CESSNA 421 TURBINE — Weight And Balance
1 weight and balance reference for the CESSNA 421 TURBINE.
Overview
Cessna Corsair Model 425 · 1981
This document provides detailed information about the Cessna 425 Corsair, a turboprop aircraft introduced by Cessna in 1979. It discusses the aircraft's design, performance specifications, systems, and operational characteristics. The Corsair is designed to be an easier transition for pilots moving from piston twins to turboprops, featuring advanced systems derived from the Citation program. The document is intended for pilots and aviation enthusiasts, offering insights into the aircraft's capabilities, handling, and maintenance considerations.
- Maximum takeoff weight: 8,200 lbs
- Fuel capacity: 2,499 lbs (2,452 lbs usable)
- Best rate of climb speed: 115 KIAS
- Maximum cruise speed: 257 knots at 30,000 feet
- Empty weight: 8,275 lbs
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