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:

 -
　
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