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时间:2011-03-28 23:25来源:蓝天飞行翻译 作者:航空
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R  ENG 2 BLEED pushbutton switch to the pin 2 of the circuit 
R  breaker 3HA2. 
R  a_  If the fault continues:
R  - Replace the AIR BLEED/ENG 2/CTL (3HA2). 
R  (2) If the circuit breaker (3HA2) is tripped: 
R  - Do the procedure (Ref. TASK 24-00-00-810-803).

 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A231
 --Feb 01/05 ---CES -


R  (3) Check of the automatic closure of the bleed pressure regulator valve 
R  (4001HA). 
R  - Remove the BMC-2 (1HA2) (Ref. AMM TASK 36-11-34-000-001). 
R  - Do a check for 28 VDC at pin AA/8A of the BMC2. 
R  (a) If there is no 28 VDC: 
R  - Do a check and repair the wiring from the BMC2 pin AA/8A to the 
R  circuit breaker 3HA2 pin 2. 
R  (b) If there is 28 VDC: 
R  - Do a check of the wiring between pin A/D1 of the ENG 2 BLEED 
R  pushbutton switch and pin AA/7A of the BMC2. 
R  1_  If there is continuity:
R  - Replace the P/BSW-ENG 2 BLEED (4HA2). 
R  a_  If the fault continues:
R  - Replace the BMC-2 (1HA2) (Ref. AMM TASK 36-11-34-000-001) 
R  and (Ref. AMM TASK 36-11-34-400-001). 
R  2_  If there is no continuity:
R  - Repair the wiring between pin A/D1 of the ENG 2 BLEED 
R  pushbutton switch and pin AA/7A of the BMC2 (Ref. ASM 36-
R  11/02).
 C. Do the test given in para. 3.

 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A232
 --Feb 01/05 ---CES - Fan Air Valves of the Engine 1 and Engine 2 Blocked in the Open Position

 


 1.
 Possible Causes

_______________


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
36-11-00-810-849 Fan Air Valve of the Engine 1 Blocked in the Open Position 36-11-00-810-850 Fan Air Valve of the Engine 2 Blocked in the Open Position AMM 36-11-54-720-001 Functional Test of the Opening of the Fan Air Valve
 3. Fault Confirmation
__________________
 A. Test

 (1) Do the test of the fan air valve (Ref. AMM TASK 36-11-54-720-001).
 4. Fault Isolation
_______________

 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
 A. If the test gives the maintenance messages:
 FAN AIR V 9HA1 OR THRM 7170HM1 and
 FAN AIR V 9HA2 OR THRM 7170HM2:

 -do the trouble shooting procedures (Ref. TASK 36-11-00-810-849) and (Ref. TASK 36-11-00-810-850).
R **ON A/C 106-149, 229-299, 303-399, 401-499,
 A. If the test gives the maintenance messages:
 THRM 7170HM1 OR FAN AIR-V 9HA1 and
 THRM 7170HM2 OR FAN AIR-V 9HA2:

 -do the trouble shooting procedures (Ref. TASK 36-11-00-810-849) and (Ref. TASK 36-11-00-810-850).
 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A233
 --Aug 01/05 ---CES -R **ON A/C ALL

 

 TASK 36-11-00-810-871
 High Bleed Pressure of the Engine 1 in Climb

 1. Possible Causes
_______________

 -VALVE-BLEED PRESS REG (4001HA)
 -VALVE-OVERPRESSURE, ENG 1 (5HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2) AMM 36-11-52-000-040 Removal of the Bleed Pressure-Regulator Valve (4001HA) AMM 36-11-52-400-040 Installation of the Bleed Pressure-Regulator Valve
 (4001HA) AMM 36-11-53-000-001 Removal of the Overpressure Valve (5HA1,5HA2) AMM 36-11-53-400-001 Installation of the Overpressure Valve (5HA1,5HA2) TSM 36 PB 101
 3. Fault Confirmation
__________________
 A. Test

 (1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
 4. Fault Isolation
_______________

 A. If the test gives a maintenance message, you can find the related trouble shooting procedure (Ref. TSM 36 PB 101).
 (1) If there is no maintenance message:
 
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