10-Eclipse - ELA Aviación S.L. | · • Secondary electrical fuel pump for the Rotax 912 ULS...

2
ELA AVIACIÓN S.L. Pol. Ind. El Blanquillo M7-P26 14290 Fuente Obejuna. Córdoba. España. Teléf. +34 957 58 51 75 ELA Aviacion Oficial @ELAaviacion www.elaaviacion.com [email protected] 10-Eclipse The ELA 10-Eclipse is the most advanced, efficient and refined gyroplane model ever created by ELA Aviacion. It is the latest model of our new generation of innovative gyroplanes, with high technology, along with the latest design techniques combined with the most delicate craftsmanship. The 10-Eclipse is a two seater in tandem configuration with closed cockpit, convertible, with a vanguard design and a “Premium” finish as standard. The 10-Eclipse is the most capable gyroplane of our history, with an endurance of 6 flight hours and a luggage capacity of 65 liters (17 gallons). Designed for travelling, its high performance and sophisticated interior finish will make your dreams come true. Standard equipment • Airframe made from AISI 4130 chromoly steel. • Monocoque fuselage, tail unit and fairings made from carbon fiber. • Rotax 912 ULS (100 hp) or 914 UL Turbo (115 hp) engine. • Rotor diameter of 8,5m (28ft). • Carbon fiber propeller. • Windscreen for summer flying. • Powerful pre-rotator system. • Pneumatic trim/rotor brake. • Hydraulic wheel brakes with parking system. • 87 l (23 gal) fuel tank with level sensor. • High quality upholstered seats. • Wide color chart: plain, metallic y matte colors. • Cabin heating. • LED landing lights. • Strobe light in mast. • 12 v or USB power plug. • Oil thermostat. • Twin muffler system. • Slipping clutch in gear box. • High performance starter for the Rotax 912 ULS engine. • Secondary electrical fuel pump for the Rotax 912 ULS engine. Standard instruments • Digital airpeed ind. • Digital altimeter / vertical speed ind. • Vertical card compass. • Rotor trim pressure ind. • Digital multi-function “Kanardia EMSIS” instrument, to control all engine parameters, rotor tachometer, fuel consumption, etc… • Radio VHF TQ Avionics KRT2-S. • 12 v power plug or USB in front seat. Rotax 912 ULS Rotax 914 UL Turbo Empty weight (Standard) 283 Kg (625 lb) 293 Kg (650 lb) Max. take-off weight** 500 Kg (1100 lb) 530 Kg (1170 lb) Useful load 217 Kg (475 lb) 237 Kg (520 lb) Velocity never exceed (VNE) 190 Km/h (120 mph) Cruise speed 150 - 165 Km/h (95-105 mph) Fuel capacity 87 litres (23 gal) Endurance 4,5 - 7 hours Fuel consumption 13 - 20 litres/h (3 – 5,5 gal/h) Range 640 Km (400 mi) Take-off distance 120 metres (400 ft) 100 metres (330 ft) Landing distance 0 - 20 metres (0-65 ft) * Max. take-off weight limited in some European countries to 450 kg (990 lb). ** Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level). Technical data* *Subject to alterations with regard to technical specifications and contents.

Transcript of 10-Eclipse - ELA Aviación S.L. | · • Secondary electrical fuel pump for the Rotax 912 ULS...

Page 1: 10-Eclipse - ELA Aviación S.L. | · • Secondary electrical fuel pump for the Rotax 912 ULS engine. Standard instruments • Digital airpeed ind. ... • Digital Altimeter and Vertical

ELA AVIACIÓN S.L.Pol. Ind. El Blanquillo M7-P26

14290 Fuente Obejuna. Córdoba. España.Teléf. +34 957 58 51 75

ELA Aviacion Oficial @ELAaviacion

www.elaaviacion.com [email protected]

10-EclipseThe ELA 10-Eclipse is the most advanced, efficient and refined gyroplane model ever created by ELA Aviacion. It is the latest model of our new generation of innovative gyroplanes, with high technology, along with the latest design techniques combined with the most delicate craftsmanship.

The 10-Eclipse is a two seater in tandem configuration with closed cockpit, convertible, with a vanguard design and a “Premium” finish as standard. The 10-Eclipse is the most capable gyroplane of our history, with an endurance of 6 flight hours and a luggage capacity of 65 liters (17 gallons). Designed for travelling, its high performance and sophisticated interior finish will make your dreams come true.

