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时间:2011-03-29 14:39来源:蓝天飞行翻译 作者:航空
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 - do a FADEC non motoring test (Ref. AMM TASK 73-29-00-710-040).
 (a) Look for failure messages including the following words in FADEC test results and class 3 report (Ref. AMM TASK 73-21-60-740-026) : N2 SNSR, PS3, VSV, T25.
 1 If any of those messages is present:
_

 - do the trouble shooting procedure (Ref. TASK 70-00-00-810-801).
 2 If no message is found:
_

 - do the engine post stall inspection (Ref. AMM TASK 72-00-00-200-008).
 (4) Do a detailed visual inspection of the VSV control linkage (Ref. AMM TASK 75-32-10-210-002) and look for any broken or loose components:

 - repair or replace as required.

 (5) If nothing is found:

 - replace the hydromechanical unit (HMU) (Ref. AMM TASK 73-21-10-000-002) and (Ref. AMM TASK 73-21-10-400-002).

 (6) If trouble repeats:


 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref.
 AMM TASK 73-21-60-400-001). R
 B. Do a minimum idle check to make sure that all engine instruments give the correct indication (Ref. AMM TASK 71-00-00-710-006).
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 TASK 80-00-00-810-834
 Slow Start Before Light off Sequence, on Engine 1 or 2
 1. Possible Causes
_______________
 - engine

 - pneumatic starter

 - starter shut off valve


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 36-12-51-200-001 Remove and Check Auxiliary Power Unit Bleed
R Check-Valve (7260HM) for Condition AMM 71-00-00-000-042 Removal of the Power Plant AMM 71-00-00-400-042 Installation of the Power Plant AMM 71-00-00-710-003 Engine Automatic Start AMM 80-11-10-000-002 Removal of the Pneumatic Starter AMM 80-11-10-400-002 Installation of the Pneumatic Starter AMM 80-11-20-000-003 Removal of the Starter Shutoff Valve AMM 80-11-20-400-003 Installation of the Starter Shutoff Valve
 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the crew observation: ENG1 or 2 -STARTING - slow start before light off sequence: - on the lower ECAM display unit, do a check of the starter air pressure
 (at least 25 PSI)
 - if no, make sure that the pack valves are off. Do a check to make sure that the air source pressure is sufficient (ground supply unit, APU).
 (1) If the fault continues:

 - do a check of the magnetic chip detectors for unwanted particles .

 (2) If the fault continues:


 - do a check to make sure that the core turns freely by handcranking.
 (a) If a blockage occurs:
 - try to turn the core each 15 mn for no more than 8 hours.
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 (b) After you tried this, if again it is not possible to turn the core:
 - replace the engine (Ref. AMM TASK 71-00-00-000-042) and (Ref. AMM TASK 71-00-00-400-042).
 (3) If the fault continues:

 - do a check of the APU bleed check valve (Ref. AMM TASK 36-12-51-200-001).

 (4) If the fault continues:

 - replace the pneumatic starter (Ref. AMM TASK 80-11-10-000-002) and (Ref. AMM TASK 80-11-10-400-002).

 (5) If the fault continues:


 - replace the starter shut off valve (Ref. AMM TASK 80-11-20-000-003) and (Ref. AMM TASK 80-11-20-400-003).
 B. Do an engine automatic start procedure (Ref. AMM TASK 71-00-00-710-003).
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 TASK 80-00-00-810-835
 Failure of the Starter Shutoff Valve on Engine 1
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - aircraft wiring

 - CTL SW-ENG/MASTER 1 (3KC)
 
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