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AFS-640

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AFS-640 ( afs-640 )

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AC 43.13-1B 9/8/98 EXAMPLE OF THE DETERMINATION OF THE NUMBER OF PASSENGERS AND BAGGAGE PERMISSIBLE WITH FULL FUEL GIVEN: Actual empty weight of the aircraft ------------------------------------------------------------------------- 1169# Empty weight center of gravity ------------------------------------------------------------------------------ 10.6” Maximum weight----------------------------------------------------------------------------------------------- 2100# Datum is leading edge of the wing Forward center of gravity limit ------------------------------------------------------------------------------ 8.5” Rearward center of gravity limit ----------------------------------------------------------------------------- 21.9” Oil capacity, 9 qts.; show full capacity --------------------------------------------------------------------- 17# at -49” Baggage, maximum-------------------------------------------------------------------------------------------- 100# at +75.5” Two passengers in rear seat, 170# x 2 ---------------------------------------------------------------------- 340# at +48” Pilot in most rearward seat equipped with controls (unless otherwise placarded) ---------------------------------------------------------------------- 170# at +16” Full fuel, 40 gals. x 6#----------------------------------------------------------------------------------------- 240# at +22” Weight (#) + 1169 + 17 + 240 + 340* + 170 + 100 + 2036 (TW) x Arm (“) = Moment (“#) Aircraft empty Oil Full Fuel Passengers 2 rear Pilot Baggage Total + 10.6 -49 +22 +48 +16 + 75.5 + 12391 - 833 + 5280 +16320 + 2720 + 7550 + 43428 (TM) Divide the TM (total moment) by the TW (total weight) to obtain the loaded center of gravity. TM = 43428 = + 21.3” TW 2036 The above computations show that with full fuel, 100 pounds of baggage and two passengers in the rear seat may be carried in this aircraft without exceeding either the maximum weight or the approved C. G. range. This condition may be entered in the loading schedule as follows: GALLONS OF FUEL NUMBER OF PASSENGERS POUNDS OF BAGGAGE Full 2 Rear 100 * Only two passengers are listed to prevent the maximum weight of 2100 lbs. from being exceeded. FIGURE 10-12. Loading conditions: determination of the number of passengers and baggage permissible with full fuel. Page 10-18 Par 10-20

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