(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.
4. Procedure
_________ Subtask 53-31-00-220-057
A. Special Detailed Inspection Procedure
(1)
Do the special detailed inspection (Ref. NTM 533140-Part.6) of the splice plates at the circumferential skin splice at FR47. Do this externally from the STGR10 LH/RH positions, to the crown centerline.
(2)
Write a report about the damage you find during the inspection procedure.
NOTE : No repair data is given in the ASRM (Ref. ASRM 53-31-11-001)
____ for the splice plates of the circumferential skin splice at FR47. If a splice plate is damaged:
-you must contact AIRBUS INDUSTRIE for the necessary corrective action procedure.
5. Close-up
________ Subtask 53-31-00-370-053
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 53-31-00-410-082
B. Close Access
(1) Remove the access platform(s). Subtask 53-31-00-860-061
C. Put the aircraft back to its initial configuration.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the flap/slat control lever.
EFF : ALL 53-31-00Page A654
May 01/04
R
CES
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 53-31-00Page A655
May 01/04
R
CES TASK 53-31-00-220-007
Special Detailed inspection of Keel Beam Box Elliptical Cutout at FR46, LH/RH
1. Reason for the Job
__________________
Refer to the MPD TASK: 533155-03
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific abrasive cloth, grade 280 No specific warning notice No specific access platform 1.5 m (4 ft. 11 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 -------------------------------------------------------------------------------
32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
Composite Material 51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only) ASRM 51-11-00-001 ASRM 51-22-00-001 ASRM 51-73-00-001 ASRM 51-74-00-001
EFF : ALL 53-31-00Page A656
May 01/04
R
CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 53-36-11-001 NTM 511008-Part.6 NTM 533155-Part.6 ASRM 51-73-00-001 (for corrective action) ASRM 51-74-00-001 (for corrective action) 53-31-00-991-035 Fig. 630
3. Job Set-up
__________
Subtask 53-31-00-010-090
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
LANDING GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
(1)
Open the MLG doors (Ref. TASK 32-12-00-010-001).
(2)
Put the warning notice in position to tell persons not to operate the landing gear.
(3)
Put the access platform in position below the MLG compartment.
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(81)
