach of stabilizer-Lizada and standardized 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, noting: - In Vapp and stabilized with the engines at the correct power; Ramp-being in the G / S and LOC axis (BMI); - In FAF / OM, configured with the FLAP landing and Final C / L complete; -VASIS Or PAPI (CMV) 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 Callout:

PNF PF

“APROXIMAÇÃO ESTABILIZADA” “ 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 NÃO ESTABILIZADA” “GO AROUND FLAPS”

- During the landing or takeoff is alert should pop the table of wind and operational constraints of the aircraft in c a s e o f a u t o - l a n d i n g operational speeds change, VIDE QRH always if in doubt.

Winds - Maximum KTThe following are the maximum demons-trated crosswind with flight controls in nor-mal 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

The following are the maximum demons-trated crosswind with flight controls in nor-mal and direct law (with or without the yaw damper)

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 is licensed for operation of ILS CAT III B;

- In APP VOR / DME NOT ACCURACY must follow in order BIRD changing the FCU HDG & V / S TRK & FPV mode and pursued APP as IAC;

- 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 landing;

PF PNF Initial approach

NAV ACCURACY MONITOR

ENG MODE SEL .................................AS RQD ENG MODE SEL .................................AS RQD

10 NM to IAF ORDER………..... “ACTIVATE APPR PHASE” APPR PHASE.......................................ACTIVE

POSITIONING ................................. MONITORCONFIRM/ANNOUNCE………”APPR PHASE ACTIVATED”

SPEED DOWN……………………....MONITOR RADAR TILT....................................... ADJUST

When cleared for ILS approach APPR P/B ................................................. ARM BOTH AP ........................................... ENGAGE FMA ..............................................ANNOUNCE FMA...............................................“CHECKED”

At green dot and below VFE ORDER.............................................“FLAPS 1” Announce ........................ “SPEED CHECKED”

FLAPS ..............................................SELECT 1 CONFIRM/ANNOUNCE ……………”FLAPS 1”

LOC CAPTURE ............................... MONITOR ANNOUNCE ..........................................“LOC٭” FMA...............................................“CHECKED” GLIDE SLOPE CAPTURE............... MONITOR ANNOUNCE ............................................ “GS٭” FMA...............................................“CHECKED” ORDER.......... “SET GO AROUND ALTITUDE” GO AROUND ALT......................................SET

ANNOUNCE .. “GO AROUND ALTITUDE xxx SET”

LOC G/S

D

PERF

APPR

When overflying the DECEL point ,

APPR phase

When they are captured the APPR PB should be fired.

12

APPR


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

Airbus 320

When FLAPS 2 ORDER.................................... “GEAR DOWN” L/G....................................... SELECT DOWN

GRND SPLRS ..........................................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 DOWN” Checar pressão residual no triple indicator.

When L/G down and below VFE ORDER.............................................“FLAPS 3” ANNOUNCE ................ “SPEED CHECKED”

FLAPS ...........................................SELECT 3 CONFIRM / ANNOUNCE……….”FLAPS 3”

I f t h e F M A p s e u d o D E S C E L Wa y p o i n t i s displayed must activate the APPR PHASE appear in magenta self-activation is possible, when it is blank

Before 3 miles from the IAF first flap should be lowered. If the APPR requires

PF PNF When FLAPS 3 and below VFE

ORDER.................................“FLAPS FULL” ANNOUNCE ................ “SPEED CHECKED” FLAPS ...................................SELECT FULL CONFIRM / ANNOUNCE ...... “FLAPS FULL”

VAPP ....................................................CHECK WING A ICE .......................................... OFF SLIDING TABLE .....................................STOW SLIDING TABLE................................STOW FINAL C/L ................................................ CALL

CABIN CREW.................................. ADVISE “Tripulação, pouso autorizado” FINAL C/L............................................READ

Passing the Outer Marker ANNOUNCE …”PASSING (FIX NAME)… xxx FT”

ANNOUNCE ............................... “CHECKED” ANNOUNCE ANY FMA modification FLT PARAMETERS ......................... CHECK

Announce any deviation in excess of: V/S 1000 ft/min IAS speed target + 10/ –5 ILS 1 dot up/down Max deviation allowed: 500 ft AGL……1 dot LOC / GS 300 ft AGL……0.5 dot LOC / 1 dot GS Pitch attitude...2.5 degrees nose down

(319/320)……..10 degrees nose up (321)…………..7.5 degrees nose up

POSITION/FLT PATH...........................CHECK BANK…………7 degrees

1000 ft GO AROUNDIn IFR

500 ft In VFR GO AROUND

Appears at 800 ft RAAppears below 2000 ft RA

vD

vD

10

SINK RATESPD

Speed Target+10 ktVAPP - 5kt

Vapp

10 10

PITCH

10 10

+10°

-2.5°

BANK

1010

7°

&

1000 ft/minVapp

GLIDE

LOC

1 dot

1 dot

not working, the pilot should add the + VLS CONF in 10kt FLAP 3 or VLS + 5 in CONF FULL F L A P, during the f inal the FMCDU is locked, then the pilot should continue its VAPP in selected mode, in case of doubt the PNF should consult the QRH.

