Cessna 195 — Specifications

This document provides detailed torque specifications for the Cleveland and McCauley wheel and brake assemblies used in the Cessna 195 and Cessna 195A aircraft models. It emphasizes the importance of proper torque settings to prevent damage to brake components and ensure safe operation. The specifications include various bolt sizes and their corresponding torque values in inch-pounds (in-lb) and Newton-meters (N-m). This reference is essential for maintenance personnel and pilots who perform inspections or repairs on the aircraft's braking system.

• Proper torque settings are critical to prevent brake system failures.
• Torque values range from 60 in-lb (6.8 N-m) to 150 in-lb (16.9 N-m) depending on the component.
• Surface depressions greater than 0.005 inch (0.127 mm) require brake cylinder replacement.
• Use specified thread lubricants to ensure accurate torque application.
• Consult the aircraft maintenance manual for detailed procedures.