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De Havilland CanadaTurboprops · Murrieta, California, USA

Dehavilland DHC-6-100

Price
On request
Location
United States
Dehavilland DHC-6-100, photo 1Dehavilland DHC-6-100, photo 2

Specifications

General

Manufacturer
DEHAVILLAND
Model
DHC-6-100
Serial Number
051
Condition
Used
Flight Rules
IFR
Based at
F70

Airframe

Total time
0
Max Takeoff Weight
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

Propeller

Prop 1 Manufacturer
HARTZELL
Prop 1 Model
HC-B3TN-3D
Prop 2 Manufacturer
HARTZELL
Prop 2 Model
HC-B3TN-3D
Number of Blades
3
  • HC-B3TN-3D/T1082N
  • "0" Since Overhaul

Avionics

The typical Garmin G950 NXi configuration is as follows
• Dual Garmin GDU1050 ten-inch (10”) Primary Flight Displays (PFD), Pilot/Co-Pilot.
  • 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.
  • 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

Interior

Number of Seats
19
Configuration
Passenger
  • Standard 19 Passenger commuter seating configuration.
  • NEW Commuter-type "hard shell" Kydex interior.

Exterior

Will be painted to meet customer Livery requirements

Maintenance

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

Engine 1

Engine 1 Make/Model
PRATT & WHITNEY PT6A-27
Engine 1 Time
0 SNEW
Engine 1 TBO
3600

OHC or Factory-New

Engine 2

Engine 2 Make/Model
PRATT & WHITNEY PT6A-27
Engine 2 Time
0 SNEW
Engine 2 TBO
3600

OHC or Factory-New

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 the seller's 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 the seller'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

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