With the LOC and GLIDE inter-ceptados the Cross Check of AMF should be checked.

During the APPR situations o n t h e RW Y s h o u l d b e observed and spoken during t h e c h e c k i l i s t B e f o r e Approach, in case of rain should be informed and RWY COND, WET, then the engine should be in START mode and the APU should be connected in the same way during a takeoff the APU and the ENG mode should also be attached.

In case of LOW Visibility should observe proce-ments described in Flight Patterm Low Visibility Approach Cir-cling.

During a crash or the pilot decide to seek a new speed VAPP case in the FMCDU PERF PAGE DING-LAN is

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.

13


IMAGE 23: Final Approach (AVSOFT, 2009).

IMAGE 24: Primary Flight Display (AVSOFT, 2009).

Airbus 320

Landing & After Landing

15

At touchdown

REV........................................................... MAX ANNOUNCE.............................“GND SPLRS” ANNOUNCE.............“REVERSERS GREEN” BRAKES........................................... AS RQRD ANNOUNCE……………………...”DECEL”

At 70 kt

ANNOUNCE.......................................... “70KT” REV...........................................................IDLEEm 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 ................................ DISENGAGE ANNOUNCE....................... “AUTO BRK OFF”

Between 50 ft and 30 ft FLARE 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,

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.

After you tap the PF should bring to the MAX reverse position from the touchdown giving birth to CALLs OUTs. (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 GRND SPLRS .................................... DISARM APU Master SW…………………………………..ON NOSE LT SW.................................................TAXI LAND LIGHTS…………………………….AS RQRD

(Desligar após confirmação do CM1) RWY TURNOFF SW……………………..AS RQRD STROBE LT AUTO.......................Ao livrar a RWY PWS………………………………………………OFF RADAR……………………………………OFF/STBY ENG MODE sel……………………………….NORM FLAPS……………………………………..RETRACT

(If SAT ≥ 30°C, maintain CONF 1+F) TCAS MODE sel...................................ABV/STBY BRAKES TEMP……………………………...CHECK APU Start SW…………………………………….ON ANTI-ICE………………...........................AS RQRD GLARESHIELD………………………….FD/LS OFF ANNOUNCE……………………..“AFTER LANDING

C/L COMPLETED” Anunciar somente após confirmação de APU AVAIL / APU Inop.

± 45 º de alinhamento com o gate solicitar “LIGHTS OFF”.

Desligar a TAXI LIGHT (e RWY TO LIGHT).

After landing, on entering the courtyard, observe the following procedure: Select brake fans ON at least 5 minutes after the temperature check or When The Brakes Hot Ecam Warning displays.

The Cm2 starts AFTER LANDING CHECKLIST must be done in silent mode after Cm1 disarm the spoiler lever, meeting the duties under scan flow and checklist.

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; -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 MAYDAY-MAYDAY-"); -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;

-ao Approaching for landing, anticipating the APPROACH PREPA-RATION and reading the 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 APU AVAIL engines should be cut. The co-pilot should not taxiing the aircraft.


Airbus 320

At MDA + 100 ANNOUNCE……“ONE HUNDRED ABOVE” FCU SELECTOR VS/FPA……………….PUSH FMA Announce…….”VERTICAL SPEED ZERO”

FMA…………………………………“CHECKED”

At VDP ou MAPT (o que ocorrer primeiro) ANNOUNCE ......... “CONTINUE or GA FLAPS”

ANNOUNCE.....”MINIMUM, VENTO XXX”

IF CONTINUE AP DISCONNECT.............................”AP OFF” POSITION/FLTPATH..........CHECK/ADJUST Quando interceptar a rampa visual. ORDER.............................................. “FD OFF” FD................................................... SET OFF .........................................................“TRK/FPA” TRK/FPA ............................................ PRESS ......................................... “INSERT RWY TRK” MAG RWY TRK............................... INSERT

At 200 FT AGL ANNOUNCE ... “CONTINUE” or “GA/FLAPS”

INFORMAR O COMPONENTE DO VENTO.

FINAL

CABIN CREW..............ADVISEDA/THR.......................SPEED /OFFECAM MEMO ...LDG NO BLUEMISSED APPR ALT......... FL SET

LG DOWN SIGNS ON

SPLRS ARM FLAPS SET

GO Around

14

1.GO AROUNDINITIATION

5.DIVERSION

2.LATERALGUIDANCE

3.THRUSTREDUCTION/ACCELERATION

ALTITUDE

4.HOLD

(missed approach)

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 levers with FLAP lever 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 / NAV is selected;

PF PNF THRUST LEVERS ................................ TOGA ANNOUNCE ........... “GO AROUND – FLAPS” FLAPS .......................... RETRACT ONE STEP ROTATION .................................... PERFORM FMA ............................................ANNOUNCE “MAN TOGA/SRS/GA TRK/ATHR BLUE”

ANNOUNCE .....................“POSITIVE CLIMB”

