T-34 Mentor
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| T-34 Mentor | |
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| 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 |
| Introduced | 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 almost six decades after it was first designed.
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[edit] 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/NJ Texan, then in use by all services of the U.S. military.
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. In 1955 production of the T-34B for the United States Navy (USN) began, this version featuring a number of differences 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].
[edit] 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]
[edit] 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[4][2]. Development proceeded at the behest of the USN, which supplied two T-34Bs for conversion[4]. 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[4]. Mentor production re-started 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].
[edit] 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, while the U.S. Navy kept the T-34B operational until the early 1970s. As of 2007, Mentors are still used by several air forces and navies.
The T-34A and C were used by the Argentine Navy during the Falklands War.[5] [6]
In 2004, due to a series of crashes involving in-flight structural failure during simulated combat flights, the entire US civilian fleet of T-34s was grounded by the Federal Aviation Administration. The grounding has since been eased to a series of restrictions on the permitted flight envelope.
The T-34C is still used as the primary training aircraft for United States Navy and Marine Corps pilots. The T-34C is currently being replaced by the T-6 Texan II but is still the primary aircraft at NAS Corpus Christi and NAS Whiting Field. NAS Pensacola has already completed the transition to the T-6 and the first T-6s are scheduled to arrive at Whiting Field in summer 2009.
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 Navy's Air Warfare Center Aircraft Division 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-18's mission support aircraft can fly. It is also used for required pilot proficiency flying. [7]
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.
[edit] Variants
- YT-34
- Prototype, three built.
- T-34A
- US Air Force trainer. Replaced by the Cessna T-37 around 1960 (450 built).
- T-34B
- US Navy trainer. Used until early 70s when it was replaced by the T-34C (423 built by Beechcraft).
- YT-34C
- 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.
- T-34C-1
- Equipped with hardpoints for training or light attack. Widely exported.
- Turbo-Mentor 34C
- Civilian version
[edit] Operators
[edit] Military operators
- Chilean Air Force
- Chilean Navy
- Being replaced by the T-35 Pillán
Colombia
Dominican Republic
Ecuador
El Salvador
France
Gabon
Greece
Indonesia
Japan
Mexico
Morocco
Peru
Philippines
Republic of China
Spain
Turkey
United States
[edit] Civil operators
- Dragon Flight
- Lima Lima Flight Team
- NASA
- The San Diego Salute[8]
[edit] Specifications (T-34C)
General characteristics
- Crew: Two
- Length: 28 ft 6 in (8.75 m)
- Wingspan: 33 ft 5 in (10.60 m)
- Height: 9 ft 7 in (2.92 m)
- Wing area: 180 ft² (16.7 m²)
- Empty weight: 2,960 lb (1,342 kg)
- Max takeoff weight: 4,400 lb (1,950 kg)
- Powerplant: 1× Pratt & Whitney Canada PT6A-25 turboprop, 550 shp (410 kW)
Performance
- Maximum speed: 280 kt IAS (320 mph, 520 km/h)
- Range: 600 nm (690 mi, 1,110 km)
- Service ceiling: 25,000 ft (7,600 m)
- Rate of climb: 1,480 ft/min (7.5 m/s)
- g limit: 4.5 positive, 2.3 negative
[edit] See also
Related development
Comparable aircraft
[edit] References
[edit] Notes
- ^ a b c d e Morris, Frank. A Short History of the Beechcraft Mentor Retrieved: 13 November 2007.
- ^ a b c d e f g h i j k l m n Phillips, Edward H. Beechcraft - Pursuit of Perfection, A History of Beechcraft Airplanes. Eagan, Minnesota: Flying Books, 1992. ISBN 0-911139-11-7.
- ^ T-6 specifications Retrieved: 13 November 2007.
- ^ a b c Taylor, M. J. H. ed. Jane's American Fighting Aircraft of the 20th Century. Mallard Press. ISBN 0-7924-5627-0
- ^ britains-smallwars.com
- ^ Morgan 2006, p. 78. Quote: "This changed around midday when Lieutenant Soapy Watson and Sharkey Ward were vectored onto three Mentor light attack aircraft about to attack a Sea King in the area of Berkeley Sound."
- ^ NASA T-34C Fact sheet
- ^ The San Diego Salute
[edit] Bibliography
- Corpus Christi 2006 accident
- Drendel Lou. T-34 Mentor in Action. Carrollton, Texas: Squadron/Signal Publications, 1990. ISBN 0-89747-249-7.
- Morgan, David. Hostile Skies: My Falklands Air War. London: Phoenix Publishing, 2006. ISBN 978-0-7538-2199-2.
[edit] External links
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Wikimedia Commons has media related to: T-34 Mentor |
- US Navy Fact File: T-34C Turbo-Mentor and T-34 history page on Navy.mil
- Hawker Beechcraft T-34 page
- T-34 Mentor/T-34C Turbo-Mentor on GlobalSecurity.org
- FAS Military Analysis Network: T-34C Turbo-Mentor
- T-34 Association: Non-profit organization dedicated to "Keep 'em flyin".
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