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РПП Часть В |
Стандартные эксплуатационные процедуры |
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Издание: 05 |
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Airbus-319/320/321 |
Standard operating procedures(SOP) |
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Изменение: 00 |
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3. |
ВЫПОЛНЕНИЕ ПОЛЕТА |
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3.1. BEFORE PUSHBACK or START |
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LOADSHEET . . . . . . . . . . . . . . . . . . . |
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CHECK BOTH |
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The CM2 should thoroughly check the Load and Trim Sheet (LTS), particularly for gross errors. Make sure that the loadsheet data are correct: Correct flight data, correct aircraft,dry operating index, configuration, Fuel On Board, etc. Check that the takeoff CG is within the LTS operational limits.
ZFWCG / ZFW / THS reminder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK / REVISE PF ZFWCG / ZFW / THS reminder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK PNF TAKEOFF DATA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PREPARE and CHECK/REVISE PF
TAKEOFF DATA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PREPARE and CHECK PNF
Revise TAKE OFF DATA if actual takeoff weight is greater than weight used for takeoff data calculation or less by 2000 and more kg.
–The PF checks or recalculates/revises the takeoff speeds and flexible temperature, using the RTOW charts.
–The PNF independently recalculates the takeoff speeds and flexible temperature and checks them on the MCDU.
Take particular care in determining the takeoff configuration.
(Refer to FCOM PER-THR-FLX DEFINITION). Confirm any takeoff weight limitation.
MCDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN TAKEOFF CONFIGURATION BOTH
Display F-PLN on the PNF side and PERF TAKEOFF on the PF side.
EXT PWR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK OFF CM1
Request external power to be removed.
SEATS, SEAT BELTS, HARNESSES, RUDDER PEDALS, ARMRESTS . . . . . ADJUST BOTH
The seat is correctly adjusted, when the pilot's eyes are in line with the red and white balls.
BEFORE START CHECKLIST down to the line . . . . . . . . . . . . . . . . . . . . . . COMPLETE BOTH ATC PUSH BACK/START UP CLEARANCE
WINDOWS and DOORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK CLOSED BOTH
–Check that the cockpit windows are closed and locked by pushing the control handle to the mechanical stop.
–Check, on the ECAM lower display, that all aircraft doors are closed.
–Check that the cockpit door is closed and locked (no cockpit door open/fault indication).
If entry is requested, identify the person requesting entry before unlocking the door.
With the cockpit door selector on NORM, cockpit door is closed and locked. If entry is requested from the cabin, and if no further action is performed by the pilot, the cabin crew will be able to unlock the door by using the emergency access procedure.
ATC mode selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO/XPNDR CM2
Use ATC transponder depending on local regulation.
ATC PUSH BACK/START UP CLEARANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OBTAIN CM2
cтр. 44 |
ВЫПОЛНЕНИЕ ПОЛЕТА |
Дата 01.02.2013 |
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РПП Часть В |
Стандартные эксплуатационные процедуры |
Издание: 05 |
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Airbus-319/320/321 |
Standard operating procedures(SOP) |
Изменение: 00 |
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NW STRG DISC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK AS RQRD CM1
In case of pushback (conventional or towbarless), the nosewheel steering selector bypass pin must be in the tow position. The ECAM N/WS DISC memo indicates this to the flight crew.
CAUTION: If NW STRG DISC is not displayed on the ECAM, but the ground crew confirms that the steering selector bypass pin is in towing position, then the push back must not be performed. This is to avoid possible nose landing gear damage at the green hydraulic pressurization. To dispatch the aircraft in such a case, refer to MEL.
In case of a powerpush by the main landing gear, the nosewheel steering selector should remain in the normal position to steer the aircraft (Refer to FCOM PRO-SUP-80-A).
BEACON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON CM1 THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLE CM1
CAUTION: Engines will start, regardless of the thrust lever position; thrust will rapidly increase to the corresponding thrust lever position, causing a hazardous situation, if thrust levers are not at IDLE.
PARKING BRAKE ACCU PRESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK CM1
The ACCU PRESS indication must be in the green band.
PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRD CM1
–If no pushback is required, check that the PARKING BRK handle is ON, and check the BRAKES PRESS indication.
–If push back is required, set the PARKING BRK to OFF.
CAUTION: If, during engine start with parking brake on, the aircraft starts to move due to a parking brake failure, immediately release the PARKING BRK handle to restore braking by pedals.
CAUTION: Do not use brakes during push back, unless required due to an emergency.
After pushback is completed, set the PARKING BRK to ON, and inform the ground crew to allow the towbar to be disconnected.
BEFORE START CHECKLIST below the line . . . . . . . . . . . . . . . . . . . . . . . COMPLETE BOTH Startup clearance from ground crew . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OBTAIN CM1
Дата 01.02.2013 |
ВЫПОЛНЕНИЕ ПОЛЕТА |
cтр. 45 |
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РПП Часть В |
Стандартные эксплуатационные процедуры |
Издание: 05 |
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Airbus-319/320/321 |
Standard operating procedures(SOP) |
Изменение: 00 |
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3.2.AUTOMATIC ENGINE START
Use the automatic engine start procedure in most circumstances. However, if the start aborts due to insufficient starter inlet air pressure (e.g. on high airfields or in the case of low pressure from an external pneumatic power group), it is recommended to proceed with the manual start procedure, rather than use the automatic one.
If, during the engine start, the ground crew reports a fuel leak from the engine drain mast, run the engine at idle for 5 minutes. If the leak disappears during these 5 minutes, the aircraft can be dispatched without maintenance action. If the leak is still present after 5 minutes, maintenance action may be required before the flight.
ENG MODE selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IGN/START CM1
The lower ECAM display shows the ENG page.
"STARTING ENGINE 2" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ANNOUNCE CM1
Engine 2 is usually started first. (It powers the yellow hydraulic, which pressurizes the parking brake).
ELAPSED TIME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START CM2
ENG 2 MASTER switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON CM1
Do not turn the MASTER switch ON before all amber crosses and messages have disappeared on the engine parameters (upper ECAM display). Parameter callouts are not mandatory.
In case the electrical power supply is interrupted during the start sequence (indicated by the loss of ECAM DUs):
abort the start by switching OFF the MASTER switch.
Then, perform a 30-second dry crank. (FCOM DSC-70-80-40P 8/14)
ON ECAM UPPER DISPLAY |
ON ECAM LOWER DISPLAY |
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N2 increases |
Corresponding start valve in line. Bleed pressure |
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indication green. Oil pressure increases. |
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At 16% N2 |
Indication of the active igniter (A or B). |
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At 22 % N2 |
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- FF increases |
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(may be crossed up to 200 kg/h) |
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15 seconds (maximum) after fuel is on |
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- N1 increases |
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- EGT increases |
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Start valve starts closing. |
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At 50 % N2 |
(It is fully closed between 50 % and 56 % N2) |
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Igniter indication off. |
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MAIN and SECONDARY ENG. IDLE PARAMETERS . . . . . . . . . . . . . . CHECK NORMAL CM1
At ISA sea level: N1 about 19.5 %
EGT about 390° С
N2 about 58.5 %
FF about 275 kg/h (600 lb/h) Grey background on N2 indication disappears.
cтр. 46 |
ВЫПОЛНЕНИЕ ПОЛЕТА |
Дата 01.02.2013 |
|
РПП Часть В |
Стандартные эксплуатационные процедуры |
Издание: 05 |
|
|
Airbus-319/320/321 |
Standard operating procedures(SOP) |
Изменение: 00 |
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"STARTING ENGINE 1" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ANNOUNCE CM1 ENG 1 MASTER switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON CM1 SAME PROCEDURE AS FOR ENGINE 2.
Both pack valves reopen with 30 second delay after the second engine N2 is above 50 %.
Note: A PTU FAULT is triggered, if the second engine is started within 40 seconds following the end of the cargo doors operation.
Дата 01.02.2013 |
ВЫПОЛНЕНИЕ ПОЛЕТА |
cтр. 47 |