FK-Lightplanes FK 9 ELA, Руководство пользователя

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Airplane Manual FK 9 ELA FK Lightplanes
Revision 7 Weight & Balance page 6-3
6.3. Determination of C.G. for the Flight
The Pilot is responsible for proper loading of the aircraft.
The C.G. can be determined by computation. The C.G. must always be
within limits (compare chapter 2)!
Example for computation:
Data in the shaded area are taken from the “Wägebericht”.
Position Weight [kg] Arm [m] Moment [mkg]
Left wheel WL = 120,1 L 2 = 0,527 63,29
Right wheel WR = 119,1 L 2 = 0,527 62,77
Nose wheel WF = 45,8 L 1 =- 0,854 - 39,11
Empty weight-
Empty weight C.G.
data 285 0,31 86,95
Pilot(s) 150 L 3 = 0,45 67,5
Fuel fuselage 10 L 4 = 1,05 10,5
Fuel wing 0 L 6 = 0,21 0
Baggage 5 L 5 = 1,30 6,5
Total Weight C.G.
(0,22 to 0,44)
Total Moments
Total 450 0,381 171,45
Form:
Position Weight [kg] Arm [m] Moment [mkg]
Left wheel WL = _____ L 2 = _____ _____
Right wheel WR = _____ L 2 = _____ _____
Nose wheel WF = _____ L 1 =-_____ _____
Empty weight- Empty weight C.G.
Data
Pilot(s) _____ L 3 = 0,45 _____
Fuel fuselage _____ L 4 = 1,05 _____
Fuel wing _____ L 6 = 0,21 _____
Baggage _____ L 5 = 1,30 _____
Total Weight C.G.
(0,22 to 0,44)
Total Moments
Total