This information is for REFERENCE ONLY and is not to be used in flight. The Pilot in Command (PIC) is responsible for the safe and proper operation of their aircraft.
We strive to be as accurate as possible throughout this website. However, in no way should the information provided supersede the aircraft’s operating handbook, aircraft’s maintenance manuals or appropriate reference material.
pc-12 dimensions |
Renderings 
|
|||||||
ENGINE VARIATIONS |
PT6A-67B v. 67P
|
|||||||
PROPELLER SPECIFICATIONS |
Hartzell HC-E4A
|
|||||||
factory specifications |
||||||||
| POWER PLANT | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
 |
||||||||
| Pratt & Whitney (Canada) | PT-6A-67B | PT-6A-67B | PT-6A-67B | PT-6A-67P | ||||
| Thermodynamic Power | 1605 SHP | 1605 SHP | 1605 SHP | 1744 SHP | ||||
| Takeoff Power (Flat Rated) | 1200 SHP* | 1200 SHP* | 1200 SHP* | 1200 SHP* | ||||
| Climb | 1000 SHP* | 1000 SHP* | 1000 SHP* | 1200 SHP* | ||||
| Cruise | 1000 SHP* | 1000 SHP* | 1000 SHP* | 1000 SHP* | ||||
| Specific Fuel Consumption | 0.53 lb/SHP/hr | 0.53 lb/SHP/hr | 0.53 lb/SHP/hr | 0.54 lb/SHP/hr | ||||
| TBO Section Interval | 3500 hours | 3500 hours | 3500 hours | 3500 hours | ||||
| HOT Section Interval | 1750 hours | 1750 hours | 1750 hours | 1750 hours | ||||
| * above sea level | ||||||||
| PROPELLER | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Hartzell | 4 Blade Aluminum | 4 Blade Aluminum | 4 Blade Aluminum | 4 Blade Aluminum | ||||
| Type | Constant Speed, Full Reverse | Constant Speed, Full Reverse | Constant Speed, Full Reverse | Constant Speed, Full Reverse | ||||
| Model: Hub | HC-E4A-3D | HC-E4A-3D | HC-E4A-3D | HC-E4A-3D/E | ||||
| Model: Blades | E10477K | E10477K | E10477K | E10477K | ||||
| Model: Spinner | D 5500-1 | D 5500-1 | D 5500-1 | D 5500-1 | ||||
| Diameter | 8 ft. 9 in. | 8 ft. 9 in. | 8 ft. 9 in. | 8 ft. 9 in. | ||||
| Propeller Speed | 1700 rpm | 1700 rpm | 1700 rpm | 1700 rpm | ||||
| Propeller Clearence | 12.5 in.* | 12.5 in.* | 12.5 in.* | 12.5 in.* | ||||
| * can depend on configurations | ||||||||
| FUEL TYPE / CAPACITY | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Fuel Type | Jet A / Jet A-1 / Jet B / JP4 |
Jet A / Jet A-1 / Jet B / JP4 |
Jet A / Jet A-1 / Jet B / JP4 |
Jet A / Jet A-1 / Jet B / JP4 |
||||
| Usable Fuel: No Serial # Variation | 402 US gal / 1522 L |
402 US gal / 1522 L |
402 US gal / 1522 L |
|||||
| Useable Fuel: Serial #101-140 | 400.4 US gal / 1515 L | |||||||
| Useable Fuel: Serial #141-higher | 402 US gal / 1522 L | |||||||
| Fuel in lbs / kgs: No Serial # Variation | 2704 lbs / 1226 kgs | 2704 lbs / 1226 kgs | 2704 lbs / 1226 kgs | |||||
| Fuel in lbs / kgs: Serial #101-140 | 2609 lbs / 1183 kgs | |||||||
| Fuel in lbs / kgs: Serial #141-higher | 2704 lbs / 1226 kgs | |||||||
| EXTERIOR DIMENSIONS | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Wing Span | 53 ft. 3 in. | 53 ft. 3 in. | 53 ft. 3 in. | 53 ft. 3 in. | ||||
| Length | 47 ft. 3 in. | 47 ft. 3 in. | 47 ft. 3 in. | 47 ft. 3 in. | ||||
| Height | 14 ft. 0 in. | 14 ft. 0 in. | 14 ft. 0 in. | 14 ft. 0 in. | ||||
| Horizontal Tail Span | 17 ft. 1 in. | 17 ft. 1 in. | 17 ft. 1 in. | 17 ft. 1 in. | ||||
| INTERIOR DIMENSIONS | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Cabin Length* | 16 ft. 11 in. | 16 ft. 11 in. | 16 ft. 11 in. | 16 ft. 11 in. | ||||
| Cabin Width | 5 ft. 0 in. | 5 ft. 0 in. | 5 ft. 0 in. | 5 ft. 0 in. | ||||
| Cabin Floor Width | 4 ft. 3 in. | 4 ft. 3 in. | 4 ft. 3 in. | 4 ft. 3 in. | ||||
