-refer to the procedure steps in the NTM (Ref. NTM 534129-Part.6), 'Preparation for Inspection'
 -measure the thickness of the paint at the inspection areas
 -make sure that the paint thickness is less than the given limit.
 (2)
 Write a report about the damage you find during the inspection procedure.

 (3)
 If you find damage:

 (a)
 Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification of the damage.

 (b)
 If you find corrosion damage:

 -
refer to the ASRM (Ref. ASRM 51-22-00-001) for the general corrosion data

 -
refer to the AMM (Ref. AMM 51-74-00-001) for the repair of the corroded areas.

 (c)
 If you find other types of damage:

 -refer to the ASRM (Ref. ASRM 53-41-11-101) for the necessary data.
 5. Close-up
________
 Subtask 53-41-00-370-061
 A. Repair of the Surface Protection
 (1) If necessary, repair the paint coatings in the inspection areas (Ref. TASK 51-75-12-300-003) or (Ref. TASK 51-75-12-300-001).

 Subtask 53-41-00-410-164
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the floor panels 162JF and 161AF (Ref. TASK 53-42-17-400-001) in the bulk cargo compartment.

 (3)
 Close the bulk cargo-compartment door (Ref. TASK 52-30-00-860-008).

 (4)
 Remove the access platform(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 INTENTIONALLY BLANK

 **ON A/C ALL

 TASK 53-41-00-210-834
 Detailed Visual Inspection of AFT Passenger/Crew Door-Cutout above Cabin Floor Level, at FR66 and FR68 from STGR22 to STGR23 and around Girt Bar Fittings
 1. Reason for the Job
__________________
R Refer to the MPD TASK: 534143-01
 2. Job Set-up Information
______________________
 A. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 11-026  GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)

 Material No. 15-005  AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 15-006  AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 25-23-45-000-003 Removal of the Door Frame Linings at the Left AFT Passenger/Crew Door 25-23-45-000-004 Removal of the Door Frame Linings at the Right AFT Passenger/Crew Door 25-23-45-400-005 Installation of the Door Frame Linings at the Right
 AFT Passenger/Crew Door
 25-23-45-400-008 Installation of the Door Frame Linings at the Left
 AFT Passenger/Crew Door

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  51-73-11-300-001 51-73-11-300-004 51-74-11-300-001 52-10-00-010-001 52-13-31-000-003 52-13-31-400-003 ASRM 51-11-00-001 ASRM 51-11-11-001 ASRM 51-22-00-001 53-41-00-991-095  Repair of Minor Damage on Aluminum Clad ComponentsRepair of Minor Damage on Unclad ComponentsRepair of Corroded AreasOpening of the Passenger/Crew Door Removal of the Girt Bar Fittings Installation of the Girt Bar Fittings(for corrective action)Fig. 663
 3. Job Set-up__________
 Subtask 53-41-00-010-170
 A. Open the AFT passenger/crew door (Ref. TASK 52-10-00-010-001).
 Subtask 53-41-00-860-069
 B. Aircraft Maintenance Configuration
 (1) Energize the ground service network (Ref. TASK 24-42-00-861-001).
 (2) Set the light switches in the passenger compartment to ON.
 Subtask 53-41-00-010-171
 C. Get Access 
R R  (1) Remove the door frame linings of the AFT passenger/crew doors (Ref. TASK 25-23-45-000-003) and (Ref. TASK 25-23-45-000-004). 
　
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3(68)