Beechcraft Denali vs Pilatus PC-12

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Beechcraft Denali
54 ft × 49 ft ⭥ 15 ft
1× Turboprop Retractable Pressurized
Pilatus PC-12
53 ft × 47 ft ⭥ 14 ft
1× Turboprop Retractable Pressurized

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.

Mission Performance

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

Mission performance specifications
Specification Beechcraft DenaliPilatus PC-12
Stall speed —93 kt
Approach speed 85 kt90 kt
Cruise speed 285 kt270 kt
Range 1600 nm1600 nm
Service ceiling 31000 ft30000 ft
Rate of climb —2000 fpm
Fuel burn —76.0 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.

Fuel Burn & Range

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

Beechcraft Denali Jet A
—

No fuel-burn estimate available.

Beechcraft Denali: no fuel-burn estimate available.
Pilatus PC-12 Jet A
76.0 gph
Baseline
1,600 nm range 3.6 nm/gal 402 gal usable $456 fuel/hr 5h 17m endurance
Pilatus PC-12: 76.0 gph at cruise, 1,600 nautical mile published range, 5 hour 17 minute endurance, 3.6 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed tank-dry · at this cruise burn

Bars show published still-air range: select a cell to view cruise-hours and fuel usage. Endurance is full tank at the displayed cruise burn rate; the extra is reserve and economy margin. 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

Takeoff over 50 ft obstacle

Landing over 50 ft obstacle

Density Altitude

Monte cristo

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

Hourly direct and annual fixed costs

Scale:
Beechcraft Denali Jet A
— /hr
Baseline
No operating-cost estimate available
Pilatus PC-12 Jet A
$1,106 /hr
Baseline
Pilatus PC-12: $1,106 per flight hour — fuel $456, maintenance and reserve $650.
Beechcraft Denali Turboprop
— /yr Baseline
No fixed-cost estimate available
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.

Estimates only. Hourly direct operating cost, based on fuel price and reserves; Annual fixed costs (insurance, hangar, and inspection). Costs vary by location, pilot profile, and market conditions.

Capability & limits

Payload vs useful load limit

+ cargo
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1
Beechcraft Denali Turboprop
11 seats — fuel — useful — MTOW
Pilatus PC-12 Turboprop
11 / 11 seats cargo 402 gal / 402 gal fuel 907 lbs wet payload 3,600 lbs useful 9,921 lbs MTOW

Shows selected occupants against full fuel, within the aircraft's useful-load limit. Fuel weight at 6.7 lb/gal jet-A, 6.0 lb/gal avgas; pax and luggage are 190 + 30 . Change payload weights in global settings.

Payload-Range Map

Origin: → · two fingers to move map

+ cargo
×
1

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