Beechcraft Premier I

Key Specifications

Overview

The Beechcraft Premier I is a light twin-engine jet designed for personal and corporate transportation. Introduced in the late 1990s, this aircraft represents a significant advancement in the light jet category, offering transcontinental capability with a focus on efficiency and performance. The Premier I features a sleek, modern design with a pressurized cabin capable of carrying up to six passengers in comfort. Equipped with two Pratt & Whitney Canada engines, it delivers impressive speed and range for its class. The aircraft is popular among fractional ownership programs, charter operators, and private owners seeking reliable, economical jet transportation. Notable features include a sophisticated avionics suite, single-pilot capability (with appropriate training and certification), and relatively low operating costs compared to midsize jets. The Premier I has proven particularly valuable in markets where runway limitations exist, thanks to its short-field performance. Its spacious cabin and modern pressurization systems make it suitable for long-distance business travel. The aircraft has maintained a solid safety record and continues to be valued in the pre-owned market, particularly among operators seeking efficient light jet performance without the expense of larger cabin-class aircraft.

Technical Specifications

Maximum Speed: 500 knots
Cruise Speed: 460 knots
Range: 1,800 nautical miles
Service Ceiling: 43,000 feet
Engines: 2x Pratt & Whitney Canada PW610F turbofans
Maximum Takeoff Weight: 10,900 pounds
Useful Load: 3,400 pounds
Cabin Pressurization: 10,000 feet cabin altitude at 43,000 feet
Runway Requirements: 3,200 feet (takeoff), 3,100 feet (landing)