Tecnam P92 Eaglet, Flight Manual

Page: 33 / 65

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
D
a
tu
m
P
lu
m
b
L
in
e
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
%
.
= ⋅ =
14
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