May 01/04
R
CES
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,
53-31-00-991-060 Fig. 636
R **ON A/C 151-199, 401-499,
53-31-00-991-060-A Fig. 636A
**ON A/C 301-399,
53-31-00-991-060-B Fig. 636B
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-31-00-941-065
A. Install the Ground Support Eqipment
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the inspection area.
Subtask 53-31-00-110-091
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. 636/TASK 53-31-00-991-060)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 636A/TASK 53-31-00-991-060-A)
**ON A/C 301-399,
(Ref. Fig. 636B/TASK 53-31-00-991-060-B)
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH Figure 636/TASK 53-31-00-991-060
R EFF : 001-049, 051-099, 101-149, 201-299, 53-31-00Page B602 May 01/05
CES
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH Figure 636A/TASK 53-31-00-991-060-A
R EFF : 151-199, 401-499, 53-31-00Page B603 Aug 01/05
CES R Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH R Figure 636B/TASK 53-31-00-991-060-B
R EFF : 301-399, 53-31-00Page B604 May 01/04
CES R **ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 53-31-00-210-086
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:
(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) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FUSELAGE 机身2(92)
