Piper PA-28 Cadet — Systems Description

This document provides a detailed description and operational guidance for the Piper PA-28-161 Cherokee Warrior II. It is intended for pilots and maintenance personnel, offering insights into the aircraft's systems, including the engine, airframe, landing gear, flight controls, fuel system, electrical system, and more. The manual outlines specifications, operational procedures, and safety considerations necessary for the effective and safe operation of the aircraft. Key sections include engine specifications, landing gear details, and descriptions of the electrical and fuel systems, ensuring that users have comprehensive knowledge of the aircraft's capabilities and maintenance requirements.

• Engine rated at 160 HP at 2700 RPM.
• Total fuel capacity of 50 gallons (48 gallons usable).
• Main gear tire pressure: 24 psi; nose gear tire pressure: 30 psi.
• Fixed pitch propeller diameter: 74 inches.
• Daily fuel drains recommended to check for water or sediment.