DA62 Product Presentation 2018 20122017 (1) Copy...DA62 Product Presentation_2018_20122017 (1)...

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DIAMOND DA62Product Presentation / Twin Engine / up to 7 seats

Last Update: December 2017, DAI-A



OVERVIEW

Avionics & Features

Saftey Concept

Fleet Concept & DA42 Worldwide

Composite Material & Maintenance

Aircraft Characteristics & Systems



DA62 CHARACTERISTICS



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



TARGET GROUPS

• Leisure Flying(private flying, travelling, etc.)

• Air-Taxi Flights(island hopping,

corporate aircraft, etc.)

• Flight Training



DIMENSIONS



KEY PERFORMANCE DATA

• 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



MAXIMUM RANGE FL140

*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.



MAXIMUM ENDURANCE

*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.



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

ENDURANCE AND RANGE



One Engine Inoperative Climb Rate, ft/min

Press. Alt. 1,999 kg 2,300 kg

SL 294 1632,000 277 1464,000 259 1286,000 241 1108,000 222 88

10,000 199 6512,000 175 4114,000 127 -516,000 69 -6118,000 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.

EXPERIENCE TRUE TWIN BENEFIT



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



DA62 AVIONICS & FEATURES



Diamond’s DA62 Standard equipped version includes:

• Glass Cockpit Garmin G1000Nxi(integrated COM, NAV, ILS)

• Automatic Flight Control System GarminGFC700

• 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

Optional features for the DA62 are: (PENDING)

AVIONICS & OPTIONAL FEATURES



AUTOPILOT GFC700

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 ofSIDs/STARs, SBAS, P-RNAV Operation and coupled procedures

• Over speed protection in VS mode



• 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.

GARMIN ESP



• Shows Jeppesen Airport Terminal charts in MFD

GARMIN CHARTVIEW



• Software add-on shows 3D Terrain in PFD

• Also shows obstacles, traffic, airports,

runways, flightpath, etc.

GARMIN SYNTHTETIC VISION



L-3WX500 STORMSCOPE

• Adds Lightning Strike Indication to Garmin G1000 NXi



GARMIN GWX70 WEATHER RADAR

• 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



TRAFFIC ADVISORY SYSTEM

• 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



GSR 56 SATELLITE TRANSCEIVER

The GSR 56 Iridium Transceiver providesan airborne low speed data link,on-demand satellite weather, IridiumSatellite Telephone service, and ShortMessage Service (SMS).

The telephone is available to the flightcrew through the audio panel andheadsets. A subscriber account must beestablished prior to using the IridiumSatellite System.



DA62 SYSTEMS



• 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)

AUSTRO ENGINE AE330



AUSTRO ENGINE AE330

Coolant Cooler

Turbo Charger

Heat Exchanger

High Pressure Pump



AUSTRO ENGINE AE330Gearbox

Oil Tank

Fuel Cooler

Alternator



• FADEC (Full Authority Digital Engine Control)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)

Easy handling because• NO Manual Leaning• NO Manual Priming• NO Manual Propeller

ControlXA

XP

XB

EECU

ECU Test Single Lever Power Control

Wizard Software Program

DUAL DIGITAL ENGINE CONTROL



• 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

ADVANTAGES OFLIQUID-COOLED SYSTEMS



• 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

AE330 TEMPERATURE LIMITATIONS



MT-PROPELLER

• Type: MT Propeller MTV-6-R-C-F/CF 190-80

• German Manufacturer: Mühlbauer / MT Propeller

• Wood-Composite blades with fiber-reinforced plasticcoating 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



• 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

RETRACTABLE LANDING GEAR SYSTEM



• 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

ICE PROTECTION I



• 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

ICE PROTECTION II

Symbol photos



Numberof users 10,000 ft 15,000 ft 18,000 ft

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

Oxygen cylinder

Oxygen outlets

Oxygen availability (hrs) depending on altitude and number of users, when using “oxysaver” cannula:

OXYGEN SYSTEM



• 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

CANOPY & PAX DOORS



• 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

SEATS I



SEATS II



LUGGAGE COMPARTMENT

• Front luggage compartment – up to 60 kg (30 LH + 30 RH)• Rear luggage compartment – up to 120 kg (5 seater config.)

