Pilatus PC-12 vs Pilatus PC-12 NGX

Side-by-side specs, range, and operating costs.

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Pilatus PC-12
53.2 × 47.2 ft 14.0 ft tall
1× Turboprop Retractable Pressurized
Pilatus PC-12 NGX
53.3 × 47.2 ft 14.0 ft tall
1× Turboprop Retractable Pressurized

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification Pilatus PC-12Pilatus PC-12 NGX
Stall speed 93 kt95 kt
Approach speed 90 kt—
Cruise speed 270 kt290 kt
Range 1600 nm1803 nm
Service ceiling 30000 ft30000 ft
Rate of climb 2000 fpm1920 fpm
Fuel burn 76.0 gph77.0 gph

Each axis is scaled independently across the compared aircraft and printed in its own units; every vertex sits at the published figure. Higher is better on all axes: Stall, Approach and Fuel Burn are inverted (lower = higher). A missing figure breaks the line at that axis.

Flight Profile

Service ceiling, range, and climb rate.

Tap legend to isolate

Arc represents the climb-cruise-descent profile based on published service ceiling and range. Climb rate annotated on ascent. FL180 (18,000 ft) shown for reference.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

Pilatus PC-12 Jet A
76.0 gph
Baseline
1,600 nm range 402 gal usable 3.6 nm/gal $456 fuel/hr 5h 17m endurance
Pilatus PC-12: 76.0 gallons per hour at cruise, 1,600 nautical mile published range, 5 hour 17 minute endurance, 3.6 nautical miles per gallon.
Pilatus PC-12 NGX Jet A
77.0 gph
Baseline
1,803 nm range 402 gal usable 3.8 nm/gal $462 fuel/hr 5h 13m endurance
Pilatus PC-12 NGX: 77.0 gallons per hour at cruise, 1,803 nautical mile published range, 5 hour 13 minute endurance, 3.8 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range. Endurance is usable fuel divided by the published cruise burn. Estimates only. Always verify against the POH.

Runway Performance

Density altitude adjusted estimates

Outside Air Temp
0°F57°F115°F
Field Elevation
SL4,0008,000 ft
Density Altitude

Takeoff over 50 ft obstacle

Landing ground roll

Base distance DA penalty
Scale: 6,000 ft

FAA 10%/1,000 ft DA rule of thumb (FAA-H-8083-25B). Turboprops and jets are less sensitive in practice. Always verify against the POH.

Estimated Operating Costs

Scale:
Pilatus PC-12 Jet A
$1,106 /hr
Baseline
Pilatus PC-12: $1,106 per flight hour — fuel $456, maintenance and reserve $650.
Pilatus PC-12 NGX Jet A
$1,130 /hr
Baseline
Pilatus PC-12 NGX: $1,130 per flight hour — fuel $462, maintenance and reserve $668.
Pilatus PC-12 Turboprop
$59,500 /yr Baseline
Pilatus PC-12: $59,500 per year — insurance $22,000, hangar $35,000, annual inspection $2,500.
Pilatus PC-12 NGX Turboprop
$72,100 /yr Baseline
Pilatus PC-12 NGX: $72,100 per year — insurance $28,000, hangar $41,600, annual inspection $2,500.

Estimates only. Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Each bar stacks your selected occupants against full fuel and the aircraft's useful-load limit (the black line). The open gap between them is spare payload. Add an occupant and the gap closes; once it's gone, fuel has to give.

lb

+ lb / pax

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1
Pilatus PC-12
11 / 11 seats 402 / 402 gal fuel 907 lb wet payload 3,600 lb useful 9,921 lb MTOW
Pilatus PC-12 NGX
11 / 11 seats 402 / 402 gal fuel 975 lb wet payload 3,668 lb useful 10,450 lb MTOW

Occupants at 190 + 30 lb each. Fuel at 6.7 lb/gal jet-A, 6.0 lb/gal avgas.

Payload-Range Map

Origin: · two fingers to move map

lb

+ lb / pax

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1

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