曝光台 注意防骗
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accordingly. Retract gear on command.
Once well clear of the ground, minimum 400 ft, the ECAM actions may be started.
It is not necessary to rush into doing the ECAM drills and 400 ft is the MINIMUM altitude at
which commencement of ECAM drills should be considered. The priority is to ensure that the
aircraft is climbing, stabilized and is flying in a safe direction. Do not get too distracted with
ECAM. Furthermore, ECAM should be interrupted when necessary to allow both pilots to
monitor level-off, configuration changes etc.
It is important to determine whether the engine has suffered a flameout or has structural
damage. The action of putting the start switch to ignition confirms the relight attempt being
made by the FADEC. If a flameout has occurred, then a relight (QRH 2.18) may be
considered at a later stage when aircraft has been cleaned up and a safe flight path
established.
There must be no movement of thrust lever, master switch or fire pb without positive
confirmation from both pilots.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.10 Page 4
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
OPERATING TECHNIQUES
CHAP03\10
ENGINE FAILURE OR FIRE AFTER V1 (CONT’D)
05 - TRAINEES’ ACTIONS(CONT’D)
ENGINE FIRE
Should an engine fire develop, follow the general series of actions described above.
However, the ECAM drill should be commenced as soon as is practicable (though not below
400 ft). Be aware that the engine may still be developing a significant amount of thrust until
the engine master switch is placed to off. Consider the use of autopilot to reduce workload.
The ECAM will count down the seconds to initial agent discharge and the time period
between discharges.
Do not attempt to restart an engine which has been shut down due to fire.
The ECAM notes that a landing should be carried out as soon as possible. Bear in mind the
prevailing weather conditions, but an engine fire which will not extinguish is a very serious
matter.
Following engine shutdown, consider all affected systems and their impact on the approach
and landing.
ECAM PROCEDURES
ECAM procedures should be started not below 400 ft. At this height, only immediate actions
to secure an engine should be carried out as shown below. ECAM actions may be
interrupted at any stage for the PNF to assist PF (e.g flap retraction). Do not allow ECAM
actions to interfere with monitoring of the flight path.
· Engine flame out, no damage - ignition on, thrust lever to idle, engine master switch off -
stop ECAM.
· Engine failure, with damage - continue ECAM to discharge of AGENT 1 - stop ECAM.
· Engine fire - continue ECAM to discharge of AGENT 2, if necessary, or until FIRE warning
is out - stop ECAM.
ECAM procedures should be recommenced once the aircraft is clean (or at ’S’ speed with
CONF 1, if returning for an immediate VMC landing) and climbing to a safe altitude .
Complete ECAM until STATUS page appears then carry out the after take-off C/L before
reading STATUS.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.10 Page 5
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
OPERATING TECHNIQUES
CHAP03\10
ENGINE FAILURE OR FIRE AFTER V1 (CONT’D)
05 - TRAINEES’ ACTIONS (CONT’D)
FMGS PROCEDURES
The two FMGS procedures which are worthy of note are the use of the EO SID prompt and
the EO CLR prompt. The in depth explanation of both these functions is contained in FCOM
4.04.30 (How to Use - Other Functions).
The use of EOSID routing is dependent on there being a EOSID defined in the database for
that particular runway. If an engine failure occurs before the point at which the EOSID differs
from the planned SID then the EOSID will appear as a TMPY F-PLAN. To follow the EOSID
all the crew has to do is to insert this as the active F-PLAN. Therefore the first leg of the
active F/PLN should be a common leg in database.
If the engine failure occurs beyond the point at which the two SIDs differ there will be no
TMPY F-PLAN created although the EOSID will be shown in yellow on the ND. To follow an
EOSID in this case the crew can perform a DIR TO one of the EOSID waypoints and then
modify the F-PLAN or, more simply follow the EOSID, which is displayed as a yellow line on
the ND, using HDG mode.
When an engine failure is detected the bank angle commanded by the FD is limited to 15°
when speed is below or at maneuvering speed of current configuration (F, S, O). The EO
CLR prompt on the active PERF page would remove this bank angle limit if depressed.
But the EO CLR prompt should be pressed ONLY in the event of a successful relight on a
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