(4)
 Get access through the opening 540QB(640QB) to RIB21.

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 (5)
 Remove the bolt of the sensor 19QJ1(19QJ2) that attaches the P clip

 (3) (Ref. TASK 28-46-15-000-001).

 (6)
 Remove and discard the cable-ties (1) from the harness 16QT1(16QT2).

 (7)
 Remove the nut (55), the washer (54) and the bolt (53) and remove the cable 4132VN1(4132VN2).

 (8)
 Disconnect the terminal connectors (2) from the terminal block of the fuel probe 34QT1(34QT2). (Ref. Fig. 408/TASK 28-42-43-991-008)

 (9)
 Remove and discard the terminal connectors (2) from the harness
 16QT1(16QT2).

 (10)
 Remove and discard the cable-ties (1) from the harness 16QT1(16QT2) and the fuel probe 34QT1(34QT2) body.

 (11)
 Attach an applicable length of string to the ends of the harness 16QT1(16QT2). This will help to install the new harness.

 (12)
 Put tape around the end of the harness 16QT1(16QT2). This will help to let it move more easily through the conduit.

 (13)
 Get access through the opening 540MB(640MB) to RIB17.

 (14)
 Carefully pull the harness 16QT1(16QT2) from the outboard part of the conduit, until the ends attached to the string come into view.

 (15)
 Get access through the opening 540KB(640KB) to RIB15.

 (16)
 Carefully pull the harness 16QT1(16QT2) from the inboard part of the conduit, until the ends attached to the string come into view.

 (17)
 Identify and mark the string. This will help to install the new harness.

 (18)
 Remove and discard the tape and remove the harness from the string.

 (19)
 Remove the harness from the aircraft.

 (20)
 Leave the string in position for the installation.

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 TASK 28-42-43-400-004 Installation of the Wing-Tank Outer-Cell Group B Harness 16QT1(16QT2) 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 crimping tool No specific safety barriers No specific tape
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cable-ties  28-42-05 20 -010
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 496 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003
28-10-00-910-001
28-10-00-910-002
28-25-00-650-001
28-25-00-650-003

28-25-00-869-001
28-42-00-740-001
28-46-00-740-001
28-46-15-400-009
57-27-11-000-002

57-27-11-400-002
R  ESPM 203222 28-42-43-991-009 28-42-43-991-008
3. Job Set-up
__________
 Subtask 28-42-43-941-062
 A. Safety Precautions
Pressure Refuel with Automatic Control
Safety Procedures When You Do Work in a Fuel Tank
Access to the Fuel Tanks and the Work Areas
Pressure Defuel
To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank
Fuel Transfer
Status Report (BITE)
Functional (BITE) Test
Installation of the Wing-Tank Fuel-Level Sensors
Removal of the Access Panel (540HB, 540JB, 540KB,
　
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