DA62 THE ULTIMATE FLYING MACHINE
Diamond DA62 · Normal Procedures
Overview
This document serves as a comprehensive overview of the Diamond DA62, a modern twin-engine aircraft designed for both private and commercial use. It highlights the aircraft's specifications, performance capabilities, and advanced features that cater to pilots and aviation enthusiasts. The DA62 is noted for its spacious cabin, fuel efficiency, and cutting-edge avionics, making it suitable for various missions, including charter operations and corporate flights. The document provides essential data on the aircraft's performance metrics, including speed, altitude, and fuel consumption, as well as details about its construction and design philosophy.
- Maximum speed: 356 km/h (192 knots)
- Maximum altitude: 6,096 m (20,000 ft)
- Useful load: 702 kg (1,545 lbs)
- Fuel consumption at 60% power: 44.7 liters/hour (11.8 gallons/hour)
- Maximum take-off mass: 2,300 kg (5,071 lbs)
Document
Source
Originally published by www.diamondaircraft.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Normal Procedures
- Year
- 2025
- Pages
- 11
- File size
- 8.5 MB
- Publisher
- www.diamondaircraft.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 1,288
- Engine (hp)
- 180
- Height (ft)
- 9
- Length (ft)
- 30
- Propeller
- MTV-6-R-C-F/CF 194-80
- Wingspan (ft)
- 48
- Engine model
- Austro Engine AE330
- Max speed (kt)
- 192
- Cruise speed (kt)
- 180
- Empty weight (lb)
- 3,523
- Fuel capacity (gal)
- 86.4
- Rate of climb (fpm)
- 1,028
- Service ceiling (ft)
- 20,000
- Max takeoff weight (lb)
- 5,071
Performance
- Fuel burn (gph)
- 11.8
- Landing over 50ft
- 2,555
- Max crosswind (kt)
- 25
- Takeoff over 50ft
- 2,730
- Landing distance (ft)
- 1,446
- Takeoff distance (ft)
- 1,574
V-speeds
- VS1
- 68
Weight & balance
- Useful load (lb)
- 1,545
- Max takeoff weight (lb)
- 5,071
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In this document
Performance Specifications
The Diamond DA62 boasts impressive performance metrics, including a maximum speed of 356 km/h (192 knots) and a maximum altitude of 6,096 m (20,000 ft). It has a maximum take-off mass of 2,300 kg (5,071 lbs) and a useful load of 702 kg (1,545 lbs). The aircraft can achieve a maximum range of 1,265 nautical miles (2,342 km) at 50% power, with a fuel consumption rate of 9.7 gallons per hour (36.7 liters per hour).
Engine and Propulsion
The DA62 is powered by two Austro Engine AE330 turbocharged jet fuel engines, each producing 180 HP. The aircraft features MT hydraulic constant speed propellers that enhance performance and reduce noise. The engines are controlled via a single power lever, simplifying operation for pilots.
Cabin and Comfort Features
The DA62 is designed with a spacious cabin that can accommodate up to seven passengers. It includes luxurious seating options, LED lighting, and easy access through gull-wing doors. The interior can be customized with various materials and styles to enhance passenger comfort.
Avionics and Technology
Equipped with the Garmin G1000 NXi flight deck, the DA62 offers advanced avionics capabilities, including a 3-axis GFC700 autopilot system and options for weather radar and synthetic vision. The avionics are designed for ease of use and maintenance, with a dedicated forward avionics bay.
Fuel Efficiency
The DA62 is noted for its fuel efficiency, burning only 17.1 gallons per hour (64.7 liters per hour) at high-speed cruise and as little as 9 gallons per hour (34.1 liters per hour) at maximum endurance speed. This efficiency makes it an attractive option for both private and commercial operations.
