Pilatus PC-21: Difference between revisions
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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 | ||
Line 24: | Line 10: | ||
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 == | ||
{| class="keytable" | |||
! Key !! Function | |||
|- | |||
| {{key press|C}} || Canopy | |||
|- | |||
| {{key press|E}} || Eject | |||
|- | |||
| {{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 | |||
== Liveries == | == Liveries == | ||
Line 39: | Line 35: | ||
* Demonstrator HB-HZB | * Demonstrator HB-HZB | ||
* Demonstrator HB-HZC | * Demonstrator HB-HZC | ||
* FGUK | |||
* Qatar Emiri Air Force 351 | |||
* Republic of Singapore Air Force 9113 | * Republic of Singapore Air Force 9113 | ||
* Royal Saudi Air Force 108 | |||
* Swiss Air Force A-105 | * Swiss Air Force A-105 | ||
* UK MFTS Evaluation System | |||
* UK MFTS Evaluation System 2 | |||
* United Arab Emirates Air Force 128 | * United Arab Emirates Air Force 128 | ||
{{#ev:youtube|MZVCmHgAX6Y}} | {{#ev:youtube|MZVCmHgAX6Y}} | ||
{{#ev:vimeo|108249462}} | |||
== Development status/Issues/Todo == | == Development status/Issues/Todo == | ||
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* Pilot models | * Pilot models | ||
* Authentic instruments | * Authentic instruments | ||
* Ejection seats | |||
* HUD | * HUD | ||
* External animations | * External animations | ||
Line 62: | Line 64: | ||
* Some parts of CHDD are not operational (ITT, Oil T, Torque %) | * Some parts of CHDD are not operational (ITT, Oil T, Torque %) | ||
Todo: | Todo: | ||
* Cockpit textures | * Cockpit textures | ||
== External links == | == External links == | ||
Line 78: | Line 75: | ||
{{Pilatus Aircraft}} | {{Pilatus Aircraft}} | ||
Latest revision as of 15:11, 21 July 2016
Type | Military trainer aircraft | |
---|---|---|
Configuration | Low wing aircraft | |
Propulsion | Turboprop aircraft, Single-engine aircraft | |
Manufacturer | Pilatus aircraft | |
Author(s) |
PC-21 team
| |
FDM | JSBSim | |
--aircraft= | PC-21 | |
Status | Beta | |
FDM | ||
Systems | ||
Cockpit | ||
Model | ||
Development | ||
Website | ||
Repository | ||
Download | ||
Forum | ||
License | ||
| ||
|
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
Maximum Speed: 428 kt
Rate of climb: 4,000 ft/min
Service Ceiling: 38,000 ft
Stall Speed Gear/Flaps Up: 106 kt, Gear/Flaps Down: 93 kt
Range: 805 mi
Aircraft help
Key | Function |
---|---|
C | Canopy |
E | Eject |
H | HUD |
M | Nose wheel steering |
Ctrl+B | Air brake |
To start or stop engine use Autostart in menu
Liveries
- Demonstrator HB-HZA
- Demonstrator HB-HZB
- Demonstrator HB-HZC
- FGUK
- Qatar Emiri Air Force 351
- Republic of Singapore Air Force 9113
- Royal Saudi Air Force 108
- Swiss Air Force A-105
- UK MFTS Evaluation System
- UK MFTS Evaluation System 2
- United Arab Emirates Air Force 128
Development status/Issues/Todo
Development status - IN DEVELOPMENT
- Detailed 3D model & textures
- Pilot models
- Authentic instruments
- Ejection seats
- HUD
- External animations
- Lights
- Particle system
- Crash detect system
Issues
- Some parts of CHDD are not operational (ITT, Oil T, Torque %)
Todo:
- Cockpit textures
External links
|