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Section 6 – Weight and Balance
WEIGHING REPORT (II)
3
rd
Edition, Rev 0
4.
W
EIGHING
R
EPORT
(II)
Model
P2002-JF
S/N
:________
Weighing no.
____
Date
:_________
Datum
: Propeller support flange without spacer.
W2=WL+WR
1337
D
B
W1
Datum
A
* 100
W2 * A - W1 * B
D =
D% =
1370
W1 + W2
D
Reference line
Kg
meters
Nose wheel weight
W
1
=
Plumb bob distance
(1)
LH wheel
A
L
=
LH wheel weight
W
L
=
Plumb bob distance
(1)
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
(1)
B =
Empty weight We = W
1
+ W
2
=
D
W
A W B
We
2
1
m
100
370
.
1
%
D
D
Empty weight moment: M = [(D+1.337)
.
We]
=
Kg
.
m
Maximum takeoff weight
W
T
=
Kg
Empty weight
We =
Kg
Maximum payload W
T
- We
Wu =
Kg
(1) To determine the Mean Aerodynamic Chord (MAC) and the plumb line see FIG.6-1.
Summary of Contents for P2002-JF
Page 22: ...Page 1 14 Section 1 General 3rd Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 46: ...Page 3 2 Section 3 Emergency procedures INDEX 3rd Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 94: ...Page 5 20 Section 5 Performances 3rd Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 134: ...Page 9 4 Section 9 Supplements SUPPLEMENTS LIST 3rd Edition Rev 0 INTENTIONALLY LEFT BLANK ...
Page 209: ...Page A08 13 Section 9 Supplements Supplement no A08 VFR Night Equipment 3rd Edition Rev 0 ...