Pilatus Aircraft Pc-9 (PC9)
ICAO PC9 Light

Pilatus Aircraft Pc-9

Single Turboprop

The Pilatus PC-9 is a Swiss-designed single-engine turboprop trainer that became one of the most successful military basic and advanced training aircraft of the 1980s and 1990s. Developed as a turboprop successor to the piston-powered PC-7, the PC-9 first flew in 1984 and entered service with the Royal Saudi Air Force in 1985, eventually equipping more than 20 air forces worldwide including Australia, Croatia, Slovenia, and Myanmar. Its Pratt & Whitney Canada PT6A-62 engine delivers 1,150 shaft horsepower, giving the aircraft a maximum speed of 345 knots and a service ceiling of 25,000 feet—performance that allows student pilots to experience jet-like handling characteristics and energy management while retaining the economy and simplicity of turboprop operations. The tandem cockpit features Martin-Baker ejection seats and a stepped configuration that provides excellent visibility for both instructor and student. The PC-9's success led Pilatus and Beechcraft to collaborate on the T-6 Texan II, a heavily modified derivative that became the U.S. Air Force and Navy's primary trainer, replacing the T-37 and T-34. While most PC-9s serve military flight schools, a small number have entered civilian hands for warbird operations and advanced aerobatic training. The type remains in frontline training service with several nations decades after introduction, a testament to its rugged Swiss engineering and effective training mission design. SkyMeter has tracked 58 flights across 14 airframes and 6 operators, with BLUE AIR TRAINING CORP the largest observed operator.

ACTIVE AIRFRAMES
14
last 7 days
🏢
OPERATORS
6
unique airlines
📊
FLIGHTS
58
tracked
AVG DURATION
1h 22m
per flight
INCIDENT RATE
12.1%
7 flagged

Safety in context

The incident rate counts flights with ANY safety event detected by SkyMeter — go-arounds (a routine response, not a failure), unstable-approach gate flags (advisory thresholds), rejected takeoffs (the system working as designed), and runway events. It is NOT an accident rate or fatality rate. For accident statistics, refer to the NTSB Aviation Accident Database (USA) or the Aviation Safety Network. See methodology for what each event type measures.

Performance

Speed envelope & approach

Vref
90 kt
Vref range
Vmo
320 kt
Mmo
Vne
345 kt
Vno
280 kt
Vs0 (landing)
67 kt
Vfe
150 kt
Approach category

Dimensions

Airframe geometry

Wingspan
Length
Tail height
Wheelbase
Gear width
Wake category
L

Weight & identification

Operating limits

MTOW
7,055 lb
MALW
Manufacturer model
PC-9
FAA designator
Registered

Recent incidents

Flagged flights of PC9

20
06/30/2026
2h 16m
△ Unstable
06/28/2026
1h 28m
△ Unstable
06/26/2026
1h 31m
△ Unstable
06/26/2026
2h 43m
△ Unstable
06/25/2026
22m
△ Unstable
06/24/2026
49m
△ Unstable
06/23/2026
1h 22m
△ Unstable
06/22/2026
25m
△ Unstable
06/22/2026
30m
△ Unstable
06/20/2026
46m
△ Unstable

Recent flights

Real flights of PC9 · airborne ≥ 20 min

30
06/30/2026
43m
No alerts
06/30/2026
2h 3m
No alerts
06/30/2026
31m
No alerts
06/30/2026
26m
No alerts
06/30/2026
20m
No alerts
06/30/2026
2h 16m
△ Unstable
06/30/2026
2h 31m
No alerts
06/30/2026
2h 36m
No alerts
06/30/2026
3h 32m
No alerts
06/30/2026
1h 55m
No alerts
06/30/2026
1h 57m
No alerts
06/30/2026
1h 54m
No alerts
06/29/2026
2h 16m
No alerts
06/29/2026
2h 22m
No alerts
06/29/2026
2h 20m
No alerts
06/28/2026
1h 28m
△ Unstable
06/28/2026
28m
No alerts
06/28/2026
33m
No alerts
06/27/2026
1h 12m
No alerts
06/26/2026
1h 31m
△ Unstable
06/26/2026
36m
No alerts
06/26/2026
1h 57m
No alerts
06/26/2026
44m
No alerts
06/26/2026
2h 43m
△ Unstable
06/26/2026
1h 15m
No alerts
06/25/2026
2h 14m
No alerts
06/25/2026
1h 5m
No alerts
06/25/2026
1h 49m
No alerts
06/25/2026
1h 12m
No alerts
06/25/2026
1h 31m
No alerts
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© SkyMeter · All flight data subject to ODbL attribution · Tracking window: 7 days (free tier)