Tecnam P92 Echo MKII - Page 89

Page 6 - 5
1
rd
Edition, Rev 0
Section 6 – Weight and Balance
WEIGHING REPORT (I)
3 WEIGHING REPORT (I)
ModelP92Echo MKIIS/N: Weighing no. Date:
Datum: Propeller support flange without spacer.
Maximum takeoff weight
W
T
=
Kg
Empty weight
We =
Kg
Maximum payload W
T
- We
Wu =
Kg
(1) To determine the Mean Aerodynamic Chord (MAC) and the plumb line see FIG.6-1.
Kg
Nose wheel weight
W
1
=
LH wheel weight
W
L
=
RH wheel weight
W
R
=
W
2
= W
L
+W
R
=
meters
Plumb bob distance
(1)
LH wheel
A
L
=
Plumb bob distance
(1)
RH wheel
A
R
=
Average distance (A
L
+ A
R
)/2
A =
Bob distance from nose wheel
(1)
B =
Empty weight We = W
1
+ W
2
=
D%

D
100 
1.400
D

W
2
 A  W
1
 B


We
Empty weight moment: M = [(D+1.519)
.
We] =Kg
.
m