Variants
- DA40
- Initial model, powered by a Textron Lycoming IO-360 M1A 180 hp (135 kW) engine and a MT Propellers MTV-12-B/180-17. Maximum gross weight is 1150 kg (2535 lb) or 1200 kg (2646 lb) with modifications installed. In increasingly refined versions marketed as the DA40-180, XL, CS and XLS.
- DA40 D
- Diesel model, powered by a Thielert TAE 125-01 (Centurion 1.7) or TAE 125-02-99 (Centurion 2.0) engine of 135 hp (101 kW) and MT Propellers MTV-6-A/187-129. Maximum gross weight is 1150 kg (2535 lb). Marketed primarily in Europe, although certified in Canada and Australia as well, as the DA40 TDI.
- DA40 F
- Fixed pitch propeller model, powered by Textron Lycoming O-360-A4M and a Sensenich 6EM8S10-0-63 or a MT-Propeller MT 188R135-4G propeller. Maximum gross weight is 1150 kg (2535 lb). Marketed as the DA40 FP. This model is no longer offered.
- DA40 NG
- Latest model, offered in select markets only (DA40 model is still offered in other markets), powered by an Austro Engine AE 300 170 hp (127 kW) running on JET A-1 fuel. EASA certified April 2010
- T-52A
- Military trainer version, 20 acquired in 2009 and used by the 557th Flying Training Squadron at USAFA The type will be replaced in 2012 with the Cirrus SR20-based T-53A.
Read more about this topic: Diamond DA40
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