Piper PA-23 Aztec — Weight And Balance
3 weight and balance references for the Piper PA-23 Aztec.
Overview
Weight & Balance for the Piper PA-23 Aztec
This document provides essential weight and balance information for the Piper PA-23 Aztec. It is designed for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe operation of the aircraft. The manual outlines the maximum takeoff weight, center of gravity limits, and provides various loading scenarios to ensure compliance with safety regulations. It serves as a critical reference for pre-flight planning and weight management, ensuring that the aircraft is operated within its certified limits.
- Maximum takeoff weight: 4,500 lbs
- Center of gravity limits: 34.0 to 39.0 inches
- Fuel weight: 6 lbs per gallon
- Total fuel capacity: 100 gallons
- Proper weight distribution is critical for safe flight.
3 documents