Specifications
Broker
DAHER KODIAK
AI Description
- Model: DAHER KODIAK 900
- Condition: New
- Range: 1,129 NM
- Max Ramp Weight: 8,100 lb
- Max Takeoff Weight: 8,000 lb
- Basic Empty Weight: 4,470 lb
- Useful Load: 3,630 lb
- Fuel Capacity: 322 gal
- Engine: PRATT & WHITNEY PT6A-140
- Engine Time: 0 SNEW
- Engine TBO: 4,000 hours
- Number of Propeller Blades: 5
- Avionics: GARMIN G1000 NXI
- Transponder: GARMIN GTX345R
- Autopilot: GARMIN GFC700
- ADS-B Equipped: Yes
- SVT (Synthetic Vision Technology): Yes
- Exterior Year Painted: 2026
- Interior Year: 2026
- Number of Seats: 6
- Location: Sandpoint, Idaho
- Limited positions available for purchase.
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.