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Diamond DA40 (Diamond Star)


Light-class Trainer / Utility Aircraft [ 1997 ]



The Diamond DA40 series of lightweight aircraft has seen adoption by various military services of the world including Austria, Singapore, and the United States.



Authored By: Staff Writer | Last Edited: 09/08/2022 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

GO TO SPECIFICATIONS [+]
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The Diamond "DA40" (Diamond Star / Star) is a lightweight, four passenger general aviation aircraft to come from Diamond Aircraft Industries of Austria. The type is a further development of the company's twin-seat "DA20", of which over 2,000 examples were produced from 1994 onwards, and follows much of its form-and-function. A first-flight for the DA40 was recorded on November 5th, 1997 and production has been ongoing since with over 2,200 units to date.

Beyond their commercial sector usage, the DA40 series has been adopted by some world military air powers to be used as a flight trainer for new generations of pilots. This includes Australia, Austria, Bangladesh, Bolivia, Ecuador, Indonesia, Jamaica, Singapore, and the United States.

The aircraft utilizes the tried-and-true single-engine configuration with the powerplant embedded in the nose. The engine drives a three-bladed propeller unit. Aft of the engine mounting is the side-by-side cockpit which seats the pilot and up to three passengers in comfort. Large windscreens are provided for excellent vision out-of-the-cockpit. The wings are of monoplane form and fitted low along the sides of the fuselage. A slight upturn of the tips is seen at the end of each mainplane member. The tail unit incorporates a Multhopp-style T-plane arrangement seating the horizontal plane high atop the vertical fin. The undercarriage is of tricycle arrangement and fixed with some versions featuring streamlined fairings over the wheels for inherent aerodynamics. Construction of the aircraft is largely of composites.

The aircraft has a running length of 26.6 feet with a wingspan of 39 feet and a height of 6.5 feet. Empty weight is 1,755lb against a gross of 2,640lb. Power is from a Lycoming IO-360-M1A 4-cylinder, air-cooled, horizontally-opposed piston engine delivering 180 horsepower. Cruising speeds reach 175 miles-per-hour with ranges out to 835 miles and a service ceiling up to 16,000 feet. Rate-of-climb is listed at 1,120 feet-per-minute.

Initial production models were designated simply as "DA40" fitted with Textron Lycoming IO-360 M1A engine of 180 horsepower. The "DA40 D" then followed and carried the Thielert TAE 125-01 or TAE 125-02-99 engines and has reduced maximum gross weights for European airspace operations. The short-lived "DA40F" / "DA40 FP" was powered by the Textron Lycoming O-360-A4M engine.

The "DA40" NG represents the current offering of the line and carries a local Austro Engine AE 300 powerplant utilizing JET A-1 fuel. European certification was granted in April 2010 and some 500 units have been produced since.

The DA40 XLT appeared in April of 2013 and numerous updates and upgrades internally. The DA40 "Tundra Star" was given a reinforced undercarriage and carries an Austro AE300 diesel engine of 168 horsepower. The eDA40 is an all-electric aircraft reveled in October 2021.

The "T-52A" marks a military trainer model operated by the United States Air Force Academy. Some twenty airframes were produced in 2009. It has since been succeeded in inventory by the Cirrus SR-20 (operated as the "T-53A)".©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.

October 2018 - A modified hybrid-electric DA40 was flown for the first time on October 31st, 2018 out of Wiener Neustadt in Austria.

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Specifications



Service Year
1997

Origin
Austria national flag graphic
Austria

Status
ACTIVE
In Active Service.
Crew
1

Production
60
UNITS


Diamond Aircraft Industries - Austria / China
(View other Aviaton-Related Manufacturers)
National flag of Australia National flag of Austria National flag of Bangladesh National flag of Bolivia National flag of Ecuador National flag of Indonesia National flag of Singapore National flag of the United States Australia; Austria; Bangladesh; Bolivia; Ecuador; Indonesia; Jamaica; Singapore; United States
(OPERATORS list includes past, present, and future operators when applicable)
Commercial Aviation
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
VIP Service
Used in the Very-Important-Person (VIP) passenger transport role, typically with above-average amenities and luxuries as standard.
Training (General)
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).


Length
26.6 ft
(8.10 m)
Width/Span
39.0 ft
(11.90 m)
Height
6.5 ft
(1.98 m)
Empty Wgt
1,764 lb
(800 kg)
MTOW
2,646 lb
(1,200 kg)
Wgt Diff
+882 lb
(+400 kg)
(Showcased structural values pertain to the Diamond DA40XL Diamond Star production variant)
monoplane / low-mounted / straight
Monoplane
Design utilizes a single primary wing mainplane; this represent the most popular mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
(Structural descriptors pertain to the Diamond DA40XL Diamond Star production variant)
Installed: 1 x Lycoming IO-360-M1A air-cooled, 4-cylinder piston engine developing 180 horsepower driving three-bladed propeller unit at the nose.
Max Speed
174 mph
(280 kph | 151 kts)
Cruise Speed
115 mph
(185 kph | 100 kts)
Max. Speed Diff
+59 mph
(+95 kph | 51 kts)
Ceiling
16,404 ft
(5,000 m | 3 mi)
Range
833 mi
(1,340 km | 2,482 nm)
Rate-of-Climb
1,120 ft/min
(341 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the Diamond DA40XL Diamond Star production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
None.


Supported Types




(Not all ordnance types may be represented in the showcase above)
DA40 - Base Series Designation; initial production model with Textron Lycoming IO-360 M1A engine of 180 horsepower.
DA40 D - Powered by Theilert TAR 125-01 / 125-02-99 engine of 135 horsepower; European market airframe.
DA40 F / DA40 FP - Textron Lycoming O-360-A4M engine.
DA40 NG - Modern offering; powered by Austro Engine AE 300 of 165 horsepower; certified 2010.
T-52A - USAF academy designation for training purposes; since succeeded by T-53A (Cirrus SR20).
DA40 XLT - Model of April 2013; internal upgrades throughout.
DA40 "Tundra Star" - Reinforced undercarriage; powered by Austro AE300 diesel-fueled engine of 168 horsepower.
eDA40 - All-electric model of 2021.


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Images Gallery



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Image from Diamond Aircraft marketing materials; DA40 XLT pictured.

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