Tecnam P96 GOLF - WEIGHING REPORT

COSTRUZIONI AERONAUTICHE
TECNAM S.r.l.
P96 Golf
P96 Golf / 100
WEIGHT & BALANCE
FLIGHT MANUAL
October ‘ 98
6-3
WEIGHING REPORT MODEL P96 GOLF 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
=
=
m
D
D
%
.
=⋅ =
14
100
D
W
A
W
B
We
=
⋅− ⋅
21
Empty weight moment: M = [(D+1.39)
.
We] = Kg
.
m
Maximum takeoff weight W
T
= 544 kg
Empty weight We =
Maximum useful load W
T
- We Wu =