(2)
Disconnect the electrical connectors (14) from the transmitter unit (3).
(3)
Put blanking caps on the disconnected electrical connectors.
(4)
Remove and discard the cotter pins (10).
(5)
Remove the nuts (9) and the washers (8).
(6)
Remove the bolts (5) and disengage the rods (7).
(7)
Remove and discard the cotter pins (13).
(8)
Hold the transmitter unit (3), remove the nuts (12), the washers (11), the bolts (4) and the transmitter unit (3).
1EFF : 401-499, 1 32-43-47Page 402 1 1 Aug 01/05 1 1 1CES 1
Brake-Pedal Transmitter Unit (103GG)
Figure 401/TASK 32-43-47-991-001
1EFF : 401-499, 1 32-43-47 Page 403
1 1 Aug 01/05
1 1
1CES 1
TASK 32-43-47-400-001
Installation of the Brake-Pedal Transmitter Unit (103GG)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific warning notice(s)
No specific access platform 1.8 m (5 ft. 11 in.)
98A27901002000 2 PIN, RIGGING - RUDDER CONTROL
B. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
10 cotter pins 32-42-01 06A-010 13 cotter pins 32-43-01 06 -030
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 32-43-00-710-001 Operational Check of Alternate Braking System
1EFF : 401-499, 1 32-43-47Page 404 1 1 Aug 01/05 1 1 1CES 1
3. Job Set-up
__________ Subtask 32-43-47-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the warning notice is in position in the cockpit to tell persons not to operate the brake pedals.
(3)
Make sure that the access platform is in position at the access door
811.
(4) Make sure that the access door 811 is open. Subtask 32-43-47-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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
4. Procedure
_________ Subtask 32-43-47-420-050
A. Installation of the Transmitter Unit
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Install the transmitter unit (3) on its mount.
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 LANDING GEAR 起落架7(110)
