GENERAL
| Description | The Beechcraft Baron is a light twin engined piston aircraft designed in 1961. A low wing monoplane, it still continues to be in production. With over 6800 units, its primary user was the United States Army. |
| Wake Turbulence Category | L |
| Aerodrome Reference Category | |
| Approach Category | |
| Variants | BARON 55, 56, 58, T-42A, SF-60 |
| Manufacturer | Beechcraft |
| First Flight | 29th Feb 1960 |
| Launch Organisation | |
| Largest Operator | |
| First Registered In India | |
| Users In India |
Takeoff 715m
Landing 396m
RUNWAY REQUIRED AT MTOW/MLW
SPECIFICATIONS
| Crew | 1 |
| Passenger Capacity | 5 |
| Length | 9.09 m |
| Wingspan | 11.53 m |
| Height | 2.97 m |
| Wing Area | 18.51 sqm |
| Max Ramp Weight | 2506 Kgs |
| Fuel Capacity | 528 Kgs |
| Engine | Continental IO-550 |
| Thrust | 300 HP |
Fleet Detail
| MSN | TAIL | MAKER | MODEL | ENGINE | CONF | FIRST FLT | LESSOR | REMARKS |
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