F
LIGHT
M
ANUAL
Date
:
Issue 3: 25
th
May 2010
6-4
P92-JS
SECTI ON 6
WEIGHT & BALANCE
WEIGHING REPORT
Model
P92-JS
S/N
: ________
Weighing n
°____
Date
:_________
Datum
: Propeller support flange w/o spacer.
–Equipment list,
date: _____
MAC:
1400 mm
Kg
meters
Nose wheel weight W
1
=
Plumb bob distance LH wheel
A
L
=
LH wheel weight
W
L
=
Plumb bob distance RH wheel
A
R
=
RH 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
(1)
We = W
1
+ W
2
=
D
W
A W B
We
2
1
m
D
D
%
.
14
100
Empty weight moment:
M
= [(D+1.405)
.
We]
=
Kg
.
m
Maximum takeoff weight
W
T
= 550 kg
W
T
= 600 kg
Empty weight
We =
We =
Sign: ____________
Maximum payload W
T
- We
Wu =
Wu =
1 - Including unusable fuel (2.3 kg).
B
W1
Plumb
L
in
e
A
W2=WL+WR
1405
DA
TU
M
D
Horizontal
Reference