曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
of ECAM DUs), abort the start by switching OFF the ENG 2 MASTER sw. Then, perform a 30 s
dry crank.
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 3/10
FCOM 19 AUG 10
ON ECAM UPPER DISPLAY ON ECAM LOWER DISPLAY
N2 increases Corresponding start valve in line.
Bleed pressure indication green.
Oil pressure increases.
At 16 % N2 Indication of the active igniter (A or B).
At 22 % N2
‐ FF increases
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.
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.
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 4/10
FCOM 19 AUG 10
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).
When idle is reached (AVAIL indication is displayed):
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 %.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 11(140)
