R (4) Make sure that the access panel (3) is correctly aligned with the
R adjacent panels.
R 5. Close-up________
R Subtask 57-41-37-865-089
R A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
R breaker(s):
R 5CV, 7CV
R Subtask 57-41-37-860-069
R B. Aircraft Maintenance Configuration
R (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat
R lever control.
R (2) Retract the slats (Ref. TASK 27-80-00-866-005).
R Subtask 57-41-37-942-065
R C. Removal of Equipment
R (1) Remove the access platform(s).
R (2) Remove the safety barriers.
R (3) Remove the warning notice(s).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
ACCESS PANELS AND COVERS - REPAIRS
__________________________________
TASK 57-41-37-350-001
Repair to the Leading Edge Pressure-Relief Panel 521AB(621AB) After it has Operated
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.
1. Reason for the Job
__________________
Self Explanatory
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 cutting tool
No specific extrusion gun
No specific lint-free cloth
No specific masking tape
R No specific non-metallic scraper No specific spatula No specific suction cup No specific warning notices No specific access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-064 GB ABP1-4053 RELEASE AGENT (Ref. 20-31-00) Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00) Material No. 09-002B F ASNA 0163 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (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) Material No. 19-004 WHITE TALCUM POWDER (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
140 seal 57-41-37 01 -150 140 seal 57-41-37 01K-150
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
SRM 514211 SRM 514411 SRM 574118 SRM 574126 57-41-37-991-008 Fig. 801 57-41-37-991-009 Fig. 802 57-41-37-991-013 Fig. 803
1EFF : ALL 1 57-41-37Page 802 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-41-37-991-016 Fig. 804
**ON A/C 301-399,
57-41-37-991-016-A Fig. 804A R **ON A/C 106-149, 157-199, 209-299, 301-399, 401-499,
57-41-37-991-017 Fig. 805
**ON A/C ALL
57-41-37-991-014 Fig. 806
3. Job Set-up
__________
Subtask 57-41-37-941-053
A. Safety Precautions
(1)
中國航空網(wǎng) m.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(146)
