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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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 (a)
 If the position on the lower ECAM display unit is different with the position indicator:

 -replace the VALVE-HP BLEED (4000HA) (Ref. AMM TASK 36-11-51-000-040) and (Ref. AMM TASK 36-11-51-400-040).

 (b)
 If the position on the lower ECAM display unit is correct with the position indicator:


 -connect the TEST SET - ENGINE BLEED SYSTEM (98D36003000000) or TEST SET - ENGINE BLEED SYSTEM (98F36003002000) to pressurize at 20 psi (1.3789 bar) the test port of the HP Bleed valve.
 1 Make sure that there are no leaks at the sense line between
_ the HP bleed valve and the bleed pressure regulator valve and to the HP bleed valve closure control solenoid (11HA1).
 2 Depressurize the system on the test set.
_
 3 Remove the TEST SET - ENGINE BLEED SYSTEM (98D36003000000) or
_ TEST SET - ENGINE BLEED SYSTEM (98F36003002000).
 a If there are leaks:
_
 -repair the sense line
 b If there are no leaks:
_
 -replace the VALVE-HP BLEED (4000HA) (Ref. AMM TASK 36-11-51-000-040) and (Ref. AMM TASK 36-11-51-400-040).
 If the fault continues:
 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 279

 --Aug 01/05 ---CES -

 

 -
replace the SOL-HP BLEED OVERRIDE, ENG1 (11HA1) (Ref. AMM TASK 36-11-58-000-001) and (Ref. AMM TASK 36-11-58-400-001)

 If the fault continues:


 -
replace the XDCR-BLEED TRANSFER PRESS, ENG 1 (7HA1), (Ref. AMM TASK 36-11-15-000-001) and (Ref. AMM TASK 36-11-15-400-001).


 If the fault continues:

 -do a check and repair the wiring from the HP bleed valve to the BMC1, pins A/1 and A/5 to pins AA/14A and AA/15A (Ref. ASM 36-11/01).
R
 -refer to Para. 4.B.
 **ON A/C ALL
 B. Test

 (1)
 Do the engine 1 start procedure (Ref. AMM TASK 71-00-00-710-003).

 (2)
 Make sure that the ECAM warning AIR ENG 1 HP VALVE FAULT is not shown on the upper ECAM DU.


 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 280
 --Aug 01/05 ---CES - Failure of the HP Bleed Valve of the Engine 2 Blocked in the Closed Position


 1. Possible Causes
_______________
 -VALVE-HP BLEED (4000HA)
 -XDCR-BLEED TRANSFER PRESS, ENG 2 (7HA2)
 -SOL-HP BLEED OVERRIDE, ENG2 (11HA2)
 -sense line
 -wiring
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) 98D36003000000 1 TEST SET - ENGINE BLEED SYSTEM 98F36003002000 1 TEST SET - ENGINE BLEED SYSTEM
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-15-000-001 Removal of the Bleed Transferred Pressure Transducer (7HA1,7HA2) AMM 36-11-15-400-001 Installation of the Bleed Transferred Pressure
 Transducer (7HA1,7HA2) AMM 36-11-51-000-040 Removal of the High Pressure Bleed Valve (4000HA) AMM 36-11-51-400-040 Installation of the High Pressure Bleed Valve
 (4000HA) AMM 36-11-58-000-001 Removal of the HP Bleed Override Solenoid (11HA1, 11HA2) AMM 36-11-58-400-001 Installation of the HP Bleed Override Solenoid
 (11HA1, 11HA2) AMM 71-00-00-710-003 Engine Automatic Start ASM 36-11/02
 3. Fault Confirmation
__________________
 A. Test
 (1) Not Applicable
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 281
 --Feb 01/05R ---CES -

 4. Fault Isolation
_______________

R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 A. If the fault symptom is identified by the maintenance message: HP BLEED-V 4000HA2 OR SENSE LINE
 -do a check of the unions of the sense line at the bleed pressure-regulator valve (4001HA) and at the HP bleed valve (4000HA).
 (1)
 If the unions are loose:

 -tighten these unions again (to 1.6 m.daN (11.79 lbf.ft)) and refer to Para. 4B.

 (2)
 If the unions are correct:


 -make sure that the indication of the HP bleed valve position on the lower ECAM display unit is correct when you manually operate the valve shaft.
 
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