POH FK 14 B
FK Lightplanes
Revision 23
Weight & Balance
page 6-3
document code: FK 14 des.002
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]
Right wheel
WR = 115,2
L 2 = 0,557
64,17
Left wheel
WL = 118
L 2 = 0,557
65,73
Nose wheel
WF = 70,7
L 1 =- 0,828
- 58,54
Empty weight-
Empty weight
C.G.
data
303,9
0,235
71,35
Pilot(s) / fuel
158,6
L 3 = 0,57
90,4
Baggage aft
5
L 4 = 1,21
6,05
Baggage forward
5
L 5 = -0,28
-1,40
Total Weight
C.G
(0,28 to 0,431)
Total Moments
Total
472,5
0,352
166,405
Form:
Position
Weight [kg]
Arm [m]
Moment [mkg]
Right wheel
WR = _____
L 2 = _____
_____
Left wheel
WL = _____
L 2 = _____
_____
Nose wheel
WF
= _____
L 1 =-_____
_____
Empty weight-
Empty weight
C.G.
Data
Pilot(s) / fuel
______
L 3 = 0,57
_____
Baggage aft
_____<
10kg
L 4 = 1,21
_____
Baggage forward
______
L 5 = -0,28
_____
Total Weight
C.G
(0,28 to 0,431)
Total Moments
Total