Tecnam P2002-JF, Flight Manual

Page: 420 / 435

Page A14-46
Section 6 – Weight and Balance (Additional Controls)
WEIGHT AND BALANCE
3
rd
Edition, Rev. 0
1.2 E
MPTY
W
EIGHT AND
B
ALANCE
D
ETERMINATION
The actual empty weight and balance of the aircraft configured as per MOD2002/141,
can be determined using the following table.
EQUIPMENT LIST D
ATE
:
R
IF
. D
ESCRIPTION
W
EIGHT
[kg]
D
ATUM
[m]
M
OMENT
[kg*m]
B
ASIC
A
IRCRAFT
(
REFER TO WEIGHING REPORTS
§§3
AND
4
OF THE BASIC
AFM)
We=_____ - M=_____
A
DDITIONAL
C
ONTROLS
(
REFER TO
E
QUIPMENT
L
IST
§1.1
OF THIS
S
UPPLEMENT
)
A=_____ - B=_____
T
OTAL
(
A
/
C EMPTY
): W
T
=______ - M
T
=______
C
ENTER OF GRAVITY
: C.G.
EMPTY
= M
T
/ W
T
= _______ m
C.G.
EMPTY
[%] = (C.G.
EMPTY
/1.370)*100 = _______
Use the §5 of the basic AFM to determine the aircraft’s take-off CG location and to
verify that take-off CG lies within the predetermined CG travel range.