Piper PA-42 Cheyenne 400 — Performance Data

This document provides detailed specifications and performance data for the Piper PA-42 Cheyenne 400LS. It is intended for pilots and aviation enthusiasts who require precise information about the aircraft's capabilities, including power plants, weights, dimensions, and performance metrics under standard atmospheric conditions. The document outlines critical data such as cruise speeds, takeoff and landing distances, climb rates, and stall speeds, which are essential for flight planning and operational safety.

• Maximum takeoff weight: 12,050 lbs (5466 kg)
• Cruise speed at 35,000 ft: 334 kts (619 kph)
• Takeoff distance over 50 ft obstacle: 2,325 ft (709 m)
• Rate of climb at sea level: 3,242 fpm (988 m/m)
• Maximum usable fuel: 570 U.S. gal. (2158 L)
• Stall speed with flaps 30°: 84 kts (156 kph)
• Service ceiling with two engines: 41,000+ ft (12497+m)