Diamond DA20-C1 Eclipse

Number of Active Aircraft: 335 Active- Map

Audries CertifiedDiamond DA20-C1 - Detailed Data
Diamond DA20 C1 - Cruise and Fuel Burn Computer


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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 1166 lbs
Max Weight 1764 lbs
Useful Load: 598 lbs
Engine Name Continental IO-240 B
Engine Number 1
Horsepower 125 HP
Never Exceed Speed: 164 kts
Stall speed: 34 kts
Service Ceiling: 13120 ft
Max Fuel 25 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 140 kts
GPH (75% BHP): 6
MPG (75% BHP) 23.3
Range (75% BHP): 467 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 36 $
MPG per 1000 lbs of Payload 13.95
F-T (Speed^2/FuelBurn) 32.7 HP
F-T Payload 19.6 kts
MPH To HP: 11.2 kts
T/O Roll - T/O over 50 FT OBST 1150 ft / 1500 ft

SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00243BO (1 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (2 OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO ( PAGE 2) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010 0:00
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (3 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (2 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 2)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02217AK (1 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10267SC  Installation of Teledyne Continental Motors IOF-240-B engine Reissued 10/31/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA2586NM (PAGE 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA593CH (2 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
ST01700NY (1 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. Issued 7/8/2003
Fusulage Construction Semimonocoque
Airframe Material Carbon Fiber Composite
Number of Doors 1
Wing Location Bottom Wing
Wing Construction CFRP Spar
Wing Rib Material Semi-monocoque Sandwhich
Wing Skin Material Composite
Aileron Type Conventional
Aileron Trim None
Aileron Control System Push Rod
Flap Type Plain
Wing Flap Actuation Electric
Empennage Type T Tail
Empennage Rib Material Semi-Monocoque sandwich
Empennage Skin Material Composite
Rudder Trim Ground Adjustable Trim Tab
Yaw Trim Actuator None
Yaw Control System Cable and Pully
Pitch Trim Servo Tab
Pitch Control System Push Rod
Pitch Trim Actuator Electric
Landing Gear
Landing Gear Type Tricycle
Retractable No
Retraction System None
Emergency Extension None
Ground Steering Rudder Pedals
Shock Absorbtion Main Gear Aluminum Spring
Shock Absorbtion Other Gear Mechanical Spring
Brake Type Hydraulic Actuated Brake Disc
Brake Controls Toe Brakes
Instrument Panel IFR non Glass
Flight Control Joystick
Number of Seats 2
Heating Engine Exhaust Shroud
Window Defrost Ducted Hot Air
Cooling Ducted Ram Air
Normal Climb Profile Speed (KIAS) 75
Maximum Climb Profile Speed (KIAS) 75
Number of Engines 1
Engine Manufacturer Continental
Engine Model IO-240-B
Engine Type Normally Aspirated Piston
Geared Direct Drive
Cooled Air Cooled
Fuel/Air Mechanism Fuel Injected
Number of Cylinders 4
Max HP 125
Starter System Electric Starter
Propeller Manufacturer Sensenich
Propeller Model W69EK7-63
Number of Blades 2
Minimum Diameter 5 ft 9 inch
Maximum Diameter 5 ft 9 inch
Propeller Type Fixed Pitch
Propeller Governor None
Fuel System
Fuel System Type Fuel Pump
Approved Fuel Type 1 100LL
Approved Fuel Type 2 100
Approved Fuel Type 3
Fuel Capacity (G) 24.5
Tank Type 1 Location Behind Passenger Compartment
Tank Type 1 Capacity (G) 24.5
Tank Type 2 Location
Tank Type 2 Capacity (G) 0
Usable Fuel (G) 24
Oil Capacity (Quarts) 6
Electrical System
Power Source Engine Driven Generator
Power Storage Battery
System Voltage 14
Alternator Amp 40
Battery Voltage 12
Battery Amp/Hour 20
Maximum T/O Weight (lbs) 1653
Maximum LDG Weight (lbs) 1653
Standard Empty Weight (lbs) 1153
Useful Load (lbs) 500
Station 1 Baggage Location Aft Portion of Flight Deck
Max Weight Station 1 (lbs) 44
Station 2 Baggage Location
Max Weight Station 2(lbs) 0
Station 3 Baggage Location
Max Weight Station 3(lbs) 0
Wing Loading (lbs/sq.ft) 13.21
Vne (KCAS) 164
Vno (KCAS) 118
Va(Max Gross) (KCAS) 106


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