Standard equipment•AirframemadefromAISI4130chromolysteel.

•Monocoquefuselage,tailunitandfairingsmadefromcarbonfiber.

•Rotax912ULS(100hp)or914ULTurbo(115hp)engine.

•Rotordiameterof8,5m(28ft).•Carbonfiberpropeller.•Windscreenforsummerflying.•Powerfulpre-rotatorsystem.•Pneumatictrim/rotorbrake.•Hydraulicwheelbrakeswithparkingsystem.

•87l(23gal)fueltankwithlevelsensor.

•Highqualityupholsteredseats.•Widecolorchart:plain,metallicymattecolors.

•Cabinheating.•LEDlandinglights.•Strobelightinmast.•12vorUSBpowerplug.•Oilthermostat.•Twinmufflersystem.•Slippingclutchingearbox.•HighperformancestarterfortheRotax912ULSengine.

•SecondaryelectricalfuelpumpfortheRotax912ULSengine.

Standard instruments•Digitalairpeedind.•Digitalaltimeter/verticalspeedind.

•Verticalcardcompass.•Rotortrimpressureind.•Digitalmulti-function“KanardiaEMSIS”instrument,tocontrol

allengineparameters,rotortachometer,fuelconsumption,etc…

•RadioVHFTQAvionicsKRT2-S.•12vpowerplugorUSBinfrontseat.

Rotax 912 ULS Rotax 914 UL TurboEmpty weight (Standard) 283 Kg (625 lb) 293 Kg (650 lb)Max. take-off weight** 500 Kg (1100 lb) 530 Kg (1170 lb)Useful load 217 Kg (475 lb) 237 Kg (520 lb)Velocity never exceed (VNE)

190 Km/h (120 mph)

Cruise speed 150 - 165 Km/h (95-105 mph)Fuel capacity 87 litres (23 gal)Endurance 4,5 - 7 hoursFuel consumption 13 - 20 litres/h (3 – 5,5 gal/h)Range 640 Km (400 mi)Take-off distance 120 metres (400 ft) 100 metres (330 ft)Landing distance 0 - 20 metres (0-65 ft)

* Max. take-off weight limited in some European countries to 450 kg (990 lb).

** Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level).

Technical data*

*Subject to alterations with regard to technical specifications and contents.

Page 2: 10-Eclipse - ELA Aviación S.L. | · • Secondary electrical fuel pump for the Rotax 912 ULS engine. Standard instruments • Digital airpeed ind. ... • Digital Altimeter and Vertical

07-AgroThe ELA 07-AGRO has been designed for professional use as an aerial crop duster. It can apply liquids at low and ultra-low volume. In addition, since it has the inherent maneuverability of the rest of the 07 series of gyroplanes, the 07-AGRO is well suited as a two-seater for training.

The fumigation boom has a 8,25 metres (27ft) wingspan, resulting in a swath width of 10 metres (33 ft) plus overlap. The boom can be easily and rapidly folded, allowing for the gyroplane to fit into minimal hangar space. It can also be flown for travelling with the boom in its folded position, greatly reducing drag. The gyroplane is fitted with a GPS to fly fumigation-specific tracks and has a 120 l (31 gal) capacity tank for spraying product.

Standard equipment

Standard instruments

Empty weight (standard) 305 Kg (675 lb)Max. take-off weight 500 Kg (1100 lb)Useful load 195 Kg (425 lb)Velocity never exceed (VNE) 160 Km/h (100 mph)Cruise speed (booms folded) 130 Km/h (80 mph)Fuel capacity 75 litres (20 gal)Endurance 3,5 – 4,5 hoursFuel consumption 15 - 20 litres/h (4 – 5,5 gal/h)Range 400 Km (250 mi)Take-off distance 180 metres (600 ft)Landing distance 0 - 20 metres (0-65 ft)

*Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level).

ADVANTAGES OF THE ELA-07 AGRO•Electricalfumigationsystem,allowingcalibrationwithoutenginepower.•“Chirurgical”cutattheendofarun(thereisnowake).•Thegyroplanedoesnotproducevorticesnordistortions.•Electricdrivendiaphragmpumpswithanominalpressureof60psi(4bar).•Pressureregulatorvalvecontrolledbythepilot.•Swathwidthof10metres(33ft)plusoverlap.

