ceD PATS AIRPLANE FLIGHT MANUAL SUPPLEMENT (AFMS) AFMS-ST01716NY-F-25 THE BOEING COMPANY 737-700 IGW SEVEN-CELL (2-FWD AND 5-AFT) AUXILIARY FUEL SYSTEM WEIGHT AND BALANCE DATA The Auxiliary Fuel System (AFS) Weight and Balance data provided in this section should be used to supplement the actual aircraft weight and balance data provided for the specific airplane. Refer to the D043A570-cccX, Boeing 737-7001GW BBJ Weight and Balance Control and Loading Manual. The individual Fuel Cell Weight and Balance data are provided in the following table. 737-700 PATS 2-FWD / 5-AFT AUXILIARY FUEL SYSTEM WEIGHT AND BALANCE DATA FUEL CELL FUEL LOADED FUEL WEIGHT BALANCE ARM MOMENT Position ID U.S. Gallons gm Ku inches in-lbs I in-kgs / Number 1000 1000 FWD 2 3A 524 3511 1593 433.00 1520 690 TANK 1 4 517 3464 1572 473.60 1641 744 GROUP FTG FTG CAPACITY VSO 1041 6975 3165 453.16 3161 1434 NOTE: Capacity weight based @6.7 @3.04 typical fuel density: lbs / gal kgs / gal 6,975 3.165 MINUS: Amount of unusable fuel (32) (15) in FWD Tank Group (5) FTG USABLE: 1036 6943 3150 AFT 1 5 447 2995 1359 754.40 2259 1025 TANK 2 6 526 3524 1599 792.00 2791 1266 GROUP 3 6 526 3524 1599 832.10 2932 1331 ATG 4 7 508 3404 1544 872.20 2969 1347 5 8 301 2017 915 914.00 1843 836 ATG CAPACITY VSO 2308 15464 7016 827.42 12795 5805 NOTE: Capacity weight based @6.7 @3.04 typical fuel density: lbs I qal kgs / aal 15,464 7,016 MINUS: Amount of unusable fuel (92) (42) in AFT Tank Group (14) ATG USABLE: 2294 15371 6974 AFS CAPACITY USABLE 3330 22314 10124 NOTE: Capacity weight based on typical fuel density of 6.7 lbs (3.04 kgs) per U.S. gallon MAXIMUM ALLOWABLE FUEL FUEL TOTALS VSO 3349 23778 10784 NOTE: Maximum allowable fuel weight based on 7.1 lbs (3.22 kgs) per U.S. gallon Table 2. Weight and Balance Data FAA APPROVED: February 21, 2014 SECT 1 - LIMITAT