(4)
Remove the warning notice(s).
(5)
Remove the safety barriers.
(6)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-51-00Page A600 1 1 May 01/04R 1 1 1CES 1
TASK 57-51-00-200-008
R Special Detailed Inspection of Outer Wing, Trailing Edge Bottom Skin Aft of R Rear Spar, Above the MLG Reinforcing
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.
1. Reason for the Job
__________________
Refer to the MPD TASK: 575160-01
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.)
98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-13-000-001 Removal of the Secondary Hinged Fairing 32-12-13-400-002 Installation of the Secondary Hinged Fairing (That
was Removed for Access Only) NTM 57-51-60 PART 2 NTM 57-51-60 PART 6 ASRM 575100 (for corrective action) 57-51-00-991-018 Fig. 617
3. Job Set-up
__________
(Ref. Fig. 617/TASK 57-51-00-991-018)
Subtask 57-51-00-941-068
A. Safety Precautions
(1)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2)
Put the safety barriers in position.
(3)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
Subtask 57-51-00-865-084
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
1EFF : ALL 1 57-51-00Page A602 1 1 May 01/04R 1 1 1CES 1
Outer-Wing Trailing-Edge, Aft of the Rear Spar - Location and Detail Figure 617/TASK 57-51-00-991-018
1EFF : ALL 1 57-51-00Page A603 1 1 May 01/04R 1 1 1CES 1
**ON A/C 001-049, 051-061, 101-103, 201-203,
Subtask 57-51-00-010-069
C. Get Access
(1)
Remove the applicable secondary hinged fairing (Ref. TASK 32-12-13-000-001).
(2)
Put the access platform below the applicable wing trailing edge at the MLG support RIB5, zone 574(674).
(3) Open the applicable access panel 574AB(674AB). R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
Subtask 57-51-00-010-069-A
C. Get Access
(1)
Remove the applicable secondary hinged fairing (Ref. TASK 32-12-13-000-001).
(2)
Put the access platform below the applicable wing trailing edge at the MLG support RIB5, zone 574(674).
(3) Remove the applicable access panel 574AB(674AB).
**ON A/C ALL
4. Procedure
_________
(Ref. Fig. 617/TASK 57-51-00-991-018)
Subtask 57-51-00-110-084
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the trailing edge bottom wing skin aft of the rear spar, above the MLG reinforcing.
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3(104)
