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NON-NORMAL PROCEDURES
CONFIG Indication
The CONFIG indicator will annunciate if center tank fuel exceeds 1600 pounds (800 kilograms) and the center tank fuel pump switches are OFF or are producing low pressure. Do not accomplish the CONFIG non-normal procedure prior to or during takeoff with less than 5000 pounds (2300 kilograms) of fuel in the center tank. Do not accomplish the CONFIG non-normal procedure during descent and landing with less than 3000 pounds (1400 kilograms) of fuel in the center tank.
Pump Failure
If one center tank fuel pump fails with fuel in the center tank, turn the failed pump switch OFF. Turn the operational pump ON, if previously turned OFF. Open the fuel crossfeed valve to prevent a fuel imbalance. Turn the remaining center tank fuel pump switch OFF when the Master Caution and FUEL system annunciator lights illuminate and close the fuel crossfeed valve.
NOTE: The fuel crossfeed valve must be closed for landing.
Fuel LOW Indication
In a low fuel non-normal situation, both center tank fuel pumps may be selected ON and all center tank fuel may be used regardless of the amount of fuel remaining in the tank.
Flight Crew Operations Manual Bulletin No. SHZ-29 R3, dated July 07, 2003 (continued)
ADDITIONAL INFORMATION
Fuel Loading
For the time period that AD 2002-19-52 and AD 2002-24-51 are in effect, the zero fuel gross weight of the airplane plus the weight of center tank fuel may exceed the maximum zero fuel gross weight by up to 5000 pounds (2300 kilograms) for takeoff, climb and cruise, and up to 3000 pounds (1400 kilograms) for descent and landing, provided the effects of balance (CG) have been considered.
Ground Procedures - Defueling and Fuel Transfer
Prior to transferring fuel or defueling, conduct a lamp test of the respective fuel pump LOW PRESSURE lights. When transferring fuel or defueling from either the center or main wing tanks, monitor the fuel pump LOW PRESSURE lights and turn the fuel pumps OFF at the first indication of fuel pump low pressure. Fuel may be transferred from tank to tank or the aircraft may be defueled with passengers on board, provided the fuel quantity in the tank from which fuel is being taken is maintained at not less than 2000 pounds (900 kilograms). Deplane all passengers and non-essential crew when defueling or transferring fuel from a tank that has a fuel quantity less than 2000 pounds (900 kilograms). Wait until the process has been completed and the respective fuel pumps turned OFF before reloading non-essential crew and passengers.
Administrative Information
This bulletin replaces SHZ-29 R2, dated November 25, 2002. Discard bulletin SHZ-29 R2. Revise the Bulletin Record page to show SHZ-29 R2 as “CANCELLED” (CANC).
Insert this bulletin behind the FCOM Bulletin Record Page in Volume 1 of your FCOM.  Amend the FCOM Bulletin Record Page to show Bulletin SHZ-29 R3 "IN EFFECT" (IE)
This bulletin will be canceled after Boeing is notified that the Master Caution system logic change and the center tank fuel pump automatic shutoff feature are incorporated and the center tank fuel pumps have been inspected via an approved inspection process to ensure proper wire bundle positioning.
Flight Crew Operations Manual Bulletin No. SHZ-29 R3, dated July 07, 2003 (continued)
Please send all correspondence regarding FCOM bulletin status to one of the following addresses:
Mailing Address:  Manager 737, Flight Technical Integration & Data 
Boeing Commercial Airplane Group 
P. O. Box 3707 MS 20-89 
Seattle, WA  98124-2207 
 USA 
Fax Number:  (206) 662-7812 
Telex:  329430 Station 627 
 SITA:  LKEBO7X 
 E-MAIL:  FTID@Boeing.com 

Flight Crew Operations Manual Bulletin No. SHZ-29 R3, dated July 07, 2003 (continued)
Intentionally
Blank

Flight Crew Operations Manual Bulletin
for
 

The Boeing Company Seattle, Washington 98124-2207

737
Number: SHZ-30 Date: September 16, 2002 Document Effectivity: 
Subject:  AD-2002-19-51, Flight Control Modules 
Reason:   This bulletin informs flight crews of the flight control module. This bulletin instructions for flight crews.  potealso  provides ntial for fa operating ilure of a 

Information in this Flight Crew Operations Manual (FCOM) bulletin is recommended by The Boeing Company, but may not be FAA approved at the time of writing.  In the event of conflict with the FAA approved Airplane Flight Manual (AFM), the AFM shall supersede.  The Boeing Company regards the information or procedures described herein as having a direct or indirect bearing on the safe operation of this model airplane.
THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT
　
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