Quest Kodiak

Turboprop • single engine • High Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Performance
183
KTAS
Cruise Speed
10
Occupants
1132
nm
Max Range
1391
lbs
Wet Payload

Estimated Ownership Costs

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About the Quest Kodiak

Overview

The Daher Kodiak 100 is a clean-sheet utility turboprop designed from the start for rugged, short-field operations, originally built by Quest Aircraft and produced under Daher since the 2019 acquisition. Unlike competitors adapted into the bush role, the Kodiak was engineered for humanitarian and backcountry operations, with a discontinuous leading-edge wing that preserves aileron authority and stall resistance at low speed. A 750-shp Pratt & Whitney PT6A-34 turns it into a STOL hauler that lifts a full cabin off short, unimproved strips.

For the GA buyer, the Kodiak 100 is the affordable end of the new-turboprop market and a genuine go-anywhere single. It carries over 3,500 lb of useful load through a large clamshell cargo door, runs a Garmin G1000 (G1000 NXi on Series II and III airframes), and operates from runways under 1,000 feet at gross weight. It cruises at up to 183 KTAS, slower than retractable turboprops, which is the price of its fixed gear and field performance.

Key Features for GA Buyers

  • Purpose-built STOL wing. The discontinuous leading edge holds aileron authority into the stall, and the airframe takes off in under 1,000 feet at maximum gross weight.
  • 750-shp PT6A-34. The Pratt & Whitney turbine carries a 4,000-hour TBO.
  • 3,500-lb useful load. A large clamshell cargo door and removable seating let the cabin convert between passengers and freight.
  • G1000 NXi avionics. Series II and III airframes carry the NXi suite with full IFR capability and synthetic vision.

Trade-offs

  • Fixed-gear drag. The robust fixed gear caps cruise speed well below retractable-gear turboprops like the TBM or PC-12.
  • Unpressurized. The 25,000-foot ceiling is academic without pressurization; practical cruise stays low enough to limit supplemental-oxygen use, and the airplane works weather rather than climbing over it.
  • Slower than retractable singles. At up to 183 KTAS the Kodiak trades block speed for field capability, so it loses to faster singles on long cross-country legs.
  • Cabin refinement. The utility focus means a plainer cabin environment than the stretched Kodiak 900 or the cabin-class PC-12.

See Also

Technical Specifications

Dimensions

Wingspan
45.0 ft
Length
34.17 ft
Height
15.25 ft
Parking area (ft2)
2154.35 ft2

Weights

Max Takeoff Weight
7,255 lbs
Max Landing Weight
7,255 lbs
Useful Load
3,535 lbs
Fuel Capacity
320 gal

Performance

Cruise Speed
183 KTAS
Never-Exceed (Vne)
182 KIAS
Max Structural Cruise (Vno)
182 KIAS
Approach Speed
74 KIAS
Stall, Clean (Vs1)
77 KIAS
Range
1132 NM
Service Ceiling
25,000 ft
Rate of Climb
867 - 1371 fpm
Takeoff over 50 ft obstacle
934 ft
Landing ground roll
705 ft

Engine

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