Piper PA-28 Dakota — Checklist

This document is a checklist for the Piper PA-28 Dakota II, specifically tailored for pilots operating the aircraft. It provides a comprehensive series of checks to be performed before and after engine start, during taxi, takeoff, and landing. The checklist is designed to ensure that all necessary safety and operational procedures are followed, enhancing the safety and efficiency of flight operations. It includes specific operational parameters, such as fuel management, engine performance checks, and preflight inspections, making it a vital tool for pilots to reference during their flight preparations and operations.

• Max Takeoff Mass: 3000 lbs (1361 kg)
• Fuel Capacity: 72 USG usable, 36 USG per wing tank
• Oil Capacity: Max 12 Qts, Min 6 Qts (1 Qt = 0.95 L)
• Cruise Power Setting: 65% at 2300 RPM
• Max RPM Drop during Magneto Check: 175 RPM, Max Difference: 50 RPM