Diamond DA40: Difference between revisions
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== Flying the DA40 == | == Flying the DA40 == | ||
The flight manual is available from [[http://support.diamond-air.at/da40_ng_afm_bas+M52087573ab0.html|Diamond Aircraft]] and is highly suggested to be read before flight. | The flight manual is available from [[http://support.diamond-air.at/da40_ng_afm_bas+M52087573ab0.html| Diamond Aircraft]] and is highly suggested to be read before flight. | ||
===Some data good to know=== | ===Some data good to know=== | ||
MTOW : 1280 kg (2822 lbs) <br/> | MTOW : 1280 kg (2822 lbs) <br/> | ||
Vmo : 101-113 kts (based on weight)<br/> | Vmo : 101-113 kts (based on weight)<br/> | ||
Vne : 172 kts <br/> | Vne : 172 kts <br/> |
Revision as of 08:54, 31 August 2019
Type | Civil utility aircraft, Civil trainer aircraft |
---|---|
Configuration | Low wing aircraft |
Propulsion | Piston aircraft, Single-engine aircraft |
Manufacturer | Diamond Aircraft |
Author(s) | Emmanuel Baranger, Bea Wolf, Noah Ryu |
FDM | JSBSim |
--aircraft= | da40ng-jsb |
Status | Beta |
Development | |
Website | |
Repository | |
Download | |
License | GPLv2+ |
|
The Diamond DA40 is a modern low-wing single-engine piston aircraft. Seating 4 people and available in a VFR or an IFR variant, it is mostly used for training and personal flights. The 'DA40NG', as modelled here, is an updated variant featuring an Austro Engines AE300 diesel engine and winglets to reduce the wing span.
Flying the DA40
The flight manual is available from [Diamond Aircraft] and is highly suggested to be read before flight.
Some data good to know
MTOW : 1280 kg (2822 lbs)
Vmo : 101-113 kts (based on weight)
Vne : 172 kts