Piper SENECA III - Weight Limits; Center of Gravity Limits

SECTION 2
PIPER AIRCRAFT
CORPORATION
LIMITATIONS
PA-34-220T,
SENECA
III
2.11
WEIGHT
LIMITS
(a)
Max.
Ramp
Weight
4773 LBS.
(b)
Max
Takeoff
Weight
4750
LBS.
(c)
Max.
Landing
Weight
4513
LBS.
(d) Max.
Weights
in Baggage
Compartments
Forward
100
LBS.
Aft
100
LBS.
(e)
Max.
Zero
Fuel
Weight
-
Standard
(Refer
to
Section
6,
Weight
and
Balance)
4470 LBS.
2.13
CENTER
OF
GRAVITY
LIMITS
Weight
Forward
Limit
Rearward
Limit
Pounds
Inches
Aft
of
Datum
Inches
Aft of
Datum
3400
82.0
94.6
4250
86.7
94.6
4750
90.6
94.6
NOTES
Straight
line
variation
between
points
given.
The
datum
used
is
78.4
inches
ahead
of
the
wing
leading
edge
at
the
inboard
edge
of
the
fuel tank.
It is
the
responsibility of
the
airplane
owner
and
the
pilot
to
ensure
that the airplane
is
properly loaded. See Section
6
(Weight
and
Balance)
for
proper
loading instructions.
REPORT:
VB-Ill0
ISSUED:
JANUARY
8, 1981
2-6