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DAHER KODIAK 900(2025)

Specifications

Year2025
Serial Number
Registration
Total Hours500
LocationSANFORD, NORTH CAROLINA
RegionNORTH AMERICA

Broker

Aircraft Details

• Equipped with Summit+ Interior Package (6 black passenger seats with dual armrests)

• 2025 Executive Package included

• Garmin G1000 NXi flight deck with Synthetic Vision

• Full weather radar (GWX 8000 StormOptix™)

• TKS ice protection (Flight Into Known Icing - FIKI)

• Garmin PlaneSync™ with GDL 60 (4G/WiFi/Bluetooth)

• Garmin Central Maintenance Computer (CMC)

• MD 302 back-up display (two-screen) with MD32 remote magnetometer

• SurfaceWatch and ChartView

• GTS 800 TAS, GDL-69A-XM

• Professionally managed and flown, always hangared

• 145 total airframe and engine hours since new

• Pratt & Whitney PT6A-140 engine (TBO 5000 hours)

• 5-blade swept propeller

• External cargo compartment, single-point refueling, 10-place oxygen system, air conditioning

• Dual aft body strakes

• Currently in annual inspection, completion expected July 17th

• Includes initial or recurrent training for 1 pilot

• Based at KTTA, Sanford, North Carolina

• Glancing bird strike on top of right wing (noted)

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.