flight-aid
ABOUT
PROGRAMMES
AIRCRAFT
PROJECTS
SUPPORT
SERVICE
CONTACT
PILATUS PC-12

Pilatus PC-12 (c) Paul Bowen (photo: Pilatus Aircraft)

 

Pilatus PC-12
Performance Specifications

Engine:  Pratt & Whitney Canada  PT6A-67B
Propeller: Hartzell, 4-blade, constant speed/
fully reversing
Horsepower: 1200 shp
Recommended TBO: 3500 hrs
Wingspan: 53.33 ft / 16.23 m
Length: 47.33 ft / 14.40 m
Height: 14.07 ft / 4.26 m
Empty Weight: 5732 lbs / 2600 kg
Gross Weight (MTOW): 9920 lbs / 4500 kg
Max. Payload: 3108 lbs / 1410 kg
Maximum Fuel: 402 US gal / 1522 litres
   
Max. Range
(30,000 ft,
VFR reserves):
2261 nm / 4190 km
Max. Operating Altitude: 30,000 ft / 9150 m
Cabin Altitude
@ 25,000 ft:
8000 ft / 2440 m
Cabin Altitude
@ 30,000 ft:
10,000 ft / 3050 m
   
Max. Cruise Speed: 270 KTAS
(502 kph, 400 mph)
Takeoff Ground Roll (MTOW): 1480 ft /  450 m
Landing Ground Roll (MTOW): 920 ft / 280 m
Rate of Climb (MTOW): 1680 ft/min
Stall Speed
(landing config.)
65 KCAS

Download your own flight-aid airplane.
Download your own flight-aid airplane. 

...and our 'PC-12' fact file