Pilatus PC-12

 

 

Pilatus PC-12 Reference List

 

 

 

 

PC-12 POWER PLANT

 

Pratt & Whitney Canada PT6A-67B

Thermodynamic power 1,605 SHP

Take-off power (flat-rated) 1,200 SHP

Climb/Cruise Power 1,000 SHP

Specific fuel consumption 0.538 lb/SHP/hr

TBO 3,500 hrs

Propeller, constant speed 4 Blade, Hartzell Al

Propeller speed 1700 RPM

 
 

 

 

 

 

 

 

 

 

 

 

 

PC-12 PERFORMANCE

 

Maximum Cruise Speed 270 KTAS

Maximum Operating Altitude 30,000 FT

Maximum range at 30,000 FT 2,261 NM

Rate of climb at sea level 1,680 FPM

Cabin altitude at 25,000 FT 8,000 FT

Take-off distance, 50 FT 1,830 FT

Landing distance, 50 FT 1,830 FT

Maximum crosswind component:

Flaps 00 30 KTS

Flaps 400 15 KTS

Stall speed, flaps 400 64 KIAS

 

 

PC-12 WEIGHTS AND CAPACITIES

 

Maximum ramp weight 9,965 LBS

Maximum take-off weight 9,920 LBS

Maximum landing weight 9,920 LBS

Basic operating weight 6,400 LBS

Zero fuel weight 9,040 LBS

Maximum payload w/full fuel 3,108 LBS

Useful load 4,233 LBS

Usable fuel 402 US GAL

Oil capacity 2.9 US GAL

 

 
 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

PC-12 RECOMENDED AIRSPEEDS

 

VMO (maximum operating) 240 KIAS

VNE (never exceed) 236 KIAS

VD (maximum diving speed) 280 KIAS

VRE (rotation) 80 KIAS

Vx (best angle of climb) 110 KIAS

VY (best rate of climb) 120 KIAS

VCLIMB (climb airspeeds)

0 160 KIAS

15,000 150 KIAS

20,000 140 KIAS

25,000 130 KIAS

30,000 115 KIAS

VA (design manuvering) 158 KIAS

VFE (maximum 150 flaps) 163 KIAS

VLE (maximum gear extended) 236 KIAS

VLO (maximum gear operating) 177 KIAS

VSI (stall, clean) 86 KIAS

VSO (stall, landing configuration) 60 KIAS