On the lower ECAM display unit, on the F/CTL page:
-
the indexes which show the position of the elevators and spoilers 2, 3 and 4 move in relation to the side stick orders.
On the overhead panel 23VU:
-
the OFF legend of the FLT CTL/SEC 1 comes on.
On the overhead panel 24VU:
-
the OFF legend of the FLT CTL/SEC 2 goes off.
On the lower ECAM display unit, on the F/CTL page:
-
the indexes which show the position of the elevators and spoilers N. 2 and 5 move in relation to the side stick orders.
On the upper ECAM display unit:
-
the F/CTL ELAC 1 FAULT and F/CTL ELAC 2 FAULT messages go out of view.
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1DA1, 1DA2, 2DA1, 2DA2, 2DA3, 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 4DG1, 4DG2, 5DA1, 5DA2, 5DA3, 5DG1, 5DG2 Subtask 27-96-00-860-084
B. Put the aircraft back to the initial configuration
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
on the overhead panel 23VU:
-push the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches, the OFF legends go off).
(3)
On the overhead panel 24VU:
-push the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend goes off).
(4)
On the overhead panel 20VU, on the ADIRS CDU:
-set the 3 OFF/NAV/ATT selector switches to OFF.
(5)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(6)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(7) Remove the warning notice. Subtask 27-96-00-410-065
C. Close Access
(1)
Install the protective cover on the battery power center 105VU.
(2)
Tighten the two screws.
(3)
Close the access door 822.
(4)
Remove the access platform(s).
1EFF : ALL 1 27-96-00Page A507 1 1 Aug 01/05R 1 1 1CES 1
TASK 27-96-00-710-020
Operational Test of the Side Stick Assembly (Activation for the BITE Test)
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1. Reason for the Job
__________________
This test is applicable only during a trouble-shooting action.
This test activates a BITE test on the EFCS in a special configuration
defined by the trouble-shooting procedure.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
B. 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 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump
1EFF : ALL 1 27-96-00Page A508 1 1 Aug 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump
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 FLIGHT CONTROLS 飛行操縱9(157)
