(b)
Push the brake pedals more than once.
1EFF : ALL 1 32-42-27Page 604 1 1 Feb 01/05 1 1 1CES 1
Brake Unit-Wear Indicator Figure 601/TASK 32-42-27-991-002-A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-42-27Page 605 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(c) Make sure that there are no leaks on the piston housing, the pistons and the hydraulic lines.
(3)
Make sure that the bleed plugs, the temperature sensor and the self-sealing couplings are in the correct position.
(4)
With the brakes on, make sure that the wear indicators are in the limits.
NOTE : Measure the wear pin when the brake is cold (Brake temperature
____
less than 60 deg.C).
NOTE : When the end of either wear pin aligns with the machined
____ surface of the piston housing, the heat pack is fully worn. You must replace the brake unit (Ref. TASK 32-42-27-000-001). (Ref. Fig. 601A/TASK 32-42-27-991-002-B)
NOTE : For a new brake, measure the distance between the end of the
____ wear pin and the machined surface of the piston housing. This distance must be 61 mm (2.40 in.) maximum. If more than the maximun value replace the brake (Ref. TASK 32-42-27-000-001) (Ref. TASK 32-42-27-400-001). (Ref. Fig. 601A/TASK 32-42-27-991-002-B)
NOTE : The brake units usually have two wear pins.
____ If you find a brake that does not have the two wear pins: -the brake is serviceable if there is one wear pin and the wear pin is in the limits.
R -you must deactivate the brake if there is no wear pin on the R brake unit (Ref. TASK 32-42-00-040-003) .
**ON A/C ALL
5. Close-up
________
Subtask 32-42-27-860-054
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
(2)
Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 32-42-27Page 606 1 1 Feb 01/05 1 1 1CES 1
R Brake Unit-Wear Indicator
R Figure 601A/TASK 32-42-27-991-002-B
R 1EFF : 301-399, 1 32-42-27 Page 607
1 1 May 01/04
1 1
1CES 1
Subtask 32-42-27-941-055
B. Removal of Equipment
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Remove the warning notice(s).
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 32-42-27Page 608 1 1 May 01/04R 1 1 1CES 1
TASK 32-42-27-210-003
Check Heat Pack Wear indicator (Parking Brake Applied)
1. Reason for the Job
__________________
Refer to the MPD TASK: 324227-01 To do an inspection of the brake unit to make sure that the disc pads are not worn.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notices
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power
29-10-00-863-002 Pressurize the Yellow Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
32-42-00-040-002 Deactivation of the Normal Braking - With
disconnection of the Green Hydraulic Supply 32-42-27-000-001 Removal of the Brake (2641GM,2642GM,2643GM,2644GM) 32-42-27-400-001 Installation of the Brake
(2641GM,2642GM,2643GM,2644GM)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
32-42-27-991-002-A Fig. 601
**ON A/C 301-399,
32-42-27-991-002-B Fig. 601A
1EFF : ALL 1 32-42-27Page 609 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
3. Job Set-up
__________
Subtask 32-42-27-860-055
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
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(21)
