Piper WARRIOR III PA-28-161 Pilot Operating Handbook page 126

SECTION 6
WEIGHT AND BALANCE
Basic Empty Weight
Pilot and Front Passenger
Passengers (Rear Seats)*
Fuel (48 Gallon Maximum)
Baggage* (200 Lbs. Maximum)
Ramp Weight (2447 Lbs. Normal,
2027 Lbs. Utility Maximum)
Fuel Allowance
For Engine Start, Taxi and Run Up
Takeoff Weight (2440 Lbs. Normal,
2020 Lbs. Utility 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.
*Utility Category Operation - No baggage or aft passengers allowed.
WEIGHT AND BALANCE LOADING FORM
REPORT: VB-1565
6-12
PIPER AIRCRAFT CORPORATION
Weight
(Lbs)
-7
Figure 6-11
PA-28-161, WARRIOR III
Arm Aft
Datum
(Inches)
80.5
118.1
95.0
142.8
95.0
ISSUED: JULY 1, 1994
Moment
(In-Lbs)
-665