DA20
Diamond DA20-C1 Eclipse · Systems Description
Overview
This document serves as a systems description for the Diamond DA20-C1 Eclipse, detailing its airframe, powerplant, avionics, and performance specifications. It is designed for pilots and aviation enthusiasts who seek a comprehensive understanding of the aircraft's capabilities and features. The DA20-C1 is known for its sporty design, advanced avionics, and impressive performance metrics, making it suitable for both training and recreational flying. Key features include a composite airframe, a 125 hp engine, and a modern glass cockpit, which together enhance safety and flying experience.
- Max Take-off Weight: 1,764 lbs
- Cruise Speed: 130 KTAS at 75% power
- Climb Rate: 930 fpm at sea level
- Max Speed: 130+ KTAS at MCP
- Take-off Distance: 1,640 ft over 50 ft obstacle
- Fuel Capacity: 24.5 USG, Unusable: 0.5 USG
- Max Demonstrated Cross Wind: 20 kts
Document
Source
Originally published by utilityair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Systems Description
- Pages
- 4
- File size
- 3.7 MB
- Publisher
- utilityair.com
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In this document
Airframe & Powerplant
The DA20-C1 Eclipse features a 125 hp Continental Motors IO-240-B32B engine paired with a Sensenich 2-blade fixed pitch propeller. The aircraft is constructed with an all-composite airframe, which contributes to its durability and low maintenance needs. The landing gear consists of fixed flat leaf aluminum spring main gear and a fixed steel nose gear, complemented by an electric flap system and safety features such as 26g cabin and seats.
Weights and Capacities
The maximum take-off weight for the DA20-C1 is 1,764 lbs, with a maximum ramp weight of 1,770 lbs. The standard empty weight is 1,180 lbs, providing a useful load of 584 lbs. The fuel capacity is 24.5 US gallons, with 0.5 US gallons considered unusable.
Performance Specifications
The DA20-C1 Eclipse has a maximum speed of over 130 KTAS at maximum continuous power and a cruise speed of 130 KTAS at 75% power, consuming 6.9 gallons per hour at 4,000 feet. It has a climb rate of 930 feet per minute at sea level and a certified ceiling of 13,120 feet. The take-off distance at maximum take-off weight is 1,640 feet over a 50-foot obstacle.
Avionics
The aircraft is equipped with a Garmin G500 glass cockpit, which includes a GTN635 GPS/COM, GTX 345 Mode S transponder, and UMA engine instrumentation. This modern avionics suite enhances situational awareness and training capabilities.
Safety Features
The DA20-C1 is designed with an integrated safety cell that surrounds the cockpit and vital systems, providing excellent crashworthiness. The composite airframe construction is resistant to hangar rash and easily repairable, ensuring longevity and safety.
Safety notes
- The aircraft features an integrated safety cell for crashworthiness.
- Composite construction enhances durability and reduces maintenance needs.
Full document text
DA20Sporty. Sleek. Exciting. Yet surprisingly affordable Contact us today at 1-888-359-3220 Or find us online at www.diamondaircraft.com With a fighter-like canopy, offering easy access to the cockpit, responsive center-stick pushrod controls and comfortable bucket seats, the DA20 will put a smile on any pilot’s face. It has pleased some of the world’s toughest customers, including the United States Air Force for over 15 years. Boasting a sea-level climb rate of 1,000 fpm, a cruise of over 130 ktas, and a take-off distance of only 1,600 feet over a 50 foot obstacle, the DA20’s performance shines, even at high density altitudes. Spin certified and with a slow 45 kcas stall speed, the DA20 is not only sporty, but stable – and has a demonstrated cross wind landing component of 20 knots! The sporty cockpit is one of the most comfortable and intuitive in its class thanks to ergonomically designed seats, available leather or sheepskin seating surfaces with 4 point inertia reel safety harnesses and a professional instrument panel with top quality equipment and materials throughout. The DA20 canopy and rear windows, together with a forward seating position relative to the wing, offer incredible outward visibility to help you navigate, spot other traffic and above all, enjoy the flight. Composite construction means strength and durability for the long run – including no defined structural life limit airframe. The smooth, rivet free construction dramatically reduces drag, saves weight and resists bumps and scrapes. The low maintenance polyurethane topcoat and underlying epoxy primer will keep your DA20 looking sharp for years. Far more resistant to hangar rash than sheet aluminum aircraft, the DA20’s composite airframe is easily repaired if the unexpected happens. Aerodynamic and tough, the rugged spring aluminum main landing