DEHAVILLAND DHC-6-100

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    Aircraft Location:Murrieta, California

    Seller Information

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    AEVEX

    Contact:Bo Alksninis

    Phone:(951) 600-0009

    Murrieta, California

    (951) 600-0009

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    Description

    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.

    Specifications

    ManufacturerDEHAVILLAND
    ModelDHC-6-100
    Serial Number051
    ConditionUsed
    FlightRulesIFR
    Based atF70
    Total Time0
    Max Takeoff Weight11,579 lb
    Airframe NotesThis 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
    Engine 1 Make/ModelPRATT & WHITNEY PT6A-27
    Engine 1 Time0 SNEW
    Engine 1 TBO3600
    Engine 1 NotesOHC or Factory-New
    Engine 2 Make/ModelPRATT & WHITNEY PT6A-27
    Engine 2 Time0 SNEW
    Engine 2 TBO3600
    Engine 2 NotesOHC or Factory-New
    Prop 1 ManufacturerHARTZELL
    Prop 1 ModelHC-B3TN-3D
    Prop 2 ManufacturerHARTZELL
    Prop 2 ModelHC-B3TN-3D
    Number of Blades3
    Prop NotesHC-B3TN-3D/T1082N "0" Since Overhaul
    Avionics/RadiosThe 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
    Exterior NotesWill be painted to meet customer Livery requirements
    Number of Seats19
    ConfigurationPassenger
    Interior NotesStandard 19 Passenger commuter seating configuration. NEW Commuter-type "hard shell" Kydex interior.
    Inspection StatusCurrent 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
    ManufacturerDEHAVILLAND|
    ModelDHC-6-100|
    Serial Number051|
    ConditionUsed|
    FlightRulesIFR|
    Based atF70|
    Total Time0|
    Max Takeoff Weight11,579 lb|
    Airframe NotesThis 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|
    Engine 1 Make/ModelPRATT & WHITNEY PT6A-27 |
    Engine 1 Time0 SNEW |
    Engine 1 TBO3600|
    Engine 1 NotesOHC or Factory-New|
    Engine 2 Make/ModelPRATT & WHITNEY PT6A-27 |
    Engine 2 Time0 SNEW |
    Engine 2 TBO3600|
    Engine 2 NotesOHC or Factory-New|
    Prop 1 ManufacturerHARTZELL|
    Prop 1 ModelHC-B3TN-3D|
    Prop 2 ManufacturerHARTZELL|
    Prop 2 ModelHC-B3TN-3D|
    Number of Blades3|
    Prop NotesHC-B3TN-3D/T1082N "0" Since Overhaul|
    Avionics/RadiosThe 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|
    Exterior NotesWill be painted to meet customer Livery requirements|
    Number of Seats19|
    ConfigurationPassenger|
    Interior NotesStandard 19 Passenger commuter seating configuration. NEW Commuter-type "hard shell" Kydex interior.|
    Inspection StatusCurrent 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|
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