Piper PA-34 Seneca III — Weight And Balance

This document provides the weight and balance information for the Piper PA-34-200 Seneca III. It includes details on standard empty weight, maximum takeoff and landing weights, and passenger weight calculations. The document is essential for pilots to ensure that the aircraft is loaded within safe limits for flight operations. It also outlines standard passenger weights for different seasons and provides formulas for calculating Vref and landing weight. This information is critical for maintaining the aircraft's performance and safety during operations.

• Standard Empty Weight: Includes unusable fuel and full oil.
• Maximum Takeoff Weight: 4200 lbs.
• Maximum Landing Weight: 4000 lbs.
• Total Fuel Capacity: 93 gallons (6.0 lbs/gallon).
• Standard passenger weights vary by season: 206 lbs male in summer, 212 lbs in winter.