Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
52-41-00-010-002 Open the Avionics Compartment Doors for Access 52-41-00-410-002 Close the Avionics Compartment Doors after Access 53-12-13-000-001 Removal of the avionics compartment floor panels 53-12-13-400-001 Installation of the avionics compartment floor panels SRM 511100 P.Block 001 (for corrective action) SRM 512200 P.Block 001 (for corrective action)
R 53-11-00-991-019 Fig. 632 CES

 3. Job Set-up__________
 Subtask 53-11-00-010-060
 A. Get Access 
R  (1) Put an access platform in position at zone 824.
 (2) Open the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-010-002). 
R  Subtask 53-11-00-020-059-A 
R R  B. Removal of the Components (Ref. Fig. 632/TASK 53-11-00-991-019) 
R R  (1) Remove the two quick-release pins (1) and lift and remove the ladder (2), if necessary. 
R R  (2) Remove the floor panel 127BG (4) of the avionics compartment (Ref. TASK 53-12-13-000-001).
 Subtask 53-11-00-110-077
 C. 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.

R  NLG Well - Rear Panel Aft Face - Lower Corners Figure 632/TASK 53-11-00-991-019
 EFF :  ALL  53-11-00 Page A619 Aug 01/03
 CES 

 4. Procedure
_________

 Subtask 53-11-00-220-082
 A. Inspection (Ref. Fig. 632/TASK 53-11-00-991-019)
 (1) Do a detailed inspection of the structure of the NLG well. This inspection is applicable to the rear panel aft face, lower corners, left and right sides.
 (2) Make sure that there is no: 
R R R  (a) Corrosion damage: - If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types of corrosion, inspection, removal and corrosion protection. 
R R  (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________ 
R  Subtask 53-11-00-420-057-A 
R R  A. Installation of the Components (Ref. Fig. 632/TASK 53-11-00-991-019) 
R R  (1) Install the floor panel 127BG (4) in the avionics compartment (Ref. TASK 53-12-13-400-001). 
R R  (2) Install the ladder (2) on the floor fittings (3), if necessary, and install the two quick-release pins (1).
 Subtask 53-11-00-410-060
 B. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Close the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-410-002).

 EFF : ALL 53-11-00Page A620 Feb 01/04
 CES

 (3) Remove the access platform(s).

 EFF : ALL 53-11-00Page A621

Aug 01/03
R
 CES  TASK 53-11-00-210-019

 Detailed Inspection of Internal Structure around Forward Passenger/Crew Door above Cabin Floor Level, between FR 15 and FR 21 and between Stringer 8 and...
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 531163-01
 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 -------------------------------------------------------------------------------
No specific masking paper Material No. 08-074 MASKING TAPE (Ref. 20-31-00)
　
中國航空網 www.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1(61)