Full document text
DA62 THE ULTIMATE FLYING MACHINE Useful Load 702 kg or 1,545 lbs Consumption at 60% 44.7 lt/h or 11.8 gal/h Max. Speed 356 km/h or 192 kts Max. Altitude 6,096 m or 20,000 ft Page 3 TRAVEL THE 21ST CENTURY WAY „Standing out on the ramp at Diamond’s base at Wiener Neustadt in Austria, the DA62 looks exactly what it is – a 21st Century aircraft.“ www.pilotweb.aero MORE OF THE BEST The all new DA62 fills the gap between high performance single pistons and entry level turboprops. With a spacious cabin, offe- ring optional three row seven passenger seating, excellent pay- load and exceptionally low fuel burn, the DA62 is best described as a flying luxury SUV. The DA62 represents the ultimate development of Diamond’s pis- ton aircraft line, incorporating decades of experience in certified composite airplane construction, safety, jet fuel piston power- plants and advanced avionics integration. The DA62 will impress pilots looking for more seats and utility, as well as charter operators and corporate flight departments wanting to complement their larger aircraft with a low cost alter- native for shorter trips. AT A GLANCE: ▪ 7 seats, three-row seating ▪ Excellent cabin access ▪ Luxurious leather interior ▪ G1000 NXi, GFC700 3-axis & yaw damper ▪ Twin 180hp jet fuel AE330 engines ▪ High fuel efficiency ▪ Superb per- formance in all phases of flight ▪ TKS known ice protection (FIKI) DA62 KEYFACTS: Page 5 SPACIOUS LUXURY MEETS HIGH TECH SPACIOUS INTERIOR DESIGN The DA62 spoils pilots and passengers alike, with an extra-large cabin, generous and adjustable front seats, a 60/40 split folding three seat second row bench and optional folding two seat third row bench. Comfortable access for all on board is assured through the two forward gull wing doors and the huge rear door that provides access to all rear seats. Baggage is stowed in the generous nose compartments and cabin, offering maximum loading flexibility for any mission. “Even at a glance you can see that the standard of finish is extremely high, while the elegant, flowing lines are extremely attractive. ” www.pilotweb.de FIRST CLASS CABIN Luxury features abound throughout, including premium interiors in several styles, colors and materials, all LED interior lighting, optional electric air conditioning and more. CARBON DESIGN The sleek all carbon composite airframe incorporates advanced aerodynamics with the latest in passive safety technology for high performance, great efficiency and superior occupant protec- tion. The composite airframe is durable, easily maintained and will keep looking great for many years to come. Page 7 ADVANCED AVIONICS Page 9 ADVANCED AVIONICS TOP-NOTCH AVIONICS The fully integrated Garmin G1000NXi flight deck with stan- dard 3-axis GFC700 Automated Flight Control System and yaw damper and Electronic Stability and Protection, is complemented by a long list of avionics options to perfectly suit your mission. Integrated weather radar, normally available only on much more expensive aircraft, is available as are Traffic Alerting, Synthetic Vision, and much more. The Line Replaceable Units (LRU’s) are located in a dedicated and externally accessible forward avionics bay, for ease of maintenance and trouble shooting. EASY PROGRAMMING The Garmin GCU 476 alphanumeric keypad is an available option in the DA62. It makes programming the G1000 NXi easier than ever! „The Diamond DA62 is a per- fect platform for our use. We fly 300-400 hrs a year - to short grass airstrip like Manchester Barton and Wickenby which is only 520m and to major inter- national airport like Luton and London Stansted Airport. The benefit of this is the airplane’s capability of high speed on the approach, no slowing down the commercial traffic behind us. The landing is as easy as it can be with its trailing link undercarriage and larger tyres and feathering props. It’s a superb aircraft for private or commercial for either day or night VFR or IFR.