1EFF : ALL 1 22-60-00Page 517 1 1 Feb 01/98 1 1 1CES 1
5. Close-up
________ Subtask 22-60-00-860-055
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
On the maintenance panel 50VU, release the ENG/FADEC GND PWR pushbuttons switches.
(3)
Close the circuits breakers 5WW and 4WW (if openned).
(4)
On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switch related to IR3 to OFF.
(5)
On the SWITCHING panel 8VU, set the AIR DATA selector switch to NORM.
(6)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(7)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 22-60-00Page 518 1 1 Feb 01/98 1 1 1CES 1
TASK 22-60-00-710-004 Windshear Procedure WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1. Reason for the Job__________________ To do the test of the windshear function.
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
Menu Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 22-60-00-991-001 Fig. 501
3. Job Set-up
__________ Subtask 22-60-00-860-056
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the ventilation of the electronics racks operates correctly.
(3)
On the overhead panel, on the ADIRS CDU:
-set the OFF/NAV/ATT selector switches to NAV.
(4)
On the center pedestal, on the SWITCHING panel 8VU:
-set the AIR DATA switch to CAPT/3, F/0/3 then NORM position (this action is mandatory to do the test correctly).
1EFF : ALL 1 22-60-00Page 519 1 1 Feb 01/98 1 1 1CES 1 (5) On the overhead panel, on the FLT CTL panels 23VU and 24VU:
-make sure that the FAC 1 and FAC 2 pushbutton switches are pushed (the FAULT and OFF legends are off).
(6)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001). Subtask 22-60-00-865-055
B.
Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION --------------------------------------- IDENT. LOCATION----------------------------------
49VU AUTO FLT/FCU/1 9CA1 B05
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
49VU AUTO FLT/FMGC/1 10CA1 B02
49VU AUTO FLT/MCDU/1 11CA1 B01
49VU FWS/FWC1/SPLY 3WW F01
121VU AUTO FLT/FCU/2 9CA2 M21
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU AUTO FLT/FMGC/2 10CA2 M17
121VU AUTO FLT/MCDU/2 11CA2 N20
121VU EIS/FWC2/SPLY 2WW Q07
4. Procedure_________
Subtask 22-60-00-710-053
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM AUTO FLIGHT 自動飛行2(10)
