(2)
Remove the hubcap (4). NOTE : Remove the hubcap along the centerline of the wheel axle to
____ prevent damage to the tachometer drive shaft.
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 417 1 1 May 01/05 1 1 1CES 1
Main Wheel Hubcap
Figure 402/TASK 32-41-00-991-035
1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 418 1 1 May 01/05 1 1 1CES 1
5. Close-up
________ Subtask 32-41-00-942-058
A. Remove the Safety Devices:
(1)
Remove the warning notice.
(2)
Remove the wheel chocks at the main landing gear.
(3)
Make an entry in the log book.
1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 419 1 1 May 01/05 1 1 1CES 1 TASK 32-41-00-440-002
Reactivation of the Main Wheel hubcap
1. Reason for the Job
__________________
Refer to the CDL TASK: 32-2
Main Wheel Hubcap
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific warning notice No specific wheel chocks
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-003 USA MIL-T-5544
GRAPHITED PETROLATUM THREAD COMPOUND (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 420 1 1 May 01/05 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-12-00-582-002 Jacking for Main Gear Wheel Change 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 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump 32-42-00-720-002 Functional test of the tachometers 32-41-00-991-035 Fig. 402
3. Job Set-up
__________
Subtask 32-41-00-941-059
A. Safety Precautions
(1)
On the panel 400VU:
-put a warning notice in position to tell persons not to operate the landing gear control lever.
(2)
Make sure that the wheel chocks are in position.
Subtask 32-41-00-865-059
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------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
1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 421 1 1 May 01/05 1 1 1CES 1 Subtask 32-41-00-860-058
C. Aircraft Maintenance Configuration
(1)
On the panel 110VU:
-Make sure that the PARK BRK control switch is set to ON.
(2)
On the panel 400VU:
-make sure that the brake pressure indication on the Yellow brake-pressure triple indicator is correct.
-If necessary pressurize the brake accumulator with the yellow pump (Ref. TASK 29-24-00-863-001).
(3)
Lift the related axle with a jack (Ref. TASK 07-12-00-582-002).
(4) Fully deflate the tire. Subtask 32-41-00-420-050
D. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(3)
Do an inspection of the component interface and/or the adjacent area.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架6(51)
