Pilatus PC-9M: Difference between revisions
Jump to navigation
Jump to search
m (→External links) |
|||
| Line 44: | Line 44: | ||
== External links == | == External links == | ||
* [http://www.pilatus-aircraft.com | * [http://www.pilatus-aircraft.com Pilatus Aircraft] | ||
* [http://http://en.wikipedia.org/wiki/Pilatus_PC-9 | * [http://http://en.wikipedia.org/wiki/Pilatus_PC-9 Wikipedia] | ||
{{Pilatus Aircraft}} | {{Pilatus Aircraft}} | ||
Revision as of 20:41, 24 January 2012
 | |
| Type | Basic, Advanced Trainer aircraft |
|---|---|
| Author(s) | Petar Jedvaj, Ernest Teuscher (based on David Culp's and Erik Hoffmans' PC-7) |
| FDM | JSBSim |
| --aircraft= | PC-9M |
| Status | beta |
| Download |
 |
The Pilatus PC-9M is a single-engine, low-wing tandem-seat turboprop training aircraft.
Performance Data
Maximum Speed: 368 mph
Cruise Speed: 343 mph
Rate of climb: 4,090 ft/min
Service Ceiling: 37,992 ft
Stall Speed Gear/Flaps Up: 88 mph, Gear/Flaps Down: 77 mph
Range: 990 mi
Development status/Issues/Todo
Development status
- In development
Issues
Todo:
External links
| ||||||||