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
What is the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications?
The 2006 Diamond DA20-C1 Eclipse Aircraft Specifications is a specifications for the Diamond DA20-C1 Eclipse, dated 2006.
How many pages is the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications?
The copy of the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications on file runs 2 pages.
Where does the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications come from?
This copy of the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications was originally published by airmart.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the 2006 Diamond DA20-C1 Eclipse Aircraft Specifications published?
The 2006 Diamond DA20-C1 Eclipse Aircraft Specifications — the Diamond DA20-C1 Eclipse specifications on file — is dated 2006.
Most owners only have the POH. Here's the essential set for the Diamond DA20-C1 Eclipse.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Diamond DA20-C1 Eclipsemanuals & documents
See all 18 →- Parts Catalog for the Diamond DA20-C1 EclipseParts Catalog
- Accuracy Examination of the SDCM Augmentation System in Aerial NavigationOther Documents
- Airplane Flight ManualFlight Manual
- DA-20-C1 Eclipse Private Pilot Flight Training TipsService Manual
- DA20-C1 AIRPLANE FLIGHT MANUALTraining Manual
- Request for Proposals: Supply of a Flight Simulation Training DeviceAvionics Manual
- DA20Weight And Balance
- DA-20-C1 Eclipse Private Pilot Flight Training TipsPilot's Operating Handbook
- AOPA PILOT • 86 • OCTOBER 2008Normal Procedures
- FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA01800SE FOR INSTALLATION OF SEATON ENGINEERING CORP. ELECTRONIC DIMMER CONTROLLERService Bulletins
- INSTRUKCJA UŻYTKOWANIA W LOCIE samolotu DA 20-C1Maintenance Manual
- DA20Systems Description
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