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ON
OF
MASTER 1 NORM TGN/
(I) Note : Refer to 1.21.10
Z
ART
INITIAL CONFIGURATION OF
CONTROLS
(engine not running).
- START IDENTIFICATION :
ECAM displays ENG page
- PACK VALVE close (I)
- LP fuel valve opens
- START VALVE opens
- ignition starts:
. on ground : when N2 > 16 %
. in flight : immediately
- HP fuel valve opens :
. on ground : when N2 > 22 %
. in flight : when N2 > 15 %
- When N2 > 50 %
. START VALVE closes
. IGNITER off if on ground
. PACK VALVE reopen with 30
seconds delay (remain
closed if the other engine
is started).
- ECAM ENG page disappears.
- After engine start, moving
the MODE SEL switch to NORM
and back to IGN/START
activates continuous relight
on the running engine (s).
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.70.80 P 6 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃l IGNITIONLAND STARTING ┃SEQ 005 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
MANUAL STARTING
The FADEC has limited authority over manual starting controlling :
- the opening of the start valve when the ENG MODE selector is set to IGN/START and
the MAN START pushbutton switch is pressed.
- the position of the HP fuel valve and the operation of both igniters, when the master
switch is turned ON
- the closing of the start valve at 50 % N2, and, on the ground, the cutting off of ignition.
The FADEC makes a passive survey of the engine during the starting sequence : the flight
crew is made aware of an abnormal start by a proper ECAM warning and has to interrupt
the start sequence. The FADEC has not the authority to abort the manual start :
- in flight
- on ground, except if the start EGT limit is exceeded before reaching 50 % N2. In this case
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual5(172)
