DIAMOND DA62 Product Presentation / Twin Engine / up to 7 seats
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 1 Last Update: December 2017, DAI-A OVERVIEW
Aircraft Characteristics & Systems
Avionics & Features
Composite Material & Maintenance
Saftey Concept
Fleet Concept & DA42 Worldwide
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 2 DA62 CHARACTERISTICS
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 3 AIRCRAFT CHARACTERISTICS
• Low wing, whole composite design • 5 to 7 seats, dual controls • Garmin G1000 NXi Glass Cockpit incl. GFC700 Autopilot • Twin Piston Engine burning Jet Fuel (2x 180 hp Austro Engine AE330-E4P) • Day/Night-VFR, IFR (Single Pilot IR certified), Flights into known or forecast icing conditions • Certification basis JAR-23 with additions acc. CRI A-01
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 4 TARGET GROUPS
• Leisure Flying (private flying, travelling, etc.)
• Air-Taxi Flights (island hopping, corporate aircraft, etc.)
• Flight Training
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• Max. Take-off Weight (MTOW) 2,300 kg / 5,071 lbs
• Typical Empty Weight (subject to optional equipment) 1,590 kg / 3,505 lbs
• Max. Cruise Speed (ISA, FL140, 95% Power) 352 km/h / 190 KTAS
• Rate of Climb, ISA, SL, Flaps up 5.2 m/s / 1,029 ft/min
• Max. Range 2,376 km / 1,283 nm
• Max. Operating Altitude 6,096 m / 20,000 ft
• Fuel Type Jet-A1 (or equiv.)
• Fuel Consumption at 60% for both engines 44.7 l / 11.8 USG/h
• Fuel capacity 327 l / 86.4 US gal
• Stall speed, 2,300 kg, Landing config. 69 / 64 KIAS
• Take-off roll (distance to 50 ft); ISA, SL, MTOW, Flaps T/O 480 (833) m / 1,575 (2,733) ft
• One engine inoperative climb ceiling ISA 3,962 m / 13,000 ft
• Max. demonstrated cross wind 46 km/h / 25 knots
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*Theoretical range, no fuel reserve, at no wind conditions. Sample Empty Weight 1,650kg, MTOW 2,300 kg, FL140, ISA conditions. Higher Flight Level will provide longer range. Not to be used for flight planning, refer to AFM.
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*Theoretical endurance, no fuel reserve. Sample Empty Weight 1,650 kg, MTOW 2,300 kg. Airspeed will depend on flight altitude. Not to be used for flight planning, refer to AFM.
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DA62 with 2,300 kg at FL160
• Optimal Cruise 75% / 180 kts, 14.8 USG/h / Economy Cruise 60% 160 kts, 11.8 USG/h
• Full Fuel 87 US gal • Max Endurance 5:52 h / 7:22 h • Max Range 1,056 nm / 1,179 nm
• Main Tanks only 50 US gal • Max Endurance 3:22 h / 4:13 h • Max Range 608 nm / 678 nm
*Max Endurance and Range theoretical examples up to zero fuel. For realistic IFR Operation consider alternate fuel, 45 min reserve, contingency fuel (3-5%) or any other required by national authority
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One Engine Inoperative Climb Rate, ft/min
Press. Alt. 1,999 kg 2,300 kg
SL 294 163 2,000 277 146 4,000 259 128 6,000 241 110 8,000 222 88 10,000 199 65 12,000 175 41 14,000 127 -5 16,000 69 -61 18,000 2 -124
*Not to be used for flight planning, refer to AFM. One Engine Inoperative Climb, ISA conditions, Power: feathered/95%, gear retracted, flaps up, Vyse KIAS.
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 11 RANGE MAP (acc. to power settings) FL140, ISA, without fuel reserve
In order to calculate the range from your city/country please visit:
http://www.diamond-air.at/twin-engine- aircraft/da62.html
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www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 13 AVIONICS & OPTIONAL FEATURES
Diamond’s DA62 Standard equipped Optional features for the DA62 are: version includes: (PENDING)
• Glass Cockpit Garmin G1000Nxi (integrated COM, NAV, ILS) • Automatic Flight Control System Garmin GFC700 • Adjustable Backrests for Pilot & Co-Pilot Seat • Electrically Adjustable Rudder Pedals • Long Range Fuel Tank (326 l / 86 US gal) • Garmin ESP (electronic stability & protection) • Sun glare shields and canopy lining • Landing and taxi lights (Xenon) & Position and strobe lights with LED technology
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Digital AFCS fully integrated within G1000 architecture
Main Operating Functions: • Flight Director (FD) • Autopilot (AP) • Manual Electric Trim (MET) • Yaw Damper
Highlights: • Flight Level Change Mode (Indicated Airspeed) • Vertical Navigation Mode • Full IFR Capabilities – automatic conduction of SIDs/STARs, SBAS, P-RNAV Operation and coupled procedures • Over speed protection in VS mode
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• Provides automatic control inputs to discourage operation outside of safe envelope.
