Piper PA-28 Dakota — Performance Data
1 performance data reference for the Piper PA-28 Dakota.
This document provides performance data for the Piper PA-28 Dakota, a six-cylinder aircraft powered by a Lycoming engine. It includes specifications on engine performance, weights, dimensions, fuel capacity, and various performance metrics such as speed, climb rate, and takeoff distances. The information is crucial for pilots and aviation enthusiasts to understand the aircraft's capabilities and limitations. The document serves as a reference for flight planning and operational procedures, ensuring safe and efficient flight operations.
- Engine: Lycoming 0-540-J3A5D, 235 hp @ 2400 RPM
- Gross Weight: 3000 lbs (1361 kg), Useful Load: 1392 lbs (631 kg)
- Maximum Speed: 148 knots (274 km/h)
- Takeoff Distance: 825 ft (251 m) ground run, 1725 ft (526 m) over 50 ft obstacle
- Service Ceiling: 17,500 ft (5334 m)
How many Performance Data documents does Sprinkle have for the Piper PA-28 Dakota?
Sprinkle has 1 Performance Data document on file for the Piper PA-28 Dakota.
How many pages is the Piper PA-28 Dakota Performance Data?
The Piper PA-28 Dakota Performance Data runs 2 pages.
Where does Sprinkle's Piper PA-28 Dakota Performance Data come from?
This Piper PA-28 Dakota Performance Data was originally published by airmart.com and is hosted on Sprinkle with full text and specs.