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时间:2011-03-28 18:26来源:蓝天飞行翻译 作者:航空
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 (1) Replace the PRESSURE REDUCING VALVE (Ref. AMM TASK 29-14-43-000-001) and (Ref. AMM TASK 29-14-43-400-001).

 (2) Take a fluid sample from each hydraulic system to make sure that the contamination of the hydraulic fluid is in the approved values (Ref. AMM TASK 12-32-29-281-001).


 B. Do the functional test of the pressurizing system of the hydraulic reservoirs again to make sure that the function is correct (Ref. AMM TASK 29-14-00-720-001).
 5. Close-up
________

 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2701GJ, 2702GJ, 3801GX, 3802GX, 3803GX
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 234
 Nov 01/04R
 CES


 TASK 29-11-00-810-811

 

 FAULT Light of the GREEN ENG 1 PUMP P/BSW is ON
 1. Possible Causes
_______________

 - BOARD-ANN LT TEST & INTFC (2LP)

 - wiring

 

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power AMM 33-14-00-710-001 Operational Test of the Annunciator Light Test System in the Cockpit AMM 33-14-33-000-001 Removal of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) AMM 33-14-33-400-001 Installation of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) ASM 33-14/05
 3. Fault Confirmation
__________________

 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).


 (2) On the overhead panel 40VU, look for the FAULT light of the GREEN/ENG 1 PUMP P/BSW.


 4. Fault Isolation
_______________

 A. If the Fault Confirmation gives:
 - the GREEN ENG 1 PUMP P/BSW FAULT on panel 40VU:

 - replace the BOARD-ANN LT TEST & INTFC (2LP) (Ref. AMM TASK 33-14-33-000-001) and (Ref. AMM TASK 33-14-33-400-001).


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 235
 May 01/05 CES

 

 (1) If the fault continues:
 - do a check and repair the wiring between the: BOARD-ANN LT TEST & INTFC (2LP) pin A/44 and the P/BSW-HYD/GREEN/ENG 1 PUMP (1705GK) pin A/7 (Ref. ASM 33-14/05).
 B. Do the operational test of the annunciator light test system (Ref. AMM TASK 33-14-00-710-001) to make sure that the operation is correct.
 5. Close-up
________

 A. De-energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-862-002).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 236
 Nov 01/04R
 CES


 TASK 29-11-00-810-812

 

 Indication of the Hydraulic Fluid Quantity of the Green Reservoir shows High Level
 1. Possible Causes
_______________
 - gas leaks

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-11-00-810-801 29-11-00-810-803
29-11-00-810-813
AMM  24-41-00-861-002 
AMM  24-41-00-862-002 
AMM  29-00-00-870-001 
AMM  29-00-00-870-002 
AMM  29-00-00-870-003 
AMM  29-10-00-200-002 
AMM  29-10-00-200-003 

AMM 29-10-00-680-001 AMM 29-14-00-614-002 AMM 31-60-00-860-001
AMM 31-60-00-860-002 Loss of the Green Reservoir PressurizationLoss of the Correct Quantity in the Green Hydraulic ReservoirIndication of the Hydraulic Fluid Quantity of the Green Reservoir shows High or Low Level or fluctuatesEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerBleeding Procedure of the Green Hydraulic System Upstream of the Engine PumpBleeding Procedure of the Green Hydraulic System Upstream of the PTUBleeding Procedure of the Green Hydraulic System Downstream of the Engine PumpCheck Reservoir Air Pressure on Reservoir GaugeCheck Nitrogen Charge Pressure on the Yellow and Green Main Hydraulic System Accumulators by Reading GaugesDrainage of the Reservoir of the Green Hydraulic SystemPressurization of the Hydraulic Reservoirs through the Ground ConnectorEIS Start ProcedureEIS Stop Procedure
 
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