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时间:2011-03-28 23:01来源:蓝天飞行翻译 作者:航空
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 1. Possible Causes
_______________
 - CYLINDER-OXYGEN STORAGE (5750HM)

 - XMTR/PRESS REG-OXY (4HT)


 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 31-60-00-860-001 EIS Start Procedure AMM 31-60-00-860-002 EIS Stop Procedure AMM 35-10-00-040-001 OXY High Pressure Indication-Direct Reading. AMM 35-11-41-000-001 Removal of the Crew Oxygen-Storage Cylinder (5750HM) AMM 35-11-41-400-001 Installation of the Crew Oxygen-Storage Cylinder
 (5750HM) AMM 35-13-15-000-001 Removal of the Oxygen Pressure Regulator/Transmitter (4HT) AMM 35-13-15-400-001 Installation of the Oxygen Pressure Regulator/Transmitter (4HT)
 3. Fault Confirmation
__________________
 A. Job Set Up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).

 (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).


 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU OXYGEN/CREW/OXY/SPLY 1HT HA01
 「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 ∞∞35-10-00∞∞∞∞∞∞∞∞∞∞Page 232
 Nov 01/02R CES

 C. Test


 (1) On the ECAM control panel:

 - push the DOOR key to get the DOOR/OXY page:

 (2) Make sure that the OXY pressure indication is between 401 and 1499PSI on the DOOR/OXY page.

 (3) Do an OXY high-pressure indication direct reading (Ref. AMM TASK 35-10-00-040-001).


 4. Fault Isolation
_______________
 A. If during the check of the pressure of the crew cylinder, the values is:
 (1) The same as the value on the SD, on the DOOR/OXY page:

 - replace the CYLINDER-OXYGEN STORAGE (5750HM) (Ref. AMM TASK 35-11-41-000-001) and (Ref. AMM TASK 35-11-41-400-001).

 (2) Different from the value on the SD on the DOOR/OXY page:


 - replace the XMTR/PRESS REG-OXY (4HT) (Ref. AMM TASK 35-13-15-000-001) (Ref. AMM TASK 35-13-15-400-001)
 (a) If the fault continues:
 - replace the CYLINDER-OXYGEN STORAGE (5750HM) (Ref. AMM TASK 35-11-41-000-001) and (Ref. AMM TASK 35-11-41-400-001).
 B. Test
 (1) Make sure that the OXY pressure indication is normal on the DOOR/OXY page:
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 (1) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF. (Ref. AMM TASK 31-60-00-860-002).

 (2) 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 ∞∞35-10-00∞∞∞∞∞∞∞∞∞∞Page 233
 Nov 01/02R
 CES R TASK 35-10-00-810-819 R Oxygen Cylinder Refilling not possible R 1. Possible Causes


_______________
R - FILL PORT-OXY SYS (5769HM) R - XMTR/PRESS REG-OXY (4HT) R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 35-11-42-000-001 R AMM 35-11-42-400-001 R AMM 35-13-15-000-001 R R AMM 35-13-15-400-001 R
R 3. Fault Confirmation
__________________
R A. Test
Removal of the Oxygen Fill Port (5769HM)
Installation of the Oxygen Fill Port (5769HM)
Removal of the Oxygen Pressure Regulator/Transmitter
(4HT)
Installation of the Oxygen Pressure
Regulator/Transmitter (4HT)

R (1) Not applicable, the fault is evident.
R 4. Fault Isolation
_______________
R A. If it is not possible to refill the oxygen cylinder:
R - replace the FILL PORT-OXY SYS (5769HM) (Ref. AMM TASK 35-11-42-000-001)
R and (Ref. AMM TASK 35-11-42-400-001).

R (1) If the fault continues:
 
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