Dry Bay Figure 006 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1201-299, 401-499, 1 1CES  1 111 57-21-00 Page 13 Aug 01/05

 Wing box - Dry Bay 
R  Figure 006A 
R 1EFF :  301-399,  1  57-21-00 Page 14 
1  1  Aug 01/04
 1  1
 1CES  1

 The closing panels are made of carbon fiber with a honeycomb core and are attached with nuts and bolts to give easy access.
 Access is also available through the front spar.
 1EFF : ALL 1 57-21-00Page 15 1 1 May 01/05R 1 1 1CES 1

 Main Structure - General
 Figure 007

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-21-00Page 16 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 Main Structure - General 
R  Figure 007A 
R 1EFF :  301-399,  1  57-21-00 Page 17 
1  1  Aug 01/04
 1  1
 1CES  1

 MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
 TASK 57-21-00-200-001
R Detailed Inspection of Outer Wing, Top Skin, Upper Surface Around Manual R Refuelling Aperture, Between RIB19 and RIB20
 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: 572122-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notices
 No specific access platform 4.0 m (13 ft. 1 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 -------------------------------------------------------------------------------
28-11-43-000-001 Removal of the Gravity Fill Cap/Adaptor 28-11-43-400-001 Installation of the Gravity Fill Cap/Adaptor ASRM 572100 (for corrective action) 57-21-00-991-035 Fig. 601
 3. Job Set-up
__________ Subtask 57-21-00-941-082
 A. Safety Precautions
 (1)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (2)
 Put warning notices in the cockpit to tell persons not to operate the flaps or slats.

 (3) Put the safety barriers in position. Subtask 57-21-00-010-074
 B. Get Access
 (1)
 Put the access platform in position at the wing leading edge, zone 522 (622).

 (2)
 Remove the overwing refuel adapter (Ref. TASK 28-11-43-000-001).

 4. Procedure
_________ (Ref. Fig. 601/TASK 57-21-00-991-035) Subtask 57-21-00-110-050
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the area around the manual refuel opening.
 1EFF : ALL 1 57-21-00Page 602 1 1 May 01/02R 1 1 1CES 1

 Manual Refuel Opening in Rib Bay 19-20 Figure 601/TASK 57-21-00-991-035
 1EFF : 1 1R 1CES  ALL  1 11 1 57-21-00 Page 603 May 01/02

 Subtask 57-21-00-210-050
 B. Inspection
 (1) Make a detailed inspection of:
 -
the wing top skin surface (3) adjacent to the manual refuel opening

 -
the interface between the overwing refuel adapter (4) and the wing

 top skin surface (3).
 Make sure that:

 -
there is no damage to the edge of the hole
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM WINGS 機(jī)翼1(116)