Winter 2025 Update from Bob – Companion is Ready

You are not yet authorized to view this page. Learn more here.

Bob’s Companion Project Update – Fall 2024

At press time the fuselage fabric is painted. A few pieces of front-end aluminum parts still need paint. The engine is finished, and is ready to be back on the airframe. Hopefully he’ll have an assembled airplane that looks like an airplane in time for the fly-in. The instrument panel, floorboards, and door sills are all in. He has taken a few antique car tours that have kept him away from the project but he’s still making steady progress.
There have been two completed Companions so far that we have weight and balance numbers for. In both cases, the empty CG was around 14-15 inches, as compared to a more typical 10-12 inches for a 4-Place. Bob says the CG on the companion is intentionally further aft, because it doesn’t need to be prepared to carry such a big load in the cabin. At a full-forward CG, the front seat occupants are aft of the CG, but approaching the aft limit, the front seat occupants become forward of the CG. Bob encountered this when carrying engines by himself. At the heaviest loads, the airplane can carry more if there is someone in the front seat than if the front seat is empty.
Bob says, if Companion builders want to carry a lot of cargo, use the constant speed prop and angle valve engine. For more reasonable/typical loads the parallel valve engine works very well. For both the 4-Place and the Companion, having the CG in the 14” range for day-to-day operations makes for an airplane that handles better, can land shorter, and feels lighter on the controls. It’s just with the 4-Place, we concede ideal solo-load handling by having the empty CG farther forward, to enable more cabin loading. Aircraft design is all about compromise!

1999 Weight and Balance Calculations

Source: 1999 Beartracks, Bob Barrows

*Hold this dimension for all engine installations unless weight and balance calculation problems are encountered

Bearhawk N33RB

Aft Sample Weight Arm Moment Forward Sample Weight Arm Moment
*Main Gear R 600 -1.63 -978 *Main Gear R 600 -1.63 -978
*Main Gear L 596 -1.63 -970 *Main Gear L 596 -1.63 -970
*Tail Wheel 75 199 14925 *Tail Wheel 75 199 14925
Front Seats 400 14 5600 Front Seats 200 14 2800
Cargo Area 530 57 30210 Cargo Area 0 57 0
Fuel lbs. 300 24 7200 Fuel lbs. 30 24 54
Totals 2500   55987 Totals 1500   15829
Gross Weight 2500     Gross Weight 2500    
C.G. Range 10.5″ – 22.5″     C.G. Range 10.5″ – 22.5″    
C.G. Range 16% – 34%     C.G. Range 16% – 34%    
C.G. Aft 22.4″     C.G. Forward 10.5″    
C.G. (MAC) 34%     C.G. (MAC) 16%    
Empty Weight – 1270* Empty Weight C.G. – 10.2″*

*As per weigh in of Proto II N33RB on 9-9-99

Note: Empty weight includes: 10 quarts oil, O-540 Lycoming Engine, no electrical system, no rear seats, utility door system and constant speed propeller (3-blade composite).

Forward C.G. = 15829/1501 = 10.5″     10.5/66 chord = 16%

Rear C.G. = 55987/2500 = 22.4″     22.4/66 chord = 34%

Do your first test flight with the c.g. between 13.5″ and 18.5″.

N6890R Weight and Balance