Manufacturer Bell Textron, year 1981 (at the end), Model Bell 206B-3, S/N 3555, Airworthy to 11. Jun 2026., Registration mark YU-HLT.
Condition: Used
Engine RR 250C20B, S/N CAE-845086 installed 28. sept. 2019., with TT 241h and TSOH 0h
No history.
Airworthy to 11. Jun 2026.

Airplane time state:
Total Time, TTAF, 9756.6h
Engine TSN H/ CSN 880.5/ 798
Engine TSOH 639.5

MRB 206-010-200-133 Time remaining to SLL 2589.9h

MRH TSOH 339,6h

MRT 206-040-002-025 Time remaining 1978,8h

TT straps rem. time 860.4h/ 550 days

TRB 206-016-201-131 Time remaining 246.9h

TRGB 206-040-400-013 Time remaining 5172.4h

Heading indicator (Directional gyro), VOR, Audio panel GMA 340, VHF COM/NAV KX 155, GPS, ELT ARTEX ME406, Transponder KT76A,
Caution panel, Attitude gyro, Pressure altimeter, Airspeed indicator, Vertical speed indicator, Dual tachometer RPM indicator NR/ Power turbine (N2), Gas-Producer RPM (N1) Tachometer, Turbine outlet temperature (TOT), Torque meter, Engine oil temp/ pressure indicator, Transmission oil temp/ pressure indicator, Fuel pressure/ Loud indicator, Quantity fuel indicator, Turn and sleep indicator.

Old, changed at the year 2012.

Old, changed at the year 2012.

Dual controls, High skid, Anti torque pedal extension, Cabin heater, Particle separator, Kamatics KAflex driveshaft (TSN 61h), Wire strike protection, Concorde RG-206 lead acid battery, Arm Expansions of the windows in the passenger cabin, Auxiliary hydraulic system Kawak model 34430/34600, Fuel range extender, Shoulder straps for pilot and passengers, Ground handling wheels BDW-245B-1801, Bear paws, Turbine shroud heater kit, Positions NAV lights, Strobe light, Talon LC keeperless cargo hook (design load 3600 Lb), Deflector kit, Cabin temperature control, Wire strike protection system, Noise camera mount Meeker AFG1, Headsets David Clark, Provision for additional equipment, Camera hole in the passenger cabin.