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T-34 Mentor
A T-34B Mentor aircraft from Training Squadron 5 (VT-5) in 1976
Role Trainer aircraft
National origin United States
Manufacturer Beechcraft
First flight 2 December 1948
Introduction 1953
Primary users United States Air Force
United States Navy
Japan Air Self Defense Force
Philippine Air Force
Produced 1953-1959
Number built 2,300+
Developed from Beechcraft Bonanza

The Beechcraft T-34 Mentor is a propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza. The earlier versions of the T-34, dating from around the late 1940s to the 1950s, were piston-engined. These were eventually succeeded by the upgraded T-34C Turbo-Mentor, powered by a turboprop engine. The T-34 remains in service more than six decades after it was first designed.

Design and development

The T-34 was the brainchild of Walter Beech, who developed it as the Beechcraft Model 45 private venture at a time when there was no defense budget for a new trainer model. Beech hoped to sell it as an economical alternative to the North American T-6/SNJ Texan, then in use by all services of the U.S. military.

A YT-34 on display at the Castle Air Museum in Atwater, California

Piston-engined T-34s of the March Field Aero Club at the March Air Reserve Base (ARB) in California in 2004

Three initial design concepts were developed for the Model 45, including one with the Bonanza's signature V-tail, but the final design that emerged in 1948 incorporated conventional tail control surfaces for the benefit of the more conservative military[1] (featuring a relatively large unswept vertical fin that would find its way onto the Travel Air twin-engine civil aircraft almost ten years later). The Bonanza's fuselage with four-passenger cabin was replaced with a narrower fuselage incorporating a two-seater tandem cockpit and bubble canopy,[2] which provided greater visibility for the trainee pilot and flight instructor. Structurally, the Model 45 was much stronger than the Bonanza, being designed for +10g and -4.5g, while the Continental E-185 engine of 185 horsepower (hp) at takeoff (less than a third of the power of the T-6's engine[3]) was the same as that fitted to contemporary Bonanzas.[2]

Following the prototype were three Model A45T aircraft,[2] the first two with the same engine as the prototype and the third with a Continental E-225,[1] which would prove to be close to the production version. Production did not begin until 1953, when Beechcraft began delivering T-34As to the United States Air Force (USAF) and similar Model B45 aircraft for export. Production of the T-34B for the United States Navy (USN) began in 1955, this version featuring a number of changes reflecting the different requirements of the two services. The T-34B had only differential braking for steering control on the ground instead of nosewheel steering, additional wing dihedral and, to cater for the different heights of pilots, adjustable rudder pedals instead of the moveable seats of the T-34A.[1] T-34A production was completed in 1956, with T-34Bs being built until October 1957 and licensed B45 versions built in Canada (125 manufactured by Canadian Car and Foundry),[2] Japan (173 built by Fuji Heavy Industries),[2] and Argentina (75 by FMA) until 1958. Beechcraft delivered the last Model B45s in 1959.[1] Total production of the Continental-engined versions in the US and abroad was 1,904 aircraft.[2]

Model 73 Jet Mentor

The Model 73 Jet Mentor.

In 1955 Beechcraft developed a jet-engined derivative, again as a private venture, and again in the hope of winning a contract from the US military.[2] The Model 73 Jet Mentor shared many components with the piston-engined aircraft; major visual differences were the redesigned cockpit which was relocated further forward in the fuselage and the air intakes for the jet engine in the wing roots, supplying air to a single jet engine in the rear fuselage.[2] The first flight of the Model 73, registered N134B, was on 18 December 1955. The Model 73 was evaluated by the USAF, which ordered the Cessna T-37, and the USN, which decided upon the Temco TT Pinto. The Model 73 was not put into production.[2] The sole protoype is on display at the Kansas Aviation Museum.[4]

T-34C Turbo-Mentor

A T-34C Turbo-Mentor, which can be distinguished from the B (piston) model by the extended nose and exhaust stacks on either side behind the prop

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.[2][5] Development proceeded at the behest of the USN, which supplied two T-34Bs for conversion.[5] After re-engining with the PT6, the two aircraft were redesignated as YT-34Cs, the first of these flying with turboprop power for the first time on 21 September 1973.[5] Mentor production restarted in 1975 for deliveries of T-34Cs to the USN and of the T-34C-1 armed version for export customers in 1977, this version featuring four underwing hardpoints.[1] The last Turbo-Mentor rolled off the production line in 1990.[2]

Since the late 1970s, T-34Cs have been used by the Naval Air Training Command to train numerous Naval Aviators and Naval Flight Officers for the U.S. Navy, U.S. Marine Corps, U.S. Coast Guard, and numerous NATO and Allied nations. With over 35 years of service, the T-34C is gradually being phased out of the U.S. Navy's inventory and will eventually be replaced by the T-6 Texan II.[6][7]

