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时间:2011-03-25 17:44来源:蓝天飞行翻译 作者:admin
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FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 3 6 6 6 6 23 23 30 30  cable tie cable tie cotter pin cotter pin tab-washer tab-washer cable tie cable tie cotter pin cotter pin  32-11-11 52F-03232-11-11 52G-03232-11-11 52F-00532-11-11 52G-00532-11-18 02B-30032-11-18 02E-30032-11-11 52F-03232-11-11 52G-03232-11-11 52F-00532-11-11 52G-005
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R  07-11-00-582-002 07-11-00-586-002 24-41-00-862-002 32-00-00-481-001 32-00-00-860-001 32-00-00-860-002 32-11-12-000-001  Jacking - GeneralLowering of the Aircraft for Maintenance OperationsDe-energize the Aircraft Electrical Circuits Supplied from the External PowerInstallation of the Safety Devices on the Landing Gears Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical PowerRemoval of the MLG Hydraulic Dressings

 

REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
32-11-12-400-001 Installation of the MLG Hydraulic Dressings 32-11-43-000-001 Removal of the 1M and 2M Harnesses from the MLG Leg 32-11-43-400-002 Installation of the 1M and 2M Harnesses on the MLG
 Leg
 32-11-00-991-018 Fig. 603
 32-11-00-991-019-B Fig. 604

 **ON A/C 001-003, 051-052,
 32-11-00-991-021 Fig. 605

R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-11-00-991-021-A Fig. 605A
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 32-11-00-941-074
 A. Safety Precautions
 (1)
 Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).

 (2)
 On the panel 400VU:

 -make sure that the landing-gear control-lever 6GA is in the DOWN position
 -put a warning notice in position to tell persons not to operate the landing gear.

 (3)
 Put warning notices in position to tell persons not to operate the landing gear doors.

 (4)
 Put the safety barriers in position.


 1EFF : ALL 1 32-11-00Page 618 1 1 Aug 01/05 1 1 1CES 1 Subtask 32-11-00-869-055


 B. Flight Configuration Precautions
 (1)
 If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (2)
 If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you lift the aircraft.


 Subtask 32-11-00-582-053
 C. Lift the Aircraft
 (1) Lift the aircraft on jacks (Ref. TASK 07-11-00-582-002).
 Subtask 32-11-00-010-064

 D. Get Access
 (1) Put the access platform adjacent to the applicable MLG.
 4. Procedure
_________
 (Ref. Fig. 603/TASK 32-11-00-991-018, 604/TASK 32-11-00-991-019-B)
 **ON A/C 001-003, 051-052,

 (Ref. Fig. 605/TASK 32-11-00-991-021) R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 605A/TASK 32-11-00-991-021-A)
 1EFF : ALL 1 32-11-00Page 619 1 1 Aug 01/05 1 1 1CES 1


 MLG Inspection Areas Figure 603/TASK 32-11-00-991-018
 1EFF : 1 1R 1CES  ALL  1 11 1 32-11-00 Page 620 Nov 01/04

 

R  MLG Side Stay Inspection Areas Figure 604/TASK 32-11-00-991-019-B
 1EFF : 1 1 1CES  ALL  1 111 32-11-00 Page 621 Nov 01/04

 

 MLG Torque Link Inspection Areas
 Figure 605/TASK 32-11-00-991-021

R 1EFF : 001-003, 051-052, 1 32-11-00Page 622 1 1 May 01/05 1 1 1CES 1


 MLG Torque Link Inspection Areas
 Figure 605A/TASK 32-11-00-991-021-A

R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 32-11-00Page 623 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 **ON A/C ALL


 Subtask 32-11-00-220-061
 A. Out-of-Roundness Dimensional Check of the MLG Shock-Absorber Sliding-Tube
 (1)
 At the point X, 125 mm (5.0 in) from the MLG axle center-line, measure the out-of-roundness of the MLG sliding tube. The sliding tube must be round within 40 microns (1600 micro-inches).

 (2)
 At the point Y, 600 mm (23.5 in.) from the MLG axle center-line, measure the out-of-roundness of the MLG sliding tube. The sliding tube must be round within 40 microns (1600 micro-inches).


 Subtask 32-11-00-220-062
 
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