• Engages when any of Pitch, Roll, Airspeed is beyond the normal flight parameters.
• Can be interrupted by the pilot (pressing and holding AP Disconnect button / pressing and holding CWS Button)
• Can be disabled or enabled in AUX-SYSTEM SETUP 2 page in G1000 NXi
• Autopilot Underspeed Protection* (USP): • in non-altitude critical mode (LVL, PIT, FLC, VS, VNV) – pitch down to maintain 90 KIAS, aural AIRSPEED alert sounds once • in altitude critical mode (ALT, GS, GP, GA) and Stall Warning active > 1 sec – maintains wings level and pitch down to eliminate Stall Warning +2 KIAS. Aural AIRSPEED alert sounds every 5 sec.
• Coupled GO-AROUND (pressing GA button will not disengage AP, but AP will attempt to capture and track FD Bars. In case of insufficient performance AP will enter USP mode, when stall warning sounds.
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• Shows Jeppesen Airport Terminal charts in MFD
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• Software add-on shows 3D Terrain in PFD
• Also shows obstacles, traffic, airports, runways, flightpath, etc.
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• Adds Lightning Strike Indication to Garmin G1000 NXi
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• GWX70 helps to detect and avoid adverse weather • Bringing full-colour storm cell tracking to the MFD • Accurate, easy-to-interpret, weather analysis in the cockpit • Weather Attenuated Color Highlight (WATCH™) can identify areas beyond the radar's capability that may contain even more hazardous areas of precipitation
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• The TAS605 system is designed to help in detection and collision avoidance of other aircraft.
• Shows other air traffic (with transponder) on
• Automatic traffic warnings
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The GSR 56 Iridium Transceiver provides an airborne low speed data link, on-demand satellite weather, Iridium Satellite Telephone service, and Short Message Service (SMS). The telephone is available to the flight crew through the audio panel and headsets. A subscriber account must be established prior to using the Iridium Satellite System.
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• 180 HP • Four cylinders, liquid-cooled, 1,991 ccm • Common-rail direct injection • Reduction gear 1:1,69 • Dual channel digital engine control (EECU) • Turbocharger • Torsional vibration damper • Max. power: (5 min time limit) 132 kW (180HP) at 2,300 RPM • Max continuous power: 126 kW (171HP) at 2,200 RPM • Current TBO 1,800 hrs (time between overhaul)
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High Pressure Pump Turbo Charger
Coolant Cooler Heat Exchanger
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Gearbox
Alternator
Oil Tank
Fuel Cooler
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• FADEC (Full Authority Digital Engine Control) Wizard Software Program state of art engine control unit • Single Lever Power Control (easy handling) • Fully automated Run-Up check • Dual ECU for redundancy • Sophisticated engine health monitoring (Wizard Software)
ECU Test Single Lever Power Control Easy handling because • NO Manual Leaning • NO Manual Priming
XB • NO Manual Propeller XP XA Control EECU
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• No shock cooling on cylinders • Cabin Heating system uses heat exchanger like in a car – no CO danger • Easy maintenance and operation: • No need to check Coolant Level in daily operation • Coolant Temperature is indicated on MFD in G1000 NXi • Coolant LVL Low annunciation is available in G1000 NXi
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• Fuel • Operation with Kerosene min. -30°C / -22 °F max. 60°C / 140°F
• Oil • Oil tempature (start) min. -30°C / -22 °F • Oil temperature max. 139°C / 282 °F
• Coolant • Coolant temp (start) min. -30°C / -22 °F • Coolant temp (full load) min. 60°C / 140°F • Coolant temp max. 100 °C / 212°F
• Gearbox • Gearbox Oil temp (start) min. -30°C / -22 °F • Gearbpx Oil temp (full load) min. 35°C / 95 °F max. 120°C / 248 °F
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• Type: MT Propeller MTV-6-R-C-F/CF 190-80
• German Manufacturer: Mühlbauer / MT Propeller
• Wood-Composite blades with fiber-reinforced plastic coating and metal leading edge protection
• Lowest weight whilst minimizing vibration
• Constant Speed function controlled by the ECU via an electromechanical governor
• Ice Protection System via TKS nozzles at hub (if TKS system is installed)
