Baron 58 Cockpit Simulator

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Beechcraft Baron 58 general information

 

The Beechcraft Baron is a light-medium twin-engine piston aircraft originally developed by Beech Aircraft Corporation and currently manufactured by the Beechcraft Division of Raytheon Aircraft. The Baron is a variant of the Beechcraft Bonanza, and was first introduced in 1961. Oddly, Beech also offered a Twin Bonanza line of airplanes which featured some design commonality with the Bonanza but in all respects were entirely different airplanes and could not be considered to be true "twin bonanzas".

As of 2006, a new Baron costs over $1.2 million. Since its inception, the Baron has always been near the top of the light airplane hierarchy. Expensive as it is to buy and to operate, the 'next step up' from a Baron is a very big one. Faster aircraft, with greater range and more load-carrying capability are generally turbine-powered and far more expensive.

Barons come in two basic types: the Baron 55 (short body) and Baron 58 (long body), with several subtypes.

Introduced in 1970, the more powerful Baron 58 has club seating, double aft doors, and a gross weight of 54005500 lb (24502500 kg), and is fitted with either the Continental IO520 or IO550 300 hp (224 kW) engine. The Baron 58 can cruise at 200 knots (370 km/h) at 7000 ft (2100 m), and is equipped with either 166 or 190 US gallon (628 or 719 L) fuel tanks.

In 1976, the turbocharged Baron 58TC and pressurized Baron 58P were introduced. These variants were powered by Continental TIO520 turbocharged engines of 310325 hp (230240 kW) and had an increased 61006200 lb (about 2800 kg) gross weight, and were certified under FAR23 with a new type certificate. The Baron 58P/58TC models were capable of cruising at 200 knots (370 km/h) at 8000 ft (2400 m) and 220 knots (410 km/h) at 20000 ft (6100 m), and were typically equipped with 190 US gallon (719 L) fuel tanks.

A big change in panel/system layout on 58/58TC/58P occurred in 1984, including relocating throttle, gear, flap, propeller and mixture controls to industry-standard positions.

Although the turbocharged 58TC/58P variants were discontinued in 1985, the normally aspirated Baron 58 is still in production as of 2006

ICAO - Aircraft Type Designator

Manufacturer Model Type Designator Description Engine Type Engine Wake Turbulence Category
BEECH 58 Baron BE58 Landplane Piston 2 L

    source: http://www.icao.int/anb/ais/8643/index.cfm

Specs

2001 Beechcraft Baron 58
Price typically equipped: $1,050,000

Specifications

Powerplant

Continental IO-550-C rated at 300 hp

Seats

6

Useful load, as tested

1,472 lb

Payload w/full fuel, as tested

478 lb

Maximum takeoff weight

5,500 lb

Maximum landing weight

5,400 lb

Fuel capacity, std

172 gal (166 gal usable)
1,032 lb (996 lb usable)

Fuel capacity, w/opt tanks

200 gal (194 gal usable)
1,200 lb (1,164 lb usable)

Baggage capacity

(nose) 300 lb, 18 cu ft
(aft) 120 lb, 10 cu ft

Performance

Takeoff distance, ground roll

1,400 ft

Takeoff distance over 50-ft obstacle

2,300 ft

Rate of climb, sea level

1,735 fpm

Single-engine ROC, sea level

390 fpm

Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption, ea engine)

@ 75% power, best power, 7,000 ft

201 kt/4.3 hr
(98 pph/16.4 gph)

Service ceiling

20,688 ft

Single-engine service ceiling

7,400 ft

Landing distance over 50-ft obstacle

1,950 ft

Landing distance, ground roll

1,500 ft

Limiting and Recommended Airspeeds

VLO (max gear operating)

152 KIAS

VNE (never exceed)

223 KIAS

VS1 (stall, clean)

84 KIAS

VSO (stall, in landing configuration)

73 KIAS

 

 

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