Tecnam P2006T, Aircraft Flight Manual

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Page 6 - 5
Section 6 – Weight and balance
WEIGHTS AND C.G.
4
th
Edition, Rev 0
2.5. W
EIGHING RECORD
Model
P2006T
S/N
:________
Weighing no.
____
Date
:_________
Datum
: leading edge vertical
Kg or Lbs Meters or feet
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
= Plumb bob distance from nose wheel B =
Empty weight We = W
1
+ W
2
= [kg] or [lbs]

  

We
B W A W
D
1 2
[m] or [Ft]
   100
339 . 1
%
D
D
Empty weight moment: M = (D
.
We)
=
[
m
.
Kg
] or [Ft
.
Lbs]
Maximum takeoff weight W
T
= [kg] or [lbs]
Empty weight We = [kg] or [lbs]
Max. useful load W
T
- We Wu = [kg] or [lbs]
Signature
____________
__________