(2)
Remove the wing access panel (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-27-11-000-001):
-
FOR 33QM, 34QM
remove 540AB
-
FOR 35QM, 36QM
remove 640AB
(3)
Open the applicable RIB2 surge door:
-
FOR 33QM, 34QM
open 540BZ
-
FOR 35QM, 36QM
open 640BZ
(4)
Install the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000)
4. Procedure_________
(Ref. Fig. 401/TASK 28-21-43-991-001)
Subtask 28-21-43-020-050
A. Removal of the Fuel-Pump Check Valve 33QM(36QM), 34QM(35QM)
(1)
Disconnect the pipe (3) at the check-valve (2).
(2)
Remove the check-valve (2).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-21-43Page 403 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Fuel-Pump Check-Valve 33QM(36QM), 34QM(35QM)
Figure 401/TASK 28-21-43-991-001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-21-43Page 404 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(3)
Put blanking plugs on the disconnected line ends.
(4)
Remove and discard the O-ring (1).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-21-43Page 405 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 TASK 28-21-43-400-001
Installation of the Fuel-Pump Check-Valve 33QM(36QM), 34QM(35QM)
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 2.8 m (9 ft. 2 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. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-21-43Page 406 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 O-ring 28-21-05 41 -190
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 28-21-00-710-002 Operational Check of Wing Tank Pump Pressure Sense
Line Check Valves 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 57-27-11-000-001 Removal of the Access Panel (540AB, 540BB, 540CB,
540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
57-27-11-400-001 Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
28-21-43-991-001 Fig. 401
3. Job Set-up
__________
Subtask 28-21-43-941-052
A. Safety Precautions
WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(1)
You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.
(2)
Make sure that the safety barriers are in position.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-21-43Page 407 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 28-21-43-860-050
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 FUEL 燃油3(31)
