C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
2 O rings 28-25-05 26D-395 2 O rings 28-25-05 26E-395 9 O-ring 28-25-05 26D-385 9 O-ring 28-25-05 26E-385 17 O-ring 28-25-41 03A-040 18 shim 28-25-41 03A-030
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control
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
57-27-11-400-002 Installation of the Access Panel (540HB, 540JB,
540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, ....)
ASRM 517612 (for corrective action)
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
28-25-41-991-002 Fig. 401
**ON A/C 051-051,
28-25-41-991-002-A Fig. 401A
**ON A/C ALL
28-25-41-991-003 Fig. 402
1EFF : ALL 1 28-25-41Page 409 1 1 Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
**ON A/C 051-051,
28-25-41-991-004 Fig. 403
**ON A/C ALL
28-25-41-991-006 Fig. 404
3. Job Set-up
__________
Subtask 28-25-41-941-058
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1) You must obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you do work on the fuel system.
(2) Make sure that the safety barriers are in position. R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 28-25-41-860-052
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is below the applicable access panel.
(2)
Make sure that the applicable access panels are removed:
-FOR 40QM, 41QM
622FB, 622HB, 622JB.
(3)
Make sure that the applicable access panel is removed (Ref. TASK 28-10-00-910-002):
-FOR 40QM
640JB.
1EFF : ALL 1 28-25-41Page 410 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 051-051,
Subtask 28-25-41-860-052-A
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is below the applicable access panel.
(2)
Make sure that the applicable access panels are removed:
-FOR 40QM, 41QM
622FB, 622HB, 622JB.
(3)
Make sure that the applicable access panel is removed (Ref. TASK 28-10-00-910-002):
-FOR 40QM
640JB.
(4)
Make sure that the applicable access panels are removed:
-FOR 100QM, 101QM
522FB, 522HB, 522JB.
(5)
Make sure that the applicable access panel is removed (Ref. TASK 28-10-00-910-002):
-FOR 100QM
540JB.
**ON A/C ALL
4. Procedure
_________
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401/TASK 28-25-41-991-002)
**ON A/C 051-051,
(Ref. Fig. 401A/TASK 28-25-41-991-002-A)
**ON A/C ALL
(Ref. Fig. 402/TASK 28-25-41-991-003)
1EFF : ALL 1 28-25-41Page 411 1 1 Aug 01/05 1 1 1CES 1
Dimensions and Positions, Right Wing Figure 402/TASK 28-25-41-991-003
1EFF : 1 1R 1CES ALL 1 11 1 28-25-41 Page 412 May 01/05
R **ON A/C 051-051,
R (Ref. Fig. 403/TASK 28-25-41-991-004) R **ON A/C ALL
Subtask 28-25-41-420-055
A. Preparation for Installation
(1)
Make sure that the sealing around the heads of the bolts (1) and (10) is not broken. If necessary repair the sealing (Ref. ASRM 517612).
(2)
Use CLEANING AGENTS (Material No. 11-026) and a clean MISCELLANEOUS (Material No. 19-003) to clean:
-
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4(61)
