C. G. Range And Weight - Piper SENECA III Pilot's Information Manual

SECTION
6
PIPER AIRCRAFT
CORPORATION
WEIGHT AND BALANCE
PA-34-220T,
SENECA HI
4750
-
MAX. T.O. WEIGHT
92
94
90
4513
-
MAX.
LANDING
WT
4470
-
MAX. ZERO FUEL W
4400
88
4200
4000
84
82
3000
2800
T
2600-p-
.:t
2400_Q_Q
<
WEIGHT
2200
I
I
VS
82
84
86 88
90 92 94
C.G. ENVELOPE
C. G. LOCATlON (INCHES AFT DATUM)
Moment
change due
to retracting
Landing Gear
=
-32
in.
-
lbs.
C.G. RANGE AND WEIGHT
Figure 6-15
REPORT: VB-1110
ISSUED: JANUARY
8, 1981
6-14