-
FOR 43QM, 45QM
remove 640PB.
**ON A/C 301-399,
Subtask 28-11-43-010-050-A
C. Get Access
(1)
Put the access platform below the applicable access panel 540PB(640PB).
(2)
Remove the applicable access panel (Ref. TASK 28-10-00-910-002), (Ref. TASK 28-12-46-000-001):
-
FOR 42QM, 44QM
remove 540PB
-
FOR 43QM, 45QM
remove 640PB.
1EFF : ALL 1 28-11-43Page 403 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
4. Procedure
_________
(Ref. Fig. 401/TASK 28-11-43-991-001)
Subtask 28-11-43-020-050
A. Removal of the Gravity Fill Cap/Adaptor
(1)
Remove the cap (2) from the adaptor (4).
(2)
Remove the lanyard (3) from the locking plate (9) and remove the cap (2).
(3)
Remove and discard the cotter-pin (12) from the cap (2) and remove the lanyard (3).
(4)
Drill out the rivets (8) from the locking plate (9) and the nut (7) and remove the locking plate (9).
(5)
Make sure that you remove all the swarf from the work area.
(6)
Remove the nut (7) from the adaptor (4) with the SPANNER-OVERWING FILLER (98D28004000000).
(7)
Remove the insulating gasket (10) and the seal ring (11) from the adaptor (4).
(8)
Remove the adaptor (4) from the wing.
(9)
Remove and discard the O-rings (5) and (6).
1EFF : ALL 1 28-11-43Page 404 1 1 May 01/04 1 1 1CES 1
Gravity Fill Cap/Adaptor. Figure 401/TASK 28-11-43-991-001
1EFF : 1 1R 1CES ALL 1 11 1 28-11-43 Page 405 May 01/04
TASK 28-11-43-400-001
Installation of the Gravity Fill Cap/Adaptor
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
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific access platform 3.5 m (11 ft. 6 in.)
No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) R 98D28004000000 1 SPANNER-OVERWING FILLER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 01-001 USA ASTM-D-1655-93 (JET A-1) FUEL, TURBO (Ref. 20-31-00) Material No. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 06-011 GB ABR 1-4055 SOLID FILM LUBRICANT (Ref. 20-31-00) Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
1EFF : ALL 1 28-11-43Page 406 1 1 May 01/04 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(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
-------------------------------------------------------------------------------
5 O-ring 28-11-05 25 -040 6 O-ring 28-11-05 25 -050 8 blind rivets 28-11-05 25 -010 12 cotter pin 28-11-43 01 -010
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas
中國航空網(wǎng) www.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1(153)
