Tecnam P92 Echo MK2 - 3.2 Weighing report

P92 LSA
Flight Manual
Rev.0
33
3.2 Weighing report
Model P92____________S/N __________________ Date ________________
Datum: Propeller support flange w/o spacer. - Equipment list, date: _____
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
Empty weight moment: M = [(D+1.519)
.
We] =Kg
.
m
Maximum takeoff weight
W
T
=
600 kg
Empty weight
We =
Sign: _______________
Maximum payload W
T
- We
Wu =
1 - Including unusable fuel