Weight And Balance Loading Form - Piper SARATOGA II HP PA-32R-301 Pilot Operating Handbook

SECTION6
WEIGHT AND BALANCE PA-32R-301, SARATOGA IT HP
,
Arm Aft
Weight Datum
Moment
(Lbs) (Inches)
(In-Lbs)
Basic Empty Weight
Pilot and Front Passenger 85.5
Passengers
(Center Seats)
119.1
Passengers (Rear Seats)
157.6
Fuel (102 Gallon Maximum)
94.0
Baggage (Forward) (100 Lb. Limit) 42.0
Baggage (Aft) (100 Lb. Limit)
178.7
Ramp Weight (3615Lbs. Max.)
Fuel Allowance for Engine
Start, Taxi & Runuo -15.0
94.0 -1410
Take-off Weight (3600 Lbs. Max.)
The center of gravity (C.G.) for the take-off weight of this loading
problem is at inches aft of the datum line; Locate this point on the C.G.
range and weight graph. Since this point falls within the weight - C.G.
envelope, this loading meets the weight and balance requirements.
Take-off Weight
Minus Estimated Fuel Bum-off
(climb & cruise)
@
6.0 Lbs/Gal.
94.0
Landing Weight
Locate the center of gravity of the landing weight on the C.G. range and
weight graph. Since this point falls within the weight - C.G. envelope, the
loading may be assumed acceptable for landing.
IT IS THE RESPONSIBILITY OF THE PILOT AND AIRCRAFT
OWNER TO INSURE THAT THE AIRPLANE IS LOADED
PROPERLY AT ALL TIMES.
WEIGHT AND BALANCE LOADING FORM
(NORMAL CATEGORY)
Figure 6-11
REPORT: VB-1669
ISSUED: JUNE 30, 1997