CESSNA 421 TURBINE — Weight & Balance
1 weight & balance reference for the CESSNA 421 TURBINE.
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
How many Weight & Balance documents does Sprinkle have for the CESSNA 421 TURBINE?
Sprinkle has 1 Weight & Balance document on file for the CESSNA 421 TURBINE.
What year is the CESSNA 421 TURBINE Weight & Balance?
The CESSNA 421 TURBINE Weight & Balance on file is dated 1981.
How many pages is the CESSNA 421 TURBINE Weight & Balance?
The CESSNA 421 TURBINE Weight & Balance runs 8 pages.
Where does Sprinkle's CESSNA 421 TURBINE Weight & Balance come from?
This CESSNA 421 TURBINE Weight & Balance was originally published by www.aeroresourcesinc.com and is hosted on Sprinkle with full text and specs.