AEVEX's demonstrator aircraft, MSN 297, is a testbed powerhouse equipped with the Vistaliner enlarged window modification, removable dual swing doors, dual sensor mounting provisions, wing hard points, supplemental cooling, mission console, operator seating, and enhanced mission electrical systems. Airframe: • Re-Life® Fuselage and Flight Controls (remaining life of 66,000 hours/132,000 cycles as of 3/7/2023) • Wing Box and Nacelles have remaining life of approximately 3,936.8 hours/15,169 cycles (This will be replaced with AEVEX Re-Life® Wing Boxes and Nacelles when due)
PT6A-34 Engines (as of 3/7/2022):
Propellers:
Right PS PCE-56605 29,142.7 Hrs. 111.2 Hrs. 40,479 89 111.2
Right GG PCE-57033 24,273.6 Hrs. 111.2 Hrs. 34,050 89 111.2
Left GG&PS PCE-56005 25,892.7 Hrs. 11,777.6 Hrs.
Serial Number: Time Since New: Time Since Overhaul: Cycles Since New: Cycles Since OH: TSHSI
Hartzell HC-B3TN-3D; 0 H C 3/7/2023
Left Right S/N: BUA24843 BUA27493
51,982 18,790
Aircraft Configuration Details:
• 14,000 lbs. MTOW Restricted Category STC; Empty Weight: 7,952 lbs. (Approx) • Total Fuel Capacity: 3,148 lbs. (allows a nominal 6.7 hrs. of loiter) • Two AEVEX High-Flow 250 Amp St-Generators with mission power cockpit control • AEVEX's enlarged aft camera portal (skin opening is 26.8" x 36.0") • Equipped with fixed support structure capable of supporting a 25" dia. Class EO/IR sensor • Nose modification reinforcement for a second 25" dia. class EO/IR sensor or radome • Wing payload hardpoints (500 lbs. payload on each wing) • Lower fuselage antenna farm (12"x24") provision aft of the camera portal • Upper fuselage antenna farm (12" x 12") provision approx. FS 250 • AEVEX Enhanced Air Conditioning Systems with Cockpit Cooling provisions • Window mounted ram air inlet & exhaust for cabin mission equipment cooling • Operator Console with mission computer, GeoFOCIS mission management software, dual monitors, solid state recording, and fully articulating/adjustable mission operator seat • Crew and Passenger Oxygen System (NOTE: This aircraft has dual airworthiness certificates allowing operation with a Standard or Special Airworthiness-Restricted Certificate and US Registry N905RT)
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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