Piper PA-28R Arrow II — Specifications

This document provides specifications for the Piper PA-28R-200, also known as the Cherokee Arrow II. It is intended for pilots and aviation enthusiasts who require detailed information about the aircraft's performance, weight, fuel capacity, and engine specifications. The document outlines critical data necessary for flight planning and operational understanding of the aircraft. Key specifications include engine details, fuel requirements, weight limits, and performance metrics, which are essential for safe and efficient operation of the aircraft.

• Engine: Lycoming IO-360-C1C, 200 HP, 4 cylinders.
• Fuel capacity: 50 gallons, minimum octane 100, average burn 10.15 gallons/hour at 75% power.
• Max takeoff/landing weight: 2,650 lbs; standard empty weight: 1,499 lbs; max useful load: 1,151 lbs.
• Max speed: 186 KCAS; max structural cruising speed: 148 KCAS; stall speed clean: 62 knots.
• Best rate of climb: 900 FPM; service ceiling: 15,000 ft.