DA42-VI fact sheet
Diamond DA42 VI · Specifications
Overview
This document is a specifications fact sheet for the Diamond DA42 VI, detailing the aircraft's performance, dimensions, and operational capabilities. It is intended for pilots, aviation enthusiasts, and those interested in the technical aspects of the DA42 VI. The fact sheet includes information on the power plant, performance metrics, fuel consumption, and physical dimensions, providing a comprehensive overview of the aircraft's specifications. The data presented is approximate and subject to change without notice, emphasizing the importance of consulting the latest information for operational planning.
- Engines: 2x Austro Engine AE 300, 168 HP each
- Max cruise speed: 365 km/h (197 kts) at 16,000 ft
- Stall speed (clean): 124 km/h (67 kts)
- Max operating altitude: 5,486 m (18,000 ft)
- Fuel capacity: 189 lt (50 US gal) standard, 289 lt (76.4 US gal) long range
Document
Source
Originally published by uploads-ssl.webflow.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 2012
- Pages
- 2
- File size
- 670 KB
- Publisher
- uploads-ssl.webflow.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 795
- Engine (hp)
- 168
- Height (ft)
- 8
- Length (ft)
- 28
- Propeller
- MT propeller MTV-6-R-C/CF 190-69
- Wingspan (ft)
- 44
- Engine model
- Austro Engine AE 300
- Max speed (kt)
- 197
- Cruise speed (kt)
- 174
- Empty weight (lb)
- 3,109
- Fuel capacity (gal)
- 50
- Rate of climb (fpm)
- 1,800
- Service ceiling (ft)
- 18,000
- Max takeoff weight (lb)
- 4,189
Performance
- Fuel burn (gph)
- 10.4
- Landing over 50ft
- 1,870
- Max crosswind (kt)
- 25
- Takeoff over 50ft
- 1,961
- Landing distance (ft)
- 1,870
- Takeoff distance (ft)
- 1,961
- Stall speed clean (kt)
- 67
- Stall speed landing (kt)
- 61
V-speeds
- VS1
- 67
- VSO
- 61
Weight & balance
- Useful load (lb)
- 1,080
- Max takeoff weight (lb)
- 4,189
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Diamond DA42 VI.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Diamond DA42 VI for sale now
Free — save the DA42 to your watchlist and track it in one place.
More Diamond DA42 VImanuals & documents
See all 36 →- DA42-VI THE DEFINITION OF PERFECTIONSystems Description
- Airworthiness Directive Schedule Aeroplanes Diamond DA 42 and DA 42 NGService Bulletins
- Pilot’s Operating HandbookPilot's Operating Handbook
- Pilot’s Operating Handbook DA42 SeriesChecklist
- Polish Defence and Security Equipment Catalogue 2024Specifications
- TCDS No. EASA.A.005 DA 42 - SeriesType Certificate
- DA42-VI EXTERIOR & INTERIOR DESIGNWiring Diagram
- DA42-VISystems Description
- Airplane Flight Manual DA 42 TDIFlight Manual
- Garmin G1000 Cockpit Reference Guide for the Diamond Da42Checklist
- DA42-VI, SN 42.N474, OE-UDOSpecifications
- Airworthiness Directives; Diamond Aircraft Industries GmbH AirplanesAirworthiness Directives
If you fly the Diamond DA42 VI, you may also be researching these.
In this document
Power Plant
The DA42 VI is powered by two Austro Engine AE 300 turbocharged diesel engines, each producing 168 HP. The engines utilize a common-rail injection system and are controlled by an EECU single lever control system. The aircraft is equipped with MT propeller MTV-6-R-C/CF 190-69 three-blade constant speed propellers.
Performance and Consumption
At maximum takeoff weight (MTOW) of 1,760 kg, the DA42 VI achieves a maximum cruise speed of 365 km/h (197 kts) at 16,000 ft. The stall speed in a clean configuration is 124 km/h (67 kts), and the rate of climb at sea level is 9.1 m/s (1,800 fpm). The aircraft has a range of 1,470 km (795 nm) at 60% power with standard tank capacity.
