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Cessna 337 Super Skymaster — Systems Description

1 systems description reference for the Cessna 337 Super Skymaster.

Overview
Turbo-System Super Skymaster · 1967

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
1 document