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9/8/98 AC 43.13-1B TO CHECK: MOST FORWARD WEIGHT AND BALANCE EXTREME. GIVEN: Actual empty weight of the aircraft -------------------------------------------------------------------------- 1169# Empty weight center of gravity------------------------------------------------------------------------------- + 10.6” *Maximum weight----------------------------------------------------------------------------------------------2100# *Forward C.G.. limit ------------------------------------------------------------------------------------------- + 8.5” *Oil capacity, 9 qts. -------------------------------------------------------------------------------------------- 17# at -49” *Pilot in farthest forward seat equipped with controls (unless otherwise placarded) ----------------------------------------------------------------------- 170# at +16” *Since the fuel tank is located to the rear of the forward C.G. limit, minimum fuel should be included. METO HP = 165 = 13.75 gal. x 6#--------------------------------------------------------------------------83# at +22” 12 12 * Information should be obtained from the aircraft specification. Note: Any items or passengers must be used if they are located ahead of the forward C.G. limit. Full fuel must be used if the tank is located ahead of the forward C.G. limit. CHECK OF FORWARD WEIGHT AND BALANCE EXTREME Weight (#) x Arm (“) = Moment (“#) Aircraft empty + 1169 Oil +17 Pilot + 170 Fuel + 83 Total + 1439 (TW) +10.6 + 12391 -49 - 833 + 16 + 22 + 2720 + 1826 + 16104 (TM) Divide the TM (total moment) by the TW (total weight) to obtain the forward weight and balance extreme. TM = 16104 = + 11.2” TW 1439 Since the forward C.G. limit and the maximum weight are not exceeded, the forward weight and balance extreme condition is satisfactory. FIGURE 10-10. Example of check of most forward weight and balance extreme. Par 10-16 Page 10-13PDF Image | AFS-640
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