Magni Gyro M-16 C, Flight Manual

Page: 92 / 105

Page 92
025-00-16C M16C FLIGHT MANUAL, Issue G
02 March 2016
Each aircraft is supplied with a weighing report from the factory detailing the empty weight and c.g.
position of the gyroplane, when new. An example of which is shown below.
Angle [degr.]
Left Weel
[kg]
Right Weel
[kg]
Tail Weel
[kg]
Empty Mass
[kg]
X
Cg
[mm] Y
Cg
[mm] X
Cg min
[mm] X
Cg max
[mm] Y
cg min
[mm] Y
cg max
[mm]
1 106,325 125,68 0,25
10,6 98,275 116,975 16,2
Item
X
Cg
[mm] Y
Cg
[mm]
Empty Gyro
2062 793
Front Bagage 870 100
Rear Bagage
1695 150
Front Pilot
870 420
Rear Pilot
1695 531
Fuel
1695 427
Em pty Gyro
275 275 275 275 275 275 275 275 275 275 275
Front Bagage 0 0 0 0 0 0 0 0 0 0 0
Rear Bagage
10 0 0 0 10 0 0 10 0 0 0
Front Pilot
60 110 55 90 70 80 90 70 80 90 100
Rear Pilot 0 55 120 55 60 55 0 0 120 55 110
Fuel 5 8 8 30 30 45 48 30 10 40 15
XXXXXX 0 0 0 0 0 0 0 0 0 0 0
Total 350 448 458 450 445 455 413 385 485 460 500
X
Cg
[m m ] 1842 1718 1816 1754 1792 1772 1760 1807 1767 1753 1732
Y
Cg
[m m ] 705 663 673 662 656 659 669 676 659 657 650
Signed: Date:
Mass
[kg]
Mass
[kg]
Inspector No:
Mass
[kg]
Mass
[kg]
Mass
[kg]
Mass
[kg]
Mass
[kg]
Mass
[kg]
Mass
[kg]
Aircraft Type Aircraft Registration
Weighing Results Empty Weight and C.G.
Fuel tank capacity Front Pilot
Volume max
[liters]
Mass max
[kg]
Rear
Pilot
742
Construction N°
Date
M16C NA 16xxxxxx 11/02/16
Mass tot
Max [kg]
C. G. Limits
274,75 2062 793 500 1717 1888 643
120
Major Items C.G.
Mass max
[kg]
Mass min
[kg]
Mass max
[kg]
72 51,8 120 55
Weight and C.G. Configurations
This aircraft is within the weight and CG requirements
Mass
[kg]
Item
Mass
[kg]
620
640
660
680
700
720
740
760
1650 1700 1750 1800 1850 1900 1950
0
100
200
300
400
500
600
1 2 3 4 5 6 7 8 9 10 11
Mass
Mass max