Tecnam P92-JS - WEIGHING REPORT

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
P92-JS
S E C T I O N 6
WEIGHT & BALANCE
6-3
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 Line
A
W2=WL+WR
1405
DATUM
D
Horizontal
Reference