(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) for types, inspection, removal and corrosion protection.
(b)
Other damage (cracks, scratches, stress, marks, dents, bumps...):
-If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
Sliding Window Frames at FR4 - Lower Forward Corners - Inspection Area Figure 615/TASK 53-11-00-991-074
R EFF : 001-049, 051-099, 101-149, 201-299, 53-11-00Page 661 May 01/05
CES 4. Procedure
_________
Subtask 53-11-00-250-052
A. Inspection
(Ref. Fig. 615/TASK 53-11-00-991-074)
(1)
Do a special detailed inspection of the lower forward corners of the sliding window frames at FR4. Refer to the Non-destructive Testing Manual (Ref. NTM 531173,P.Block-601).
(2)
Make a report of damage after NDT inspection:
(a)
Corrosion damage:
-If you find 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 this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
5. Close-up
________
Subtask 53-11-00-410-086
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the FWD passenger/crew door 831 (841), (Ref. TASK 52-10-00-410-001).
**ON A/C ALL
TASK 53-11-00-210-013
Detailed Inspection of Windshield Center Post, Upper Attachment Area, Internal Side
1. Reason for the Job
__________________
Refer to the MPD TASK: 531131-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 3.50 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
R SRM 511100,P.Block 001 (for corrective action)
R SRM 512200,P.Block 001 (for corrective action) 53-11-00-991-014 Fig. 616
EFF : ALL
53-11-00Page 663
3. Job Set-up
__________
Subtask 53-11-00-010-056
A. Get Access R (1) Put an access platform in position at the zone 831 (841). R (2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(3) Remove the vertical lining panels 211MC, 211MW from the windshield center post.
R (4) Remove the ceiling panels 211LC, 212LC. Subtask 53-11-00-110-068
B. Cleaning of the Structure 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) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure
_________
Subtask 53-11-00-220-078
A. Inspection
(Ref. Fig. 616/TASK 53-11-00-991-014)
(1) Do a detailed inspection of the structure of the upper attachment of the windshield center post, internal side. 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(49)
