-If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types, inspection, removal and corrosion protection.
(b)
other damage (cracks, scratches, stress, marks, dents, bumps,...):
-If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
5. Close-up
________ Subtask 53-11-00-410-057
A. Close Access
(1)
Install the lining panel 211NW (212NW).
(2)
Install the lining panel 211PW (212PW).
(3)
Close the sliding window.
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
(5)
Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-001).
(6)
Remove the access platform(s).
R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
TASK 53-11-00-210-029
Special Detailed Inspection of Windshield Side Post at FR 4, Lower Attachment, Internal Side, LH/RH
1. Reason for the Job
__________________
Refer to the MPD TASK: 531133-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.5 m (11 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door
52-10-00-410-001 Closing of the Passenger/Crew Door
NTM 531133,P.Block-601
SRM 511100,P.Block 001 (for corrective action)
SRM 512200,P.Block 001 (for corrective action)
53-11-00-991-040 Fig. 617
53-11-00-991-075 Fig. 619
R EFF : 001-049, 051-099, 101-105, 151-154, 53-11-00Page 672 201-207, May 01/05
CES 3. Job Set-up
__________
Subtask 53-11-00-010-069
A. Get Access
(1)
Put an access platform in position at the zone 831 (841).
(2)
Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-001).
(3)
Open the sliding window.
(4)
Remove the lining panel 211PW (212PW).
(Ref. Fig. 617/TASK 53-11-00-991-040)
(5)
Remove the lining panel 211NW (212NW) from the side post at FR4. (Ref. Fig. 617/TASK 53-11-00-991-040)
Subtask 53-11-00-110-070
B. Preparation of the Inspection Area
(Ref. Fig. 619/TASK 53-11-00-991-075)
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.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1)
Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
(2)
Make sure that the surface of the inspection area is clean and smooth.
(3)
Do a check of the inspection area for damage or discontinuities.
R EFF : 001-049, 051-099, 101-105, 151-154, 53-11-00Page 673 201-207, May 01/05
CES
Lower Attachment Area of the Windshield Side Post at FR4 - Internal Side Figure 619/TASK 53-11-00-991-075
R EFF : 001-049, 051-099, 101-105, 151-154, 53-11-00Page 674 201-207, May 01/05
CES (4) Make sure that there is no:
(a)
Corrosion damage:
-If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block 001) types, inspection, removal and corrosion protection. 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1(51)
