DA40 NG - fact sheet

Diamond DA40 NG · Specifications

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Overview

This document serves as a fact sheet for the Diamond DA40 NG, detailing its specifications and performance metrics. It is intended for pilots, aviation enthusiasts, and potential buyers who are interested in understanding the capabilities and features of this aircraft model. The fact sheet includes information on the power plant, performance, dimensions, weight, and fuel capacity, providing a comprehensive overview of the aircraft's operational parameters. The data presented is approximate and subject to change without notice, emphasizing the importance of consulting the latest information for accurate specifications.

Engine: Austro Engine AE 300, 168 HP
Max cruise speed: 285 km/h (154 kts) at 14,000 ft
Stall speed (clean): 117 km/h (63 kts)
Empty weight: 880 kg (1,940 lbs)
Max takeoff mass: 1,280 kg (2,822 lbs)
Fuel capacity: 106 lt (28 US gal) standard tank, 147 lt (39 US gal) long range tank
Takeoff distance (50 ft): 560 m (1,837 ft)

Document

Source

Originally published by www.sueair.co.uk. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Specifications
Year: 2011
Pages: 2
File size: 736 KB
Publisher: www.sueair.co.uk

Specifications & performance

Extracted from this document.

Specifications

Range (nm): 675
Engine (hp): 168
Height (ft): 6
Length (ft): 26
Propeller: MT propeller MTV-6-R-/190-69
Wingspan (ft): 38
Engine model: Austro Engine AE 300
Max speed (kt): 154
Cruise speed (kt): 125
Empty weight (lb): 1,940
Fuel capacity (gal): 28
Rate of climb (fpm): 690
Service ceiling (ft): 16,400
Max takeoff weight (lb): 2,822

Performance

Fuel burn (gph): 5.2
Landing over 50ft: 1,968
Max crosswind (kt): 25
Takeoff over 50ft: 1,837
Landing distance (ft): 1,968
Takeoff distance (ft): 1,837
Stall speed clean (kt): 63
Stall speed landing (kt): 58

V-speeds

VS1: 63
VSO: 58

Weight & balance

Useful load (lb): 882
Max takeoff weight (lb): 2,822

Documentation completeness

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In this document

Power Plant

The Diamond DA40 NG is powered by the Austro Engine AE 300, a turbocharged common-rail injected 2.0 liter diesel engine that produces 168 horsepower. It features an EECU single lever control system for ease of operation.

Performance and Consumption

At a maximum cruise altitude of 14,000 feet, the DA40 NG achieves a maximum cruise speed of 285 km/h (154 knots) and a cruise speed of 231 km/h (125 knots) at 60% power. The stall speed in a clean configuration is 117 km/h (63 knots), while in landing configuration it is 107 km/h (58 knots). The aircraft has a rate of climb of 3.5 m/s (690 ft/min) at sea level.

Dimensions and Weight

The DA40 NG has a length of 8.06 m (26 ft 5 in), a height of 1.97 m (6 ft 6 in), and a wingspan of 11.63 m (38 ft 2 in). It seats four passengers and has an empty weight of 880 kg (1,940 lbs) with a maximum takeoff mass of 1,280 kg (2,822 lbs), allowing for a payload of 400 kg (882 lbs).

Fuel Capacity

The aircraft is available with standard and long-range fuel tanks, with capacities of 106 liters (28 US gallons) and 147 liters (39 US gallons) respectively.

Takeoff and Landing Performance

The takeoff distance to clear a 50-foot obstacle at sea level is 560 m (1,837 ft), with a ground roll of 370 m (1,214 ft). For landing, the distance to clear a 50-foot obstacle is 600 m (1,968 ft), with a ground roll of 270 m (886 ft).

Full document text

DA40 NG - fact sheet DA40 NG - fact sheet Version: February 18 th , 2011 S_30613E © 2011 Diamond Aircraft Industries GmbH 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 Power plant Engine Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control system Propeller MT propeller MTV-6-R-/190-69 3-blade constant speed propeller Fuel grades Jet A-1, Jet A, TS-1 Performance/ consumption (max. mass) Max. cruise speed (14,000 ft, MCP) 285 km/h TAS 154 kts TAS Cruise speed at 60% (14,000 ft) 231 km/h TAS 125 kts TAS Stall speed, clean 117 km/h CAS 63 kts CAS Stall speed, landing configuration 107 km/h CAS 58 kts CAS Rate of climb (ISA SL) 3.5 m/s 690 ft/min Rate of climb (10,000 ft) 3.2 m/s 630 ft/min Range at 60%, standard-/ long range tank 1,250 km/ 1,741 km 675 nm/940 nm Consumption at 60% 19.7 lt/hr 5.2 US gal/hr Take-off distance 50ft (ISA SL) 560 m 1,837 ft Take-off ground roll (ISA SL) 370 m 1,214 ft Landing distance 50ft (ISA SL) 600 m 1,968 ft Landing ground roll (ISA SL) 270 m 886 ft Max. operating altitude 5,000 m 16,400 ft Max. demonstrated crosswind 46 km/h 25 kts Dimensions/ mass/ loading Length 8.06 m 26 ft 5 in Height 1.97 m 6 ft 6 in Wing span 11.63 m 38 ft 2 in Seats 4 4 Empty weight 880 kg 1,940 lbs MTOM 1,280 kg 2,822 lbs Payload 400 kg 882 lbs Fuel capacity standard-/ long range tank 106 lt/ 147 lt 28 US gal/ 39 US gal 1.97 m/ 6 ft 6 in 8.06 m/ 26 ft 5 in 11.63 m/ 38 ft 2 in Specifications apply to standard equipped aircraft, if not otherwise stated. The above data are approximately specifications and may change without notice.

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