1993 BELL 206B III

    $565,000 
    Aircraft Location:Roswell, Georgia

    Seller Information

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    Jason Fritz

    Contact:Jason Fritz

    Phone:(770) 727-2727

    Roswell, Georgia

    (770) 727-2727

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    Description

    1993 Bell 206B III JetRanger, N6181A, S/N 4277, featuring dual controls, high skids, Onboard Systems cargo hook, cargo mirror, wire-strike protection, Garmin GTX 345 transponder, Garmin GRA 55 radar altimeter, Van Horn tail rotor blades, and utility/maintenance access equipment. Powered by a Rolls-Royce/Allison M250-C20B. 9,348.3 hours aircraft total time and 12,228.2 hours engine total time as of June 5, 2026. Annual inspection completed June 2026 with extensive component, AD/ASB, and maintenance tracking records available for review. Major component highlights include 2,990.9 hours remaining to transmission overhaul, 2,187.0 hours remaining to main rotor hub overhaul, 1,081.8 hours remaining on the compressor, and 799.1 hours remaining on the turbine assembly as of June 5, 2026. Well-equipped five-place JetRanger with blue-and-white exterior, navy-blue seating, rear baggage compartment, and utility equipment suitable for a variety of missions.

    Specifications

    Year1993
    ManufacturerBELL
    Model206B III
    Serial Number4277
    Registration #N6181A
    ConditionUsed
    FlightRulesVFR
    Based atKCNI
    Total Time9,348.3
    Range374 NM
    Max Takeoff Weight3,200 lb
    Basic Empty Weight1,938.8 lb
    Useful Load1,261.2 lb
    Max Cruise Speed121.66 knots
    Fuel Capacity Volume91 gal
    Airframe Notes• Registration: N6181A • Serial Number: 4277 • Aircraft Total Time: 9,348.3 Hours as of June 5, 2026 • Basic Empty Weight: 1,938.8 lb • Dual-Control Configuration • High Skids • Annual Inspection Completed June 5, 2026 • Extensive Component and AD/ASB Tracking Records Available
    Main Rotor Blade Time Remaining651.8
    Main Rotor Hub Time Remaining2187
    Main Rotor Gearbox Time Remaining2990.9
    Anti-Torque SystemTail Rotor
    Tail Rotor Blade Time Remaining925
    Tail Rotor Gearbox Time Remaining2596.1
    Rotor Notes• Main Rotor Blades: 651.8 Hours Remaining • Main Rotor Hub: 2,187.0 Hours Remaining to Overhaul; 987.0 Hours Remaining to Interim Inspection • Main Rotor Mast: 1,190.9 Hours Remaining to Overhaul • Transmission: 2,990.9 Hours Remaining to Overhaul • Main Driveshaft: 2,690.9 Hours Remaining • Van Horn Tail Rotor Blades • Tail Rotor Hub: 925.0 Hours Remaining • Tail Rotor Gearbox: 2,596.1 Hours Remaining to Overhaul • Tail Rotor Gearbox Inspection: 2,787.0 Hours Remaining • Component Times as of June 5, 2026
    Engine 1 Make/ModelROLLS ROYCE M250-C20B
    Engine 1 Serial NumberCAE-836631
    Engine 1 Shaft Horsepower317 HP
    Engine 1 Time12,228.2 SOH
    Engine 1 TBO3500
    Engine 1 Notes• Rolls-Royce/Allison M250-C20B • S/N CAE-836631 • Engine TT: 12,228.2 Hours • Engine Cycles: 12,599 • Compressor: 2,468.2 TSO / 1,081.8 Hours Remaining • Turbine Assembly: 2,700.9 TSO / 799.1 Hours Remaining • Turbine 1,750-Hour Inspection: 970.8 TSI / 779.2 Hours Remaining • 1st-Stage Turbine Wheel: 1,562.5 Hours Remaining • 2nd-Stage Turbine Wheel: 1,562.5 Hours Remaining • 3rd-Stage Turbine Wheel: 1,849.1 Hours Remaining • 4th-Stage Turbine Wheel: 1,849.1 Hours Remaining • Fuel Nozzle: 403.2 TSO / 1,596.8 Hours Remaining • Fuel Control: 868.7 TSO / 1,631.3 Hours Remaining • Governor: 564.7 TSO / 1,435.3 Hours Remaining • Fuel Pump: 1,122.0 TSO / 2,878.0 Hours Remaining • Times as of June 5, 2026
