(2)
Put the access platform below the applicable access panel:
-
for the left wing, below 550CB
-
for the right wing, below 650CB.
4. Procedure
_________
(Ref. Fig. 401/TASK 28-12-45-991-001) Subtask 28-12-45-020-050
A. Removal of the Panel Assembly 550CB(650CB)
CAUTION : YOU MUST REMOVE AND INSTALL THE BOLTS IN THE SPECIFIED
_______ SEQUENCE. THIS WILL PREVENT DAMAGE TO THE ACCESS PANEL.
(1)
Remove the bolts (4) in the sequence X thru A.
(2)
Remove the access panel (3) together with the overpressure protector (1).
(3)
Put a protective cover around the overpressure protector (1). NOTE : Removal of the overpressure protector 46QM (47QM) is given in
____
the AMM TASK 28-12-41-000-001.
1EFF : ALL 1 28-12-45Page 402 1 1 Feb 01/98 1 1 1CES 1
Panel Assembly 550CB (650CB)
Figure 401/TASK 28-12-45-991-001
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1 1 Feb 01/98
1 1
1CES 1
TASK 28-12-45-400-002
Installation of the Panel Assembly 550CB(650CB)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blank
No specific non metallic scraper
No specific safety barriers
No specific access platform 2.5 m (8 ft. 2 in.)
No specific container 20 l (5.2833 USgal)
No specific access platform 4.0 m (13 ft. 1 in.)
R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN) No specific Torque Wrench : range 36.00 to 220.00 lbf.in
(0.40 to 2.60 m.daN)
97A28002117002 3 PURGING TOOL
1EFF : ALL 1 28-12-45Page 404 1 1 May 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 05-002 USA MIL-P-8116 R PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 09-007 USA MIL-S-4383 BRUSHABLE FUEL RESISTANT COATING (Ref. 20-31-00) 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. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
sealing ring 28-12-45 01 -070
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 20-28-00-912-002 Electrical Bonding of Components With Conductive Bolts and Screws in the Tanks
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
28-00-00-910-001 Fuel Safety Procedures 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-12-44-000-004 Removal of the Check Valve 93QM 28-12-44-400-001 Installation of the Check Valve (93QM) 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
Center Tank 28-25-00-869-001 Fuel Transfer 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
1EFF : ALL 1 28-12-45Page 405 1 1 Aug 01/05 1 1 1CES 1 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油2(23)
