Piper SENECA III - C. G. Range and Weight

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