(2)
Remove the necessary floor panels (Ref. TASK 53-42-12-000-002).
(3)
Remove the lower door frame lining.
(4)
Remove the lateral galley lining.
(5)
Cleaning
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE
_______
SPECIAL MATERIAL.
THIS MATERIAL IS DANGEROUS.
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.
(a) Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and a lint free cloth.
4. Procedure
_________
R (Ref. Fig. 664/TASK 53-41-00-991-096-A)
Subtask 53-41-00-210-136
A. Inspection:
(1) Examine the cabin floor structure and structure below AFT entrance area, between FR66 and FR68 and lateral shear plates between FR66 and FR70 for corrosion. If necessary, refer to the ASRM (Ref. ASRM 53-43-00-001) for the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-916-089
A. After visual inspection do the following:
(1)
Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the cabin floor structure (Ref. TASK 51-75-13-916-002).
(2)
Apply STORAGE PRESERVATION (Material No. 15-007) or STORAGE PRESERVATION (Material No. 15-008) or equivalent to the cabin floor structure (Ref. TASK 51-75-13-916-002).
R R Cabin Floor Structure - FR66 thru FR70 Figure 664/TASK 53-41-00-991-096-A
EFF : ALL 53-41-00 Page C657 Aug 01/05
CES
R Subtask 53-41-00-410-168
R B. Close Access:
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the lateral galley lining.
R (3) Install the lower door frame lining.
R (4) Install the floor panels removed (Ref. TASK 53-42-12-400-002).
R (5) Install the cabin attendants seat(s) (if removed) (Ref. TASK 25-22-
R 41-400-001) (Ref. TASK 25-22-42-400-001).
CES
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at
Stringer 18, LH/RH to Bottom Centerline, External Surface
Figure 665/TASK 53-41-00-991-060
CES
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at Stringer 18, LH/RH to Bottom Centerline, External Surface Figure 665A/TASK 53-41-00-991-060-A
CES
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at Stringer 18, LH/RH to Bottom Centerline, External Surface R Figure 665B/TASK 53-41-00-991-060-B
CES
MAIN STRUCTURE - CLEANING/PAINTING
__________________________________
TASK 53-41-00-916-001
Apply Type I Grade 2 or 3 Temporary Protection to Fuselage External Surface and Belly Fairing Support Structure, under the belly fairing.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform No specific lint free cloth No specific non metallic scraper No specific warning notice 98D27803000000 2 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身3(70)
