SECTION 6
PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE
PA-28-236, DAKOTA
REPORT: VB-910
ISSUED: JUNE 1, 1978
6-10
REVISED: NOVEMBER 22, 1982
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 (3011 Lbs. Maximum)
Fuel allowance for engine start, taxi,
and run-up
-11
95.0
-1045
Takeoff Weight (3000 Lbs. Maximum)
Totals must be within approved weight and C.G. limits. It is the responsi bility
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 6-5). If the airplane has been altered, refer to the Weight and Balance
Record for this information.
WEIGHT AND BALANCE LOADING FORM
Figure 6-11
Summary of Contents for PA-28-236 DAKOTA
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