Operational history

The first flight of the Model 45 was on 2 December 1948, by Beechcraft test pilot Vern Carstens.[2] In 1950 the USAF ordered three Model A45T test aircraft, which were given the military designation YT-34.[2] A long competition followed to determine a new trainer, and in 1953 the Air Force put the Model 45 into service as the T-34A Mentor, while the USN followed in May 1955 with the T-34B.[2]

The US Air Force began to replace the T-34A at the beginning of the 1960s, their role taken over by the propeller-driven T-41 Mescalero and the T-37 Tweet primary jet trainer. Many USAF T-34A aircraft were turned over to the USAF Auxiliary, the Civil Air Patrol, for use as search aircraft. However, the T-34's low wing limited its utility in a search and rescue role, and maintenance issues, particularly expensive wing spar repairs that became apparent in the late 1990s, resulted in the T-34As being withdrawn from CAP service beginning in 2003.[8]

The U.S. Navy kept the T-34B operational as a Naval Air Training Command initial primary trainer until the mid-1970s and as a Navy Recruiting Command aircraft until the early 1990s when the last examples were retired as an economy move. Others continue to remain under U.S. Navy control as part of flying clubs at naval air stations and marine corps air stations.

As of 2007, Mentors are still used by several air forces and navies.

From 1978, the T-34C Turbo-Mentor was the Argentine Naval Aviation basic trainer used by the 1st Naval Aviation Force (Training), alongside 15 T-34C-1 light attack aircraft forming the Fourth Naval Air Attack Squadron.[9] During the 1982 Falklands War, four T-34C-1s were deployed to Port Stanley on 25 April 1982, primarily to be employed in a reconnaissance role. The main encounter with British forces occurred on 1 May 1982 when three Turbo-Mentors attacked a Royal Navy Westland Sea King helicopter in the area of Berkeley Sound but were intercepted by Royal Navy Sea Harriers flown by Lt 'Soapy' Watson and Lt Cdr 'Sharky' Ward of 801 Naval Air Squadron flying from HMS Invincible,[10][11] with one of the T-34Cs being damaged by cannon fire from Ward's aircraft. The four T-34C-1 Turbo-Mentors continued to operate, flying a few reconnaissance missions, but were redeployed to Borbon Station where they were ultimately destroyed by the SAS Raid on Pebble Island on 15 May 1982.[12] Although all four hulks remained on the island for a considerable length of time, eventually, 0729/(1-A)411 was recovered on 10 June 1983 and stored for future display at the Fleet Air Arm Museum.[13]

Julie Clark in the T-34 "Free Spirit" c. 2006

In 2004, due to a series of crashes involving in-flight structural failure during simulated combat flights, the entire US civilian fleet of T-34A/Bs was grounded by the Federal Aviation Administration. The grounding has since been eased to a slate of restrictions on the permitted flight envelope. Via a series of Airworthiness Directives (ADs) established by or Alternate Methods of Compliance (AMOCs) negotiated with the FAA, including installation of certain, approved structural modifications to the wing spar and other repairs, the T-34A and T-34B fleet in 2011 has been restored to full flight status by FAA at the Mentor's originally designed limitations, provided each individual example is compliant with those ADs and AMOCs.

The T-34C is still used as a primary training aircraft for United States Navy and Marine Corps and Coast Guard student pilots, although it is currently being replaced by the T-6 Texan II. Training Air Wing SIX at NAS Pensacola, Training Air Wing FIVE at NAS Whiting Field and Training Squadron TWENTY-SEVEN at NAS Corpus Christi have transitioned to the T-6A and T-6B models, respectively. Training Squadron TWENTY-EIGHT is the only remaining squadron flying the T-34C with plans to begin transition in 2014.

NASA Dryden Flight Research Center has operated two T-34C aircraft. The first was previously flown at the Glenn Research Center in Cleveland, Ohio, for propulsion experiments involving turboprop engines, and then came to Dryden as a chase aircraft in 1996. That aircraft was returned to the US Navy in 2002. Dryden obtained its second T-34C in early 2005 from the Naval Air Warfare Center Aircraft Division (NAWCAD) at NAS Patuxent River, where it was due to be retired. At Dryden, the T-34C is primarily used for chasing remotely piloted unmanned air vehicles which fly slower than NASA's F/A-18's mission support aircraft can fly. It is also used for required pilot proficiency flying.[14]

The United States Army received six ex-US Navy T-34C, used as test platforms and chase planes at Edwards Air Force Base and at Fort Bragg.[15]

The Mentor is the aircraft used by the Lima Lima Flight Team and Dragon Flight, both civilian demonstration teams. It is also used by aerobatic pilot Julie Clark, who flies her T-34 "Free Spirit" (registration N134JC) at air shows.


