Beechcraft Premier I — Type Certificate

This document is the Type Certificate Data Sheet No. A00010WI for the Beechcraft 390, also known as the Premier I. Issued by the Federal Aviation Administration, it outlines the conditions and limitations under which the aircraft meets airworthiness requirements. The data sheet includes critical information regarding engine specifications, fuel requirements, airspeed limits, weight and balance, and control surface movements. It serves as an essential reference for pilots and maintenance personnel to ensure compliance with operational standards and safety regulations. The document is particularly relevant for operators of the Beechcraft 390, providing necessary details for safe and efficient operation.

• Maximum takeoff weight: 12,500 lbs
• Maximum operating altitude: 41,000 feet
• Static thrust per engine: 2300 lbs
• Maximum operating speed (Vmo): 320 KCAS
• Fuel capacity: 552.8 gallons (gravity fill)