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DART Brochure

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DART Brochure DART SERIES THE NEXT LEVEL OF VERSATILITY FROM CONCEPT TO PRESENT general information The all-carbon-fiber DART Series, envisioned as an aerobatic (+7/- MAIDEN FLIGHT DART-450 4G) tandem trainer, features centre stick control, ejection seats, a 17 MAY 2016 five-blade MT propeller and a Garmin avionics system. ENGINE VARIANTS ▪ Turboprop engine AI-450 CP (450 SHP) manufactured by Motor Sich for DART-450 ▪ Turboprop engine GE H75-A (550 SHP) manufactured by General Electric for DART-550 KINDS OF OPERATION ▪ VFR (day and night) and IFR ▪ Take-off and landing on paved surfaces or grass surfaces APPLICATIONS Basic to advanced flight training, Aerobatic, Formation, Multi Role STRUCTURE All composite aircraft CFRP (Carbon Fiber Reinforced Polymer). MOCK UP DART-450 From the very beginning, DEC 2015 CERTIFICATION STANDARD Diamond Aircraft knew that the DART series will be something CS/FAR23 1) unmatched on the market and will eliminate old generation CATEGORY trainer from the market for a Aerobatic / Utility (Multi Role) very long period of time. KICK OFF DART-450 ROLL OUT DART-450 MAIDEN FLIGHT DART-550 MAY 2015 APRIL 2016 03 MAY 2018 1) Certification ongoing Page 3 DART FEATURES TANDEM SEAT, CENTRE STICK CONTROL, EJECTION SEATS, TOUCH SCREEN AVIONICS dart FEATURES HOTAS, NVIS CANOPY WITH SUPERIOR LARGEST SURROUND VIEW INTERNAL FUEL TANK CAPACITY IN TRAINER CLASS ENDURANCE: >5.5 HOURS 15’’ CAMERA HATCH FOR MULTI ROLE OPERATION DOUBLE SLOTTED FLAPS FOR MAXIMUM LIFT LOW STALL SPEED SHORT LANDING DISTANCES LEADING EDGE DE - ICE SYSTEM FULL COMPOSITE AIRFRAME ALLOWS FOR SUPERB HARD POINTS AERODYNAMIC DESIGN ROBUST LANDING GEAR FOR UNPAVED SURFACE OPERATION TWO STATIONS PER WING SIDE COMPOSITE 5 BLADE PROPELLER PROVEN HIGH SPEED WING POWERED BY FUEL & COST EFFICIENT TURBINE (WIND TUNNEL TESTED UP TO M0.65) Page 5 DART VARIANTS DART-450 DART-550 Turboprop engine AI-450 CP (450 SHP) manufactured by Motor Turboprop aerobatic engine GE H75-A (550 SHP) manufactured by Sich. General Electric. DART-450 KEY FACTS: DART-550 KEY FACTS: Load Factor Endurance Max. Take-off power Load Factor Endurance Max. Take-off power +7 / -4 5 hours + 495 SHP or 369 kW +7 / -4 5.5 hours + 550 SHP or 404 kW The DART-550 is the next massive push into being the only aircraft manufacturer in AEROBATIC UTILITY (MULTI ROLE) offering the full range for basic CONFIGURATION 1) CONFIGURATION 1) flight training, reaching its peak with the DART-550 aero- Load factor +7 / -4,0 Load factor +5 / -2,4 batic trainer. MTOM 2,080 kg / 4586 lbs MTOM 2,300 kg / 5071 lbs 1) Applies to the complete DART Series Page 7 COCKPIT & EJECTION SEATS AVIONICS Garmin G3000 dual glass cockpit: ▪ Touchscreen control ▪ Synthetic Vision Technology (SVT™) ▪ 14.1-inch diagonal WXGA high-resolution cockpit displays ▪ 5.7-inch high-resolution GTC 585 ▪ Extended 16:9 width-to-height ratio ▪ Fully integrated 3-axis autopilot ▪ HUD - Head Up Display ▪ FMS – Flight Management System Avionic system can be extended on customer demand. COCKPIT ▪ Superior surround view canopy ▪ Real and fully independent tandem cockpit concept Having the opportunity to ▪ most reliable MK 16 installation 0/0 Seat EJECTION SEAT include state of the art glass Martin Baker MK16 Lightweight Escape System: ▪ OBOGS – On-board Oxygen Generating System cockpit technology, world’s JPATS (Joint Primary Aircraft Training System) ▪ Air Condition ▪ number one ejection seat multi variate body size cases 2 to 7 ▪ NVG Capable brand, using General Electric Minimal maintenance overhead ▪ turbine know-how - embedded 65 kg mass per seat + 8 kg ground ▪ in a full carbon fiber airframe survival equipment will make it very difficult for ▪ Electric height adjustment system DART’s competition when ▪ Speed range 0 KIAS – 370 KIAS performance and commercial ▪ Altitude 0 ft – 50,000 ft arguments become a critical ▪ Pilot Mass: 62.3 kg - 123 kg decision making factor. Alternative: ▪ Diamond standard seat (Non-ejection seat) ▪ Zwezda KC-2012, pneumatic ejection seat Page 9 AEROBATIC TRAINING ADVANCED TRAINING ONE AIRPLANE - TWO CONFIGURATIONS Powered by the General Electric GE H75-A turboprop engine with ▪ With partial fuel (300 l) the airplane can be operated within the 550 SHP or the Motor Sich AI-450 SR turboprop engine with 450 aerobatic category hp. This engine variants combined with operating simplicity makes ▪ With full fuel (760 l) the airplane can be operated within the utility it the ideal platform for learning the first steps of flying all the way (mulit role) category to pushing the envelope