POH / AFM
AQUILA AT01-100C
Section 6
WEIGHT AND BALANCE
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
FM-AT01-1010-103
A.08
A.02 (15.10.2013)
25.05.2020
6 - 3
6.2 AIRCRAFT WEIGHING
Reference Datum (BE):
Leading edge of wing root rib
Horizontal reference line:
Place a wedge (800 : 77) 63 in (1600 mm) ahead of the
leading edge of the horizontal stabilizer. Place a level on the
wedge and level the aircraft.
Lever D
B
:
Distance from nose wheel to Reference Datum (BE)
Lever D
L
, D
R
:
Distance from main wheel to Reference Datum (BE)
Lever D
SL
:
Distance of C.G. to Reference Datum (BE)
Aircraft Weighing: Example in [kg, m]
Position
Weight [kg]
*
Lever [m]
=
Moment [kg*lb]
Nose Wheel
m
B
= 106
*
D
B
= - 0,840
=
M
B
= - 89
Left Main Wheel
m
L
= 200
*
D
L
= + 0,780
=
M
L
= + 156
Right Main Wheel
m
R
= 200
*
D
R
= + 0,780
=
M
R
= + 156
Total
m
Ges
= 506
M
Ges
= 223
Center of Gravity
M
Ges
/ m
Ges
=
D
SL
= 0,440
63 in
1600 mm
