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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