822.
(2)
Make sure that the access door 822 is open.
4. Procedure
_________ (Ref. Fig. 401/TASK 32-43-34-991-002) Subtask 32-43-34-420-050
A. Installation of the ABCU
(1)
Clean the component interface and/or the adjacent area.
(2)
Do a visual inspection of the component interface and/or the adjacent area.
(3)
Make sure that the bonded points are in the correct condition.
1EFF : 401-499, 1 32-43-34Page 405 1 1 Aug 01/05 1 1 1CES 1
(4)
Remove the blanking caps from the electrical connectors.
(5)
Make sure that the electrical connectors are clean and in the correct condition.
(6)
Put and hold the ABCU (6) on the bracket (7) .
(7)
Attach the bonding braid (8) (Ref. ESPM 205125) with the screw (5) and the washer (3) but do not tighten it at this step.
(8)
Install the other three screws (4) and washers (3).
(9)
Tighten the screws (4) and (5) .
(10)
Connect the electrical connectors (1) and (2).
(11)
Apply electrical bonding coating PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No. 07-001) on the screw (5).
Subtask 32-43-34-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ABCU &/Y BRK/PRESS IND 61GG C10 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33 121VU ABCU/HOT BUS/SPLY 110GG P30
Subtask 32-43-34-710-050
C. BITE Test
(1) Do the BITE test of the BSCU (Ref. TASK 32-46-00-740-001).
1EFF : 401-499, 1 32-43-34Page 406 1 1 Aug 01/05 1 1 1CES 1 NOTE : If the airline operates the aircraft in CAT 3 conditions, do
____
the LAND CAT 3 capability test:
(a)
Make sure that the CAT 3 DUAL INOP indication is not shown on the lower ECAM DU with the FADEC GND PWR 1 and 2 pushbutton switches (maintenance panel 50VU) pushed (ON legends on) and the 3 IRs aligned (Ref. TASK 34-10-00-860-004).
(b)
Do the operational test of the LAND CAT III CAPABILITY (Ref. TASK 22-97-00-710-001).
NOTE : As an alternative procedure, you can do this test without
____ the CFDS (Ref. TASK 32-42-00-710-001) and (Ref. TASK 32-51-00-720-003).
(2) On the center pedestal, on the MCDU, do the bite test of the BSCU (LRU IDENTIFICATION) (Ref. TASK 32-46-00-740-003).
5. Close-up
________ Subtask 32-43-34-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access doors 822.
(3)
Remove the access platform(s).
(4)
De-energize the aircraft electrical cicuits (Ref. TASK 24-41-00-862-002).
1EFF : 401-499, 1 32-43-34Page 407 1 1 Aug 01/05 1 1 1CES 1 DIRECT DRIVE VALVE-ALTERNATE BRAKE (97GG,98GG) - REMOVAL/INSTALLATION
_____________________________________________________________________
TASK 32-43-35-000-001
Removal of the Alternate-Brake Direct Drive Valve 97GG(98GG)
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.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架7(106)
