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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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 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 71-00-00-710-003 Engine Automatic Start 71-00-00-710-004 Engine Manual Start 71-00-00-710-028 Engine Shutdown
 3. Job Set-up
__________
 Subtask 30-21-00-861-051
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 Subtask 30-21-00-860-060
 B. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (2)
 Start the engine (Ref. TASK 71-00-00-710-003) or (Ref. TASK 71-00-00-710-004).

 (3)
 On the ANTI ICE section of the panel 25VU:


 -make sure that the ENG1(2) pushbutton switch is released (the FAULT and ON legends are off).
 1EFF : ALL 1 30-21-00Page 505 1 1 Aug 01/02R 1 1 1CES 1


 Subtask 30-21-00-865-063
 C. 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
 4. Procedure
_________ R **ON A/C 001-049, 056-056, 058-058, 061-099, 101-105, 151-199, 201-211,
 Subtask 30-21-00-710-051
 A. Operational Test of the Engine Air Intake Protection
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ANTI ICE section of the panel 25VU: - push the ENG1(2) pushbutton switch  On the ANTI ICE section of the panel25VU, on the ENG 1(2) pushbuttonswitch:- the ON legend comes on - the FAULT legend comes on for a short time during movement of the valve (the engine air intake anti ice valve opens). On the upper ECAM DU: - the ENG A.ICE message comes into view - on the MEMO section, the IGNITION
 message comes into view.
 2. On the ANTI ICE section of the panel 25VU: - release the ENG1(2) pushbutton switch  On the ANTI ICE section of the panel25VU, on the ENG 1(2) pushbuttonswitch:- the ON legend goes off - the FAULT legend comes on for a short time during movement of the valve (the engine air intake anti ice valve closes). On the upper ECAM DU: - the messages go out of view.

 


R **ON A/C 051-055, 057-057, 059-060, 106-149, 212-299, 301-399, 401-499,
 Subtask 30-21-00-710-051-A
 A. Operational Test of the Engine-Air-Intake Ice Protection
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ANTI ICE section of the panel 25VU: - push the ENG1(2) pushbutton switch  On the ANTI ICE section of the panel25VU, on the ENG 1(2) pushbuttonswitch:- the ON legend comes on - the FAULT legend comes on for a short time during movement of the valve (the anti ice valve of the engine air intake opens). On the upper ECAM DU: - the ENG A.ICE message comes into view.
 2. On the ANTI ICE section of the panel 25VU: - release the ENG1(2) pushbutton switch  On the ANTI ICE section of the panel25VU, on the ENG 1(2) pushbuttonswitch:- the ON legend goes off - the FAULT legend comes on for a short time during movement of the valve (the anti ice valve of the engine air intake closes). On the upper ECAM DU: - the message goes out of view.
 **ON A/C ALL
 5. Close-up________
 Subtask 30-21-00-860-061

 A. Put the aircraft back to its initial configuration.
 (1) Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 (2) Stop the engine (Ref. TASK 71-00-00-710-028). Subtask 30-21-00-862-051
 B. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).


 TASK 30-21-00-710-003


 Operational Test of the NAI Valve
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D36003000001 1 TEST SET - ENGINE BLEED SYSTEM
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 
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