Cessna 195 — Parts Catalog

This document provides installation instructions for corrugated control skins manufactured by McFarlane Aviation, Inc., specifically designed for various Cessna aircraft models including the Cessna 195. It outlines the part numbers eligible for installation, the materials used, and the necessary procedures for removing old skins and installing new ones. The document emphasizes the importance of following FAA guidelines and using qualified personnel for the installation process. It serves as a technical reference for aircraft mechanics and maintenance personnel involved in the upkeep of Cessna aircraft.

• The document is specifically for Cessna 120, 140, 140A, 170, 170A, 190, and 195 aircraft.
• Installation requires adherence to FAA guidelines and should be performed by qualified personnel.
• Part numbers for eligible skins include MC0424000-10, MC0424000-20, and others listed in the document.
• The minimum acceptable drill bit diameter for rivet holes is #30 for spar locations and #40 for trailing edges.
• All control skins should be replaced simultaneously upon first installation of McFarlane skins.