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 S 024-009
 (1) Disconnect the harness at the applicable IFQT (safe-side) (J2)
 connector (Fig. 401).
 S 024-010
 (2) Disconnect the harness at the pressure seal connector (Fig. 401).
 S 024-078
 (3) For airplanes with an auxiliary fuel tank, do the subsequent steps:
 (a) Remove the vapor bundle seal and the access cover at the tank.
 (b) Disconnect the harness from the tank connector.
 S 024-011
 (4) Remove all clamps and remove the harness (Fig. 401).
 F.  External Pressure Hull to Center Tank Wire Harness Removal
 S 024-012
 (1) Remove all the clamps from the wire harness (Fig. 401).
 S 024-013
 (2) Disconnect the harness at the bussing plug and pressure seal
 connector (Fig. 401).
 S 024-014
 (3) Remove the two screws that hold the bonding strap to the ground
 bracket at the tank bussing plug (Fig. 401).
 G.  External Pressure Hull to Left or Right Main Tank Harness Removal
 S 034-015
 (1) Find the closure panel on the leading edge of the flap well of the
 vapor seal (Fig. 402).
 S 024-016
 (2) Remove the two screws that hold the two halves of the bundle seal
 feedthrough to the panel (Fig. 402).
 S 024-017
 (3) Remove the seal components (Fig. 402).
 S 024-018
 (4) Remove all screws that hold the vapor seal closure panel to the wing
 (Fig. 402).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY  ú 28-41-45
 TRANSMITTER (IFQT)  ú ú 01.1 Page 409 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 034-019
 (5)  
Slide the panel along the vapor seal to permit access to the safe-side harness pressure seal connector (Fig. 402).

 S 024-020

 (6)  
Remove clamps and disconnect the safe-side harness from the pressure seal connector.

 S 024-021

 (7)  
Remove the harness from the vapor seal closure panel.

 S 024-022

 (8)  
Remove all clamps and disconnect the harness at bussing plug connector.

 S 024-023

 (9)  
Remove the two screws securing the bonding strap to the ground bracket at the tank bussing plug (Figure 401).

 S 024-024

 (10)
 Remove the IFQT wire harness.

 TASK 28-41-45-404-025
 3. IFQT (Safe-Side) Wire Harness Installation
__________________________________________
 A. General
 (1)  This task has these procedures:
 (a)  
Internal Pressure Hull to Left or Right Wing IFQT (Safe-Side) Wire Harness Installation

 (b)  
Internal Pressure Hull to Center Tank IFQT (Safe-Side) Harness Installation

 (c)  
Auxiliary Tank to IFQT (J2) (Safe-Side) Harness Installation

 (d)  
Right/Left Wing tank to External Pressure Hull IFQT (Safe-Side) Harness Installation

 (e)  
Center Tank to External Pressure Hull IFQT (Safe-Side) Harness Installation

 B. References
 (1)  
AMM 12-31-21/201, Access Door and Panels

 (2)  
AMM 24-22-00/201, Electrical Power

 (3)  
AMM 25-52-65/401, Cargo Compartment Ceiling Lining

 (4)  
AMM 25-52-73/401, Cargo Compartment Side Wall Lining

 (5)  
AMM 27-81-00/501, Leading Edge Flap and Slat Control System

 (6)  
AMM 28-41-02/501, Fuel Quantity Indicating System

 (7)  
AMM 32-00-01/201, Ground Lock Assemblies

 (8)  
D6-5446 Boeing Standard Wiring Practice Manual

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY ú  28-41-45
 úTRANSMITTER (IFQT) ú ú ú 01.101 Page 410 ú ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 C.
D.
E.
F.

A
　
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