1967 Dehavilland DHC-2TTurboprop Aircraft

This 1967 DeHavilland DHC-2T represents a complete factory-new turbine conversion with zero time since major overhaul. The aircraft features a comprehensive BX conversion package including new BX wings certified under SA97-88, a factory-new PT6A-34 turbine engine with 3,600-hour TBO, and a new Hartzell 106-inch three-bladed reversible propeller with full feathering capabilities. Performance metrics show impressive short-field capabilities with a 453-foot ground roll takeoff and 474-foot landing roll at gross weight under standard conditions.

The conversion includes extensive modern upgrades such as a redesigned instrument panel with new avionics and an Electronics International MVP-50T engine monitoring system, with panel customization available. Notable enhancements include carbon fiber air inlets and cowlings, an electrical inertial particle separator with ice bypass, and a completely redesigned fuel system. The aircraft is equipped with a 200 AMP Ametek starter generator, new bleed air cabin heat, and a Concorde lead-acid battery in a stainless steel encapsulation. With a maximum gross weight of 5,999 lbs and 148.2 USG main wing fuel capacity plus 64 USG in auxiliary tanks, this amphibious turbine Beaver offers substantial payload flexibility in a newly rebuilt airframe.