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R C. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 51-73-11-300-001 R 51-73-11-300-003 R 51-73-11-300-004 R 51-74-11-300-001 R 51-74-11-300-002 R 51-75-12-300-001 R R 51-75-12-300-003 R ASRM 51-11-00-001 R ASRM 51-22-00-001 R ASRM 51-23-11-001 R ASRM 53-51-11-101 R ASRM 53-51-11-201 R 53-51-00-991-021
R 3. Job Set-up
__________
R Subtask 53-51-00-941-067 Repair of Minor Damage on Aluminum Clad Components Repair of Dents in Skin Panels Repair of Minor Damage on Unclad Components Repair of Corroded Areas Removal of the Corrosion on Unpainted Light Alloy Repair of Major Paint Damage on Light Alloy and Composite Material Repair of Minor Paint Damage (Topcoat Only)
(for corrective action) Fig. 619
R A. Install the Ground Support Equipment
R (1) Put a WARNING NOTICE in position to tell persons not to operate the R APU.
R (2) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position at the R inspection area.
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R Subtask 53-51-00-110-068
R B. Preparation of the Inspection Area
R (1) Make sure that the surface of the inspection area is clean.
R WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL_______
R MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
R OBEY THE MANUFACTURERS INSTRUCTIONS.
R PUT ON PROTECTIVE CLOTHING.
R DO NOT GET THEM IN YOUR MOUTH.
R DO NOT SMOKE.
R DO NOT BREATHE THE GAS.
R THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
R GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R (2) If necessary, clean the inspection area with a lint-free cotton
R cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS
R (Material No. 11-004).
R 4. Procedure_________
R (Ref. Fig. 619/TASK 53-51-00-991-021)
R Subtask 53-51-00-210-073
R A. Inspection Procedure
R (1) Do a general visual inspection of the external surface of the rear
R fuselage and the tail cone. Do this between FR70 and FR87:
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 53-51-11-101) 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).
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R R Inspection Areas of the Rear Fuselage and the Tail Cone, between FR70 and FR87 Figure 619/TASK 53-51-00-991-021
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CES
R (e) For damage that is more than the limits for minor damage, refer
R to the ASRM (Ref. ASRM 53-51-11-201) 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.
R 5. Close-up________
R Subtask 53-51-00-942-070
R A. Remove the Ground Support Equipment
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Remove the warning notice(s).
R (3) Remove the access platform(s).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
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