PLANEFILE

BellHelicopters · Roswell, Georgia, USA

1993 Bell 206B III

Price: $565,000
Year: 1993
Total time: 9,348 hours
Location: United States

Specifications

General

Manufacturer: BELL
Model: 206B III
Serial Number: 4277
Registration #: N6181A
Condition: Used
Flight Rules: VFR
Based at: KCNI

Airframe

Total time: 9,348.3
Range: 374 NM
Max Takeoff Weight: 3,200 lb
Basic Empty Weight: 1,938.8 lb
Useful Load: 1,261.2 lb
Max Cruise Speed: 121.66 knots
Fuel Capacity Volume: 91 gal

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

Avionics

ADS-B Equipped: Yes
Artificial Horizon: Yes
Radar Altimeter: Yes
Single Pilot Operation: Yes
ELT: Yes
Wire Strike Protection System: Yes

Garmin GTX 345 ADS-B In/Out Transponder
Garmin GRA 55 Radar Altimeter
Conventional Analog Flight and Engine Instrumentation

Equipment

Dual Controls: Yes
Cargo Hook: Yes
Baggage Compartment: Yes

Van Horn Tail Rotor Blades
Paravion Engine Relight Kit
Facet External Oil Filter System
FliteStep / FloatStep
Preflight Step / Handle
Folding Maintenance Step

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

Interior

Configuration: Passenger / Utility
Number of Seats: 5

• 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.

Exterior

• Blue-and-white exterior with coordinating accent stripes.

• High-skid configuration with wire-strike protection system, cargo mirror, and exterior utility equipment.

Maintenance

Airworthy: Yes

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

Engine 1

Engine 1 Make/Model: ROLLS ROYCE M250-C20B
Engine 1 Serial Number: CAE-836631
Engine 1 Shaft Horsepower: 317 HP
Engine 1 Time: 12,228.2 SOH
Engine 1 TBO: 3500

Rotor

Main Rotor Blade Time Remaining: 651.8
Main Rotor Hub Time Remaining: 2187
Main Rotor Gearbox Time Remaining: 2990.9
Anti-Torque System: Tail Rotor
Tail Rotor Blade Time Remaining: 925
Tail Rotor Gearbox Time Remaining: 2596.1

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.

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 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

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