Beechcraft Beechjet 400A — Specifications

This document provides detailed specifications for the 1999 Beechcraft Beechjet 400A, including performance metrics, engine specifications, avionics, and maintenance status. It is intended for potential buyers and aviation professionals interested in the operational capabilities and current condition of the aircraft. Key performance figures such as maximum takeoff weight, cruise speeds, and range are highlighted, along with detailed engine hours and maintenance history. The document also lists the avionics suite and additional equipment installed on the aircraft, ensuring that prospective buyers have a comprehensive understanding of the aircraft's features and performance.

• Ramp Weight: 16,500 lbs
• MTOW: 16,300 lbs
• Max Landing Weight: 15,700 lbs
• Max Cruise Speed: 468 knots
• NBAA Range: 1,457 nautical miles
• Service Ceiling: 45,000 feet
• Engine TBO: 625.3 hours (LH), 406.4 hours (RH)