Daher Kodiak 900 vs Pilatus PC-12

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Daher Kodiak 900
45.0 × 37.7 ft 16.1 ft tall
1× Turboprop Fixed Unpressurized
Pilatus PC-12
53.2 × 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 Daher Kodiak 900Pilatus PC-12
Stall speed 78 kt67 kt
Approach speed 85 kt90 kt
Cruise speed 210 kt270 kt
Range 1129 nm1600 nm
Service ceiling 25000 ft30000 ft
Rate of climb 1724 fpm2000 fpm
Fuel burn 58.0 gph66.0 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.

Daher Kodiak 900 Jet A
58.0 gph
Baseline
1,129 nm range 322 gal usable 3.6 nm/gal $348 fuel/hr 5h 33m endurance
Daher Kodiak 900: 58.0 gallons per hour at cruise, 1,129 nautical mile published range, 5 hour 33 minute endurance, 3.6 nautical miles per gallon.
Pilatus PC-12 Jet A
66.0 gph
Baseline
1,600 nm range 402 gal usable 4.1 nm/gal $396 fuel/hr 6h 05m endurance
Pilatus PC-12: 66.0 gallons per hour at cruise, 1,600 nautical mile published range, 6 hour 5 minute endurance, 4.1 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:
$667 /hr
Baseline
Daher Kodiak 900: $667 per flight hour — fuel $348, maintenance and reserve $319.
$1,130 /hr
Baseline
Pilatus PC-12: $1,130 per flight hour — fuel $396, maintenance and reserve $734.
$27,868 /yr Baseline
Daher Kodiak 900: $27,868 per year — insurance $14,800, hangar $10,568, annual inspection $2,500.
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. 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.

190 + 30 lb Occupants
×
1
Daher Kodiak 900
10 / 10 seats 322 / 322 gal fuel 1,473 lb wet payload 3,630 lb useful 8,000 lb MTOW
Pilatus PC-12
9 / 9 seats 402 / 402 gal fuel 907 lb wet payload 3,600 lb useful 9,921 lb MTOW

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

Payload-Range Map

Full fuel ← → Max payload

Origin: · two fingers to move map

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