Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 147

SECTION 6
WEIGHT AND BAJ..ANCE
PIPER AIRCRAFT CORPORATION
PA-18R-201, ARROW
6.7 WEIGHT AND BALANCE DETERMINATION FOR FLIGHT
(continued)
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 Gallons Maximum)
95.0
Baggage (200 Lbs. Maximum)
142.8
Ramp Weight (2758 Lbs.
Maximum)
Fuel Allowance For Engine
Start. Taxi. and Run Up -8
95.0
-760
Moment due to Retraction
of Landing Gear 819
Takeoff Weight (2750 Lbs.
Maximum)
Totals must
be
within approved weight and e.G. limits. It is the
responsibility ofthe airplane owner and the pilot to insure that the airplane is
loaded properly. The Basic Empty Weight e.G. is noted on the Weight and
Balance Data Form (Figure 6-5). Iftheairplane has been altered. referto the
Weight and Balance Record for this information.
WEIGHT
AND
BALANCE LOADING FORM
Figure 6-11
REPORT: VB·1365
6-10
ISSUED: SEPTEMBER 15, 1988
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