Diamond DA20-C1 Eclipse — Specifications
2 specifications references for the Diamond DA20-C1 Eclipse.
This document provides detailed specifications for the 2006 Diamond DA20-C1 Eclipse aircraft. It includes critical information about the aircraft's engine, performance, dimensions, and weight limits. Designed for pilots and aviation enthusiasts, the specifications outline the capabilities and operational limits of the DA20-C1 Eclipse, ensuring that users have the necessary data for safe and efficient flight operations. The document serves as a quick reference for understanding the aircraft's performance metrics, weight distribution, and fuel requirements.
- Engine: Continental IQ-240B3B, 125 HP, TBO 2000 hrs
- Max ramp weight: 1764 lbs; Gross weight: 1764 lbs; Empty weight: 1164 lbs
- Cruise speed: 138 knots at 75% power; 130 knots at 65% power
- Fuel consumption: 5.5 gph at 75% power; 4.8 gph at 65% power
- Best rate of climb: 1000 fpm; Max operating altitude: 13,120 ft
How many Specifications documents does Sprinkle have for the Diamond DA20-C1 Eclipse?
Sprinkle has 2 Specifications documents on file for the Diamond DA20-C1 Eclipse.
What year is the Diamond DA20-C1 Eclipse Specifications?
The Diamond DA20-C1 Eclipse Specifications on file is dated 2006.
How many pages is the Diamond DA20-C1 Eclipse Specifications?
The Diamond DA20-C1 Eclipse Specifications runs 2 pages.
Where does Sprinkle's Diamond DA20-C1 Eclipse Specifications come from?
This Diamond DA20-C1 Eclipse Specifications was originally published by airmart.com and is hosted on Sprinkle with full text and specs.