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 AIRPLANES WITH ISOLATED FUEL QUANTITY ú  28-41-45
 úTRANSMITTER (IFQT) ú ú ú 01.101 Page 417 ú ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 424-060
 (2)  Connect harness connector plug to mating pressure seal assembly connector on external pressure hull (Figure 401).
 S 424-061
 CAUTION: ROUTE THE IFQT (SAFE-SIDE) WIRE HARNESS WITH A MINIMUM 0.5 INCH
_______ (12.7 MILLIMETERS) CLEARANCE FROM OTHER AIRPLANE WIRING IN NON-PRESSURIZED AREAS. THE ROUTING OF THE SAFE-SIDE WIRE HARNESS IS CRITICAL FOR CORRECT OPERATION AND INTRINSIC SAFETY OF THE FQIS.
 (3)  
Install the clamps and tighten to secure the harness (Fig. 401).

 S 434-063

 (4)  
Prepare faying surface of grounding tab on grounding bracket for an electrical bond (SWPM 20-20-00).

 S 424-064

 (5)  
Install the ground strap from the backshell of new harness to existing bracket near the tank wall bussing plug (Fig. 401).

 S 424-065

 (6)  
Tighten the ground tab mounting bolts to 25-35 inch-pounds (2.8-3.9 Newton-meters).

 NOTE: Maximium permissible length of the grounding strap from the
____ backshell to the grounding bracket is 6.0 inches (152 millimeters).
 S 704-066
 (7)  Perform a bonding test from the newly installed safe-side harness as follows:
 (a)  Connect one lead of the bonding test meter to the outer lightning braid near the safe-side harness connector plug.
 NOTE: This will require sliding the probe under the
____ protective expando sleeving to get access to the metallic braid.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY ú  28-41-45
 úTRANSMITTER (IFQT) ú ú ú 01.101 Page 418 ú ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Connect the other end of the bonding meter to the grounding bracket.

 (c)  
Make sure the measured resistance is less than 0.001 ohms.

 S 434-067
 (8)  Apply BMS 5-95 sealant on all grounding bracket surfaces
 (BSWPM 20-10-20).

 J. Put the Airplane Back To Its Usual Condition
 S 724-068
 (1)  
Do the Fuel Quantity Indicating System Adjustment/Test procedure (AMM 28-41-03/501).

 S 414-029

 (2)  
Install all panels and liners (AMM 25-52-65/401).

 S 024-073
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ LEADING EDGE FLAPS SAFETY LOCKS. THE LEADING EDGE FLAPS CAN MOVE QUICKLY IF YOU DO NOT REMOVE THE SAFETY LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (3)  For tank 1 or 2, remove the flap safety locks on the leading edge flaps (AMM 27-81-00/201).
 S 034-074
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING
_______ EDGE AND TRAILING EDGE FLAP AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAPS CONTROL LEVER. THE FLAPS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (4)  For tanks 1 or 2, retract the leading edge flaps if you extended them at the start of this procedure (AMM 27-81-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY ú  28-41-45
 úTRANSMITTER (IFQT) ú ú ú 01.101 Page 419 ú ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FUEL QUANTITY INDICATOR - REMOVAL/INSTALLATION
______________________________________________
 1. General
_______
 A. This procedure has two tasks:
 (1)  A task to remove the fuel quantity indicator
 (2) A task to install the fuel quantity indicator. ú ú TASK 28-41-51-004-001 ú2. Fuel Quantity Indicator Removal (Fig. 401)
_______________________________
 A. Access
　
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