| Cabin Height | 4 ft. 9 in. | 4 ft. 9 in. | 4 ft. 9 in. | 4 ft. 9 in. | ||||
| Cabin Volume* | 330 cu. ft. | 330 cu. ft. | 330 cu. ft. | 330 cu. ft. | ||||
| Baggage Compartment Volume | 40 cu. ft. | 40 cu. ft. | 40 cu. ft. | 40 cu. ft. | ||||
| Forward Cabin Door | 2 ft. 1 in. x 4 ft. 5 | 2 ft. 1 in. x 4 ft. 5 | 2 ft. 1 in. x 4 ft. 5 | 2 ft. 1 in. x 4 ft. 5 | ||||
| Cargo Door | 4 ft. 5 in. x 4 ft. 4 | 4 ft. 5 in. x 4 ft. 4 | 4 ft. 5 in. x 4 ft. 4 | 4 ft. 5 in. x 4 ft. 4 | ||||
| Emergency Exit | 1 ft. 7 in. x 2 ft. 2 | 1 ft. 7 in. x 2 ft. 2 | 1 ft. 7 in. x 2 ft. 2 | 1 ft. 7 in. x 2 ft. 2 | ||||
| * cockpit / cabin bulkhead to rear pressure bulkhead | ||||||||
| WING AREA / WING LOAD | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Wing Area | 277.8 ft. | 277.8 ft. | 277.8 ft. | 277.8 ft. | ||||
| Wing Loading | 35.7 lb / sq.ft. | 35.7 lb / sq.ft. | 35.7 lb / sq.ft. | 35.7 lb / sq.ft. | ||||
| Power Loading | 8.2 lb / shp | 8.2 lb / shp | 8.2 lb / shp | 8.2 lb / shp | ||||
| PRESSURIZATION | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Differential | 5.75 | 5.75 | 5.75 | 5.75 | ||||
| Cabin Altitude at 25,000 feet | 8000 ft. | 8000 ft. | 8000 ft. | 8000 ft. | ||||
| Cabin Altitude at 30,000 feet | 10,000 ft. | 10,000 ft. | 10,000 ft. | 10,000 ft. | ||||
| Maximum Certified Altitude | 30,000 ft. | 30,000 ft. | 30,000 ft. | 30,000 ft. | ||||
| WEIGHTS | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Maximum Ramp Weight | 9040 lbs / 4100 kgs |
9965 lbs / 4520 kgs |
10,495 lbs / 4760 kgs |
10,495 lbs / 4760 kgs |
||||
| Maximum Take Off Weight | 9040 lbs / 4100 kgs |
9920 lbs / 4500 kgs |
10,450 lbs / 4740 kgs |
10,450 lbs / 4740 kgs |
||||
| Maximum Landing Weight | 9040 lbs / 4100 kgs |
9920 lbs / 4500 kgs |
9920 lbs / 4500 kgs |
9920 lbs / 4500 kgs |
||||
| TAKE OFF / LANDING DATA | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| Take Off: Max Weight, Sea Level | |
|||||||
| (ISA / No Wind) | ||||||||
| Take Off Distance: Over 50' Obstacle* | N/A Flaps 30 | 2300 ft. | 2650 ft. | 2650 ft. | ||||
| Take Off: Ground Roll* | N/A Flaps 30 | 1350 ft. | 1450 ft. | 1450 ft. | ||||
| * 30 degress of flaps | ||||||||
| Landing: Max Weight, Sea Level | |
|||||||
| ISA / No Wind, No Reverse | 1100 ft. | 1250 ft. | 1250 ft. | 1250 ft. | ||||
| Landing Distance: Over 50' Obstacle* | 1700 ft. | 1830 ft. | 1830 ft. | 1830 ft. | ||||
| Landing Ground Roll* | 820 ft. | 945 ft. | 945 ft. | 945 ft. | ||||
| * 40 degress of flaps, with reverse | ||||||||
| AIRSPEEDS | PC-12 / 41 | PC-12 / 45 | PC-12 / 47 | PC-12 / 47 NG | ||||
|
||||||||
| VMO (Maximum Operating) | 240 KCAS | 240 KCAS | 240 KCAS | 240 KCAS | ||||
| VNE (Never Exceed) | 236 KIAS | 236 KIAS | 236 KIAS | 236 KIAS | ||||
| VD (Maximum Dive Speed) | 280 KIAS | 280 KIAS | 280 KIAS | 280 KIAS | ||||
| VR (Rotation) | 78 KIAS | 79 KIAS | 81 KIAS | 82 KIAS | ||||
| VX (Best Angle of Climb) | 110 KIAS | 110 KIAS | 110 KIAS | 120 KIAS | ||||
| VY (Best Rate of Climb) | 120 KIAS | 120 KIAS | 120 KIAS | 130 KIAS | ||||
| VA (Design Maneuvering) | 151 KIAS | 158 KIAS | 163 KIAS | 163 KIAS | ||||
| VFE (Maximum 15 Degree Flaps) | 163 KIAS | 163 KIAS | 163 KIAS | 165 KIAS | ||||
| VLE (Maximum Gear Extended) | 236 KIAS | 236 KIAS | 236 KIAS | 240 KIAS | ||||
| VLO (Maximum Gear Operating) | 177 KIAS | 177 KIAS | 177 KIAS | 180 KIAS | ||||
| VSI (Stall; Clean) | 86 KIAS | 91 KIAS | 93 KIAS | 93 KIAS | ||||
| VSO (Stall; Landing Configuration) | 59 KIAS | 64 KIAS | 66 KIAS | 66 KIAS | ||||
