CESSNA T-182 Turbo Skylane — Type Certificate

This document provides specifications for certificated aircraft engines, focusing on various piston engine models, including four, six, and eight-cylinder configurations. It serves as a technical reference for aviation professionals, including pilots and maintenance personnel, detailing engine types, performance metrics, and installation guidelines. The document includes information on engine designations, horsepower ratings, RPM, fuel types, and compression ratios, which are critical for understanding engine performance and compatibility with different aircraft models. The data is structured to facilitate quick reference for engine specifications, making it a valuable resource for those involved in aircraft operation and maintenance.

• The O-235-C1 engine produces 115 HP at 2800 RPM with a compression ratio of 6.75:1.
• Engine designations include critical information such as cylinder configuration and fuel type.
• Different engine mounts (conical, dynafocal) affect installation and performance.
• Fuel specifications include 100LL and 80 octane, which are essential for engine operation.