J\EVEX
Specifications and Aircraft Details MSN 297 and 644
A E R O S P A C E
AEVEX is a worldwide leader in supporting the DHC-6 Twin Otter series aircraft. Applications vary between civil operator use such as airline, charter, and provate operations, to specialized configurations for scientific and government use such as coast guard, fishery management, mineral and petroleum exploration, paramilitary, scientific research, border and maritime patrol, wildfire management, test range clearance, telemetry, atmospheric research, pollution control, oil slick management, sensor testing, mosquito/vector management, spraying, etc. Contact AEVEX with your cha lenge!
Our DHC-6-300 Twin Otter Testbed Fleet is available for:
• Developing new technologies • Demonstrating new systems • Supporting special exercises
• Person in-the-loop UAV surrogate testing • Capturing new business opportunities
DHC-6 and T WIN OTTE R are trademarks of Viking Air L imited
J\EVEX
AEVEX.COM
A E R O S P A C E
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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.
J\EVEX
AEVEX.COM
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Avionics
The avionics system is provided with a Garmin G950NXi/G1000NXi configuration with all Factory-New equipment: • Dual Garmin GDU1050 ten-inch (10") Primary Flight Displays (PFD), Pilot/Co-Pilot • Garmin GDU1550 fifteen-inch (15") Multi-Functional Display (MFD) • Garmin GCU477 MFD Controller • Dual Garmin GDC7400 Air Data Computers (ADC)
• Dual Garmin GRS79 Attitude and Heading Reference System (AHRS) • Dual Garmin GIA 64W WAAS GPS/NAV/COM Integrated Avionics Units • Garmin GTX 345R ADS-B Transponders • Garmin GTS 855 TCAS-I • Dual Garmin GEA 71B Engine/Airframe Interface units • Dual Garmin GMA 1360D Audio Panels • Garmin TAWS-Class B
• Mid-Continent MD302 Standby Attitude Module • Cobham 251 Paging Passenger Address system • Artex 406 AF ELT with whip antenna
DHC-6 and TWIN OTTER are trademarks of Viking Air Limited
Bo Alksninis Sr. Director, Business Development Phone : 818-554-5906 Email : balksninis@aevex.com
Contact Us►
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.
The DHC-6-300 MSN 644 is currently undergoing modification, refurbishment, maintenance to bring the aircraft current with all required inspections (Basic A, B, C12, and D Checks per DHC PSM 1-6-7) and a baseline five (5) year corrosion inspection (I.AW. DHC-6 Corrosion Inspection Manual, PSM 1-6-5). Airframe: TSN: 57,088 hours/97,436 cycles (remaining life 8,912 hours/34,564 cycles as of 6/26/2023)
PT6A-27 Engines (as of 6/26/2023)
Propellers:
Left PCE-52430 6,594.3 Hrs. 1,996.4 Hrs.
Right PCE-52433 5,593.4 Hrs. 1,973.7 Hrs.
Hartzell HC-B3TN-3D; OHC December 2023
Serial Number: Time Since New: Time Since Overhaul: Cycles Since New: Cycles Since OH:
Left Right S/N: BUA24843 BUA27493
3,197 1,781
5,371 1,814
Aircraft Configuration Details:
• Garmin G950 Avionics (see Avionics specification below) • 12,500 lbs. MTOW; Empty Weight 7,184 lbs. (Approx)
• Total Fuel Capacity: 2,548 lbs. (allows a nominal 5.1 hrs. loiter); Option for incorporating Factory SOO 6095 (3148 lbs.) or AEVEX's Wing Extended Range Fuel Systems-WERFS (3686.8 lbs.) • PT6A-27 Engines (620 SHP), mid-time since initial overhaul • Two AEVEX High-Flow 250 Amp St-Generators with mission power cockpit control option • Standard Commuter hardshell interior • Utility or Commuter seating • Third rail seat track provisions for mounting mission equipment This aircraft is an "open canvas" for re-configuration as a multi-purpose platform to include any of the same modifications currently applied to MSN 297 or other customizations as required.
(NOTE: This aircraft is currently operating with a Standard Airworthiness Certificate and US Registry: N300DZ)
DHC-6 and TWIN OTTER are trademarks of Viking Air Limited
Bo Alksninis Sr. Director, Business Development Phone : 818-554-5906 Email : balksninis@aevex.com
Contact Us
J\EVEX
A E R O S P A C E
Available Options:
AEVEX provides a variety of customizations that provide improved utility, enhanced safety, and meet specific customer brand identity needs:
• Crew Oxygen System installed per FAA STC number SA03266NY/TCCA STC number SA12-46 with demand or constant flow masks (includes microphone) and smoke goggles • Customized seating and interiors: Commuter, VIP, Utility, Paratroop • Air Conditioning system with/without cockpit cooling • Wing Extended Range Fuel System (WERFS), STC Pending • Enclosed lavatory (forward or aft cabin) • Camera hatches (forward and aft) for special airborne sensors • Wing Hardpoints (single or dual per wing) allowing external sensor stores up to 500 lbs. per side
• Special Missions customizations • Amphibious or Float Landing Gear • Passenger entry door options • Floor mounted emergency pathway luminescent lighting • Satcom System upgrades • Enhanced Vision System (EVS) Max-Viz EVS 2300 • APU for high-power mission systems • CLICK HERE to learn more about our available options
DHC-6 and TWIN OTTER are trademarks of Viking Air Limited
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