WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let the area dry.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 644/TASK 53-41-00-991-056)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 644A/TASK 53-41-00-991-056-A)
**ON A/C 301-399,
(Ref. Fig. 644B/TASK 53-41-00-991-056-B)
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 53-41-00-210-112
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
-the fuselage external surface between FR47 and FR70, from stringer 23 LH/RH to bottom centerline, exept the area that is covered by the belly fairing.
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline Figure 644/TASK 53-41-00-991-056
R EFF : 001-049, 051-099, 101-149, 201-299, 53-41-00Page B600 May 01/05
CES
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline Figure 644A/TASK 53-41-00-991-056-A
R EFF : 151-199, 401-499, 53-41-00Page B601 Aug 01/05
CES
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline Figure 644B/TASK 53-41-00-991-056-B
R EFF : 301-399, 53-41-00Page B602 Nov 01/04
CES NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
R **ON A/C 151-199, 401-499,
Subtask 53-41-00-210-112-A
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
-the fuselage external surface between FR47/51 and FR70, from stringer 23 LH/RH to bottom centerline, exept the area that is covered by the belly fairing.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
**ON A/C ALL
5. Close-up
________
Subtask 53-41-00-942-090
A. Remove the ground support equipment.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
TASK 53-41-00-210-811
General Visual Inspection of Upper Skin of Longitudinal Lap Joints, including Crack Stopper Areas at Stringer 18 LH/RH, External Surface
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 TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______ FALL CAN INJURE OR KILL YOU.
1. Reason for the Job
__________________
Refer to the MPD TASK: 534114-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
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