SECTION 6
WEIGHT AND BALANCE PA-28-181, ARCHER III
SECTION 6
WEIGHT AND BALANCE PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
6-10
REPORT: VB-1611 ISSUED: JULY 12, 1995
6-10
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 rear passengers allowed.
Arm Aft
Weight Datum Moment
(Lbs) (Inches) (In-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 (2558 Lbs. Normal,
2138 Lbs. Utility Maximum)
Fuel Allowance
For Engine Start, Taxi and Run Up -8 95.0 -760
Takeoff Weight (2550 Lbs. Normal,
2130 Lbs. Utility Maximum)
WEIGHT AND BALANCE LOADING FORM
Figure 6-11
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 rear passengers allowed.
Arm Aft
Weight Datum Moment
(Lbs) (Inches) (In-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 (2558 Lbs. Normal,
2138 Lbs. Utility Maximum)
Fuel Allowance
For Engine Start, Taxi and Run Up -8 95.0 -760
Takeoff Weight (2550 Lbs. Normal,
2130 Lbs. Utility Maximum)
WEIGHT AND BALANCE LOADING FORM
Figure 6-11
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