Specifications and Aircraft Details - MSN 297 and 644

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Features, Capabilities, and Options:

Customized for any mission system:

• ISR systems, including EO/IR up to dual 25" diameter class • Wide Area Motion Imagery (WAMI) sensors • SIGINT/COMINT/ELINT • Radar: Multi-mode surveillance, AESA, SAR/ISAR/SLAR, GMTI, Weather etc. • Automatic identification system (AIS) • Lidar, Multi-Spectral, RF, and Microwave sensors • New Communication systems testing (Satellite BLOS communications, RF alternative, LOS Data link, etc.) • Command and Control/Wildfire management • Racks, consoles, and mission seating • We provide DESIGN-BUILD-FLY solutions

• Short Takeoff & Landing (STOL) • Stable high-wing flight characteristics • Ideal aircraft for sensors needing slow loitering speeds • Unpressurized cabin with Crew and Passenger Oxygen systems allowing a 25,000 ft. ceiling • "Best-in-Class" payload capabilities • Increased MTOW to 14,000 lbs. (Restricted or Standard category STC) • Roomy cabin for mission crew and equipment • 500 amps of engine driven electrical power • Supplemental APU power • Ram Air and supplemental cooling • Enlarged, observation, removable, and special windows • Special modifications for sensor installation provisions: • Camera portals (single or dual) • Wing payload hard points • Fuselage antenna provisions • Airworthiness Certification and operation support as necessary

DHC-6 and TWIN OTTER are trademarks of Viking Air Limited

All data provided in this document is approximate, for discussion purposes only and may be subject to certain conditions. This document does not constitute an offer, commitment, representation, or warranty of any kind. All data 1s subject to change without prior written notice. Aircraft subject to prior sale.

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