CESSNA 185 — Performance
1 performance reference for the CESSNA 185.
This document presents an informal evaluation of the Cessna Model 185 and the Helio L-28A airplanes conducted by the United States Army Aviation Board. The evaluation focuses on the general characteristics, flight characteristics, and performance data of both aircraft. The Cessna 185 is highlighted as a six-place, all-metal, high-wing monoplane powered by a Continental IO-470-F engine. The report includes detailed performance metrics such as takeoff and landing distances, climb rates, and cruise speeds, providing valuable insights for pilots and aviation enthusiasts interested in the operational capabilities of the Cessna 185. The document serves as a reference for understanding the aircraft's performance under various conditions and its suitability for utility missions.
- Gross weight: 3,200 lbs
- Empty weight: 1,625 lbs
- Useful load: 1,575 lbs
- Takeoff distance over 50 ft: 1,115 ft
- Landing distance over 50 ft: 959 ft
- Best rate of climb: 850 fpm at 82 knots
- Cruise speed: 130 knots at 70% power
- Maximum range: 820 nautical miles at 144 knots
How many Performance documents does Sprinkle have for the CESSNA 185?
Sprinkle has 1 Performance document on file for the CESSNA 185.
What year is the CESSNA 185 Performance?
The CESSNA 185 Performance on file is dated 1962.
How many pages is the CESSNA 185 Performance?
The CESSNA 185 Performance runs 21 pages.
Where does Sprinkle's CESSNA 185 Performance come from?
This CESSNA 185 Performance was originally published by apps.dtic.mil and is hosted on Sprinkle with full text and specs.