Tecnam P92 Echo MKII, Руководство по эксплуатации самолета

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Page 6 - 6
1
rd
Edition, Rev 0
Section 6 – Weight and Balance
WEIGHING REPORT (II)
4 W
EIGHING
R
EPORT
(II)
Model P92Echo MKII S/N : Weighing no. Date :
Datum : Propeller support flange without spacer.
D

W
2

A

W
1

B


We
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.
D %

D

100

1.400
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
=
Empty weight moment: M = [(D+1.519)
.
We] =Kg
.
m