A U.S. Navy T-34B assigned to Saufley Field.

Prototype, three built.
US Air Force trainer. Replaced by the Cessna T-37 around 1960 (450 built).
US Navy trainer. Used as a trainer until early 1970s when it was replaced by the T-34C (423 built by Beechcraft). T-34B's were flown by pilots assigned to the Navy Recruiting Command until the mid-1990s.
Two T-34Bs were fitted with turboprop engines, and were used as T-34C prototypes.
T-34C Turbo-Mentor
Two-seat primary trainer, fitted with a turboprop engine.
Equipped with hardpoints for training or light attack, able to carry 1,200 lb (540 kg) of weapons on four underwing pylons. The armament could include flares, incendiary bombs, rocket or gun pods and antitank missiles. Widely exported.
Turbo-Mentor 34C
Civilian version


Military operators

Military T-34 operators

A T-34A Mentor at the National Museum of the USAF

TAIWAN Air Force T34

T-34C of the Ecuadorian Air Force

Beech T-34C Turbo Mentor operated by NASA

 Dominican Republic
 El Salvador
United States

Specifications (T-34C)


Data from Janes's All The World's Aircraft 1988-89[17]

General characteristics

  • 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)
  • Wing area: 179.6 ft² (16.69 m²)
  • 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 × Pratt & Whitney Canada PT6A-25 turboprop, 715 shp (533 kW) (derated to 400 shp (298 kW))


  • Never exceed speed: 280 knots (518 km/h, 322 mph) (IAS)
  • Cruise speed: 214 knot (396 km/h, 246 mph) max cruise at 17,000 ft (5,180 m)
  • Stall speed: 53 knots (98 km/h, 61 mph) flaps down, power off
  • 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)
  • Rate of climb: 1,480 ft/min (7.5 m/s)
  • g limit:+4.5, -2.3


  • Hardpoints: 4 with a capacity of 600 lb (272 kg) inner, 300 lb (136 kg) outer, 1,200 lb (544 kg) total

See also


  1. 1.0 1.1 1.2 1.3 1.4 Morris, Frank. "A Short History of the Beechcraft Mentor." Retrieved: 13 November 2007.
  2. 2.00 2.01 2.02 2.03 2.04 2.05 2.06 2.07 2.08 2.09 2.10 2.11 2.12 2.13 Phillips, Edward H. Beechcraft - Pursuit of Perfection, A History of Beechcraft Airplanes. Eagan, Minnesota: Flying Books, 1992. ISBN 0-911139-11-7.
  3. "T-6 specifications." Retrieved: 13 November 2007.
  4. "Kansas Aviation Museum". Retrieved 17 April 2012. 
  5. 5.0 5.1 5.2 Taylor, M. J. H., ed. Jane's American Fighting Aircraft of the 20th Century. Lombard, IL: Mallard Press, 1991. ISBN 0-7924-5627-0.
  9. Villarino, Horacio. Exocet (in Spanish). Buenos Aires: Siete Dias, First edition 1983. ISBN 950-10-0116-4.
  10. "Beechcraft T-34A & C Mentor." Retrieved: 30 August 2010.
  11. Morgan 2006, p. 78. Quote: "This changed around midday when Lieutenant Soapy Watson and Lieutenant Commander Sharkey Ward were vectored onto three Mentor light attack aircraft about to attack a Sea King in the area of Berkeley Sound."
  12. Freedman, Sir Lawrence. The Official History of the Falklands Campaign. Abingdon, Oxon, UK: Routledge, 2005. ISBN 0-7146-5207-5.
  13. "Beech T-34C." Retrieved: 30 August 2010.
  14. "T-34C Fact sheet." NASA. Retrieved: 30 August 2010.
  15. 15.0 15.1 Harding 1990, pp. 27–28.
  16. 16.0 16.1 16.2 16.3 16.4 16.5 16.6 16.7 16.8 Taylor 1988, p. 329.
  17. Taylor 1988, pp. 329–330.
  • Drendel Lou. T-34 Mentor in Action. Carrollton, Texas: Squadron/Signal Publications, 1990. ISBN 0-89747-249-7.
  • Harding, Stephen. U.S. Army Aircraft Since 1947. Shrewsbury, UK: Airlife Publishing, 1990. ISBN 1-85310-102-8.
  • Morgan, David. Hostile Skies: My Falklands Air War. London: Phoenix Publishing, 2006. ISBN 978-0-7538-2199-2.
  • Taylor, John W.R. Jane's All The World's Aircraft 1988-89. Coulsdon, UK: Jane's Defence Data, 1988. ISBN 0-7106-0867-5.

External links

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