Dimensions and Mass
The DA42 VI has a length of 8.56 m (28 ft 1 in), a height of 2.49 m (8 ft 2 in), and a wingspan of 13.55 m (44 ft 4 in). It seats four and has an empty weight of 1,410 kg (3,109 lbs) with a maximum takeoff mass of 1,900 kg (4,189 lbs). The payload capacity is 490 kg (1,080 lbs).
Fuel Capacity
The aircraft can be equipped with either a standard fuel tank of 189 liters (50 US gallons) or a long-range tank of 289 liters (76.4 US gallons). It is compatible with various diesel fuel grades including Jet A-1 and EN 590.
Operational Limits
The maximum operating altitude for the DA42 VI is 5,486 m (18,000 ft), with a demonstrated maximum crosswind component of 46 km/h (25 kts). Take-off distance over a 50 ft obstacle is 598 m (1,961 ft), and landing distance over a 50 ft obstacle is 570 m (1,870 ft).
Full document text
DA42-VI fact sheet Diamond Aircraft Industries GmbH | N. A. Otto-Straße 5 | A-2700 Wiener Neustadt, Austria T +43 2622 26700 | F +43 2622 26700-1199 | www.diamond-air.at Version: April 16 th , 2012 S_30649E © 2012 Diamond Aircraft Industries GmbH *) Specifications apply to standard equipped aircraft (with DME, TAS, WX500, AUX, TKS, standard light weight interior without adjustable seats), if not otherwise stated. The above data are approximately specifications and may change without notice. DA42-VI fact sheet Power plant Engines 2x Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HPand EECU single lever control system Propellers MT propeller MTV-6-R-C/CF 190-69 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/ consumption (MTOW) Max. cruise speed (16,000 ft, MCP), 1760 kg TOW 365 km/h TAS 197 kts TAS Max. cruise speed (16,000 ft, MCP) 353 km/h TAS 193 kts TAS Cruise speed at 60% (16,000 ft) 322 km/h TAS 174 kts TAS Stall speed, clean 124 km/h CAS 67 kts CAS Stall speed, landing configuration 113 km/h CAS 61 kts CAS Rate of climb (ISA SL), 1760 kg TOW 9.1 m/s 1,800 fpm Rate of climb (ISA SL) 7.1 m/s 1,400 fpm Rate of climb (18,000 ft) 5.0 m/s 1,000 fpm Single Engine Service Ceiling 5,486 m 18,000 ft Range at 60%, standard-/ long range tank 1,470 km/ 2,245 km 795 nm/ 1,215 nm Consumption at 60% 39.4 lt/hr 10.4 US gal/hr Take-off distance 50 ft (ISA SL) 598 m 1,961 ft Take-off ground roll (ISA SL), 1760 kg TOW 280 m 919 ft Take-off ground roll (ISA SL) 354 m 1,161 ft Landing distance 50 ft (ISA SL) 570 m 1,870 ft Landing ground roll (ISA SL) 340 m 1,115 ft Max. operating altitude 5,486 m 18,000 ft Max. demonstrated crosswind 46 km/h 25 kts Dimensions/ mass/ loading Length 8.56 m 28 ft 1 in Height 2.49 m 8 ft 2 in Wing span 13.55 m 44 ft 4 in Seats 4 4 Empty weight *) 1,410 kg 3,109 lbs MTOM 1,900 kg 4,189 lbs Payload *) 490 kg 1,080 lbs Fuel capacity standard-/ long range tank 189 lt/ 289 lt 50 US gal/ 76.4 US gal 8.56 m / 28 ft 1 in 13.55 m / 44 ft 4 in 2.49 m / 8 ft 2 in Diesel EN 590
283 Diamond DA42 VI parts for sale
See all →
Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.