CG Longitudinal WEIGHT (lbs) x CG/ARM (in) = MOMENT (in-lbs)

Basic Empty Weight x =Passengers & Bags x 79 =

1) Total W&M Only C(without fuel weight) Box (C) to Graph (A)

2) Main Tank (19.2 gal) x 108.6 =3) Aux Tank (10.5 gal) x 103.8 =

Total 1/2/3 W&M Only D(with fuel weight) Box (D) to Graph (A)

A

A

BCG Lateral WEIGHT (lbs) x CG/ARM (in) = MOMENT (in-lbs)

Basic Empty Weight x =Right Seat (+) x 10.7 =Left Seat (-) x -9.3 =

4) Total W&M Only E(without fuel weight) Box (E) to Graph (B)

5) Main Tank (19.2 gal) x -11 =6) Aux Tank (10.5 gal) x 11.2 =

Total 4/5/6 W&M Only F(with fuel weight) Box (F) to Graph (B)

B

Weight and Balance Info for R22 Alpha, Beta and Beta II FormulasMax Gross Weight 1370lbs. W x A = MMin Gross Weight 920lbs. M / W = A (CG)Max Per Seat & Bags 240lbs. CG = ARMMax Bags Under Seat 50lbs.Min Solo Weight (with Aux Tank) 135lbs.Min Solo Weight (without Aux Tank) 130lbs.

R22 ALPHA, BETA AND BETA II CENTER OF GRAVITY LIMITSWeight and Balance WorksheetRobinson R22 (Alpha, Beta and Beta II)

AircraftLongitudinal C.G.

Lateral C.G.

Basic Empty Weight

Fuel Calculator Total Gal Fuel Weight TotalMain Tank (19.2gal) x 6.0 lbs =Aux Tank (10.5gal) x 6.0 lbs =