S 024-067

 (9)  
Remove the float valve.

 S 144-067

 (10)
 Remove the unwanted sealant from the float valve area.

 TASK 28-15-11-404-074
 5. Float Valve in the No./2 and 3 Main Tank Installation (Fig. 401)
_____________________________________________________
 A. General
 (1)  
The installation of the float valves in the No. 2 and 3 main tanks is almost the same. Use this procedure to install the float valves in the No. 2 or 3 main tanks.

 B.
Equipment

 (1)  
Bonding Meter (AMM 20-22-01/601)

 C.
Consumable Materials

 (1)  
D00128 Petrolatum - Technical, VV-P-236

 (2)  
Use one of these sealants:

 (a)  
A00908 Sealant - Pro-seal 860, B 1/6

 (b)  
A00702 Sealant - BMS 5-26 Type II Class B

 D.
References

 (1)  
AMM 20-11-15/401, Bonding Jumpers and Ground Leads

 (2)  
AMM 20-22-01/601, Electrical Bonding

 (3)  
AMM 28-11-00/201, Fuel Tanks

 (4)  
AMM 28-11-02/401, Reserve and Main Tank Access Doors

 E.
Access

 (1)  
Location Zones 544 Inbd Main Tank (Part), Mid Spar to Rear Spar, left 644 Inbd Main Tank (Part), Mid Spar to Rear Spar, right

 (2)  
Access Panels
 544AB Main Tank Access Door, Left
 644AB Main Tank Access Door, Right

 F.
Install the Float Valve(s)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 03 Page 410 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 014-077
 WARNING:_______OBEY ALL THE FUEL TANK PURGING AND ENTRY PRECAUTIONS. YOU CAN CAUSE AN INJURY TO A PERSON AND CAUSE DAMAGE TO THE AIRPLANE.
 (1)  
Go into the applicable No. 2 or 3 main tank.

 S 424-076

 (2)  
Use the sealant to apply a faying surface seal to the float valve and the structure.

 S 424-078

 (3)  
Put the float valve in the correct position.

 S 424-080

 (4)  
Attach the bolt, washer and nut (4 locations) but do not tighten the bolts until the couplings are attached to the float valve.

 S 434-082

 (5)  
Tighten the tube coupling nut to the float valve.

 S 434-084

 (6)  
Tighten the bolts.

 S 434-086

 (7)  
Install the lockwire on the coupling nut and the structure.

 S 434-088

 (8)  
Tighten the bonding clamp(s) and the tube support brackets if they were loosened for removal (AMM 20-11-15/401).

 S 284-071

 (9)  
Measure the bonding resistance between these components
 (AMM 20-22-01/601):

 NOTE: The bonding resistance must not be more than 0.010 ohm.
____
 (a)  
The float valve and the structure

 (b)  
The bonding jumpers (if the bonding jumpers were loosened for the removal).

 G.
Put the Airplane Back to the Usual Condition

 S 864-061
 (1)  Remove all of the unwanted material from the applicable main tank (AMM 28-11-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 414-070
 (2)
Install the applicable access door (AMM 28-11-02/401):

 (a)
Main tank No. 2 access door - 544AB

 (b)
Main tank No. 3 access door - 644AB.

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 ALL  ú ú 03 Page 412 ú Feb 10/93
　
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