Pilatus PC-9M

Pilatus PC-9
Type	Trainer aircraft, Military aircraft, Military trainer aircraft
Configuration	Low wing aircraft
Propulsion	Turboprop aircraft, Single-engine aircraft
Manufacturer	Pilatus aircraft
Author(s)	PC-9M team Petar Jedvaj; David Culp; Erik Hoffman; Ernest Teuscher; Johan G; Hyde Yamakawa; Gary Brown;
FDM	JSBSim
--aircraft=	PC-9M
Status	Early production
FDM
Systems
Cockpit
Model
Development
Website
Repository
Download
Forum
License
	This aircraft is NOT available under the GNU GPL 2, the primary license of the FlightGear project. This means that parts cannot be reused in the official FlightGear repositories.
	This aircraft is NOT available under the GNU GPL 2, the primary license of the FlightGear project. This means that parts cannot be reused in the official FlightGear repositories.
	v; t; e;

Pilatus PC-9M is a single-engine, low-wing tandem-seat turboprop training aircraft designed by Pilatus Aircraft in Switzerland.

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

Key	Function
`C`	Toggle canopy
`E`	Eject
`L`	Toggle landing lights
`M`	Nose wheel steering
`Ctrl`+`B`	Toggle air brake
`Ctrl`+`A`	Toggle autopilot altitude lock
`Ctrl`+`G`	Toggle autopilot glide slope lock
`Ctrl`+`H`	Toggle autopilot heading lock
`Ctrl`+`N`	Toggle nav1 lock
`Ctrl`+`O`	A/P engage/disengage
`Ctrl`+`S`	Toggle auto throttle arm
`F11`	Pop up autopilot dialog
`F12`	Radio stack