DEHAVILLAND DHC 6 100

DEHAVILLAND

DHC-6-100

051

Used

IFR

F70

This aircraft can be delivered as a -100/-200 with 550 SHP or as -100HP™/-200HP™ with 620 SHP both operating at 11,579 lbs. or as an AEVEX DHC-6-200HG™ Increased Gross Weight to 12,500 lbs MTOW per FAA STC No. SA02252LA with the equivalent capabilities of a DHC-6-300 series. Aircraft will be configured to meet customer requirements and is available with: • Long nose forward baggage compartment. • Aft baggage shelf extension. • Enlarged aft baggage door. • Emergency exit window hatches. • DHC-6 Wing Boxes with AEVEX's Life Extension STC per FAA STC SA00827LA or DHC-6 Re-Life® Wing Boxes • Fixed wheeled landing gear, with Goodyear wheels and brakes. • Airstair or forward passenger "Swing" entry door. • Current maintenance status in accordance with DHC-6 PSM 1-6-7 (IC) Index Card 1. • Baseline Five-year corrosion inspection per DHC PSM 1-6-5. • Exterior painted Matterhorn white with DuPont Imron AF400 polyurethane enamel, no stripes, wing exhaust path painted black, with fuselage registration markings. • Lead Acid battery Contact us to discuss options, AEVEX has many tools in our "Twin Otter Tool Box" allowing flexibility to meet our customers unique requirements.

0

11,579 lb

This aircraft is available as an IKHANA RWMI DHC-6-200HG with Increased Gross Weight to 12,500 lbs MTOW per FAA STC No. SA02252LA. - Aircraft may be configured with: * Long nose forward baggage compartment. * Aft baggage shelf extension. * Enlarged aft baggage door. * Emergency exit window hatches. * IKHANA RWMI DHC-6 Wing Boxes with Life Extension STC per FAA STC SA00827LA or RWMI DHC-6 Re-Life Wing Boxes * Fixed wheeled landing gear, with Goodyear wheels and brakes. * Airstair or forward passenger "Swing" entry door. * Current maintenance status in accordance with DHC-6 PSM 1-6-7 (IC) Index Card 1. * Baseline Five year corrosion inspection per DHC PSM 1-6-5. * Exterior painted Matterhorn white with DuPont Imron AF400 polyurethane enamel, no stripes, wing exhaust path painted black, with fuselage registration markings. * Lead Acid battery

PRATT & WHITNEY

PT6A-27

0

SNEW

3600

OHC or Factory-New

PRATT & WHITNEY

PT6A-27

0

SNEW

3600

OHC or Factory-New

HARTZELL

HC-B3TN-3D

HARTZELL

HC-B3TN-3D

3

HC-B3TN-3D/T1082N "0" Since Overhaul

The avionics system will be customized to meet customer’s specifications. The Garmin G950 NXi system is recommended as an integrated system with flexibility to meet specific capabilities you may need. The typical Garmin G950 NXi configuration is as follows: • 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 ADS-B Transponder (Single or Dual). • Dual Garmin GEA 71B Engine/Airframe Interface units. • Dual Garmin GMA 1360D Audio Panels. • Mid-Continent MD302 Standby Attitude Module. • Cobham 251 Paging Passenger Address system. • Artex 406 AF ELT with whip antenna. • Garmin TAWS – Class B is standard

Will be painted to meet customer Livery requirements

19

Passenger

Standard 19 Passenger commuter seating configuration. NEW Commuter-type "hard shell" Kydex interior.

Current maintenance status in accordance with DHC-6 PSM 1-6-7 (IC) Index Card 1 Baseline Five year corrosion inspection per DHC-6 PSM 1-6-5