Piper Aircraft PA-42T

No PA-42T-specific manual on file — this overview is from the Piper Aircraft PA-42 family documentation.

This document serves as the Pilot's Operating Handbook for the Piper PA-42 Cheyenne IIIA, detailing its specifications, operational procedures, and safety features. It is intended for pilots and aviation enthusiasts who require comprehensive information about the aircraft's performance, systems, and handling characteristics. The handbook provides critical data on engine specifications, weight limits, fuel capacities, and performance metrics, ensuring that operators can safely and effectively manage the aircraft in various flight conditions. Additionally, it covers emergency procedures and training recommendations to enhance pilot proficiency and safety.

• Maximum takeoff weight: 11,200 lbs
• Cruise speed at 25,000 ft: 310 KTAS
• Rate of climb at sea level: 2,380 fpm
• Maximum operating altitude: 35,840 ft
• Fuel capacity: 3,820 lbs (3,753 lbs usable)