Tecnam P92 Eaglet - Weighing Report; Center of Gravity Limits

P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
33
3.2 Weighing report
Model P92Eaglet____________S/N_____________Date ________________
Horizontal Reference
Datum
Plumb Line
W 1
W 1 =W L +W R
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
D
D
%
.
= ⋅ =
1
4
100
Empty weight moment: M = [(D+1.430)
.
We] = Kg
.
m
Maximum takeoff weight W
T
= 600 kg
Empty weight
We =
Sign: _______________
Maximum payload W
T
- We Wu =
1 - Including unusable fuel (2.3 kg).
3.2.1 Center of Gravity Limits
Forward limit 20% MAC 1.743 m (68,6”)
Aft limit 33% MAC 1.925 m (75.8”)
Datum Propeller support flange w/o spacer
Bubble Level Cabin floor