(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 ASRM (Ref. ASRM 51-74-00-001) for the repair of the corroded areas.
EFF : ALL 53-31-00Page A643
May 01/04
R
CES (c) If you find other types of damage:
-refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of the minor damage
NOTE : No repair data is given in the ASRM (Ref. ASRM 53-31-14-
____ 001) for the upper flanges of the longitudinal floor beams at FR42 and FR46. If you find damage which is more than the limits for minor damage:
-you must contact AIRBUS INDUSTRIE for the necessary corrective action procedure.
5. Close-up
________ Subtask 53-31-00-370-050
A. Repair of the Surface Protection
(1) If necessary, refer to the ASRM (Ref. ASRM 51-75-12-001) and repair the paint coating in the inspection areas.
Subtask 53-31-00-410-078
B. Close Access
(1)
Connect the electrical wire bundles to the floor beams at FR42 and FR43.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Install the floor panels 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF (Ref. TASK 53-32-12-400-002).
(4)
Install the equipment and furnishing, removed to get access to the cabin floor panels.
Subtask 53-31-00-860-055
C. Put the aircraft back to its initial configuration.
(1) De-energize the ground service network
(Ref. TASK 24-42-00-862-001)
EFF : ALL 53-31-00Page A644
May 01/04
R
CES TASK 53-31-00-220-004
Special Detailed Inspection of Lower Skin of Longitudinal Lap Joint at Stringer 18LH and Stringer 18RH, in Runout Area at FR42, Internal
1. Reason for the Job
__________________
Refer to the MPD TASK: 533138-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific abrasive cloth, grade 280
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 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power 25-23-43-000-001 Removal of the Upper Sidewall Panel(s) 25-23-43-400-001 Installation of the Upper Sidewall Panel(s) 25-80-00-000-001 Removal of the Insulation Blankets 25-80-00-400-001 Installation of the Insulation Blankets ASRM 51-11-00-001 ASRM 51-22-00-001
EFF : ALL 53-31-00Page A645
May 01/04
R
CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
NTM 533138-Part.6
ASRM 51-73-00-001 (for corrective action)
ASRM 51-74-00-001 (for corrective action)
ASRM 51-75-12-001 (for corrective action)
ASRM 53-31-11-101 (for corrective action)
ASRM 53-31-11-201 (for corrective action)
53-31-00-991-029 Fig. 623
3. Job Set-up
__________
Subtask 53-31-00-860-056
A. Aircraft Maintenance Configuration
(1) Energize the ground service network
(Ref. TASK 24-42-00-861-001).
Subtask 53-31-00-010-081
B. Get Access
(1)
Remove the necessary upper sidewall panels LH/RH in the area of FR42 and FR43 (Ref. TASK 25-23-43-000-001).
(2)
Remove the necessary insulation blankets in the area of STGR18 LH/RH at FR42 (Ref. TASK 25-80-00-000-001).
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2(78)
