Piper PA-28 Dakota — Systems Description

This document serves as a systems description and training guide for the Piper PA-28 Dakota, specifically the PA-28-236 model introduced in 1979. It provides essential information for pilots preparing for their checkout in the Dakota, focusing on its systems, operational procedures, and performance characteristics. The document includes a questionnaire designed to familiarize pilots with the aircraft's systems and operational requirements, ensuring they are well-prepared for flight. It emphasizes the importance of understanding the Dakota's unique features, such as its engine specifications, fuel system, electrical system, and emergency procedures, to enhance safety and efficiency during operations.

• The Dakota PA-28-236 has a Lycoming O-540 engine with 235 HP.
• Total fuel capacity is 77 US gallons, with 72 gallons usable.
• Normal oil pressure range is 25-100 PSI; maximum oil temperature is 245°F.
• Maximum takeoff weight is 3000 lbs; maximum ramp weight is 3011 lbs.
• Key airspeeds include Vr at 60-65 KIAS and Vx at 73 KIAS.