C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-73-11-300-001 Repair of Minor Damage on Aluminum Clad Components 51-73-11-300-003 Repair of Dents in Skin Panels 51-73-11-300-004 Repair of Minor Damage on Unclad Components 51-74-11-300-001 Repair of Corroded Areas 51-74-11-300-002 Removal of the Corrosion on Unpainted Light Alloy 51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
Composite Material
51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only)
ASRM 51-11-00-001
ASRM 51-22-00-001
ASRM 51-23-11-001
ASRM 53-31-11-101
ASRM 53-31-11-201 (for corrective action)
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-31-00-991-061 Fig. 637
R **ON A/C 151-199, 401-499,
53-31-00-991-061-A Fig. 637A
**ON A/C 301-399,
53-31-00-991-061-B Fig. 637B
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-31-00-941-066
A. Install the Ground Support Equipment
(1) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position at the inspection area.
Subtask 53-31-00-110-092
B. Preparation of the Inspection Areas
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.
(1)
Make sure that the surfaces of the inspection areas are clean.
(2)
If necessary, clean the inspection areas with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004).
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 637/TASK 53-31-00-991-061)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 637A/TASK 53-31-00-991-061-A)
**ON A/C 301-399,
(Ref. Fig. 637B/TASK 53-31-00-991-061-B)
Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline Figure 637/TASK 53-31-00-991-061
R EFF : 001-049, 051-099, 101-149, 201-299, 53-31-00Page B612 May 01/05
CES
Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline Figure 637A/TASK 53-31-00-991-061-A
R EFF : 151-199, 401-499, 53-31-00Page B613 Aug 01/05
CES
R R Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline Figure 637B/TASK 53-31-00-991-061-B
EFF : 301-399, 53-31-00 Page B614 May 01/04
CES
R **ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 53-31-00-210-087
A. Inspection Procedure
(1)
Do a general visual inspection of the external surface of the center fuselage:
-examine the areas between FR35 and FR47, from STGR23 LH/RH to the crown centerline
-do not examine the areas below the belly fairing.
(a) Look for scratches, dents, cracks, corrosion and damage to the surface protection.
(2)
If you find scratches, dents and/or cracks:
(a)
Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.
(b)
Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable damage limits for this structure.
(c)
Repair the scratches which are in the limits (Ref. TASK 51-73-11-300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
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