Piper Malibu PA-46-310P Pilot Operating Handbook page 238

SECTION 6
WEIGHT AND BALANCE
PIPER AIRCRAFT CORPORATION
PA-46-310P, MALIBU
Arm Aft
Weight
Datum
Moment
(Lbs)
( Inches)
(In-Lbs)
Basic Empty Weight
Pilot and Front Passenger 135.50
Passengers (Center Seats) 177.0
Passengers (Rear Seats) 218.75
Fuel ( I 20 Gallon Maximum Usable) 150.31
Baggage (Forward) ( 100 Lb. Limit)
88.60
Baggage (Aft) ( JOO Lb. Limit)
248.23
Ramp Weight (4118 Lbs. Max.)
Fuel Allowance for Engine
Start, Taxi & Runup -18 150.3 I
-2706
Takeoff Weight (4100 Lbs. Max.)
The center of gravity (C.G.) for the takeoff weight of this loading problem
is at inches aft of the datum line. Locate this point ( ) on the
C.G. range and weight graph (Figure 6-15). If this point falls within the
weight - C.G. envelope. this loading meets the weight and balance require- '..,)
men ts.
Takeoff Weight
Minus Estimated Fuel Burn-off
(climb & cruise)
@
6.0 Lbs/ Gal.
150.31
Landing Weight
Locate the center of gravity of the landing weight on the C.G. range and
weight graph (Figure 6-15). If this point falls within the weight - C.G.
envelope, the loading is 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)
REPORT: VB-1200
6-12
Figure 6-1 I
ISSUED: JANUARY
II,
1984