Range Map

Origin: · two fingers to move map

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1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

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Mission Profile

Used market Only available used
270
KTAS
Cruise Speed
1,600
nm
Max Range
30,000
ft
Service Ceiling
11
Occupants
907
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Instrument
Pilatus PC-12/45 (N292P), Steelman Aviation, 2005. Photo: Tomas Del Coro, CC BY-SA 4.0.
Pilatus PC-12/45 (N292P), Steelman Aviation, 2005. Photo: Tomas Del Coro, CC BY-SA 4.0.

Estimated Ownership Costs

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About the Pilatus PC-12

Type certificated 1996

Overview

The Pilatus PC-12/45 is the second-series version of Switzerland’s single-engine turboprop, built from 1996 and the configuration that turned the PC-12 into the best-selling pressurised turboprop single of its era. It mates a Pratt & Whitney Canada PT6A-67B to a cavernous pressurised cabin with a standard rear cargo door, carrying up to nine passengers at a 30,000 ft cruise while still working the short, unimproved strips that close out comparable business aircraft.

For a buyer the /45 is the value way into the family: the same fuselage, cargo door, and rough-field utility as the current PC-12 NGX for a fraction of the acquisition cost, behind a deep used fleet and a worldwide service network. What it gives up is the NGX’s FADEC engine, winglets, and glass cockpit, in exchange for a legacy panel and slightly lower cruise, and like any turboprop single its resale lives and dies on engine condition and program status. It is the one to buy when you want real turboprop capability and a jet-sized cabin at the lowest cost of entry into the type.

Key Features for GA Buyers

  • Jet-class cabin and cargo. Cabin volume rivals a mid-size jet, and a standard 53 in aft cargo door swallows pallets, motorcycles, or stretchers; executive interiors seat six to nine in pressurised comfort.
  • Rough-field utility. Trailing-link gear and a strong wing let the /45 work from grass, gravel, and short runways, opening thousands of airfields a light jet cannot touch.
  • Single-engine economics. One PT6A burns far less than a comparable twin turboprop or light jet while still turning in 270 KTAS cruise and useful range.
  • Proven safety and support. Redundant systems, a slow 65 KCAS landing-configuration stall, and Pilatus’s global network underpin one of the strongest dispatch and safety records among owner-flown turbines.

Trade-offs

  • Single-engine acceptance. Some flight departments and insurers still want twin redundancy for night or overwater work, legendary as the PT6A-67B’s reliability is.
  • Legacy avionics. The /45 carries an earlier panel rather than the NGX’s Honeywell Advanced Cockpit Environment; an avionics upgrade is a common and worthwhile investment.
  • Speed. At 270 KTAS it is quick for a turboprop but slower than light jets like the Phenom 100 or Citation M2.
  • Heavy controls. Control feel, in roll especially, is firm; most owners fly behind the autopilot on the longer legs.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 53 ft
Height
14 ft
Length
47 ft
Parking area (ft²2)
3,305 ft²
Max Takeoff Weight
9,921 lbs
Max Landing Weight
9,921 lbs
Useful Load
3,600 lbs
Fuel Capacity
402 gal

Performance

Cruise Speed
270 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 240 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 240 KIAS
Approach Speed
90 KIAS
Stall, Clean (VS1)
Source: FAA Type Certificate Data Sheet 93 KIAS
Range
1600 NM
Service Ceiling
30,000 ft
Rate of Climb
2000 fpm
Takeoff over 50 ft obstacle
1,821 ft
Landing over 50 ft obstacle
1,837 ft

Engine

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Sources

Where the figures on this page come from. Pilatus PC-12 specifications are traced to published references; estimated values are flagged inline next to the figure.

Similar to the Pilatus PC-12

Similar Turboprops

Pilatus PC-12 NGX

Cruise
290 kts (higher than this aircraft)
Range
1803 nm (higher than this aircraft)
Seats
11
Compare

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