Piper PA-46 Malibu Mirage — Performance Data

This document provides performance specifications for the Piper PA-46 Mirage, a six-seat, low-wing aircraft powered by a Lycoming TIO-540-AE2A engine. It details the aircraft's engine specifications, weight limits, dimensions, and performance metrics, making it a valuable reference for pilots and aviation enthusiasts. The document outlines critical performance data such as cruise speeds, fuel consumption rates, and takeoff and landing distances, which are essential for flight planning and operational safety. This information is particularly useful for pilots operating in various conditions and helps ensure compliance with performance limitations.

• Engine: Lycoming TIO-540-AE2A, 350 HP
• Max ramp weight: 4358 lbs
• Cruise speed at 75% power: 213 knots
• Max operating altitude: 25,000 ft
• Takeoff distance over 50-ft obstacle: 2090 ft
• Landing distance over 50-ft obstacle: 1965 ft
• Useful fuel capacity: 120 gallons