2006 Diamond DA20-C1 Eclipse Aircraft Specifications
Diamond DA20-C1 Eclipse · Specifications
Overview
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
Document
Source
Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 2006
- Pages
- 2
- File size
- 38 KB
- Publisher
- airmart.com
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In this document
Engine Specifications
The Diamond DA20-C1 Eclipse is powered by a Continental IQ-240B3B engine, delivering 125 horsepower at takeoff. The engine has a time between overhaul (TBO) of 2000 hours and requires 100/100LL fuel.
Weight and Capacity
The aircraft has a maximum ramp weight of 1764 lbs, which is also its gross weight and landing weight. The empty weight is 1164 lbs, providing a useful load of 600 lbs. With full standard fuel, the payload capacity is 456 lbs.
Performance Metrics
At 75% power, the cruise speed is 138 knots, while at 65% power, it is 130 knots. Fuel consumption at 75% power is 5.5 gallons per hour, and at 65% power, it is 4.8 gallons per hour. The best rate of climb at sea level is 1000 feet per minute.
Dimensions
The wingspan of the DA20-C1 Eclipse measures 35 feet 8 inches, with an overall length of 23 feet 6 inches and a height of 7 feet 2 inches. The wing area is 125 square feet.
Takeoff and Landing Performance
The takeoff ground roll is 1280 feet, and it requires 1640 feet to clear a 50-foot obstacle. The landing ground roll is 661 feet, with a requirement of 1360 feet to land over a 50-foot obstacle.
Full document text
2006 Diamond DA20-C1 Eclipse Aircraft Specifications 2006 Diamond DA20-C1 Eclipse Engine make/model: Continental IQ-240B3B Horsepower on takeoff: 125 TBO hrs.: 2000 Fuel type: 100/100LL Propeller: Sensenich FP Landing gear type: Tri/Fixed Max ramp weight (lbs.) 1764 Gross weight (lbs.): 1764 Landing weight (lbs.): 1764 Empty weight, std. (lbs.): 1164 Useful load, std. (lbs.): 600 Useful fuel, std. (gals.): 24 Payload, full std. fuel (lbs.): 456 Wingspan: 35 ft. 8 in. Overall length: 23 ft. 6 in. Height: 7 ft. 2 in. Wing area (sq. ft.): 125 Wing loading (lbs./sq. ft.): 14.1 Power loading (lbs./hp): 14.1 Wheel size (in.): 6.00 x 6 Seating capacity: 2 PERFORMANCE Cruise speed (kts.): • 75% power: 138 • 65% power: 130 Fuel consumption (gph): • 75% power: 5.5 • 65% power: 4.8 Vs (kts.): 45 Best rate of climb, SL (fpm): 1000 Maximum Operating Altitude (ft.): 13,120 Takeoff ground roll (ft.): 1280 Takeoff over 50-ft. obstacle (ft.): 1640 Landing ground roll (ft.): 661 Landing over 50-ft. obstacle (ft.): 1360
What's in the Diamond DA20-C1 Eclipse TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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