Beechcraft Premier I — Pilot's Operating Handbook

This document is an article from Business & Commercial Aviation, published in October 2001, focusing on the Beechcraft Premier I, a light turbofan business jet developed by Raytheon Aircraft. The article provides a comprehensive overview of the aircraft's design, performance, and operational characteristics. It highlights the Premier I's spacious cabin, advanced avionics, and performance metrics, comparing it to other aircraft in its class. The document is intended for pilots, aviation enthusiasts, and industry professionals interested in the specifications and capabilities of the Premier I.

• Maximum Takeoff Weight: 12,500 lbs (5,670 kg)
• Range: 1,385 nautical miles with full payload
• Takeoff Field Length: 3,792 feet
• Cabin Width: 5 feet 6 inches (1.68 m)
• Cruise Speed: 0.785 Mach