Weight Limits; Center Of Gravity Limits - Piper SENECA III Pilot's Information Manual

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