(d)
Repair the dents which are in the limits (Ref. TASK 51-73-11-300-003).
(e)
For damage that is more than the limits for minor damage, refer to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(3)
If you find corrosion:
(a)
Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data.
(b)
Repair the corroded areas (Ref. TASK 51-74-11-300-001) or (Ref. TASK 51-74-11-300-002), as necessary.
(4)
If you find damage to the surface protection:
(a)
Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data about the paint coating of the aircraft.
(b)
Repair the damage to the paint system (Ref. TASK 51-75-12-300-001) or (Ref. TASK 51-75-12-300-003), as necessary.
R **ON A/C 151-199, 401-499,
Subtask 53-31-00-210-087-A
A. Inspection Procedure
(1)
Do a general visual inspection of the external surface of the center fuselage:
-examine the areas between FR35 and FR47/51, 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.
(d)
Repair the dents which are in the limits (Ref. TASK 51-73-11-300-003).
(e)
For damage that is more than the limits for minor damage, refer to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(3)
If you find corrosion:
(a)
Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data.
(b)
Repair the corroded areas (Ref. TASK 51-74-11-300-001) or (Ref. TASK 51-74-11-300-002), as necessary.
R EFF : 001-049, 051-099, 101-149, 151-199, 53-31-00Page B616 201-299, 401-499, Aug 01/05
CES (4) If you find damage to the surface protection:
(a)
Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data about the paint coating of the aircraft.
(b)
Repair the damage to the paint system (Ref. TASK 51-75-12-300-001) or (Ref. TASK 51-75-12-300-003), as necessary.
**ON A/C 301-399,
Subtask 53-31-00-210-087-B
A. Inspection Procedure
(1)
Do a general visual inspection of the external surface of the center fuselage:
-examine the areas between FR35.8 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.
(d)
Repair the dents which are in the limits (Ref. TASK 51-73-11-300-003).
(e)
For damage that is more than the limits for minor damage, refer to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(3)
If you find corrosion:
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data.
R R (b) Repair the corroded areas (Ref. TASK 51-74-11-300-001) or (Ref. TASK 51-74-11-300-002), as necessary.
R (4) If you find damage to the surface protection:
R R (a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data about the paint coating of the aircraft.
R R (b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-001) or (Ref. TASK 51-75-12-300-003), as necessary.
**ON A/C ALL
5. Close-up________
Subtask 53-31-00-942-079
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 access platform(s).
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