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Beech Aircraft
T-34C Turbo Mentor

T-34C of the Ecuadorian Air Force

Service: United States Navy, United States Marine Corps

Propulsion: Model PT6A-25 turbo-prop engine (Pratt & Whitney Aircraft of Canada).

Airspeed: Max: 280 Knots

Range: Approximately 600 nm

Crew: 2 (instructor pilot, student pilot).

Armament: None

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History Beech Aircraft Corporation
Beechcraft T-34C Turbo Mentor



After a production hiatus of almost 15 years, the T-34C Turbo-Mentor powered by a Pratt & Whitney Canada PT6A-25 turboprop engine was developed in 1973. The original T-34's modified Bonanza/Debonair-style wing was replaced with a variant of the larger Beech Baron wing, and the original Bonanza/Debonair-style landing gear was replaced with the landing gear from the even-larger Beech Duke.

Design and development

The T-34C Turbomentor is an unpressurized two-seat, tandem cockpit low-wing turboprop trainer whose mission is to train Navy and Marine Corps pilots.

The T-34C is used to provide primary flight training for student pilots. As a secondary mission, approximately 10 percent of the aircraft provide pilot proficiency and other aircraft support services to Commander, Naval Air Force, U.S. Atlantic Fleet; Commander, Naval Air Force, U.S. Pacific Fleet; and Naval Air Systems Command's "satellite sites" operated throughout the continental United States.

The T-34C was procured as a commercial-derivative aircraft certified under an FAA Type Certificate. The T-34C was derived from the civilian Beechcraft Bonanza. Throughout its life, the aircraft has been operated and commercially supported by the Navy using FAA processes, procedures and certifications.

Testing


On 7 May 1944, Beech Test Pilot Vern Carstens Flew The XA-38 On Its Maiden Flight From The Company's Wichita Airfield. The Aircraft Proved Satisfactory In All Respects And Better Than Expected In Some, Including Top Speed.

 
9.1
Km

Ceiling

1311
Km

Max Range

396
Km/h

Performance

2
Crew

Max Crew

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Beech Aircraft Corporation Beechcraft T-34C Turbo Mentor

Beech Aircraft Corporation
Beechcraft T-35B/C Turbo Mentor

1

General Info

        • Crew: Two
          Length: 28 ft 8½ in (8.75 m)
          Wingspan: 33 ft 3⅞ in (10.16 m)
          Height: 9 ft 7 in (2.92 m)

2

Powerplant

    • Empty weight: 2,960 lb (1,342 kg)
      Max. takeoff weight: 4,300 lb (1,950 kg) (T-34C-1 weapons trainer - 5,500 lb (2,494 kg))
      Powerplant: 1 × Model PT6A-25 turbo-prop engine (Pratt & Whitney Aircraft of Canada)

plane
3

Performance

  • Never exceed speed: 515 km per hour
    Cruise speed: (396 km/h, 246 mph) max cruise at (5,180 m)
    Range: 708 nmi (1,311 km, 814 mi) at 180 knots (333 km/h, 207 mph) and 20,000 ft (6,100 m)
    Service ceiling: 30,000 ft (9,145 m)

4

Armament

    • None
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Special Links Beech Aircraft Corporation Beechcraft T-34C Turbo Mentor

Links to Youtube & Others

World War II
The Beechcraft T-34 Mentor is an American propeller-driven, single-engine, military trainer aircraft derived from the Beechcraft Model 35 Bonanza

Beechcraft Aircraft Beechcraft T-35 Turbo

The Beechcraft T-34 Mentor is an American propeller-driven, single-engine, military trainer aircraft derived from the Beechcraft Model 35 Bonanza.

interior

Youtube Link

The earlier versions of the T-34, dating from around the late 1940s-1950s, were piston-engined. These were succeeded by the upgraded T-34C Turbo-Mentor, powered by a turboprop engine.

interior
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