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Pilatus PC-21: Difference between revisions
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Moving cockpit image to to infobox; Template:Key press; mph → kt, I assume nautical miles per hour, knots, was intended
m (liveries update) |
(Moving cockpit image to to infobox; Template:Key press; mph → kt, I assume nautical miles per hour, knots, was intended) |
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{{infobox Aircraft | {{infobox Aircraft | ||
|image = PC-21.png | |image = PC-21.png | ||
|image2 = PC-21-cockpit.png | |||
|name = Pilatus PC-21 | |name = Pilatus PC-21 | ||
|type = Advanced trainer | |type = Advanced trainer | ||
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| | | | ||
}} | }} | ||
The '''Pilatus PC-21''' is a single-turboprop, low wing swept monoplane advanced trainer with a stepped tandem cockpit developed by Pilatus Aircraft in Switzerland. | The '''Pilatus PC-21''' is a single-turboprop, low wing swept monoplane advanced trainer with a stepped tandem cockpit developed by Pilatus Aircraft in Switzerland. | ||
== Performance Data == | == Performance Data == | ||
Maximum Speed: 428 | Maximum Speed: 428 kt | ||
Rate of climb: 4,000 ft/min | Rate of climb: 4,000 ft/min | ||
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Service Ceiling: 38,000 ft | Service Ceiling: 38,000 ft | ||
Stall Speed Gear/Flaps Up: 106 | Stall Speed Gear/Flaps Up: 106 kt, Gear/Flaps Down: 93 kt | ||
Range: 805 mi | Range: 805 mi | ||
== Aircraft help == | == Aircraft help == | ||
* | * {{key press|C}} - Canopy | ||
* | * {{key press|H}} - HUD | ||
* | * {{key press|M}} - Nose wheel steering | ||
* | * {{key press|Ctrl|B}} - Air brake | ||
* To start or stop engine use Autostart in menu | * To start or stop engine use Autostart in menu | ||
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* United Arab Emirates Air Force 128 | * United Arab Emirates Air Force 128 | ||
{{#ev:youtube|MZVCmHgAX6Y}} | {{#ev:youtube|MZVCmHgAX6Y}} | ||