(6)
 Install the torque link pin (3) through the shaped spacer (6), the
 top torque link assembly and the sleeve (7).

 (7)
 Install the torque link damper (2) on the shaped spacer (6) with the washers (8), the bolts (9), the washers (11) and the bolts (10).

 NOTE : The pair of longer bolts (10) and washers (11) are installed
____
 through the bracket (12).

 (8)
 TORQUE tighten the bolts (9) and (10) in a diagonal sequence to
 between 2.7 and 2.9 m.daN (19.91 and 21.38 lbf.ft).

 (9)
 Safety the top and bottom bolts (9) and (10) together in pairs with MISCELLANEOUS (Material No. 19-010).

 (10)
 Align the apex of the top and bottom torque link assemblies.

 (11)
 Put and hold the spacer (15) in position between the top and bottom torque link assemblies.

 (12)
 Push the torque link pin (3) through the torque link damper (2) and the top and bottom torque link assemblies. Push the torque link pin

 (3) until the head is against the flange of the torque link damper (2).

 (13)
 Install the spacer (17) and the nut (18) on the torque link pin (3).

 (14)
 Hold the torque link pin (3) with the TORQUE REACTION ADAPTOR (460007242) and TORQUE tighten the nut (18) to 22.3 m.daN (164.45 lbf.ft).

 (15)
 Loosen the nut (18) and do the torque sequence two more times.

 (16)
 Loosen the nut (18) and TORQUE tighten to between 13.5 and 22.3 m.daN

 (99.55 and 164.45 lbf.ft). Make sure that the slot in the nut (18) aligns with the hole in the torque link pin (3).

 (17)
 Install the bolt (19) through the nut (18) and the torque link pin (3).

 (18)
 Install the washer (22) and the nut (21) on the bolt (19).

R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 32-11-29Page 413 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (19)
 TORQUE tighten the nut (21) to between 0.5 and 1.0 m.daN (44.24 and

 88.49 lbf.in).

 (20)
 Safety the nut (21) with the new cotter pin (20).

 (21)
 Install the cover (5) and safety with the new cable tie (4).

 (22) Fill the torque link damper (2) (Ref. TASK 12-12-32-611-006). **ON A/C ALL
 5. Close-up
________ Subtask 32-11-29-410-050
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2)
 Install the MLG wheels (Ref. TASK 32-41-11-400-006). Subtask 32-11-29-586-050

 B. Lower the Aircraft

 (1)
 Lower the aircraft off the jacks (Ref. TASK 07-12-00-582-002). Subtask 32-11-29-942-050

 C. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 32-11-29Page 414 1 1 May 01/05R 1 1 1CES 1

 HARNESS - MLG SYSTEMS, 1M, 2M - REMOVAL/INSTALLATION
____________________________________________________
 TASK 32-11-43-000-001
 Removal of the 1M and 2M Harnesses from the MLG Leg
 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. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job__________________ Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific access platform 2.0 m (6 ft. 7 in.)
 1EFF : ALL 1 32-11-43Page 401 1 1 May 01/04R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM LANDING GEAR 起落架2(110)