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The Yakovlev Yak-58, a twin-engine turboprop aircraft developed by the Yakovlev Design Bureau, holds a significant place in aviation history. Its development began in the late 1990s, with a focus on creating a capable and versatile utility transport aircraft.

 

One of the most notable features of the Yak-58 is its ability to operate from unprepared airstrips, allowing for operations in remote and challenging environments. This adaptability made it invaluable in various roles, including cargo transport, medical evacuation, aerial survey, and passenger transportation.

 

The Yak-58's design emphasizes durability, reliability, and ease of maintenance. Its robust construction, combined with advanced avionics and navigation systems, ensures safe and efficient operations in both civilian and military applications. Furthermore, the aircraft can accommodate up to 20 passengers or carry approximately 3,000 kilograms of cargo, making it a versatile asset for a wide range of missions.

 

In terms of performance, the Yak-58 boasts impressive specifications. Powered by two turboprop engines, it can achieve a top speed of 480 kilometers per hour and has a maximum range of over 2,500 kilometers. These capabilities allow for efficient regional operations, making the Yak-58 an excellent choice for operators involved in short-haul transportation or special missions.

 

Additionally, the Yakovlev Design Bureau prioritized safety during the aircraft's development. The Yak-58 is equipped with modernized avionics, including state-of-the-art navigation systems, communication equipment, and weather radar. These features enhance situational awareness and foster a safe operating environment for both the crew and passengers.

 

As the Yak-58 embodies the expertise and innovation of the Yakovlev Design Bureau, highlighting its history, design, capabilities, and performance would undoubtedly captivate aviation enthusiasts, professionals, and history aficionados alike.

 

General characteristics

• Crew: 1
• Capacity: 5 pax
• Length: 8.55 m (28 ft 1 in)
• Wingspan: 12.7 m (41 ft 8 in)
• Height: 3.16 m (10 ft 4 in)
• Wing area: 20 m² (220 sq ft)
• Empty weight: 1,270 kg (2,800 lb)
• Gross weight: 2,800 kg (6,173 lb)
• Powerplant: 1 × Vedeneyev M14PT 9-cylinder air-cooled radial piston engine, 269 kW (361 hp)
• Propellers: 3-bladed constant-speed pusher propeller

Performance

• Maximum speed: 300 km/h (190 mph, 160 kn)
• Cruise speed: 285 km/h (177 mph, 154 kn)
• Range: 1,000 km (620 mi, 540 nmi)
• Service ceiling: 4,000 m (13,000 ft)