Kodiak 900

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

210
KTAS
Cruise Speed
10
Occupants
1129
nm
Max Range
1473
lbs
Wet Payload

Estimated Ownership Costs

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About the Kodiak 900

Overview

The Kodiak 900 is a significant evolution of the rugged Kodiak 100, offering a 3.9-foot fuselage stretch and a substantial power boost via the 900-shp Pratt & Whitney PT6A-140A. While it retains the legendary Short Takeoff and Landing (STOL) heritage of its predecessor, the 900 is refined for the owner-pilot and corporate market, featuring a ‘Summit+’ executive interior and a 210-knot cruise speed that makes it a viable cross-country machine.

Key Features for GA Buyers

  • Versatility: Transition from a 10-seat executive transport to a massive cargo hauler in minutes thanks to track-mounted, removable seating.
  • Modern Avionics: Standard Garmin G1000 NXi suite with GFC 700 autopilot, Synthetic Vision, and PlaneSync™ technology for a connected cockpit experience.
  • STOL Performance: Maintains the ability to operate out of unimproved strips under 1,500 feet, even with the larger airframe.
  • Refined Cabin: Significantly improved environmental control systems (dual-zone heating/cooling) and better soundproofing than the utility-focused Series III.

Trade-offs

  • Not Pressurized: Despite the executive feel and 25,000 ft service ceiling, the aircraft is unpressurized, requiring oxygen for high-altitude flight.
  • Speed vs. Competitors: While faster than the Kodiak 100, it is still outpaced by Daher’s TBM series or the Pilatus PC-12.
  • Fixed Gear Drag: The fixed landing gear (even with aerodynamic fairings) limits top-end efficiency compared to retractable turboprops.

Technical Specifications

Dimensions

Wingspan
45.0 ft
Length
37.7 ft
Height
16.1 ft

Weights

Max Takeoff Weight
8,000 lbs
Max Landing Weight
7,900 lbs
Useful Load
3,630 lbs
Fuel Capacity
322 gal

Performance

Cruise Speed
210 KTAS
Range
1129 NM
Service Ceiling
25,000 ft
Rate of Climb
1273 - 1724 fpm

Engines

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