“ Steven Viner, Chief Pilot, Morson International, UK Page 11 JET-FUEL POWER The turbocharged Austro AE330 jet fuel piston engines perfectly match the DA62’s aerodynamically efficient airframe, burning only 17.1 gph, combined, at a high speed cruise of 192 ktas, and little as 9 gph at max endurance speed. PROPULSION CONTROL Control is jet-engine simple, with each engine / propeller combination controlled by a single power lever and power settings displayed in % power. Simplified power control means that you can focus on more important things – and that is not just more convenient, but safer too. PROPELLERS The 3 blade MT hydraulic constant speed propellers feature advanced blade geometry for efficient performance, smoothness and low noise. They are automatically controlled by each engine’s digital engine control through conventional hydraulic governors. Feathering is as simple as flipping a single switch. „A case can be made that the twin-diesel DA62 from Aust- ria’s Diamond Aircraft repre- sents a new pinnacle in piston aircraft design. Its long list of positive attributes includes superb efficiency, quality cons- truction, technological sophi- stication and aesthetic appeal from every angle. With so much going for it, there’s little question this is an airplane that belongs on the shortlist of the greatest light twins ever. In a word, it’s a winner.“ www.flyingmag.com SALES UNITS DA62 in global operation (Year 2016-2024) WORLDWIDE 400+ UNITS The DA62 moves more passengers and equipment further and faster than anything else in its class, with exceptional fuel efficiency, luxury and twin-engine security. North America 160+ Units Latin America 25+ Units Europe 180 Units Middle East / Africa 15+ Units Asia and Pacific 5+ Units DA62 RANGE POWER: 50% (white circle on map) Range: 1,265 nm (2,342 km) Time: 8.9 h Speed: 142 kts (263 km/h) Consumption: 9.7 gal/h (36.7 l/h) POWER: 95% (yellow circle on map) Range: 887 nm (1,643 km) Time: 4.7 h Speed: 190 kts (352 km/h) Consumption: 18.5 gal/h (70 l/h)
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DA62 RANGE (incl. auxiliary tank) The above data are approximately specifications and may change without notice. Range calculation does not consider additional fuel consumption for taxi, takeoff, climb, descend or reserve. Page 19 DA62 FACTS AND SPECIFICATIONS POWER PLANT Engine 2x Austro Engine AE330 turbocharged common-rail injected 2.0 liter jet fuel engine with 180 HP and EECU single lever control system Propeller 2x MT propeller MTV-6-R-C-F/CF 194-80 3-blade constant speed propeller Fuel grades Jet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8 PERFORMANCE (MTOM, ISA) Max. speed (14,000 ft, MCP) 356 km/h TAS 192 kts TAS Cruise speed at 85% (12,000 ft) 333 km/h TAS 180 kts TAS Stalling speed, landing configuration 126 km/h 68 kts CAS Max. rate of climb (MSL) 5.2 m/s 1,028 ft/min Max. range (incl. auxiliary tank) (FL160, 50% PWR) incl. climb, no reserves 2,385 km 1,288 nm Fuel consumption at 60% (12,000 ft) in total 44.7 lt/hr 11.8 US gal/hr Take-off performance (MSL, ground roll / take-off obstacle) 480 m / 833 m 1,574 ft / 2,730 ft Landing performance (MSL, ground roll / landing distance) 441 m / 779 m 1,446 ft / 2,555 ft Certified service ceiling 6,096 m 20,000 ft Single engine service ceiling (MTOM, ISA, rate of climb: 50 ft/min.) 3,354 m 11,000 ft Single engine absolute ceiling (MTOM, ISA, rate of climb: 0 ft/min.) 4,116 m 13,500 ft Max. demonstrated crosswind 46 km/h 25 kts DIMENSIONS / MASS / LOADING Length 9.17 m 30 ft 1 in Height 2.82 m 9 ft 3 in Wingspan 14.57 m 47 ft 10 in Seats up to 7 up to 7 Empty weight without options 1,598 kg 3,523 lbs Maximum useful load 702 kg 1,545 lbs Max. take-off mass 1) 2,300 kg 5,071 lbs Fuel capacity total (usable fuel) main tank auxiliary tank 327 lt / 261 kg 189 lt / 151 kg 138 lt / 110 kg 86.4 US gal / 576 lbs 50 US gal / 333 lbs 36.4 US gal / 243 lbs Specifications apply to standard equipped aircraft, if not otherwise stated. The above data are approximately specifications and may change without notice. 1) The DA62 is also available with an MTOM of 1,999 kg (4,407 lbs). Our sales team will be happy to provide you with the necessary information: +43 2622 26700 1317 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. ©2025, Diamond Aircraft Industries GmbH. For additional information on Diamond Aircraft and its products please visit www.diamondaircraft.com. 09/2025 S_30691E www.diamondaircraft.com #WeFlyDiamondAircraft EUROPE, MIDDLE EAST, AFRICA, RUSSIA/CIS, ASIA (HQ): N. A. Otto-Strasse 5, 2700 Wiener Neustadt, Austria Phone: +43 2622 26700, sales-austria@diamondaircraft.com NORTH & SOUTH AMERICA, AUSTRALIA, NEW ZEALAND: 1560 Crumlin Sideroad, London, ON, Canada, N5V1S2 Phone: +1 800 268 4001, sales-canada@diamondaircraft.com CHINA: Wanfeng Airpark, Dashiju Town Xinchang County, Zhejiang Province, P. R. China www.youtube.com/diamondaircraftmedia www.facebook.com/diamondaircraftind www.twitter.com/diamondaircraft www.linkedin.com/company/diamond-aircraft www.instagram.com/diamondaircraftind AVIATION AS UNIQUE AS YOU ARE
What's in the Diamond DA62 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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