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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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 (3) If the fault continues:

 - Do a check of the RELAY-PWR SPLY (10WR) and replace it if necessary (Ref. ASM 35-23/01).

 (4) If the fault continues:


 (a) Do a check and repair the wiring if necessary between:
 - SW (16WR) connector A/A and CB (1WR)

 - SW (16WR) connector A/C and RELAY (8WR) connector A/X1

 - RELAY (8WR) connector A/X2 and GND

 - SW (16WR) connector A/C and RELAY (9WR) connector A/X1

 - RELAY (9WR) connector A/X2 and GND

 - SW (16WR) connector A/C and RELAY (10WR) connector A/X1

 - RELAY (10WR) connector A/X2 and GND, (Ref. ASM 35-23/01).


R **ON A/C 401-499,

R A. For A/C with the Gaseous Oxygen System and the HIGH ALTITUDE SWITCH
R installed:

R (1) If the test confirms the fault:
R - Replace the ALTITUDE SWITCH (16WR) (Ref. AMM TASK 35-23-15-000-001)
R and (Ref. AMM TASK 35-23-15-400-001).

R (2) If the fault continues:
R - Do a check of the HIGH ALTITUDE SWITCH (899WR) and replace it if
R necessary (Ref. ASM 35-23/01).

 「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 ∞∞35-23-00∞∞∞∞∞∞∞∞∞∞Page 202
 Aug 01/05 CES


R  (3) If the fault continues: 
R  - Do a check of the OPEN RELAY 1 (930WR) and replace it if necessary 
R  (Ref. ASM 35-23/01). 
R  (4) If the fault continues: 
R  - Do a check of the OPEN RELAY 2 (931WR) and replace it if necessary 
R  (Ref. ASM 35-23/01). 
R  (5) If the fault continues: 
R  (a) Do a check and repair the wiring if necessary between: 
R  - ALT SW (16WR) connector A pin A and GND 
R  - ALT SW (16WR) connector A pin B and OPEN RELAY 1 (930WR) 
R  connector A pin D2 and OPEN RELAY 2 (931WR) connector A pin D2 
R  - HIGH ALT SW (899WR) connector A pin A2 and OPEN RELAY 1 (930WR) 
R  connector A pin D2 and OPEN RELAY 2 (931WR) connector A pin D2 
R  - SW (16WR) connector A pin C and HIGH ALT SW (899WR) connector A 
R  pin A3. 
R  **ON A/C ALL
 B. Do the test as given in the Para. 3.A.
 5. Close-up________
 A. Put the aircraft back to its initial configuration.


 TASK 35-23-00-810-802


 OXYGEN/PASSENGER P/BSW SYS ON Legend Fault
 1. Possible Causes
_______________
 - PUSHBUTTON SW-OXYGEN/PASSENGER (12WR)

 - RELAY-CTL PWR SPLY (11WR)


 - wiring R - RELAY (6LP) R - OXYGEN REGULATORS (910WR1 and 910WR2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 33-14-00-710-001 Operational Test of the Annunciator Light Test System in the Cockpit AMM 35-23-00-710-001 Operational Check of Manual Mask Release R AMM 35-23-00-710-005 Operational Check of Manual Mask Release ASM 35-23/01
 3. Fault Confirmation
__________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 A. Do the operational test of the manual mask release (Ref. AMM TASK 35-23-00-710-001).
R **ON A/C 401-499,
R A. Do these tests:
R (1) Do the operational test of the annunciator-light test system (Ref. R AMM TASK 33-14-00-710-001).
R (2) Do the operational test of the manual mask release (Ref. AMM TASK 35-R 23-00-710-005).
R NOTE : After activation of the oxygen system the OXYGEN/PASSENGER
____ R P/BSW SYS ON legend stays on until the pressure in the R distribution lines is below 0.045 bar (0.6526 psi). The time R to depressurize is between 0.4 and 22 minutes. Time decreases R if cabin pressure is lower or if more oxygen masks are used.
 「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 ∞∞35-23-00∞∞∞∞∞∞∞∞∞∞Page 204
 Aug 01/05 CES 4. Fault Isolation


_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 A. If the SYS ON legend on the pushbutton switch OXYGEN/PASSENGER, which is installed on the panel 21VU, does not come on during the test:
 - Do a check of the PUSHBUTTON SW-OXYGEN/PASSENGER (12WR) and replace it if necessary (Ref. ASM 35-23/01).
 (1) If the fault continues:

 - Do a check of the RELAY-CTL PWR SPLY (11WR) and replace it if necessary (Ref. ASM 35-23/01).
 
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