•Stainlesssteelframe.•Carbonfibercockpitandtailunit.•Rotax914ULTurbo(115hp)engine.

•Rotordiameterof8,5m(28ft).•Carbonfiberpropeller.•Largefrontwindscreen.•Powerfulpneumaticpre-rotator.•Pneumatictrim/rotorbrake.•Rolltrim.•Hydraulicwheelbrakeswithparkingsystem.

•75l(20gal)fueltankwithlevelgauge.

•Highqualityupholsteredseats.•Frontseatwithpocket.•Landinglight.•12vpowerplug.•Oilthermostat.•Stainlesssteelexhaustsystem.•120l(31gal)producttank.•Sprayingsystemwithboomsof8,25m(27ft).

•Pressureregulatorvalveforthesprayingsystem.

•DigitalAirspeedindicator.

•DigitalAltimeterandVerticalspeedindicator.

•Verticalcardcompass.•Rotortrimpressureind.

•Rotortachometer.•Enginetachometer.•Cylinderheadtemperatureind.

•Oilpressureind.•Fuelpressureind.

•Fuellevelind.•Hour-count.•Pressuregaugeforthesprayingsystem.

•GPSEZGuide250.

Technical data*

07-CougarThe 07-Cougar is born from the solid and tested base of the 07S. It is our most sporty, dynamic and configurable model, from the basic version. We have created a gyroplane that provides a true sensation of freedom under its controls. The 07-Cougar is noted for its exceptional performance, agility, maneuverability, along with a powerful pre-rotator.

From the standard model, you can go further and configure your 07-Cougar to create a personalized one that can compete with our “top-models”.

Thanks to its high performance, the ELA 07-Cougar was able to beat the FAI World distance and speed records in the category of light gyroplane.

Standard equipment

Standard instruments

•Stainlesssteelframe.•Carbonfibercockpitandtailunit.•Rotax912ULS(100hp)or914ULTurbo(115hp)engine.

•Rotordiameterof8,5m(28ft).•Carbonfiberpropeller.•Largefrontwindscreen.•Frontseatwithpocket(standard).

•Powerfulpneumaticpre-rotator.•Pneumatictrim/rotorbrake.•Rolltrim.•Hydraulicwheelbrakeswithparkingsystem.

•75l(20gal)fueltankwithlevelsensor.

•Highqualityupholsteredseats.•Oilthermostat.•Stainlesssteelexhaustsystem.•SlippingclutchfortheRotax912ULSengine.

•HighperformancestarterfortheRotax912ULSengine.

•SecondaryelectricalfuelpumpfortheRotax912ULSengine.

•CarburettorheaterfortheRotax912ULSengine.

•DigitalAirspeedindicator.

•DigitalAltimeterandVerticalspeedindicator.

•Verticalcardcompass.

•Rotortrimpressureind.•Rotortachometer.•Enginetachometer.•Cylinderheadtemperatureind.

•Oilpressureind.•Fuelpressureind.•Fuellevelind.•Hour-count.

Rotax 912 ULS(100hp)

Rotax 914 UL Turbo (115 hp)

Empty weight (standard) 260 Kg (575 lb) 265 Kg (585 lb)Max. take-off weight** 500 Kg (1100 lb) 500 Kg (1100 lb)Useful load 240 Kg (530 lb) 235 Kg (520 lb)Velocity never exceed (VNE)

160 Km/h (100 mph)

Cruise speed 120 - 145 Km/h (75 - 90 mph)Fuel capacity 75 litres (20 gal)Endurance 3,5 – 4,5 hoursFuel consumption 15 - 20 litres/h (4 – 5,5 gal/h)Range 400 Km (250 mi)Take-off distance 120 metres (400 ft) 100 metres (330 ft)Landing distance 0 - 20 metres (0-65 ft)

*Max. take-off weight limited in European Type Certificates to 450 kg (990 lb).

**Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level).

Technical data*

Standard equipment

Standard instruments•DigitalAirspeedindicator.

•DigitalAltimeterandVerticalspeedindicator.

•Verticalcardcompass.

•Digitalmulti-functionKanardiaEmsistocontrolallengineparameters.

•Rotortrim/brakepressure.

•Fuellevelindicator.

