Indicative 2010 market price$3.6m (€3.33m) to $4.31m (€3.99m)
Estimated annual cost at 80 h$300k (€278k)
Five-year cash outlay$5.42m (€5.01m)

A Pilatus PC-12 NG costs approximately $3.6m (€3.33m) to $4.31m (€3.99m) to buy at 2010 market values, and about $300k (€278k) a year to own flying 80 hours, roughly $3,753 (€3,475) per flight hour all-in. It seats 10, cruises at 285 kt (328 mph) and has a published range of 1,845 nm (3,417 km), needing about 2,487 ft (758 m) of runway. Figures are indicative planning estimates compiled 2026-07, not a quote for any specific airframe.

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The PlaneFit verdict

The PC-12 NG is the previous-generation of the definitive single turboprop, and on the used market it offers the same versatile, pressurised, cabin-and-cargo-door capability that makes PC-12s so sought after, at a more accessible price than the NGX. It remains a superb do-everything aircraft. The costs are professional: interior condition, engine-programme coverage and high annual fixed costs mean it is priced and operated like the serious machine it is. Buyers who need the versatility and will use it get exceptional capability; the airframe rewards professional ownership, not casual utilisation.

Manufacturer-verified data

Extended technical specifications

First-party reference values for this model. They are shown separately from PlaneFit planning estimates and do not enter Finder or cross-model rankings until each field is normalised across the catalogue.

Maximum takeoff weight4,740 kg
Usable fuel1,522 L
Maximum operating altitude30,000 ft
EnginePratt & Whitney Canada PT6A-67P, 1,200 shp

Key figures

Indicative planning data, compiled 2026-07. Verify against the AFM and records.

Seats10
Realistic payload with mission fuel2,150 lb (975 kg)
Published planning range1,845 nm (3,417 km)
Practical planning radius (4 people)1,236 nm (2,289 km)
Cruise speed285 kt (328 mph)
Runway need~2,487 ft (758 m)
Landing gearRetractable tricycle
PressurisedYes
FuelJet A-1
Fixed annual base$167k (€155k)
Direct cost per flight hour$1,296 (€1,200)

The ownership trade-off

Exceptional cabin, payload and runway versatility, but interior, engine programme and high annual fixed costs demand professional ownership.

Cost picture at different usage

Indicative cash costs at 2010 market values, before financing, depreciation and tax. The fixed base is the same whether the aircraft flies or not, so the effective hourly cost falls as utilisation rises.

Annual useAnnual cash costEffective cost / hFive-year cash outlay
40 h / year$248k (€230k)$6,210 (€5,750)$5.16m (€4.77m)
80 h / year$300k (€278k)$3,753 (€3,475)$5.42m (€5.01m)
120 h / year$352k (€326k)$2,934 (€2,717)$5.67m (€5.25m)
180 h / year$430k (€398k)$2,388 (€2,211)$6.06m (€5.61m)

What the estimate covers

Every figure above is built from a $167k (€155k) fixed annual base, covering hangarage, insurance, scheduled maintenance reserves and recurring airworthiness costs, plus $1,296 (€1,200) per hour flown for fuel, reserves and consumables. It is a planning model for comparing aircraft and testing utilisation, not a maintenance programme quote, insurance quote or pre-buy assessment.

Older examples add calendar-driven maintenance: a 2011-built airframe is estimated at $295k (€274k) per year at 80 hours. Airframe and engine time, maintenance and damage history, avionics, equipment, geography and tax treatment move a real transaction further than the model year does, so price the aircraft in front of you, not the model. A cheaper example carrying deferred maintenance can be the more expensive aircraft once the first annual inspection is complete.

Pilatus PC-12 NG cost guide answers the same figures as standalone purchase and ownership questions, and the ownership cost calculator lets you replace these assumptions with your own hours and fixed costs.