30 kg

30 kg

6 kg

6 kg 68 kgBelow the barrier

40 kgAbove the barrier



VENTILATION SYSTEM

• Air intake under the right wing provide sufficient RAM Air for ventilation



• 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

AIR CONDITION



Short BaggageCompartment

RACC

RACC CompartmentVentilation

Cold Air Duct w/ 2 Nozzles f. Pax aft

Head-Up Unit w/+ Nozzle f. Pilot

+ Nozzle f. Copilot+ Map Light w/ switch

2 O2 Connectors (optional)

Hot Air Outlet (at bottom of A/C)

AIR CONDITION



• 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

FUEL SYSTEM



ELECTRICAL SYSTEM

• 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



3 mooring points4 refueling pointsTow bar

GROUND HANDLING

Aux tank ref. port Oil filling port Tail fin mooring point



AIRCRAFT COMPOSITE STRUCTURE



Diamond Aircraft has extensive experience (over 25 years) in composite manufacturing, including design andproduction 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 theAirbus A380 and Boeing 787 Dreamliner as well asFormula 1 cars

COMPOSITE MATERIAL



Advantages of Composite Materials

• Light weight with the same strength compared to traditional metal structure

• Perfect aerodynamic shape

• Low drag (no rivets)

• Unlimited structure life length(first Major Structural Inspection after 6,000 hrs)

• High reparability

• No corrosion

Diamond Structure

• Computer aided design

• Whole composite structure

• Fail-safe wing structure (dual spar design)

ADVANTAGES COMPOSITE



High reparability compared to traditional metal structure

Please watch this video on Diamond’s Youtube Channel:

https://www.youtube.com/watch?v=4ps0uUuETlQ&list=PLvn7gmFeFtCr6yhBEsgROu1H1tTV_DkZ6

COMPOSITE REPAIR



DA62 SAFETY



Aluminium tank vs. wet wing

DIAMOND SAFETY CONCEPT

Advanced avionics

Advantage of being „young“! (Certification requirements have increased significantly in the past, older competition wouldn’t make it today)

Damage tolerant airframe



• Crash elements under the seat

• 26g crash test

• 10g flight tolerance

• Monocoque (like Formula 1 cars)

DAMAGE TOLERANT AIRFRAME



• Aluminium tank system instead ofwet wing concept

• The dual spar design and aluminum fuelcells protect the fuel in the wing(no fire after a crash)

• Diamond uses TSO Stainless Steel braidedfuel lines throughout the airframe, not just forward of the firewall

FUEL PROTECTION SYSTEM



One picture worth 1,000 words …

SAFETY CONCEPT EXAMPLE



Source: Aviation Consumer (2012)

SAFETY RECORD IN FIGURES



DA62 MAINTENANCE



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 ManualSee here: http://support.diamond-air.at/da62_amm_bas.html

MAINTENANCE INTERVALLS



“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

DA62 SUMMARY & KEY DATA



WHY DIAMOND?

Innovative Design Concept Economic Jet-A1 Engine

Low Operating CostsGreat Flying Experience



Innovative Design Concept

• Industry leading safety record (lowest accident and injury rates)

• Modern glass cockpit (G1000 NXi) combined with composite material andJet-A1 engine

• Ultra modern and aerodynamiccomposite construction withpanoramic canopy and excellent visibility

WHY DIAMOND?



WHY DIAMOND?

Economic Jet-A1 Engine

• Huge fuel savings(Jet-A1 is cheaper than AvGas)

• More than 30% less fuel consumptioncompared to Avgas engines

• Environmentally friendly(compared to AvGas)

• Jet-A1 engines are quietand barely vibrate



WHY DIAMOND?

Low Operating Costs

• Highly economic design and engine capabilities

• Low fuel and maintenance cost result in high operating efficiency



WHY DIAMOND?

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



SINGLE POINT OF CONTACTDiamond 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.

FLEET CONCEPT



• For detailed information on the performance and limitations please refer to the DA62 AFM which is publishedon 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‘sWebsite. 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

Follow us #WeFlyDiamondAircraftfacebook.com/diamondaircraftind | instagram.com/diamondaircraftat | youtube.com/diamondaircraftmedia

CONTACT DETAILS



JOIN THE DIAMOND FAMILY TODAY

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