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时间:2011-03-24 08:55来源:蓝天飞行翻译 作者:admin
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 External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors 30-21-00-991-001 Fig. 501
 3. Job Set-up
__________
 Subtask 30-21-00-861-052
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 1EFF : ALL 1 30-21-00Page 508 1 1 Aug 01/02R 1 1 1CES 1


 Subtask 30-21-00-865-064

 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ANTI ICE/ENG/2 1DN2 W10 122VU ANTI ICE/ENG/1 1DN1 X10
 Subtask 30-21-00-860-067
 C. Aircraft Maintenance Configuration
 (1) On the ANTI ICE section of 25VU:
 -make sure that the ENG1 (2) pushbutton switch is released.
 Subtask 30-21-00-010-064
 D. Get Access
 (1) Open the right fan cowl door (Ref. TASK 71-13-00-010-040):
 -
FOR 1000EM1
 438AR,


 -
FOR 1000EM2
 448AR.

 

 Subtask 30-21-00-010-065
 E. Open the right thrust reverser door (Ref. TASK 78-36-00-010-040):
 FOR 1000EM1
 452AR
 FOR 1000EM2
 462AR

 4. Procedure
_________
 Subtask 30-21-00-710-056
 A. Fonctional test of the NAI valve.
 (Ref. Fig. 501/TASK 30-21-00-991-001)

 (1)
 Disconnect the muscle pressure hose (2) on the NAI valve (1).

 (2)
 Connect the TEST SET - ENGINE BLEED SYSTEM (98D36003000001) to the anti-ice valve muscle pressure port.


 1EFF : ALL 1 30-21-00Page 509 1 1 Aug 01/02R 1 1 1CES 1


 Location of the Muscle Pressure Hose Figure 501/TASK 30-21-00-991-001
 1EFF : 1 1R 1CES  ALL  1 11 1 30-21-00 Page 510 Aug 01/02

 

 (3)
 Pressurize the NAI valve to 10 psig (0.6895 bar).


 (4)
 On the ANTI ICE section of 25VU:

 -Push the ENG 1 (2) pushbutton switch ON.

 (5)
 Check that the ECAM show: no disagree and no fault warning.

 (6)
 Check that the position indicator shows OPEN on the NAI valve.

 (7)
 On the ANTI ICE section of 25VU:

 -Push the ENG 1 (2) pushbutton switch OFF.

 (8)
 Check that the ECAM show: no disagree and no fault warning.

 (9)
 Check that the position indicator shows CLOSED on the NAI valve.


 (10)
 Depressurize the NAI valve.

 (11)
 Disconnect the TEST SET - ENGINE BLEED SYSTEM (98D36003000001) to the anti-ice valve muscle pressure port.

 (12)
 Connect the muscle pressure hose (2) on the NAI valve (1).


 5. Close-up
________ Subtask 30-21-00-410-064
 A. Close Access
 (1) Close the right fan cowl-door (Ref. TASK 71-13-00-410-040):
 -
FOR 1000EM1
 438AR,


 -
FOR 1000EM2
 448AR.

 

 Subtask 30-21-00-410-065
 B. Close the right thrust reverser door (Ref. TASK 78-36-00-410-040):
 FOR 1000EM1
 452AR
 FOR 1000EM2
 462AR

 Subtask 30-21-00-862-052
 C. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 DUCTS - ANTI ICE - REMOVAL/INSTALLATION
_______________________________________
 TASK 30-21-49-000-043
 Removal of the Muscle Pressure Tubes and Hoses

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific protective covers
 No specific warning notice
 No specific access platform 0.5 m (1 ft. 8 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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