at +7g / -4g during the aerobatic training phase. The DART aerobatic trainer will be available in different vari- ants differing in engine power ratings, seat configuration and/ or avionics options for diverse customer needs. Page 11 MULTI ROLE APPLICATION EO/IR Camera für Reconnaissance & Border Patrol ADDITIONAL ATTACHMENT POINTS ▪ Fuselage: Integrated sensor hatch for EO/IR gimbals with optional camera lift ▪ Wing: Two mounting stations per wing side Wing mounting stations for external sensors or fuel tanks Page 13 THE NEXT LEVEL OF VERSATILITY DART-450 PRELIMINARY FACTS AND SPECIFICATIONS Power plant Dimensions / mass / loading Aerobatic Utility (Multi Role) Engine Motor Sich AI-450 CP turboprop engine Configuration Configuration Configuration MT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering Propeller and reverse functionality Load factors +7 / -4 +5 / -2.4 Maneuvers Aerobatic Cat. Utility Cat. Fuel grades Jet A, Jet A1, RT, TS1 and T1, No.3 Jet Fuel 2,080 kg / 2,300 kg / MTOM 4,586 lbs 5,071 lbs 1,450 kg / 1,450 kg / Basic empty mass Calculated Performance 3,197 lbs 3,197 lbs Max. take off power 495 SHP 369 kW 240 kg or 300 ltr / 662 kg or 760 ltr / Total fuel capacity 529 lbs or 1,459 lbs or Max. continuous power (ISA, SL) 400 SHP 298 kW 79 US gal 201 US gal Seats 2 2 Max. operating speed (Vmo) 490 km/h TAS 265 KTAS Typical cruise speed 352 km/h TAS 190 KTAS (10.000ft, 75%, 97 kg/h) 3.43 m / Endurance 5 hours + 5 hours + 11 ft 3 in Max. rate of climb 8.9 m/s 1,750 ft/min 11.79 m / 38 ft 8 in 9.75 m / 34 ft Service ceilling 7,000 m 23,000 ft Take-off distance (ISA, SL) ≤ 600 m ≤ 1,970 ft Landing distance (ISA, SL) ≤ 400 m ≤ 1,300 ft The above quoted data are preliminary specifications and may change without notice. Page 17 DART-550 PRELIMINARY FACTS AND SPECIFICATIONS Power plant Dimensions / mass / loading Aerobatic Utility (Multi Role) Engine General Electric GE H75-A turboprop engine Configuration Configuration Configuration MT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering Propeller and reverse functionality Load factors +7 / -4 +5 / -2.4 Maneuvers Aerobatic Cat. Utility Cat. Fuel grades Jet A, Jet A1, RT, TS1 and T1, No.3 Jet Fuel 2,080 kg / 2,300 kg / MTOM 4,586 lbs 5,071 lbs 1,550 kg / 1,550 kg / Basic empty mass Calculated Performance 3,417 lbs 3,417 lbs Max. take off power 550 SHP 404 kW 240 kg or 300 ltr / 608 kg or 760 ltr / Total fuel capacity 529 lbs or 1,340 lbs or Max. continuous power (ISA, SL) 550 SHP 404 kW 79 US gal 201 US gal Seats 2 2 Max. operating speed (Vmo) 490 km/h TAS 265 KTAS Max level cruise speed (V ) H 404 km/h TAS 218 KTAS (10.000ft) 3.43 m / Endurance 5.5 hours + 5.5 hours + 11 ft 3 in Max. rate of climb 10.7 m/s 2,100 ft/min 11.79 m / 38 ft 8 in 9.75 m / 34 ft Service ceilling 7,600 m 25,000 ft Take-off distance (ISA, SL) ≤ 600 m ≤ 1,970 ft Landing distance (ISA, SL) ≤ 400 m ≤ 1,300 ft The above quoted data are preliminary specifications and may change without notice. Page 19 AVIATION AS UNIQUE AS YOU ARE NORTH & SOUTH AMERICA, AUSTRALIA, NEW ZEALAND: EUROPE, MIDDLE EAST, AFRICA, RUSSIA/CIS, ASIA (HQ): CHINA: 1560 Crumlin Sideroad, London, ON, Canada, N5V1S2 N. A. Otto-Strasse 5, 2700 Wiener Neustadt, Austria Wanfeng Airpark, Dashiju Town Phone: +1 800 268 4001, [email protected] Phone: +43 2622 26700, [email protected] Xinchang County, Zhejiang Province, P. R. China www.diamondaircraft.com www.facebook.com/diamondaircraftind www.instagram.com/diamondaircraftind www.youtube.com/diamondaircraftmedia #WeFlyDiamondAircraft All specifications, weights, representations, colors, equipment, use of materials and model references provided herein are for purely illustrative purposes and legally non-binding, subject to alterations and not warranted or guaranteed to be true or accurate. Actual useful load will vary depending on options installed on the aircraft. Any and all information given in this brochure cannot exempt the person operating the aircraft to use actual data for flight planning. The aircraft and/or product, and the chosen optional equipment (if any) shall meet exclusively the characteristics and specifications as defined and agreed in the written agreement with Diamond Aircraft Group. Referenced Diamond Aircraft trademarks are owned by Diamond Aircraft Industries GmbH or its subsidiaries. All other brands, product names, company names, trademarks and service marks are the properties of their respective owners. All rights reserved. ©2020, Diamond Aircraft Industries GmbH. For additional information on Diamond Aircraft and its products please visit www.diamondaircraft.com. 10/2020 S_00005E.
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