Tecnam P92 Echo Super - Weight and CG Table; Information Only

P92 Echo Super
Maintenance
Manual
17
Revision Date:
10-29-2007
Revision Number: 3.01
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6.1 Weight and CG Table
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e:
! 1405 mm = 55 31”
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Meters
Distance from bob to LH wheel
A
L
=
Distance from bob to RH wheel
A
R
=
Average distance (AL+ AR)/2
A = 560 mm
Distance from bob to nose wheel
B = 1062 mm
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DATUM
FILO A
PIOMBO
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3.
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1405
D
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RIFERIMENTO
ORIZZONTALE
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W1
W2=WL+WR
B
A
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Not
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! A = 560 mm (22.05”)
! B = 1062 mm (41.8”)
Information Only - Adapted from AC 43.13-1B CHG 1
C.G. = D-((F * L) / W)
C.G. = Distance from datum to center of gravity of the airplane.
W = The weight of the aircraft at the time of weighing.
D = The horizontal distance measured from the datum to the main wheel weighing point.
L = The horizontal distance measured from the main wheel weighting point to the nose wheel weighing point.
F = Weight at nosewheel weighing point
D = 1965 mm
L = 1622 mm
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Kg
Fwd wheel weight
W
1
=
Main wheel left
W
L
=
Main wheel right
W
R
=
W2=WL+WR
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Empty weight
! W
ef
=W
1
+ W
2
=
W
# A $ W # B
D
%
2 1
%
Meters
We
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Kg
Arm (meters) D
Moment (Kg m) D # We
Net weight Wef
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Weight unusable fuel (2.6
liter 2.75 quarts)
1.9 (4.2#)
1.660 (65.35”)
3.2 (274.47 #”)
TOTAL
We =
De = Me/We =
Me =
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CG position as wing chord %
De%=De/1.4
# 100=