Piper PA-28R Arrow — Weight And Balance

This document provides the weight and balance information for the Piper PA-28R Arrow. It is intended for pilots and aviation personnel who need to ensure that the aircraft is loaded within its weight limits for safe operation. The document outlines the maximum weight limits, loading procedures, and how to calculate the center of gravity (CG) for various loading scenarios. Proper weight and balance calculations are critical for flight safety, as they affect the aircraft's performance and handling characteristics.

• Maximum takeoff weight: 2,800 lbs
• CG limits: 76 inches to 84 inches from the datum
• Follow specific loading procedures for safe weight distribution
• Example calculations help ensure accurate weight and balance assessments