(1)  
B00129 Solvent, Isopropyl alcohol or equivalent

 (2)
A00247 Sealant, BMS 5-95Access

 (1)  
Location Zones 210 Aft End of Forward Cargo Compartment (MX bay) 216 Left Main Gear Wheel Well 218 Forward End of Aft Cargo Compartment (Aux Tank) 302 Left Wing Outboard Leading Edge 303 Left Wing Inboard Leading Edge 402 Right Wing Outboard Leading Edge 403 Right Wing Inboard Leading Edge

Internal Pressure Hull to Left or Right Wing IFQT (Safe-Side) Wire Harness Installation
 S 424-026
 CAUTION: THE ROUTING OF THE MULTI-CONDUCTOR SAFE-SIDE WIRE HARNESS IS
_______ CRITICAL FOR PROPER OPERATION AND INTRINSIC SAFETY OF THE FQIS. THE SAFE-SIDE HARNESSES ARE TO BE ROUTED WITH A MINIMUM 0.5 INCH (12.7 MILLIMETERS) CLEARANCE FROM OTHER AIRPLANE WIRING IN NON-PRESSURIZED AREAS. A MINIMUM OF A 0.25 INCH (6.35 MILLIMETERS) MUST BE MAINTAINED FROM OTHER AIRPLANE WIRING IN PRESSURIZED AREAS.
 WIRE BUNDLE ROUTING AND INSTALLATION SHALL BE IN ACCORDANCE WITH SWPM SECTIONS 20-10-11 AND 20-10-12.
 ALL WORK SHALL BE IN ACCORDANCE WITH THE SAFETY PRACTICES DESCRIBED IN SWPM 20-00-10.
 (1)  Connect new harness connector plug to applicable IFQT safe-side (J2) connector
 NOTE: Installation of any new safe-side harness must follow the
____
 routing of the old harness that was removed.

 S 424-080
 (2)  Connect harness connector plug to mating pressure seal assembly connector on pressure hull (Furgure 401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY  ú 28-41-45
 TRANSMITTER (IFQT)  ú ú 01 Page 411 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 424-027
 CAUTION: ROUTE THE IFQT (SAFE-SIDE) WIRE HARNESS A MINIMUM OF A 0.25
_______ INCH (6.35 MILIIMETERS) FROM OTHER AIRPLANE WIRING IN PRESSURIZED AREAS. IF THE MINIMUM SEPARATION DISTANCE IS NOT MET, A DANGEROUS CONDITION COULD OCCUR.
 (3)  Install harness clamps and tighten to secure harness (Fig. 401).
 NOTE: Make sure harness seperation is a minimum of 0.25 inches
____
 (6.35 millimeters) from all other airplane wiring.
 S 414-030
 CAUTION: THE ROUTING OF THE MULTI-CONDUCTOR SAFE-SIDE WIRE HARNESS IS
_______ CRITICAL FOR PROPER OPERATION AND INTRINSIC SAFETY OF THE FQIS. THE SAFE-SIDE HARNESSES ARE TO BE ROUTED WITH A MINIMUM 0.5 INCH (12.7 MILLIMETERS) CLEARANCE FROM OTHER AIRPLANE WIRING IN NON-PRESSURIZED AREAS. A MINIMUM OF A 0.25 INCH (6.35 MILLIMETERS) MUST BE MAINTAINED FROM OTHER AIRPLANE WIRING IN PRESSURIZED AREAS.
 WIRE BUNDLE ROUTING AND INSTALLATION SHALL BE IN ACCORDANCE WITH (SWPM 20-10-11 AND 20-10-12).
 ALL WORK SHALL BE IN ACCORDANCE WITH THE SAFETY PRACTICES DESCRIBED IN (SWPM 20-00-10).
 (4)  
Connect the safe-side harness connector plug to J2 of the center tank IFQT connector (Fig. 401).

 S 424-031

 (5)  
Connect harness connector plug to mating pressure seal assembly connector on pressure hull.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH ISOLATED FUEL QUANTITY  ú 28-41-45
 TRANSMITTER (IFQT)  ú ú 01 Page 412 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 414-032
 CAUTION: ROUTE THE IFQT (SAFE-SIDE) WIRE HARNESS WITH A MINIMUM
_______ SEPARATION OF 0.25 INCH (6.35 MILLIMETERS) FROM OTHER AIRPLANE WIRING IN PRESSURIZED AREAS. FAILURE TO MAINTAIN THE MININUM SEPARATION COULD CAUSE A DANGEROUS CONDITION.
 (6)  Install the harness clamps and tighten to secure harness (Fig. 401).
 NOTE: Make sure harness seperation is a minimum of 0.25 inches
____
 (6.35 millimeters) from all other airplane wiring.
 S 724-033
 (7)  Do the fuel quantity indicating system adjustment test
 (AMM 28-41-03/501).

 G. Auxiliary Tank to IFQT (J2) (Safe-Side) Harness Installation
 S 424-035
 CAUTION: THE ROUTING OF THE MULTI-CONDUCTOR SAFE-SIDE WIRE HARNESS IS
　
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