(2)
Write a report if you find damage during the inspection procedure.
(3)
If you find damage:
(a)
Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.
(b)
If you find corrosion damage:
-
refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data
-
refer to the ASRM (Ref. ASRM 51-74-00-001) for the repair of the corroded areas.
R EFF : 001-049, 051-099, 101-149, 151-199, 53-41-00Page C602 201-299, 401-499, Aug 01/05
CES (c) If you find other types of damage:
-
refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of the minor damage
-
refer to the ASRM (Ref. ASRM 53-41-11-101) for the allowable damage limits for this structure
-
refer to the ASRM (Ref. ASRM 53-41-11-201) for the repair data for this structure.
**ON A/C 301-399,
Subtask 53-41-00-220-050-B
A. Special Detailed Inspection Procedure
(1)
Do the special detailed inspection of the lower skin of the longitudinal lap joint in the crack stopper areas. Do this at the lower rivet row at STGR 32 LH, between FR47 and FR48, external surface, from the inside (Ref. NTM 534116-Part.6).
(2)
Write a report if you find damage during the inspection procedure.
(3)
If you find damage:
(a)
Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.
(b)
If you find corrosion damage:
-
refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data
-
refer to the ASRM (Ref. ASRM 51-74-00-001) for the repair of the corroded areas.
(c)
If you find other types of damage:
-
refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of the minor damage
-
refer to the ASRM (Ref. ASRM 53-41-11-101) for the allowable damage limits for this structure
-
refer to the ASRM (Ref. ASRM 53-41-11-201) for the repair data for this structure.
**ON A/C ALL
5. Close-up
________
Subtask 53-41-00-370-053
A. Repair of the Surface Protection
(1) If necessary, repair the paint coatings in the inspection areas (Ref. TASK 51-75-12-300-003) or (Ref. TASK 51-75-12-300-001).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 53-41-00-410-080
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the insulation (Ref. TASK 25-80-00-400-001).
(3)
Install the sidewall panels in the AFT cargo-compartment (Ref. TASK 25-55-11-400-003).
(4)
Install the belly-fairing access panels 197BB and 197GB (Ref. TASK 53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
**ON A/C 301-399,
Subtask 53-41-00-410-080-A
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the insulation (Ref. TASK 25-80-00-400-001).
(3)
Install the sidewall panels in the AFT cargo-compartment (Ref. TASK 25-55-11-400-003).
(4)
Install the belly-fairing access panels 197KB and 197GB (Ref. TASK 53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
**ON A/C ALL
Subtask 53-41-00-860-056
C. Put the aircraft back to its initial configuration.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the flap/slat control lever.
(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 C605
Nov 01/04
R
CES TASK 53-41-00-220-006
Special Detailed Internal Inspection of the Lock Fittings and Adjacent Structure at the AFT Cargo-Compartment Door.
1. Reason for the Job
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