Reims-Cessna F177RG Cardinal — Weight And Balance

This document provides essential weight and balance information for the Reims-Cessna F177RG Cardinal. It is designed for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution of the aircraft. Proper weight and balance calculations are crucial for safe flight operations, ensuring that the aircraft remains within its performance parameters. The document outlines the maximum weight limits, center of gravity (CG) ranges, and provides tables and formulas for calculating the weight and balance based on various loading scenarios.

• Maximum takeoff weight: 2,550 lbs (1,157 kg)
• CG limits: 34.0 inches to 40.0 inches from the leading edge of the wing
• Weight and balance calculations are critical for flight safety
• Proper loading distribution is essential for aircraft stability
• Use provided tables and formulas for accurate weight calculations.