ANNOUNCE………………………“CHECKED” ORDER...........................................“GEAR UP” L/G LEVER…………………..……SELECT UP GRND SPLRS ...................................DISARM RWY TO / TAXI LT ................................... OFF ANNOUNCE ............“GEAR UP – FLAPS XX” FCU HDG/TRK-SELECTOR….ORDER PUSHOR PULL (NAV OR HDG)

NAV or HDG……..…SELECT ORDERED FMA……………………………….. ANNOUNCE FMA………………………..…….…CHECKED

At GA thrust reduction altitude

THRUST LEVERS ........................................CL

At GA acceleration altitude SPEED............................................. MONITOR FLAPS ...............RETRACT ON SCHEDULE

- Pressing the FCU HDG / TRK the SELECTOR (NAV) mode becomes active, the aircraft will follow the F-PLN programmed into FMGS; - In a selected rise due to restrictions in the IAC must be pressed the elevation knob and use the FPA 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

<- ALTN


IMAGE 25: Go Around (AVSOFT, 2009).

IMAGE 26: Enable ALTN (AVSOFT, 2009).

Airbus 320 16

Parking & Securing ACFT

CM1 CM2 PARKING BRAKE……………………………………ON PARKING BRK ACCU PRESS.......................CHECK APU ..................................................... CHECK AVAIL ENG MASTER 1 – 2 ............................................ OFF

Checar engine cooling down time. ORDER................................ “PORTAS EM MANUAL”

Aguardar N1 <10%

ANNOUNCE...................................... “TRIPULAÇÃO, PORTAS EM MANUAL”

FUEL PUMPS… ................................................ ..OFF APU BLEED.......................................................... ON BEACON LT........................................................ OFF

Anunciar “slides disarmed”. SEAT BELTS....................................................... OFF ELAPSED TIME............................................... STOP EXT LT ....................................................... AS RQRD

Aguardar N2 XX

PARKING BRAKE ............................................... OFFMantenha contato com a equipe de solo para certificar que a aeronave esteja calçada e olhe para fora garantindo que a aeronave não está em movimento antes de selecionar o PRK BRK para OFF.

PARKING C/L.................................................... CALL PARKING C/L ................................................. ..READ STATUS page................................................ CHECK IRS PERFORMANCE .................................... CHECK O Comandante deverá reportar qualquer item em pane no RTA ou a palavra NIL (em inglês, se necessário).

Realizar Drift Check e Residual Ground Speed Check pela POSITION MONITOR page (FCOM 3.03.25 – pág 2 e 3).

CM1 CM2 PARKING BRAKE ................................................. ON DU’s..................................................................... DIM DU’s..................................................................... DIM

Reduzir o brilho do PFD, ND e MCDU, exceto do ECAM. Ajustar o RADAR em MAX. A manutenção desligará os DU.

ADIRS (1+2+3) .................................................... OFF OXY CREW SUPPLY .......................................... OFF EXT LT ................................................................ OFF APU BLEED........................................................ OFF EXT PWR ...................................................AS RQRD EMER EXIT LT .................................................... OFF NO SMOKING ..................................................... OFF APU MASTER SW............................................... OFF BAT 1+2 .............................................................. OFF Aguardar 2 min. após a luz AVAIL apagar, antes de desligar as baterias, para permitir o fechamento do Flap da APU.

ORDER......................... “SECURING AIRCRAFT C/L” SECURING AIRCRAFT C/L.............................. READ

.

During the taxi speeds for this operation must be remembered, with a letter in her hands and ADC fol-orders of the ground, with the aircraft at the gate the parking brake must be disabled after confirmation of shims posed by the handling. With the aircraft fully stopped with the engines off and the doors should be placed at the manual for the safe landing of the crew and passengers. After following the order of execution of the checks the aircraft will be ready to be delivered to maintenance. The parking checklist can be done

silently or normal, depending on the standard of operation (SOP) of the company. Good communication between the pilots is critical to the safe operation of the flight factor, all procedures done within booth must be clear to both crew members, in case of non-standard operations, one abnormal procedures, should be consulted in the QRH company if there is any doubt of the procedures after an abnormal procedure after completing the crash pilots must remain vigilant and head down to which both signs of breakdowns and unwanted modifications by MCDU the plane. The airplane must only be flown if the pilots possess high degree of knowledge of the books and operations of the limitations of the

A320 as 320 \ Miscellaneous, 320 \ INSTRUCTOR'S CORNER, 320 \ SYSTEMS and 320 \ FLIGHT PATTERNS. after that GOOD FLIGHT.


REFERENCE

AVSOFT. Aircraft General. CBT/WBT for Pilots. Warsaw: 2009. Acess: 06/20/2012. Available: http://www.avsoft.com/index.php?q=node/5.HOMA, Jorge M. Aerodinâmica e Teoria de Voo: Noções Básicas. Ed. 29. São Paulo: ed. ASA, 2010.JEPPESEN. Joint Aviation Authorities Airline Transport Pilot's Licence. Theoretical Knowledge Manual. 050 Meteorology. Oxford Aviation Service Limited. Published by Jeppesen GmbH, Frankfurt, Germany, 2001. TAM. Manual Geral de Operações. Rev. 5. Flight Standarts. São Paulo: 1 jan. 2011.

Documents

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