Where it fits well

  • 285 kt (328 mph) cruise supports fast regional travel.
  • 1,845 nm (3,417 km) published range creates a practical planning radius of about 1236 nm with 4 occupants.
  • 2,150 lb (975 kg) realistic payload proxy and 10 seats define the usable cabin mission.

Limitations to price honestly

  • Exceptional cabin, payload and runway versatility, but interior, engine programme and high annual fixed costs demand professional ownership.
  • $167k (€155k) fixed annual planning base before flying a single hour.
  • Approximate 2,487 ft (758 m) take-off requirement must be checked against runway, surface, slope, temperature and loading.

Recommended missions

  • Family and small-group touring with a weight-and-balance check for every trip.
  • Longer regional missions, with reserves and payload reducing brochure range.
  • Time-sensitive business travel where dispatch reliability justifies the cost.

What you need to be qualified to fly a Pilatus PC-12 NG

On top of a pilot certificate, this aircraft obliges the person flying it to hold the following. Each one is time and money before the first trip, and insurers usually attach their own minimums on top.

  • Type rating, if it exceeds 12,500 lb. 14 CFR 61.31(a) requires a type rating for any airplane above 12,500 lb maximum takeoff weight. Most owner-flown turboprops sit below it and the cabin-class types sit above, so this is the line that separates a checkout from a formal type course. PlaneFit does not store maximum takeoff weight, so check this type's certificated weight rather than assuming either way.
  • Complex airplane endorsement. Retractable gear puts this aircraft in the complex class of 14 CFR 61.31(e), alongside flaps and a controllable-pitch propeller, which retractable types carry as a matter of course. It is a one-time instructor endorsement in your logbook, but the insurance condition behind it is the part that costs money: underwriters usually want a stated number of hours in retractable-gear aircraft before they will write the risk at standard rates.
  • High-altitude training, if it flies above 25,000 ft. 14 CFR 61.31(g) requires ground and flight training for a pressurised aircraft whose service ceiling or maximum operating altitude is above 25,000 ft. PlaneFit does not store service ceiling, so check this type's certified ceiling rather than assuming either way.

US requirements under 14 CFR 61.31, stated for orientation and not as advice. PlaneFit is not an aviation authority or a training organisation. Other authorities set different rules, and the current regulation and your instructor are what govern.

Common questions about the Pilatus PC-12 NG

How much does a Pilatus PC-12 NG cost?

An indicative 2010 market price for a Pilatus PC-12 NG is $3.6m (€3.33m) to $4.31m (€3.99m). This is a planning estimate normalised across the market, not a quote for a specific airframe. Condition, engine time remaining, avionics and damage history move the real number more than the model year does.

What does a Pilatus PC-12 NG cost per hour to operate?

Flying 80 hours a year, a Pilatus PC-12 NG works out at roughly $300k (€278k) annually, which is about $3,753 (€3,475) per flight hour all-in once fixed costs are spread across those hours. The direct cost per hour alone, covering fuel, reserves and consumables, is about $1,296 (€1,200).

How far can a Pilatus PC-12 NG fly?

Published range is 1,845 nm (3,417 km). With 4 people aboard and realistic reserves, plan on a practical radius of about 1236 nm rather than the brochure figure.

What do you need to be qualified to fly a Pilatus PC-12 NG?

Beyond a pilot certificate, a Pilatus PC-12 NG requires type rating, complex airplane endorsement and high-altitude training. 14 CFR 61.31(a) requires a type rating for any airplane above 12,500 lb maximum takeoff weight. Most owner-flown turboprops sit below it and the cabin-class types sit above, so this is the line that separates a checkout from a formal type course. PlaneFit does not store maximum takeoff weight, so check this type's certificated weight rather than assuming either way. These are US requirements and are stated for orientation; confirm them against the current regulation and an instructor.

What runway does a Pilatus PC-12 NG need?

Plan on approximately 2,487 ft (758 m) for take-off. Check this against the actual runway, surface, slope, temperature and loading, all of which extend the requirement.

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