• Full-Feathering / Unfeathering Function
• Time between Overhaul: 2,400 flight hours
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• Hydraulically operated; electrically controlled • Extend gear at any speed up to VNE (convenience and “speed brake”) • Gear is held up by hydraulic pressure, in case of pressure loss or electrical failure gear is lowered down by gravity • Emergency Free Fall allows to manually extend the Gear • Gear warning – optional mute for training • Nose Wheel Steering • Low pressure tires – improved grass runway performance
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• Flight into known icing (FIKI) certified • TKS System, based on Freezing Point Depressant Fluid (FPD) • Uses spray nozzles (windshield and props) and porous skin panels on leading edges • Normal, High and MAX operating modes
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• 36 l usable capacity in the tank
• Deice fluid amount indicated in G1000 NXi
• Operating time capability:
• NORM Mode: ~ 3 hrs
• HIGH Mode: ~ 1.5 hrs
• MAX Mode: ~ 45 min
Symbol photos
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Oxygen cylinder
Oxygen outlets
Oxygen availability (hrs) depending on altitude and number of users, when using “oxysaver” cannula:
Number 10,000 ft 15,000 ft 18,000 ft of users
1 125.6 62.8 48.3 2 62.8 31.4 24.1 3 41.8 20.9 16.1 4 31.4 15.7 12.0 5 25.1 12.5 9.6 6 20.9 10.4 8.0 7 17.9 8.9 6.9
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• Two forward gull wing doors and the large cargo door that provides access to the rear seats and cargo compartment • Doors hydraulically lifted • Passenger door: “Child protection”/ Emergency Exit • Sun protection / Sun visors • Separate door warning for each door, displayed on PFD
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• Durable leather interior (available in different colors) • Integrated Key Pad (if option chosen) • Adjustable PIC/Co-PI seats • Electric adjustable rudder pedals (standard feature) • 3 points seat belts
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• Front luggage compartment – up to 60 kg (30 LH + 30 RH) • Rear luggage compartment – up to 120 kg (5 seater config.)
Above the barrier 40 kg 30 kg
6 kg
Below the barrier 6 kg 68 kg
30 kg
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• Air intake under the right wing provide sufficient RAM Air for ventilation
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• The air condition called “RACC” (re-circulating air cabin cooling) consists of a central unit (aft of baggage compartment), an additional alternator and an AUX power switch (center console) • APU can be used to precool airplane on ground • Weight of total installation of the air-condition is approx. 41 kg (incl. 2nd Generator) • Luggage compartment is reduced
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Cold Air Duct w/ Short Baggage 2 Nozzles f. Pax aft Compartment RACC
Head-Up Unit w/ + Nozzle f. Pilot + Nozzle f. Copilot + Map Light w/ switch RACC Compartment 2 O2 Connectors (optional) Ventilation Hot Air Outlet (at bottom of A/C)
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 41 FUEL SYSTEM
• Dry wing – separate aluminum tank – increased safety Two main tanks in the wings left and right 2 x 25 USG • Two AUX Tanks in Engine nacelles 2 x 18.2 USG • Usable fuel capacity 86.4 USG ~ 327 liter ~ 262 kg
• Electric low pressure fuel pumps (2 per engine for redundancy) • Cross Feed / Fuel Shut Off valve per engine • 4 fillers, two transfer pumps to transfer fuel from AUX tanks • 2 draining points under each wing
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• 28 V DC Electric System • 24 V / 13.6 Ampere Main Battery lead acid battery • 2 Alternators (LH and RH) +3rd Alternator for RACC ( if installed ) • ECU Backup Batteries • Standard 3 Pin AUX Power Connector In case of total electrical failure ECU Backup batteries will provide power to ECUs for at least 30 minutes.
Avionics Master
Electric Master
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Tow bar 4 refueling points 3 mooring points
Aux tank ref. port Oil filling port Tail fin mooring point
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www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 45 COMPOSITE MATERIAL
Diamond Aircraft has extensive experience (over 25 years) in composite manufacturing, including design and production of own composite equipment.
Advantages of composite materials :
• High strength related to weight, corrosion resistance, high impact strength, design flexibilty, durability.
