Dayton Pilots' Club
N8078X Weight and Balance Computations
Based on Archer II Information Manual
Report VB-1120 (rev July 20, 1983), Figure 6-9
DPC Aircraft Information Jan. 17, 2004
Weight and Balance
Weight (lbs)
CG Arm (inches)
Moment (lb*ins/1000)
Basic Empty Weight
(including unusable fuel and full oil)
1606.6
87.75
141.2961
Usable fuel:
Max 48 gal: . . . . . . . . . . . . . . . . . . . .
Pilot and front passenger
(max 500 lbs) (station 80.5 in)
Rear passengers
(max 400 lbs) (station 118.1 in)
Baggage area
(max 200 lbs) (station 142.8 in)
RAMP WEIGHT AND MOMENT
Fuel allowance for engine start, taxi, and run-up
-8.0
95.0
-0.76
TAKEOFF WEIGHT AND MOMENT
(max 2550 lbs)
Center of Gravity Moment Envelope
Min CG
Max CG
Start by entering the number of gallons of fuel. Then tab through the fields entering the weight for each remaining item. The arms will automatically be entered and the individual moments computed. The totals and C.G. will be calculated and analyzed for out-of-range conditions.
Zodiac 701DP
Archer 4506W
The PIC is responsible for performing Weight & Balance
using current Aircraft and POH information, as well as proper loading of the aircraft.
This reference tool is not warranted by the author or Dayton Pilot's Club