Cessna 337 Super Skymaster — Systems Description
1 systems description reference for the Cessna 337 Super Skymaster.
The document provides a detailed overview of the Cessna 337 Super Skymaster, a high-performance twin-engine aircraft introduced by Cessna in 1967. It highlights the aircraft's capabilities, including its impressive takeoff performance, service ceiling, and cruising speed. The Super Skymaster is notable for its centerline thrust configuration, which distinguishes it from other light twin aircraft. The document also mentions its military applications and export success, indicating its popularity in the aviation market. This information is valuable for pilots and aviation enthusiasts interested in understanding the specifications and operational characteristics of the Super Skymaster.
- Takeoff distance at full gross weight: less than 2,000 feet
- Service ceiling: 31,000 feet
- Cruising speed at 75% power: 225 mph at 24,000 feet
- Cruise range: 860 miles
- Engine power: two 210 horsepower engines
How many Systems Description documents does Sprinkle have for the Cessna 337 Super Skymaster?
Sprinkle has 1 Systems Description document on file for the Cessna 337 Super Skymaster.
What year is the Cessna 337 Super Skymaster Systems Description?
The Cessna 337 Super Skymaster Systems Description on file is dated 1967.
How many pages is the Cessna 337 Super Skymaster Systems Description?
The Cessna 337 Super Skymaster Systems Description runs 1 pages.
Where does Sprinkle's Cessna 337 Super Skymaster Systems Description come from?
This Cessna 337 Super Skymaster Systems Description was originally published by aeroresourcesinc.com and is hosted on Sprinkle with full text and specs.