Piper CHEROKEE TURBO ARROW III 1976 Pilot Operating Handbook page 122

$ECTION 6
PIPER AIRCRAFT CORPORATION
WEIGHT AND
BALANCE PA-28R-201T, CHEROKEE TURBO ARROW IH
Arm Aft
Weight Datum
Moment
(Lbs) (Inches)
(In-Lbs)
Basic Empty Weight
Pilot and Front Passenger 80.5
Passengers (Rear Seats)
118.1
Fuel
(72
Gallon Maximum)
95.0
Baggage
142.8
Moment due
to
Retraction
of Landing Gear 8
19
Total Loaded Airplane
Totals must be within approved weight and C.G. limits. lt is
the
responsibility of the
airplane owner and
the
pilot
to
insure that the
airplane
is
loaded properly. The Basic Empty Weight C.G. is noted on the
Weight
and Balance Data
Form (Figure 6- S
).
If the airplane has been altered,
refer
to the
Weight and Balance
Record for
this
information.
WEIGHT AND BALANCE LOADING FORM
Figure 6-11
REPORT: VB-800
ISSUED: DECEMBER 20, 1976
6-12