P92 Classic
Deluxe
WEI GH T & BA LA N CE
F
LIGHT MANUAL
1
st
edition – 23
th
March 2009 Doc. n° 92-13-030-00
6-3
WEIGHING REPORT
Model
P92 C
LASSIC
DELUXE
s/n
:______
Weighing n
°______
Date
:_________
Datum
: Propeller support flange
without spacer
Kg
meters
Nose wheel weight W
1
=
Plumb bob distance from LS wheel A
L
=
LS wheel weight W
L
=
Plumb bob distance from RS wheel A
R
=
RS wheel weight
W
R
=
Average distance (A
L
+ A
R
)/2
A =
W
2
= W
L
+W
R
=
Bob distance from nose wheel.
B =
Empty weight
We = W
1
+ W
2
=
D
W
A W B
We
2
1
m
D
D
%
.
1 4
100
Empty weight moment:
M = [(D+1.39)
.
We]
=
Kg
.
m
Maximum takeoff weight
W
T
=
450 kg
Empty weight
We =
Maximum useful load
W
T
- We
Wu =