B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 53-00-29-101 (for corrective action) 53-41-00-991-017 Fig. 613 53-41-00-991-030 Fig. 614
EFF : ALL
53-41-00Page 660
May 01/04
R
CES
3. Job Set-up
__________
Subtask 53-41-00-941-058
A. Get Access
(1) Put the access platform in position adjacent to the window forging. 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.
(2) Carefully clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
4. Procedure
_________
(Ref. Fig. 613/TASK 53-41-00-991-017, 614/TASK 53-41-00-991-030) Subtask 53-41-00-210-072
A. Inspection
(1) Examine the window forgings at FR47 thru FR65 for cracks. NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-00-29-101) for
____
the correct repair procedure.
5. Close-up
________ Subtask 53-41-00-942-073
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-41-00Page 661
May 01/04
R
CES
Window Forgings FR47 thru FR65 Figure 613/TASK 53-41-00-991-017
R EFF : CES ALL 53-41-00 Page 662 May 01/04
Window Forgings - Allowable Damage Figure 614/TASK 53-41-00-991-030
R EFF : CES ALL 53-41-00 Page 663 May 01/04
TASK 53-41-00-210-018
Detailed Visual Inspection of Skin in Circumferential Splice at FR70 between STGR10 LH/RH and Crown Center Line, including Cutout Corners for Fin
1.
Reason for the Job
__________________
Refer to the MPD TASK: 534110-01
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific lint-free cloth
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
53-55-11-000-001 Removal of the Fairings 323AL/323AR
53-55-11-400-001 Installation of the Fairings 323AL/323AR
ASRM 53-41-11-101 (for corrective action)
53-41-00-991-018 Fig. 615
EFF : ALL
53-41-00Page 664
3. Job Set-up
__________
Subtask 53-41-00-010-091
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
- 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FUSELAGE 机身3(4)
