Tecnam P2008 - Weighing Report; Center of Gravity Limits; Distances from the Datum

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3.2 Weighing report
Model P2008____________S/N ________________ Date ________________
Datum
Reference line
Plumb line
W1
W2=WL+WR
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
=⋅= 100
373.1
%
D
D
Empty weight moment: M = [(D+1.567)
.
We] =Kg
.
m
Maximum takeoff weight W
T
= 600 kg
Empty weight
We =
Sign: _______________
Maximum payload W
T
- We Wu =
1 - Including unusable fuel
NOTE: The distances A and B vary from the aircraft with pivoting NLG configuration and the aircraft with steerable NLG.
This weighing report remains valid.
3.2.1 Center of Gravity Limits
Forward limit
20% MAC for all weights
Aft limit
33% MAC for all weights
Datum
Propeller support flange w/o spacer
Bubble Level
Cabin floor
3.2.2 Distances from the datum
The mean distances of the occupants, baggage and fuel from the datum are: