R **ON A/C 151-199, 401-499,
 Subtask 53-31-00-210-086-A
 A. Inspection Procedure
 (1)
 Do a general visual inspection of the external surfaces of the lower skins of the longitudinal lap joints in the crack stopper areas. Do this at STGR18 LH/RH, between FR35 and FR47/51:

 (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.

 (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 301-399, 
R  Subtask 53-31-00-210-086-B 
R  A. Inspection Procedure 
R  (1) Do a general visual inspection of the external surfaces of the lower 
R  skins of the longitudinal lap joints in the crack stopper areas. Do 
R  this at STGR18 LH/RH, between FR35.8 and FR47: 
R  (a) Look for scratches, dents, cracks, corrosion and damage to the 
R  surface protection. 
R  (2) If you find scratches, dents and/or cracks: 
R  (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification 
R  of the damage. 
R  (b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable 
R  damage limits for this structure. 
R  (c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
R  300-001) or (Ref. TASK 51-73-11-300-004), as necessary. 
R  (d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
R  003). 
R  (e) For damage that is more than the limits for minor damage, refer 
R  to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data. 
R  (3) If you find corrosion: 
R  (a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general 
R  corrosion data. 
R  (b) Repair the corroded areas (Ref. TASK 51-74-11-300-001) or 
R  (Ref. TASK 51-74-11-300-002), as necessary. 
R  (4) If you find damage to the surface protection: 
R  (a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data 
R  about the paint coating of the aircraft. 
R  (b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
R  001) or (Ref. TASK 51-75-12-300-003), as necessary.

 CES  **ON A/C ALL

 5. Close-up
________ Subtask 53-31-00-942-078
 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).

 TASK 53-31-00-210-038
 General Visual Inspection of Fuselage External Surface between FR35(FR35.8) and FR47, from STGR23 LH/RH to Crown Centerline, except areas below Belly Fairing
 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.
　
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