About the HAWKER BEECHCRAFT CORP 390
The Hawker Beechcraft 390, also widely known as the Beechcraft Premier I, is a significant model in the realm of light business jets. Initially developed by Raytheon Aircraft Company, later known as Hawker Beechcraft, the Premier I made its maiden flight on December 22, 1998, and received FAA certification in 2001. Its design catered to a growing demand for faster and more efficient business travel, targeting small to medium-sized businesses that required corporate jets with superior performance but at a more accessible price point compared to larger jets.
The development of the Premier I was driven by the need to introduce a revolutionary aircraft that incorporated advanced materials and production techniques. Notably, the Premier I was one of the first business jets to utilize a composite fuselage, which provided significant weight savings and improved aerodynamic performance. The aircraft was powered by twin Williams FJ44-2A engines, offering a good balance of power and efficiency.
Key Features and Capabilities
The Premier I's niche within the market is defined by its combination of speed, range, and comfort. It was designed to comfortably accommodate up to six passengers in a luxurious cabin that features a flat floor, which is uncommon among light jets. The Premier I boasts a maximum cruise speed of around 450 knots and a range of approximately 1,500 nautical miles, making it an excellent choice for regional travel and even some transcontinental routes within the United States.
Production ran from 1998 until 2013, and during this period, the aircraft saw incremental improvements in avionics and interior appointments, leading to the introduction of the Premier IA variant. The Premier I and IA stand out due to their advanced use of materials and emphasis on passenger comfort within the light jet category. This blend of technological innovation and market need fulfillment secured the Premier I's place as a notable and impactful aircraft in the general aviation landscape.