The Yakovlev Yak-58 is a small multi-role utility transport and business aircraft with a pusher engine and a twin boom tail, built in limited numbers in the late 1990s. It was the first design the Yakovlev bureau produced after the Soviet collapse, when military contracts dried up and the firm turned to civilian aircraft. The low-winged monoplane has a Vedeneyev M14PT radial engine mounted at the rear of the fuselage nacelle driving a three-bladed propeller, two highly swept fins fixed directly to the wing and joined by the tailplane, and a retractable tricycle undercarriage. It seats a pilot and five passengers, or carries 450 kg of cargo in place of the passengers. The first prototype flew at Tbilisi in December 1993 and crashed at the ILA Berlin Air Show in May 1994, and limited production followed at Tbilisi despite funding and political difficulties.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineVedeneyev M14PT 9-cylinder air-cooled radial piston engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Yakovlev Yak-58 (Wikipedia)
Of Make
Source Yakovlev Yak-58 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Yakovlev Yak-58 (Wikipedia)LeadQuote, Lead
The Yakovlev Yak-58 is a small, multi-role utility transport and business aircraft.
Sources
1. Yakovlev Yak-58 (Wikipedia)
Lead
The Yakovlev Yak-58 is a small, multi-role utility transport and business aircraft.
Testing, first flight
The first prototype made its maiden flight at Tbilisi, Georgia on 26 December 1993
Specifications, powerplant
Powerplant: 1 × Vedeneyev M14PT 9-cylinder air-cooled radial piston engine
Specifications, engine fitted
Powerplant: 1 × Vedeneyev M14PT 9-cylinder air-cooled radial piston engine
Specifications, empty weight
Empty weight: 1,270 kg
Specifications, maximum weight
Gross weight: 2,800 kg
Specifications, maximum speed
Maximum speed: 300 km/h
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