(3)
 Install the applicable access panels (Ref. TASK 57-55-11-400-001):
 -for the left wing, install 533AT, 533CB
 -for the right wing, install 633AT, 633CB. R **ON A/C 106-149, 215-299, 401-499,
 Subtask 57-53-00-410-067-A
 A. Close Access
 (Ref. Fig. 618A/TASK 57-53-00-991-019-A)
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.
 (2)
 Install the applicable access panels (Ref. TASK 57-55-11-400-001):
 -
for the left wing, install 533AT, 533CB
 -
for the right wing, install 633AT, 633CB.
 (3) Install the rubber grommets in the applicable inspection holes. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-53-00-865-098
 B. Make sure that this(these) circuit breaker(s) is(are) closed: 6CV, 8CV.
 Subtask 57-53-00-860-118
 C. Aircraft Maintenance Configuration
 (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009).
 Subtask 57-53-00-942-073
 D. Removal of Equipment
 (1)
 Remove the warning notice(s).
 (2)
 Remove the access platform(s).
 (3)
 Remove the safety barriers.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A623 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
 (4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A624 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 57-53-00-220-010
 Special Detailed Inspection of Outboard Flap, Support at Track 4, Including RIB14, Fitting Assembly, Pendulum Support and Attachment Structure ....
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 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.
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 575313-02 Special detailed inspection of outboard flap, support at track 4, including RIB 14, fitting assembly, pendulum support and attachment structure, internal and external, LH/RH
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notices
 No specific access platform 2.5 m (8 ft. 2 in.)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A625 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-061A  D DAN 220
 ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-62-000-003 Removal of the Leading Edge Panels 2 and 5 on the
 Outboard Flap 27-54-62-400-003 Installation of the Leading Edge Panels 2 and 5 on
 the Outboard Flap 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
 4
 NTM 57-53-13 PART 9
 ASRM 575300 (for corrective action)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 57-53-00-991-020  Fig. 619 
R **ON A/C 106-149, 215-299, 401-499,
 57-53-00-991-020-A  Fig. 619A 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A626 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 
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 WINGS 机翼4(97)