(2)  
Access Panels
 7201 Boost Pump Access Door
 7202 Boost Pump Access Door

 C. Procedure
 S 282-060
 (1)  Do these steps to do an inspection of the left boost pump for the center tank:
 (a)  
Remove the access panel 7201 in the bottom wing skin to get access to the left boost pump for the center tank.

 (b)  
Do a check of the electrical bond between the left fuel boost pump for the center tank and the airplane structure (SWPM 20-20-00). 1) The resistance must not be more than 0.0002 ohms.

 (c)  
Install the access panel for the boost pump.

 S 282-061
 (2)  Do these steps to do an inpsection of the aft boost pump for the No. 1 tank:
 (a)  
Remove the access panel 7203 in the bottom wing skin to get access to the aft boost pump for the No. 1 tank.

 (b)  
Do a check of the electrical bond between the aft fuel boost pump for the No. 1 tank and the airplane structure (SWPM 20-20-00). 1) The resistance must not be more than 0.0002 ohms.

 (c)  
Install the access panel for the boost pump.

 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE
_______ LE AND TE FLAPS AND FLAP DRIVE MECHANISMS. THE LEADING EDGE AND THE TRAILING EDGE CONTROL SURFACES CAN EXTEND AND RETRACT QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (d)  Extend the leading edge flaps (AMM 27-81-00/201) to get accss to the forward fuel boost pump for the No. 1 tank.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 28-00-00
 ALL  ú ú 01 Page 215 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO
_______ INSTALL THE LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE SAFETY LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (e)  
Install the flap locks on the leading edge flaps (AMM 27-81-00/201).

 (f)  
Do a check of the electrical bond between the forward fuel boost pump for the No. 1 tank and the airplane structure (SWPM 20-20-00). 1) The resistance must not be more than 0.0002 ohms.

 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO
_______ REMOVE THE LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT REMOVE THE SAFETY LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (g)  Remove the flap locks from the leading edge flaps if you installed them (AMM 27-81-00/201).
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE
_______ THE LE AND TE FLAPS AND FLAP DRIVE MECHANISMS. THE LEADING EDGE AND THE TRAILING EDGE CONTROL SURFACES CAN EXTEND AND RETRACT QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (h)  Retract the leading edge flaps if they are extended (AMM 27-81-00/201).
 TASK 28-00-00-282-062
 8.  Fuel System Fault Current, No. 2 Tank - Inspection__________________________________________________
 A. References
 (1)  
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 (2)  
SWPM 20-20-00, Standard Wiring Practices Manual

 B. Access
 (1)  
Location Zones
 403 Right Inboard Wing Leading Edge
 405 Right Fuel Tank

 (2)  
Access Panels
 7401 Boost Pump Access Door
 7402 Boost Pump Access Door

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 28-00-00
 ALL  ú ú 01 Page 216 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 C. Procedure
 S 282-063
 (1)  Do these steps to do an inspection of the right boost pump for the center tank:
 (a)  
Remove the access panel 7401 in the bottom wing skin to get access to the right boost pump for the center tank.
　
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