Piper M600 — Weight And Balance

This document provides essential weight and balance information for the Piper M600 aircraft. 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 capacities, center of gravity limits, and methods for calculating weight and balance. Understanding these parameters is crucial for flight safety and compliance with aviation regulations. The document serves as a reference for pre-flight planning and loading procedures, ensuring that the aircraft is operated safely and efficiently.

• Maximum Takeoff Weight: 6,000 lbs
• Maximum Landing Weight: 6,000 lbs
• Maximum Zero Fuel Weight: 5,500 lbs
• CG Limits: 84.0 inches to 108.0 inches
• Weight and balance calculations are essential for safe flight operations.