Rotax 914 UL Turbo(115hp)

Empty weight (standard) 275 Kg (585 lb)Max. take-off weight** 500 Kg (1100 lb)Useful load 225 Kg (515 lb)Velocity never exceed (VNE)

160 Km/h (100 mph)

Cruise speed 120 - 145 Km/h (75 - 90 mph)Fuel capacity 75 litres (20 gal)Endurance 3,5 – 4,5 hoursFuel consumption 15 - 20 litres/h (4 – 5,5 gal/h)Range 400 Km (250 mi)Take-off distance 100 metres (330 ft)Landing distance 0 - 20 metres (0-65 ft)

*Max. take-off weight limited in European Type Certificates to 450 kg (990 lb).

** Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level).

Technical data*

•Rotax914ULTurboof115hp.•Aluminumrotorblades.•Drop-downentrydoorforfwdseat.•Largeforwardwindscreen.•Foldablewindscreenforrearseat.•Key-lockableglove/accessoriescompartment.

•100litersofstoragecapacity.•75litersfueltankcapacity.•Four-pointharnessinbothseats.•Powerfulpneumaticpre-rotator.•Carbonfiberpropeller.•Wheelpants.•Landinggearwings/fairings.•Electro-pneumaticrotorbrakeandpitchtrim.

•Mechanicalrolltrim.•Hydraulicwheelbrakeswith

parkingsystem.•Gyrocolourchoice.•Highqualityseatcovers.•Frontseatwithpocket.•Landinglight.•USBor12Vpowerplug.•Oilthermostat.

09-JuniorEasy, affordable and with all the reliability of ELA.

With an aggressive and functional design, the 09-Junior gives you that pure direct experience of authentic flight, with nothing between you and the delight of soaring through the air. Moreover, a gyroplane which is light, agile and most of all fun.

The 09-Junior is a “1+1” design, which enables you to enjoy its great maneuverability, while also being able to fly together.

Ultra-short take offs, agility, and most of all extended fun!

Standard equipment

Standard instruments

•Stainlesssteelframe.•Rotax912ULS(100hp)engine.

•Rotordiameterof8,25m(27ft).•Carbonfiberpropeller.•Powerfulpre-rotator.•Pneumatictrim/rotorbrake.•Rolltrim.•Hydraulicwheelbrakeswithparkingsystem.

•45l(12gal)fueltank.•Oilthermostat.•Stainlesssteelexhaustsystem.•SlippingclutchfortheRotax912ULSengine.

•Highperformancestarter.•Secondaryelectricalfuelpump.•Carburettorheater.

•DigitalAirspeedindicator.

•DigitalAltimeterandVerticalspeedindicator.

•Verticalcardcompass.•Rotortrim/brakepressureind.

•Rotortachometer.•Enginetachometer.

•Cylinderheadtemperatureind.

•Oilpressureind.•Fuelpressureind.•Hour-count.

Empty weight (standard) 245 Kg (540 lb)Max. take-off weight 450 Kg (990 lb)

Useful load 205 Kg (450 lb)Velocity never exceed (VNE) 150 Km/h (95 mph)Cruise speed 100 - 120 Km/h (60 - 75 mph)Fuel capacity 45 litres (12 gal)Endurance 2 – 2,5 hoursFuel consumption 15 - 20 litres/h (4 – 5,5 gal/h)Range 250 Km (150 mi)Take-off distance 100 metres (330 ft)Landing distance 0 - 20 metres (0-65 ft)

*Parameters determined during the flight test campaign in ISA conditions (15ºC and sea level).

Technical data*

07-ScorpionThe value of the “S”.

A popular and performing design, more than 10 years in the market. This two-seater, semi-enclosed gyroplane has been “the reference” of the last decade. A design icon, dynamic, with brilliant performance and lines that appeal to the world. The sales record endorses its attractive features. Now much better in a new versión 07-Scorpion. It is equipped with a side door for easy access to the cockpit, a storage compartment of 100 liters, a rear instrument panel integrated into the fairing for instruction activities (optional) and an attractive tail unit design that ensures great stability and control.

One new feature of the ELA 07-Scorpion is, the higher distance between the front wheel and the landing gear, offering great stability. But if there is something that is really impressive it is the spacious cockpit with comfortable enveloping seats for both pilot and co-pilot.

The new ELA 07-Scorpion is equipped with aluminium rotor blades. Our selection of individual blades, precise fitting and adjustment systems ensure a very low level of vibration and unparalleled aerodynamics.