gear and elastomeric-shock nose gear are tough enough for flight training and are virtually maintenance free. The optional aerodynamic wheel fairings add speed, fuel economy and overall good looks. The DA20 has an integrated safety cell, surrounding the cockpit and vital systems for excellent crashworthiness and flammable fluid fire protection. The airframe is modular and all replacement parts, from control surfaces to entire wings and other major assemblies can be replaced individually, in case of damage, minimizing cash draining AOG situations. The fuel injected 125 hp Continental Motors IO-240 with 2-blade fixed pitch propeller, installed in the DA20-C1, offers excellent climb and cruise performance, even at higher density altitudes. This reliable and well proven conventional AVGAS engine has logged millions of flight hours, is well known to technicians everywhere, with ready access to parts and service worldwide. The engine installation is designed for durability and easy maintenance with crackproof composite forward and aft baffles, robust stainless steel exhaust, easy access to filters and regular maintenance items, and quickly removable cowlings. The DA20’s instrumentation and avionics are designed for safety, positive learning transfer, reliability and value. The current version of the DA20-C1 is equipped with the latest industry leading avionics by Garmin, new and improved engine gauges and centrally located conventional standby instrumentation for conventional and partial panel training. The standard Garmin G500 combines a high-resolution primary flight display (PFD) and multi-function display (MFD) in one 10-inch wide bezel to bring the basic training cockpit into the 21st century and provides a great foundation for anyone moving up to Garmin’s G1000. A comprehensive list of options let you select exactly what you need and nothing you don’t. Airframe Propulsion Avionics Contact us today at 1-888-359-3220 Or find us online at www.diamondaircraft.com Airframe & Powerplant • 125hp Continental Motors IO-240-B32B engine • Sensenich 2 blade fixed pitch propeller • All composite airframe structure • Fixed flat leaf aluminum spring main landing gear • Fixed steel nose landing gear • Electric flap system • 26g cabin and seats • Sheepskin seat cushions • Inertia reel seat belts • Adjustable rudder pedals • 14 VDC power outlet • Canopy lining • HID landing and taxi lights • LED position and strobe lights • Rear baggage area Avionics Options • Garmin GMA340 (replaces PM1000), 1.1 lbs • Garmin GTN650 GPS/COM/NAV (replaces GTN635), 0.8 lbs • Garmin GTR225 VHF COM (number 2 com), 3 lbs • Avidyne TAS600 Traffic Advisory System, 15 lbs • Garmin Synthetic Vision Technology (SVT), 0 lbs • Stand-by attitude indicator, 2.5 lbs Weights Max Take-off Weight: 1,764 lbs Max Ramp Weight: 1,770 lbs Max Zero Fuel Weight: N/A Max Landing Weight: 1,764 lbs Standard Empty Weight1: 1,180 lbs Useful Load1: 584 lbs Max Fuel Weight1, 2: 144 lbs Full Fuel Payload1, 2: 440 lbs Avionics GARMIN G500 glass cockpit with: • GTN635 GPS/COM • GTX 345 Mode S Transponder (ADS-B In and Out) • PS Engineering PM 1000 intercom • UMA engine instrumentation • Standby Instruments (Air Speed Indicator & Altimeter) • 406 Mhz ELT Airframe Options • Premium leather interior, 0 lbs • Wheel fairings, 7 lbs • “Push to Engage” ignition system, 0 lbs • External power unit receptacle, 2.5 lbs • Engine pre-heater, 1.5 lbs • Heated pitot, 0.5 lbs Fuel & Capacity Fuel Capacity: 24.5 USG, Unusable: 0.5 USG STANDARD FEATURES & OPTIONS 1 Weights and Loads shown are for standard configuration. Selection of optional features may affect these weights. S/N specific Production variances can occur. 1, 2 Fuel density assumed at 6 lbs / USG Contact us today at 1-888-359-3220 Or find us online at www.diamondaircraft.com Contact us today at 1-888-359-3220 Or find us online at www.diamondaircraft.com Speeds Vne 164 KIAS Vr 44 KIAS Vf1 (T/O) 100 KIAS Vf2 (LDG) 78 KIAS Max Demonstrated Cross Wind 20 kts Runway Performance T/O Dist @ MTOW (grnd roll / over 50 ft obst): 1,256 ft / 1,640 ft LDG Dist @ MTOW (grnd roll / over 50 ft obst):
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661 ft / 1,360 ft Cruise Performance Max Speed 130+ KTAS @ MCP (Sea Level, ISA) Cruise Speed 130 KTAS @ 75% / 6.9 gph (4,000 ft, ISA+100C) Max Endurance1 5.1 hrs @ 45% Power / 4.7 gph (12,000 ft, ISA) Max Range1 544 nm @ 52% Power / 5.2 gph (12,000 ft, ISA) Ceiling Certified Ceiling, Normal Ops 13,120 ft Climb Performance 930 fpm @ 100% power1 Sea Level, ISA PERFORMANCE Note: 1 @ 1,600lbs Diamond Aircraft Industries Inc. 1560 Crumlin Sideroad, London, ON, Canada N5V 1S2 1-888-359-3220 ● sales@diamondair.com ● www.diamondaircraft.com CONTACT US TODAY:
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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