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Tecnam P2010 2015 - Center of Gravity Range; Flight Crew

Tecnam P2010 2015
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13.
WEIGHTS
Condition
W
eight
Maximum takeoffweight I
160kg
25571b
Maximum landing weight 1160 kg
2557lb
Maximum baggage weight 40 kg
881b
Baggage C
ompartment
Weight
Maximum weight 40 kg 881b
Maximum specific pressure
0.72 kg/dm
2
14.9 lb/ft
2
Refer to Section 6
for
proper aircraft
and
baggage loading.
14.
CENTER
OF
GRAVITY
RANGE
Datum
Levelling
Forward limit
Aft limit
Vertical plane tangent
to
the wing leading edge (the aircraft
must be levelled
in
the longitudinal plane)
Refer to the seat track supporting beams (see procedure
in
Section 6)
0.262 m (10.3 in)
(19%
MAC) aft
of
datum for all weights
0.440 m (17.3 in)
(32%
MAC) aft
of
datum for all weights
The
pilot is responsible
for
ensuring that the
G1rplane
is
properly loaded. Refer
to
Section 6
for
appropriate instruc-
tions.
15.
FLIGHT
CREW
Minimum crew: I pilot
Maximum seating configuration:
4 people (including the pilot)
Approved
2"d
Ed1110n
, Rev. I
Section
2 -
Limitations
WEIGHTS

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