Pilatus PC 9M
The Air Corps currently operates seven Pilatus PC-9M aircraft. These aircraft first entered service in 2004 and operate as the main pilot training aircraft for the Air Corps.
The PC-9M is equipped with a comprehensive, fully tandem-capable VFR/IFR avionics package for navigation, communication and identification, using state of the art equipment. The PC-9M features modern avionics including a Head Up Display (HUD) and Electronic Flight Instrumentation System (EFIS) where primary instruments are displayed. The PC-9M is fitted with a Martin-Baker CG-A Ejection Seat which provides safe escape for the pilot from sea level to its operational ceiling at any airspeed greater than 65 knots.
Roles
- Ab Initio Pilot Training
- Advanced Pilot Training
- Instructor Pilot Training
- Close Air Support
|
Aircraft Type |
Pilatus PC-9M |
|---|---|
|
Role(s) |
Ab Initio, Advanced & Instructor Pilot Training and Close Air Support |
|
Crew |
1 Pilot & 1 Student |
|
Powerplant |
1 x Pratt & Whitney PT6A-62 turbo prop |
|
Wing Span |
10.19 metres (33 feet, 5 inches) |
|
Height |
3.25 metres (10 feet, 8 inches) |
|
Length |
10.16 mts. (33 feet, 4 inches) |
|
Armament |
2 x Rocket Pods - Holding x 2.75” (70mm) ‘FN LAU 7’ Folding Fin Aerial Rockets |
|
Entered Service |
2004 |
Pilatus PC-9M Training Flight
-
PC9 Training Flight
|
Max T/O Weight |
3,200 Kilogrammes (7,050 pounds) |
|---|---|
|
Service Ceiling |
25,000 feet |
|
Cruise Speed |
275 knots |
|
Maximum Speed |
320 knots |
|
Endurance |
4 hours, 30 minutes |
|
Range |
850 Nautical Miles |
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