Piper Pilot 100i — Specifications

This document provides detailed specifications for the Piper Pilot 100i, a single-engine piston aircraft designed primarily for flight training. It outlines the aircraft's dimensions, weight capacities, fuel specifications, engine details, and avionics features. The Pilot 100i is positioned as an affordable yet capable training aircraft, emphasizing reliability and safety. Key performance metrics such as range, takeoff and landing distances, and cruise speed are also included, making this document a valuable resource for flight schools and aviation enthusiasts interested in the capabilities of the Piper Pilot 100i.

• Usable fuel capacity: 48 US gallons (182 liters)
• Maximum takeoff weight: 2,550 lb (1,157 kg)
• Maximum range: 522 nautical miles (967 km)
• Takeoff distance (over 50' obstacle): 1,608 ft (490 m)
• Maximum cruise speed: 128 ktas (237 km/h)