    Modifications/Conversions• Van Horn Tail Rotor Blades • Paravion Engine Relight Kit • Facet External Oil Filter System • FliteStep / FloatStep • Preflight Step / Handle • Folding Maintenance Step
    ADS-B EquippedYes
    Artificial HorizonYes
    Radar AltimeterYes
    Single Pilot OperationYes
    ELTYes
    Wire Strike Protection SystemYes
    Avionics/Radios• Garmin GTX 345 ADS-B In/Out Transponder • Garmin GRA 55 Radar Altimeter • Conventional Analog Flight and Engine Instrumentation
    Dual ControlsYes
    Cargo HookYes
    Baggage CompartmentYes
    Additional Equipment• Dual Controls • High Skids • Onboard Systems Cargo Hook • Cargo Mirror • Wire-Strike Protection System • Fire Extinguisher • First Aid Kit • Opening / Sliding Cabin Windows • Passenger Restraints • Rear Baggage Compartment • ELT
    Exterior Notes• Blue-and-white exterior with coordinating accent stripes. • High-skid configuration with wire-strike protection system, cargo mirror, and exterior utility equipment.
    ConfigurationPassenger / Utility
    Number of Seats5
    Interior Notes• Five-place cabin configuration featuring two-place front seating and three-place rear bench seating. • Navy-blue seating with tan cabin trim, passenger restraints, opening/sliding cabin windows, fire extinguisher, first-aid equipment, and rear baggage compartment. • Dual controls and rear baggage compartment.
    Inspection Status• Annual Inspection Completed June 5, 2026 • 100-Hour Airframe Inspection Completed June 5, 2026 • 300-Hour Airframe Inspection Completed June 5, 2026 • 150-Hour Engine Inspection Completed June 5, 2026 • 300-Hour Engine Inspection Completed June 5, 2026 • Pitot/Static & Altimeter Inspection Completed May 20, 2025 – Due May 20, 2027 • Transponder Inspection Completed February 27, 2026 – Due February 27, 2028 • Weight & Balance Completed May 19, 2025 – Due May 19, 2027 • ELT Inspection/Functional Test Completed June 5, 2026 • 1,200-Hour Airframe Inspection: 987.0 Hours Remaining as of June 5, 2026 • Extensive AD/ASB and Component Tracking Records Available
    AirworthyYes
    Year1993|
    ManufacturerBELL|
    Model206B III|
    Serial Number4277|
    Registration #N6181A|
    ConditionUsed|
    FlightRulesVFR|
    Based atKCNI|
    Total Time9,348.3|
    Range374 NM|
    Max Takeoff Weight3,200 lb|
    Basic Empty Weight1,938.8 lb|
    Useful Load1,261.2 lb|
    Max Cruise Speed121.66 knots|
    Fuel Capacity Volume91 gal|
    Airframe Notes• Registration: N6181A • Serial Number: 4277 • Aircraft Total Time: 9,348.3 Hours as of June 5, 2026 • Basic Empty Weight: 1,938.8 lb • Dual-Control Configuration • High Skids • Annual Inspection Completed June 5, 2026 • Extensive Component and AD/ASB Tracking Records Available|
    Main Rotor Blade Time Remaining651.8|
    Main Rotor Hub Time Remaining2187|
    Main Rotor Gearbox Time Remaining2990.9|
    Anti-Torque SystemTail Rotor|
    Tail Rotor Blade Time Remaining925|
    Tail Rotor Gearbox Time Remaining2596.1|
