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Beechcraft T-34 Mentor

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

Its early models, dating back to the late 1940s and 1950s, featured piston engines.

These were later replaced by the more advanced T-34C Turbo-Mentor, equipped with a turboprop engine.

Remarkably, the T-34 has remained in service for over seventy years since its inception.

Conceived by Walter Beech as the Beechcraft Model 45 during a period without a defence budget for new trainers, the T-34 was intended as a cost-effective substitute for the North American T-6/SNJ Texan used by all U.S. military branches.

The Model 45 underwent several design iterations, including one with the Bonanza’s distinctive V-tail.

However, the final design, completed in 1948, featured conventional tail controls to suit the military’s conservative preferences, including a large unswept vertical fin that would later be seen on the Travel Air twin-engine civil aircraft nearly a decade later.

The Bonanza’s four-passenger fuselage was modified to a slimmer version with a two-seat tandem cockpit and bubble canopy, enhancing visibility for both trainee and instructor.

In terms of strength, the Model 45 was significantly more robust than the Bonanza, designed to withstand +10g and −4.5g forces.

Its Continental E-185 engine, delivering 185 horsepower on take-off, was identical to that used in contemporary Bonanza models, albeit less than a third as powerful as the T-6’s engine.

Model 73 Jet Mentor

In 1955, Beechcraft developed a jet-powered derivative as a private venture, aiming to secure a contract from the US military.

The Model 73 Jet Mentor retained many elements of the piston-engined predecessor, with notable changes including a repositioned cockpit further forward in the fuselage and wing root air intakes for the jet engine, which fed a single 920 lbf (4.1 kN) Continental J69 in the rear fuselage.

The Model 73’s maiden flight, under the registration N134B, occurred on December 18, 1955.

The USAF evaluated the Model 73 but chose the Cessna T-37, while the USN opted for the Temco TT Pinto.

Following tests at the Naval Air Test Center in NAS Patuxent River, Maryland, the Navy explored the TT Pinto as a jet trainer in 1959 but ceased its use by December 1960, reverting to the piston-powered T-34B Mentor and North American T-28 Trojan for primary flight training.

The Beechcraft Model 73 never entered production, and the only prototype is exhibited at the Kansas Aviation Museum.

T-34C Turbo-Mentor

Following a production break of nearly 15 years, the T-34C Turbo-Mentor, equipped with a Pratt & Whitney Canada PT6A-25 turboprop engine, was developed in 1973.

The development was initiated by the US Navy (USN), which provided two T-34Bs for conversion.

These aircraft, after being fitted with the PT6 engines, were redesignated as YT-34Cs, with the first flight under turboprop power occurring on September 21, 1973.

Production of the Mentor resumed in 1975, with the T-34Cs delivered to the USN and the armed T-34C-1 version for export customers in 1977, which included four underwing hardpoints.

The final Turbo-Mentor came off the production line in 1990.

Since the late 1970s, the T-34Cs have been utilized by the Naval Air Training Command to train a multitude of Naval Aviators and Naval Flight Officers for the U.S. Navy, Marine Corps, Coast Guard, and various NATO and allied countries.

After more than 35 years of service, the T-34C has been fully replaced by the T-6 Texan II.

Variants

YT-34

Prototype, three built.

T-34A

US Air Force trainer.

Replaced by the Cessna T-37 around 1960 (450 built).

T-34B

The US Navy utilized the trainer until 1976, coinciding with the decommissioning of VT-1 and VT-5.

Subsequently, it was succeeded by the T-34C, with Beechcraft constructing 423 units.

Pilots affiliated with the Navy Recruiting Command continued to operate T-34Bs until the mid-1990s.

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

Designed with hard points for training or light attack missions, this aircraft can carry up to 1,200 lb (540 kg) of armaments on four under-wing pylons.

The armament could include flares, incendiary bombs, rocket or gun pods and antitank missiles.

Widely exported.

Turbo-Mentor 34C

Civilian version

Allison Turbine Mentor

Conversion of surplus T-34 Mentors to be powered by Allison Model 250 turboprop engines.

Model 73 Jet Mentor

Equipped with a 920 lbf (4.09 kN) Continental J69-T-9 turbojet engine, the unique aircraft took its maiden flight on December 18, 1955.

Specifications

(T-34C)

Crew

2

Length

28 ft 8+12 in (8.750 m)

Wingspan

33 ft 3+78 in (10.157 m)

Height

9 ft 7 in (2.92 m)

Wing area

179.6 sq ft (16.69 m2)

Empty weight

2,960 lb (1,343 kg)

Max take-off weight

4,300 lb (1,950 kg) (T-34C-1 weapons trainer 5,500 lb (2,500 kg))

Fuel capacity

130 US gal (110 imp gal; 490 L)

Powerplant

1 × Pratt & Whitney Canada PT6A-25 turboprop,

550 shp (410 kW)

Propellers

3 bladed Hartzell constant speed

Performance

Cruise speed

214 kn (246 mph, 396 km/h) at 17,000 ft (5,200 m) (max cruise)

Stall speed

53 kn (61 mph, 98 km/h) (flaps down, power off)

Never exceed speed

280 kn (320 mph, 520 km/h)

Range

708 nmi (815 mi, 1,311 km) at 180 kn (210 mph; 330 km/h)

&

20,000 ft (6,100 m)

Service ceiling

30,000 ft (9,100 m)

G limits

+6

-3

Rate of climb

1,480 ft/min (7.5 m/s)

Armament

Hardpoints

4 with a capacity of 600 lb (272 kg)

Inner, 300 lb (136 kg)

Outer, 1,200 lb (544 kg) total

Sources
Beech Aircraft and their Predecessors-Alain Pelletier.
National Museum of the United States Air Force.
Beechcraft Aircraft.

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