Piper PA-34 Seneca III — Specifications
1 specifications reference for the Piper PA-34 Seneca III.
Overview
Specifications for the Piper PA-34 Seneca III · 1985
This document provides detailed specifications and performance data for the Piper PA-34-220T Seneca III, a light twin aircraft known for its operational flexibility and comfort. The Seneca III has evolved from earlier models, incorporating improvements in weight limits, engine performance, and cockpit design. It is designed for both private and commercial use, making it a popular choice among pilots. The document outlines the aircraft's dimensions, weight limits, performance metrics, and operational capabilities, making it a valuable resource for pilots and aviation enthusiasts.
- Maximum takeoff weight: 4,750 lb
- Single-engine rate of climb: 240 fpm
- Takeoff distance (ground roll): 920 ft
- Maximum operating altitude: 25,000 ft
- Fuel capacity: 128 gallons (123 gallons usable)
1 document