Piper PA-28-161 Pilot Operating Handbook page 121

SECTION 6
WEIGHT AND BALANCE
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR ll
Arm Aft
Weight Datum
Moment
(Lbs) (Inches) (ln-Lbs)
Basic Empty Weight
Pilot and Front Passenger
80.5
Passengers (Rear Seats)* 118.1
Fuel (48 Gallon Maximum) 95.0
Baggage* (200 Lbs. Maximum) 142.8
Ramp Weight (2447 Lbs. Normal,
2027 Lbs. Utility Maximum)
Fuel Allowance -7 95.0 -665
For Engine Start, Taxi and Run Up
Total Loaded Airplane (2440 Lbs. Normal,
2020 Lbs. Utility Maximum)
Totals must be within approved weight and e.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 e.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
Figure 6-11
REPORT: VB-1180
6-12
ISSUED: AUGUST 13, 1982