Daher Kodiak 100

Turboprop single engine • High Wing • Fixed gear

Range Map

Origin:

nm at current load

• two fingers to move map

Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lb + lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

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.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • High-Performance
174
KTAS
Cruise Speed
1,132
nm
Max Range
25,000
ft
Service Ceiling
9
Occupants
1391
lbs
Wet Payload
In production Aircraft available new or used

Estimated Ownership Costs

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About the Daher Kodiak 100

Type certificated 2007 Source: FAA Type Certificate Data Sheet

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 174 KTAS, slower than retractable turboprops, which is the price of its fixed gear and field performance. Choose the Kodiak 100 when the mission is rough-field access and payload on a working budget, and the runway is short or unimproved.

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 174 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 & Weights

Wingspan 45.0 ft
Height
Source: FAA Type Certificate Data Sheet 14.7 ft
Length
34.17 ft
Parking area (ft2)
2154.35 ft2
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 7,255 lbs
Max Landing Weight
7,255 lbs
Useful Load
3,535 lbs
Fuel Capacity
320 gal

Performance

Cruise Speed
Source: manufacturer figure 174 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 182 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 182 KIAS
Approach Speed
74 KIAS
Stall, Clean (VS1)
Source: manufacturer figure 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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