-
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
__________________
Refer to the MPD TASK: 572656-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
No specific access platform 3.0 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) 98D57004028000 1 EXTRACTOR-PYLON SLEEVE 98D57004029000 1 SPANNER-PYLON SLEEVE B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-002 USA MIL-S-8802 TYPE I CLASS B FUEL TANK SEALANTPOLYSULFID(NO LONGER AVAILABLE (Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (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)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
4 cotter pin 57-26-05 23A-280
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
54-51-41-000-001 Removal of the Spigot Ball Joint 54-51-41-400-001 Installation of the Spigot Ball Joint ASRM 572600 (for corrective action) 57-26-00-991-003 Fig. 603 57-26-00-991-015 Fig. 604
1EFF : ALL 1 57-26-00Page 614 1 1 May 01/04R 1 1 1CES 1
3. Job Set-up
__________ Subtask 57-26-00-941-052
A. Safety Precautions
(1) Put a warning notice in the cockpit to tell persons not to start the engine 1(2).
(2) Put the safety barriers in position. Subtask 57-26-00-010-052
B. Get Access
(1)
Put the access platform below the applicable engine pylon, zone 471 (481).
(2)
Remove the applicable access panels:
-
for the left wing, remove 471AL, 472AR
-
for the right wing, remove 481AL, 482AR.
(3)
Remove the spigot ball joint (Ref. TASK 54-51-41-000-001).
4. Procedure
_________ (Ref. Fig. 603/TASK 57-26-00-991-003, 604/TASK 57-26-00-991-015) Subtask 57-26-00-020-050
A. Removal of the Pylon Spigot Sleeve
(1)
Remove and discard the cotter pin (4).
(2)
Install the SPANNER-PYLON SLEEVE (98D57004029000) on the nut (2). NOTE : It may be necessary to remove the sealant from the recess of
____ the nut (2) and from around the top of the spigot sleeve (1). This will make the removal of the nut (2) easier.
(3)
Remove the nut (2).
(4)
Clean the threads of the spigot sleeve (1):
(a) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026), to clean the threads of the spigot sleeve (1).
1EFF : ALL 1 57-26-00Page 615 1 1 May 01/04R 1 1 1CES 1
Outer Wing Pylon - Spigot Fitting Figure 603/TASK 57-26-00-991-003
1EFF : 1 1R 1CES ALL 1 11 1 57-26-00 Page 616 May 01/04
Extractor - Pylon Spigot Sleeve Figure 604/TASK 57-26-00-991-015
1EFF : 1 1R 1CES ALL 1 11 1 57-26-00 Page 617 May 01/04
(5) Install the EXTRACTOR-PYLON SLEEVE (98D57004028000): NOTE : It may be easier to remove the hydraulic cylinder (23) from
____ the body assembly (19) before you attach it to the support structure (16).
(a)
Loosen the clamp screw (24) and remove the hydraulic cylinder
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼2(19)
