(11)
 Install the applicable MLG door swivel-joint assembly (Ref. TASK 32-31-38-400-001).

 (12)
 Install the applicable MLG door-actuating cylinder (Ref. TASK 32-31-35-400-001).

 (13)
 Install the bonding straps (5), the bolts (6), the washers (3) and the nuts (2) to the hinge attachment points (4) (Ref. TASK 20-28-00-912-004).

 (14)
 Safety the nuts (2) with a new cotter pin (1).

 (15)
 Apply SEALANTS (Material No. 09-016) to the heads of the bolts (6) and the nuts (2).

 (16)
 Install the applicable MLG door assembly (Ref. TASK 32-12-11-400-001).

 1EFF : ALL 1 32-12-00Page 436 1 1 Nov 01/00R 1 1 1CES 1

 Subtask 32-12-00-640-050
 B. Lubrication
 (1) Lubricate the applicable door hinge connection points (Ref. TASK 12-22-32-640-001).
 Subtask 32-12-00-710-054
 C. Operational Test
 (1) Do an operational test of the main landing gear doors (Ref. TASK 32-31-00-710-002).
 Subtask 32-12-00-420-062
 D. Installation of the Secondary Hinged Fairing and Attachments
 (Ref. Fig. 404/TASK 32-12-00-991-010)

 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
 CARBONFIBER REINFORCED PLASTIC.

 (1)
 Remove the applicable fixed fairing assembly (Ref. TASK 32-12-14-000-001).

 (2)
 Clean the component interfaces and/or the adjacent area.

 (3)
 Do an inspection of the component interfaces and/or the adjacent area.

 (4)
 Make sure that the parts retained from the removed components are clean and in the correct condition.

 (5)
 Put the actuating rod (74) between the lugs of the transfer block (80).

 1EFF : ALL 1 32-12-00Page 437 1 1 Nov 01/00R 1 1 1CES 1

 (6)
 Install the threaded insert (81), the spacer (76), the pin (77), the washer (78) and the bolt (79) to the transfer block (80).

 (7)
 Install the nut (75), the bonding strap (84), the washer (82) and the bolt (83) to the transfer block (80) (Ref. TASK 20-28-00-912-004).

 (8)
 Apply SEALANTS (Material No. 09-016) to the heads of the bolts (79) and (83) and the nut (75).

 (9)
 Install the packer (72), the shim (71), the hinged fairing mounting plate (66), the washer (70) and loosely install the nut (68).

 (10)
 Install the screws (67) and loosely install the nuts (73).

 (11)
 Hold the mounting plate (66) in the position identified before removal.

 (12)
 Tighten the nuts (73) and the nut (68).

 (13)
 Safety the nut (68) with a new cotter pin (69).

 (14)
 Apply SEALANTS (Material No. 09-016) to the heads of the screws (67) and the nuts (68) and (73).

 (15)
 Install the applicable secondary-hinged-fairing attachment (Ref. TASK 57-26-21-400-001).

 (16)
 Install the applicable secondary hinged fairing (Ref. TASK 32-12-13-400-001).

 Subtask 32-12-00-420-063
 E. Installation of the MLG Fixed Fairing Assembly and Attachments
 (Ref. Fig. 403/TASK 32-12-00-991-009)

 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
 CARBONFIBER REINFORCED PLASTIC.

 1EFF : ALL 1 32-12-00Page 438 1 1 Nov 01/00R 1 1 1CES 1

 (1)
 Clean the component interfaces and/or the adjacent area.

 (2)
 Do an inspection of the component interfaces and/or the adjacent area.

 (3)
 Make sure that the parts retained from the removed components are clean and in the correct condition.

 (4)
 Remove and discard the cotter pin (51) from the nut (50).

 (5)
 Remove the nut (50), the washer (49) and the bolt (48) from the bracket (46).

 (6)
 Install the bonding strap (47), the bolt (48), the washer (49) and the nut (50) (Ref. TASK 20-28-00-912-004).
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護(hù)手冊 AMM LANDING GEAR 起落架3(15)