Pilatus PC-12/47

Pilatus Aircraft

ICAOPC12
Pilatus PC-12/47 aircraft
Pilatus AircraftPilatus PC-12/47
Photo: Alan Wilson from Peterborough, Cambs, UK · CC BY-SA 2.0 · Modified

About

The /47 reaches 4,740 kg take-off weight, and is the first PC-12 whose landing weight is lower than its take-off weight — 4,500 kg, so it can no longer turn straight round at maximum weight. The cruise speed, range, ceiling, climb rate and take-off distance are EUROCONTROL's figures for the PC12 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

4,760kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

4,740kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

4,500kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

4,100kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

9passengers
0
100
132

7% of A318 maximum capacity

Crew

Total
1
Cockpit
1

Dimensions

Length

14.4m

Wingspan

16.3m

Height

4.3m

Wing Area

25.8m²

Engine Specifications

Engine Count

1×

Engine Model

Pratt & Whitney Canada PT6A-67B turboprop

Fuel & Cargo

Fuel Capacity

1,522 L

Production & History

Production Status

Out of production

Business jets and the API are coming

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