    Rotor Notes• Main Rotor Blades: 651.8 Hours Remaining • Main Rotor Hub: 2,187.0 Hours Remaining to Overhaul; 987.0 Hours Remaining to Interim Inspection • Main Rotor Mast: 1,190.9 Hours Remaining to Overhaul • Transmission: 2,990.9 Hours Remaining to Overhaul • Main Driveshaft: 2,690.9 Hours Remaining • Van Horn Tail Rotor Blades • Tail Rotor Hub: 925.0 Hours Remaining • Tail Rotor Gearbox: 2,596.1 Hours Remaining to Overhaul • Tail Rotor Gearbox Inspection: 2,787.0 Hours Remaining • Component Times as of June 5, 2026|
    Engine 1 Make/ModelROLLS ROYCE M250-C20B |
    Engine 1 Serial NumberCAE-836631|
    Engine 1 Shaft Horsepower317 HP|
    Engine 1 Time12,228.2 SOH |
    Engine 1 TBO3500|
    Engine 1 Notes• Rolls-Royce/Allison M250-C20B • S/N CAE-836631 • Engine TT: 12,228.2 Hours • Engine Cycles: 12,599 • Compressor: 2,468.2 TSO / 1,081.8 Hours Remaining • Turbine Assembly: 2,700.9 TSO / 799.1 Hours Remaining • Turbine 1,750-Hour Inspection: 970.8 TSI / 779.2 Hours Remaining • 1st-Stage Turbine Wheel: 1,562.5 Hours Remaining • 2nd-Stage Turbine Wheel: 1,562.5 Hours Remaining • 3rd-Stage Turbine Wheel: 1,849.1 Hours Remaining • 4th-Stage Turbine Wheel: 1,849.1 Hours Remaining • Fuel Nozzle: 403.2 TSO / 1,596.8 Hours Remaining • Fuel Control: 868.7 TSO / 1,631.3 Hours Remaining • Governor: 564.7 TSO / 1,435.3 Hours Remaining • Fuel Pump: 1,122.0 TSO / 2,878.0 Hours Remaining • Times as of June 5, 2026|
    Modifications/Conversions• Van Horn Tail Rotor Blades • Paravion Engine Relight Kit • Facet External Oil Filter System • FliteStep / FloatStep • Preflight Step / Handle • Folding Maintenance Step|
    ADS-B EquippedYes|
    Artificial HorizonYes|
    Radar AltimeterYes|
    Single Pilot OperationYes|
    ELTYes|
    Wire Strike Protection SystemYes|
    Avionics/Radios• Garmin GTX 345 ADS-B In/Out Transponder • Garmin GRA 55 Radar Altimeter • Conventional Analog Flight and Engine Instrumentation|
    Dual ControlsYes|
    Cargo HookYes|
    Baggage CompartmentYes|
    Additional Equipment• Dual Controls • High Skids • Onboard Systems Cargo Hook • Cargo Mirror • Wire-Strike Protection System • Fire Extinguisher • First Aid Kit • Opening / Sliding Cabin Windows • Passenger Restraints • Rear Baggage Compartment • ELT|
    Exterior Notes• Blue-and-white exterior with coordinating accent stripes. • High-skid configuration with wire-strike protection system, cargo mirror, and exterior utility equipment.|
    ConfigurationPassenger / Utility|
    Number of Seats5|
    Interior Notes• Five-place cabin configuration featuring two-place front seating and three-place rear bench seating. • Navy-blue seating with tan cabin trim, passenger restraints, opening/sliding cabin windows, fire extinguisher, first-aid equipment, and rear baggage compartment. • Dual controls and rear baggage compartment.|
    Inspection Status• Annual Inspection Completed June 5, 2026 • 100-Hour Airframe Inspection Completed June 5, 2026 • 300-Hour Airframe Inspection Completed June 5, 2026 • 150-Hour Engine Inspection Completed June 5, 2026 • 300-Hour Engine Inspection Completed June 5, 2026 • Pitot/Static & Altimeter Inspection Completed May 20, 2025 – Due May 20, 2027 • Transponder Inspection Completed February 27, 2026 – Due February 27, 2028 • Weight & Balance Completed May 19, 2025 – Due May 19, 2027 • ELT Inspection/Functional Test Completed June 5, 2026 • 1,200-Hour Airframe Inspection: 987.0 Hours Remaining as of June 5, 2026 • Extensive AD/ASB and Component Tracking Records Available|
    AirworthyYes|
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