(2)
Drain the remaining fuel from the applicable fuel tank (Ref. TASK 28-25-00-650-003).
1EFF : 301-399, 1 28-43-21Page 426 1 1 Aug 01/04 1 1 1CES 1 1EFF : 301-399, 1 28-43-21Page 427 1 1 May 01/04 1 1 1CES 1
R Subtask 28-43-21-010-051
R C. Get Access
R (Ref. Fig. 404/TASK 28-43-21-991-004)
R (1) Put the adjustable access platform in the applicable position.
R (2) Remove the applicable access panel (Ref. TASK 28-10-00-910-001),
R (Ref. TASK 57-27-11-000-001) or (Ref. TASK 57-27-11-000-002):
R - FOR 56QM
R remove 540AB
R - FOR 57QM
R remove 640AB
R - FOR 58QM
R remove 540BB
R - FOR 59QM
R remove 640BB
R - FOR 60QM
R remove 540DB
R - FOR 61QM
R remove 640DB
R - FOR 62QM
R remove 540GB
R - FOR 63QM
R remove 640GB
R - FOR 208QM
R remove 540KB
R - FOR 209QM
R remove 640KB
R - FOR 200QM
R remove 540NB
R - FOR 201QM
R remove 640NB.
R (3) Get access to the housing 56QM(57QM) through the applicable
R spring-loaded surge door in the RIB 2.
R - FOR 56QM
R through 540BZ
R - FOR 57QM
R through 640BZ.
R (4) Install the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000) to safety
R open the applicable spring-loaded surge door.
R Magnetic-Level-Indicator Assembly
R Figure 404/TASK 28-43-21-991-004
1EFF : 301-399, 1 28-43-21 Page 428
1 1 May 01/04
1 1
1CES 1
R 4. Procedure_________
R (Ref. Fig. 404/TASK 28-43-21-991-004)
R Subtask 28-43-21-020-053
R A. Removal of the Magnetic-Level-Indicator Assembly
R (1) Remove the nuts (3) from the bolts (6).
R (2) Remove the bolts (6) from the base (2)
R (3) Remove the magnetic-level-indicator (7) from the fuel tank.
R (4) Remove and discard the O-rings (4) and (5).
1EFF : 301-399, 1 28-43-21Page 429 1 1 May 01/04 1 1 1CES 1 TASK 28-43-21-400-004
Installation of the Magnetic-Level-indicator Assembly 56QM Thru 63QM, 200QM, 201QM, 208QM, 209QM
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
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. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (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)
1EFF : 301-399, 1 28-43-21Page 430 1 1 Aug 01/04 1 1 1CES 1R C. Expendable Parts
R -------------------------------------------------------------------------------R FIG.ITEM |DESIGNATION |IPC-CSN R -------------------------------------------------------------------------------
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6(50)