• Composite materials are also used in major parts of the Airbus A380 and Boeing 787 Dreamliner as well as Formula 1 cars
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Advantages of Composite Materials Diamond Structure
• Light weight with the same strength • Computer aided design compared to traditional metal structure • Whole composite structure • Perfect aerodynamic shape • Fail-safe wing structure (dual spar • Low drag (no rivets) design) • Unlimited structure life length (first Major Structural Inspection after 6,000 hrs)
• High reparability
• No corrosion
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High reparability compared to traditional metal structure
Please watch this video on Diamond’s Youtube Channel: https://www.youtube.com/watch?v=4ps0uUuETlQ&list=PLvn7gmFeFtCr6yhBE sgROu1H1tTV_DkZ6
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 48 DA62 SAFETY
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 49 DIAMOND SAFETY CONCEPT
Damage tolerant airframe Advanced avionics
Advantage of being „young“! Aluminium tank vs. wet wing (Certification requirements have increased significantly in the past, older competition wouldn’t make it today)
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• Crash elements under the seat • 26g crash test • 10g flight tolerance • Monocoque (like Formula 1 cars)
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• Aluminium tank system instead of wet wing concept
• The dual spar design and aluminum fuel cells protect the fuel in the wing (no fire after a crash)
• Diamond uses TSO Stainless Steel braided fuel lines throughout the airframe, not just forward of the firewall
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One picture worth 1,000 words …
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 53 SAFETY RECORD IN FIGURES
Source: Aviation Consumer (2012)
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www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 55 MAINTENANCE INTERVALLS
Scheduled Maintenance: • 100 hrs • 200 hrs (Annual Inspection) • 1,000 hrs • 6,000 hrs Major Structural Inspection (MSI)
Unscheduled Maintenance: • Hard landings • Propeller strike • Engine fire • Lightning strike • Occurence of other malfunctions and damage
For more details plese refer to the Airplane Maintenance Manual See here: http://support.diamond-air.at/da62_amm_bas.html
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 56 DA62 SUMMARY & KEY DATA
“The DA62 is very easy to fly, even for a non-professional pilot like me. My flying experience includes mostly Robin DR-400 and a few hours in the DA42. For me, the DA62 is the ideal aircraft for both my business trips (IFR with a professional pilot) and family trips throughout Europe: fast, excellent range, good seating, very stable, fun to fly. I recommend highly.” François Goy, France
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 57 WHY DIAMOND?
Innovative Design Concept Economic Jet-A1 Engine
Great Flying Experience Low Operating Costs
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Innovative Design Concept
• Industry leading safety record (lowest accident and injury rates)
• Modern glass cockpit (G1000 NXi) combined with composite material and Jet-A1 engine
• Ultra modern and aerodynamic composite construction with panoramic canopy and excellent visibility
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Economic Jet-A1 Engine
• Huge fuel savings (Jet-A1 is cheaper than AvGas)
• More than 30% less fuel consumption compared to Avgas engines
• Environmentally friendly (compared to AvGas)
• Jet-A1 engines are quiet and barely vibrate
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Low Operating Costs
• Highly economic design and engine capabilities
• Low fuel and maintenance cost result in high operating efficiency
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Great Flying Experience
• Easy handling due to SINGLE LEVER CONTROL (Other manufacturers: 3 control levers/ fuel supply, Propeller, fuel and oil mix)
• A safe, smooth, quiet and fun to fly aircraft
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 62 FLEET CONCEPT
SINGLE POINT OF CONTACT Diamond supplies Flight Schools with a single-engine trainer (DA40 NG), a multi-engine trainer (DA42-VI) as well as a FNPT II (simulator). All products are equipped with the JET- A1 powered Austro Engine AE300 and modern Garmin G1000 (NXi) glass cockpit.
www.diamond-air.at AVIATION AS UNIQUE AS YOU ARE #WeFlyDiamondAircraft 63 CONTACT DETAILS
• For detailed information on the performance and limitations please refer to the DA62 AFM which is published on Diamond‘s Website. See here: http://support.diamond-air.at/da62_afm.html
• For detailed information on maintenance please refer to the DA62 AMM which is published on Diamond‘s Website. See here: http://support.diamond-air.at/da62_amm_bas.html
• For Diamond Aircraft Support please contact [email protected] • For Austro Engine Support [email protected] • For Sales please contact [email protected] • For Marketing please contact [email protected] • For Pilot Training please contact [email protected] • For Maintenance Training please contact [email protected] • For Spare Parts please contact [email protected] • Diamond Website: www.diamond-air.at
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