Specifications
Aircraft Details
- Model: DAHER KODIAK 100 SERIES I
- Engine: PT6A-34, 750 SHP
- Propeller: Hartzell 3-blade, constant speed
- Max Takeoff Weight: 3,402 kg (7,485 lbs)
- Payload Capacity: 1,134 kg (2,500 lbs)
- Range: 1,200 nautical miles
- Cruise Speed: 150 knots
- Cabin: Spacious cabin with seating for up to 10 passengers
- Avionics: Equipped with advanced Garmin G1000 system
- Landing Gear: Tricycle landing gear with large tires for rough terrain
- Fuel Capacity: 1,200 lbs
- Safety Features: Equipped with modern safety systems and emergency equipment
The listing implies co-ownership or fractional sale due to the nature of the aircraft's availability and typical market practices.
About this Model
Overview
The Kodiak 100 Series I is a fixed-gear, single-engine turboprop designed around practical utility: short and unimproved runway capability, straightforward loading, and predictable handling at low speeds. It is commonly configured for commuter-style seating, mixed passenger/cargo layouts, or high-cycle special-mission work where dispatch reliability and field performance matter more than cruise speed or a pressurized cabin.
Mission Fit
This model fits operators who need consistent access to constrained airports and backcountry strips while carrying meaningful payload. It is most effective on regional stage lengths where takeoff/landing performance and turn-time drive schedule. If typical routes routinely demand higher cruise speeds, higher-altitude comfort, or long legs with larger reserves, a faster pressurized turboprop or light jet may align better.
Cabin
Cabin experience is utilitarian and mission-driven. Interiors vary widely, from higher-density seating to executive-style layouts, and many aircraft are equipped with durable materials to tolerate frequent loading and field conditions. Large doors and a practical cabin volume support quick passenger flow and cargo handling, but noise levels and ride comfort are closer to working turboprop norms than to pressurized business aircraft.