曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

FCOM 19 AUG 10
AUTOMATIC ENGINE START
Applicable to:
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 case of low pressure from an
external pneumatic power group), it is recommended to use the manual start procedure, instead the
automatic procedure.
If, during the engine start, the ground crew reports a fuel leak from the engine drain mast, run the
engine at idle for 5 min. If the leak disappears during these 5 min, the aircraft can be dispatched
without maintenance action. If the leak is still present after 5 min, maintenance action may be
required before the flight.
ENG MODE selector........................................................................................................... IGN/START
The lower ECAM displays the ENG SD page.
START ENGINE 2..............................................................................................................ANNOUNCE
Engine 2 is usually started first. It powers the yellow hydraulic system, that pressurizes the parking
brake.
ENG 2 MASTER sw..........................................................................................................................ON
Do not turn the ENG 2 MASTER sw 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 ENG 2 MASTER sw. Then, perform a 30 s
dry crank.
ON ECAM UPPER DISPLAY ON ECAM LOWER DISPLAY
N2 increases Corresponding start valve inline.
Bleed pressure indication green.
Oil pressure increases.
At 16 % N2 Indication of the active igniter (A or B).
At 22 % N2
‐ FF increases (1)
15 s (maximum) after fuel is on
‐ EGT increases
‐ N1 increases
At 50 % N2 Start valve starts closing. (It is fully closed between 50 %
and 56 % N2).
Igniter indication off.
(1)With the current ECU standard, the FF indication may be crossed up to approximately 200 kg/h (440 lb/h).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - ENGINE START
A318/A319/A320/A321 FLEET PRO-NOR-SOP-08 P 2/10
FCOM 19 AUG 10
MAIN AND SECONDARY ENG. IDLE PARAMETERS.............................................CHECK NORMAL
At ISA sea level : N1 about 19.5 %
N2 about 58.5 %
EGT about 390 °C
FF about 275 kg/h (600 lb/h)
Grey background on N2 indication disappears.
START ENGINE 1..............................................................................................................ANNOUNCE
ENG 1 MASTER sw..........................................................................................................................ON
Same procedure as for engine 2.
Both pack valves reopen with 30 s delay after the second engine N2 is above 50 %.
Note: A PTU FAULT is triggered, if the second engine is started within 40 s following the end of
the cargo doors operation.
AUTOMATIC ENGINE START
Applicable to:
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 case of low pressure from an
external pneumatic power group), it is recommended to use the manual start procedure, instead the
automatic procedure.
If, during the engine start, the ground crew reports a fuel leak from the engine drain mast, run the
engine at idle for 5 min. If the leak disappears during these 5 min, the aircraft can be dispatched
without maintenance action. If the leak is still present after 5 min, maintenance action may be
required before the flight.
ENG MODE selector........................................................................................................... IGN/START
The lower ECAM displays the ENG SD page.
START ENGINE 2..............................................................................................................ANNOUNCE
Engine 2 is usually started first. It powers the yellow hydraulic system, that pressurizes the parking
brake.
ENG 2 MASTER sw..........................................................................................................................ON
Do not turn the ENG 2 MASTER ‐ sw 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
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 11(139)