Specifications
Aircraft Details
• Approximately 36 hours total time as of May 2026; delivered new January 2026, one-owner, hangared since new, no damage history
• Latest Model Year 2025 upgrades, including full WAT lighting, Garmin G1000 NXi suite with PlaneSync GDL 60 4G/Wi-Fi, GWX 8000 StormOptix weather radar, GTS 800 traffic advisory, GDL-69A-XM datalink with audio, GRA 55 radar altimeter, MD 302 digital backup display (no whiskey compass)
• Powered by PT6A-140A engine (900 SHP) with Hartzell 5-blade composite propeller; enrolled in Pratt & Whitney Extended Engine Support Program (5-year/2,500 hr warranty extension, TBO up to 6,000 hrs, FAST Box telemetry)
• Full FIKI-certified TKS ice protection with removable cargo-pod tank, single-point high-pressure refueling, 322 US gal fuel capacity, vinyl coin-dot utility flooring, Ebony black Summit interior (2 crew + 6 passenger seats), 10-place oxygen system, air conditioning, 8 USB ports, 8 cup holders, 3 fire extinguishers
• Custom factory paint: deep blue with vibrant yellow accent stripe over white; HID landing lights, LED taxi/nav/strobe/beacon lights, wheel pant fairings, large cargo door
• Located in Orange County, CA, available for immediate delivery; first annual inspection due Jan 2027, no open squawks
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.