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Information About

T-34 Mentor




The Beechcraft T-34 Mentor is a military Trainer Aircraft derived from the Beechcraft Bonanza . The signature V-tail of the Bonanza was replaced with conventional tail control surfaces. The four-passenger cabin was replaced with a two-seater tandem cockpit and bubble canopy. The T-34A and T-34B used a conventional, Piston Driven Engine while the '''T-34C Turbo Mentor''' is Turboprop -powered. The T-34C is still used as the primary training aircraft for United States Navy and Marine Corps pilots. The T-34C is currently scheduled to be replaced by the T-6 Texan II but is still the primary aircraft at NAS Corpus Christi and NAS Whiting Field.

The Mentor is the aircraft used by the Lima Lima Flight Team .

In 2004 , due to a series of crashes involving in-flight structural failure during simulated combat flights, the entire U.S. civilian fleet of T-34s was grounded by the Federal Aviation Administration . The grounding has since been eased to a series of restrictions on permitted flight envelope.

This year (2006) two T-34C Turbo Mentors crashed during training at NAS Corpus Christi.


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 replace by the T-34C. (423 built by Beechcraft)

  • 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.

  • --- Turbine Mentor 34C - Civil version

  • --- YT-34C - Two T-34Bs were fitted with turboprop engines, and were used as T-34C prototypes.



SPECIFICATIONS (T-34C)

  plane Or Copter plane
  jet Or Prop prop
  <!-- Now, Fill Out The Specs Please Include Units Where Appropriate (main Comes First, Alt In Parentheses) If An Item Doesn't Apply, Like Capacity, Leave It Blank For Instructions On Using ref , more general=, more performance=, power original=, and thrust original= see -->
  crew Two
  length Main 28 ft 9 in
  length Alt 875 m
  span Main 33 ft 4 in
  span Alt 1060 m
  height Main 9 ft 7 in
  height Alt 292 m
  area Main 180 ft&2
  area Alt 167 m&2
  empty Weight Main 2,960 lb
  empty Weight Alt 1,342 kg
  max Takeoff Weight Main 4,300 lb
  max Takeoff Weight Alt 1,950 kg
  engine (prop) Pratt & Whitney Canada PT6 A-25
  type Of Prop Turboprop
  number Of Props 1
  power Main 550 Shp
  power Alt 410 kW
  max Speed Main 280 kt IAS
  max Speed Alt 320 mph, 520 km/h
  range Main 600 nm
  range Alt 690 mi, 1,110 km
  ceiling Main 25,000 ft
  ceiling Alt 7,600 m
  climb Rate Main 1,480 ft/min
  climb Rate Alt 75 m/s




MILITARY OPERATORS

  • Algeria, Argentina, Canada, Chile, Colombia, the Dominican Republic, Ecuador, El Salvador, France, Gabon, Greece, Indonesia, Japan, Mexico, Morocco, Peru, Philippines, Spain, United States (Air Force, Navy, Marine Corps, Coast Guard), Uruguay, Venezuela.



EXTERNAL LINKS



RELATED CONTENT

  sequence (US military):'''
  sequence (Beechcraft):'''