R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-15-41Page 404 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 28-15-41-650-050

 B. Fuel Configuration
 (1)
 Defuel the applicable fuel tank (Ref. TASK 28-25-00-650-001).

 (2)
 Drain the remaining fuel from the applicable fuel tank (Ref. TASK 28-25-00-650-003).

 Subtask 28-15-41-865-050
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/XFR VALVE1/WING/R 2QP A11 49VU FUEL/XFR VALVE1/WING/L 1QP A10 121VU FUEL/XFR VALVE2/WING/R 4QP M23 121VU FUEL/XFR VALVE2/WING/L 3QP M22
 Subtask 28-15-41-010-050
 D. Get Access
 (1)
 Put the access platform below the applicable zone 540(640).

 (2)
 Remove the applicable access panels (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-27-11-000-002):

 -
FOR 27QM, 28QM
 remove 540JB, 540KB

 -
FOR 29QM, 30QM
 remove 640JB, 640KB.

 4. Procedure
_________ **ON A/C 001-001, 051-052,
 (Ref. Fig. 401/TASK 28-15-41-991-001)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-15-41Page 405 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 28-1077 For A/C 001-001,051-052, (Ref. Fig. 401A/TASK 28-15-41-991-001-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 28-15-41-020-050
 A. Removal of the Transfer Valve
 (1)
 Hold the transfer valve (5) and remove the bolts (1). FOR 28QM, 30QM

 (2)
 Remove the bracket (2).

 (3)
 Pull the transfer valve (5) away from the transfer valve drive (6) and remove the transfer valve (5).

 (4)
 Remove and discard the O-ring(s) (3) and/or (4).

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-15-41Page 406 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 28-15-41-400-001

 Installation of the Transfer Valve 27QM (29QM), 28QM (30QM)
 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 safety barriers
 No specific access platform 3.0 m (9 ft. 10 in.)

 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. 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) FOR FIN 27QM, 29QM Material No. 09-007 USA MIL-S-4383
 BRUSHABLE FUEL RESISTANT COATING (Ref. 20-31-00) FOR FIN 28QM, 30QM Material No. 09-007 USA MIL-S-4383
 BRUSHABLE FUEL RESISTANT COATING (Ref. 20-31-00)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-15-41Page 407 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
3 O-ring 28-15-05 01 -110 4 O-ring 28-15-05 01 -110
 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 28-15-00-710-002 Operational Check of Individual Transfer Valves to
 Ensure Valve Shaft Rotates Valve to Open Position 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
　
中國(guó)航空網(wǎng) www.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 FUEL 燃油2(64)