Beechcraft T-34 Mentor

Airplanes

Length

8.5344 m

Flat Wing Span

10.0584 m

Height

2.7432 m

Flat Wing Area

16.6854 m²

Cruise Speed

396.3277 km/h

Max Ceiling

9144 m

Number of Engines

Aircraft Engine

First Flight

1948-12-02

Entry Into service

1953-01-01

Number Built

2300

Maximum Take-Off Weight

1.9504 t (paragliders: kg)

Total Fuel Capacity

492.1035

Maximum Range

1311.216 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Beechcraft T-34 Mentor	1.9504	492.1035	1311.216

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Bellanca Skyrocket II	Continental IO-520	8.2296	10.3632	Compare
Berliner-Joyce P-16		8.59	10.36	Compare
Avia B-534		8.1	9.4	Compare
Armstrong Whitworth Scimitar	Armstrong Siddeley Panther	7.62	10.0584	Compare
Arado SSD I	BMW VI	8.5	10	Compare
Arado Ar 64		8.43	9.9	Compare

All data (25 fields)

Name: Beechcraft T-34 Mentor
Manufacturer: Allison Gas Turbine Division GMC
Description: The Beechcraft T-34 Mentor is an American propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza.
First Flight: 1948-12-02
Entry Into service: 1953-01-01
Production End: 1959-01-01
Designer: Allison Gas Turbine Division GMC
Type: Trainer aircraft
Length (m): 8.5344
Height (m): 2.7432
Cockpit Crew: 2
Cruise Speed (km/h): 396.3277
Min Speed (km/h): 98.1559
Max Ceiling (m): 9144
Rate of Climb (m/s): 7.5184
Armament: 4
National Origin: United States of America
Number Built: 2300
Powerplant Description: 1 × Pratt & Whitney Canada PT6A-25 turboprop, 410 kW (550 hp) each
Primary Users: United States Air Force, United States Navy , Japan Air Self-Defense Force , Republic of China Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Beechcraft_T-34_Mentor
Flat Wing Span (m): 10.0584
Flat Wing Area (m²): 16.6854
Aircraft Engine: Pratt & Whitney Canada PT6
Number of Engines: 1