Specifications
AI Description
- Model: KODIAK 900
- Condition: New
- Flight Rules: IFR
- Airframe Features:
- Air Conditioning
- 10-Place Oxygen System
- Single-point Refueling
- External Cargo Compartment
- Cargo Door Width: 49.25 inches
- Engine:
- Make/Model: Pratt & Whitney Canada PT6A-140
- Horsepower: 900
- Time Between Overhaul (TBO): 4,000 hours
- Propeller:
- Type: Hartzell 5-Blade Composite Propeller
- Avionics:
- Manufacturer/Model: Garmin G1000 NXi
- ADS-B Equipped: Yes
- WAAS: Yes
- Synthetic Vision Technology (SVT): Yes
- Dual VOR/ILS and GPS Receivers
- GTX 345R Mode-S Transponder (ADS-B In/Out)
- GFC 700 Autopilot with various features
- Class-B Terrain Awareness and Warning System
- Additional Equipment:
- Flight Into Known Icing (FIKI): Yes
- Optional Garmin GWX 75 Weather Radar
- Interior:
- Summit+ Interior with 6 club seats
- Non-slip flooring or carpet
- LED Lighting, AC Control, USB Charging Ports
- Exterior: Customizable schemes and colors available.
About this Model
Overview
The DAHER Kodiak 900 is a fixed-gear, single-engine turboprop built around backcountry/utility missions—carrying people and cargo into shorter, rougher strips than typical business-oriented turboprops. Compared with earlier Kodiak variants, the 900 emphasizes more cruise speed and mission efficiency while retaining high-lift, STOL-oriented handling and a large, flexible cabin. It is commonly configured for mixed passenger/cargo work, remote access flying, and specialized roles where runway quality and infrastructure are limited.
Mission Fit
Mission planning typically centers on short-field performance, payload/cabin flexibility, and the ability to operate with minimal ground support. It suits operators who value getting in and out of constrained strips and moving real payload rather than maximizing cruise altitude and speed. As a non-pressurized, single-engine platform, it is less aligned with missions that prioritize high-altitude weather avoidance, airline-style climb profiles, or maximum cruise comfort over longer legs.
Cabin
The cabin is designed for utility: a relatively tall, boxy cross-section, durable interior choices, and straightforward access that supports quick turns between passenger and cargo tasks. Seating is commonly arranged for multiple passengers with club or forward-facing layouts depending on operator needs, but the core value is modularity—removing or reconfiguring seats for freight, equipment, or mission kits. Noise, vibration, and temperature management depend heavily on interior specification and mission profile, with comfort typically prioritized less than capability and payload flexibility.