1991 Bell 206b3
Single Turbine Helicopter
Aircraft Details
Seller reportedDescription
By exclusive mandate by of the owner, we proudly present this H125 in excellent utility/passenger transport configuration! Delivered from Airbus in 2017, operated and based in Norway. 150 H / 6 M inspection performed in Sept. 23 New starter generator installed Aug. 22 Fully operative and available!
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Listing Source
helitrader.com
|
Contact for Price
|
Turkey | Apr 01, 2026 | 107 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Bell 206b3
This 1991 Bell 206b3 (N612) is a single turbine helicopter with 8,113 hours on the airframe. There are currently 3 206b3 aircraft listed for sale .
NTSB records show 0 incidents for this airframe — a clean safety record. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Ownership & Registration
FAA registration data pending for N612.
Location & Ownership
Aircraft Location
Turkey
TR
Seller reportedTitle Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB safety data coming soon.
We'll check N612 against the NTSB accident database.
Service Difficulty Reports — Bell 206b3
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING INSPECTION, FOUND CORRODED HARDWARE ON CARGO HOOK ATTACHMENT. INSTALLED 4EA NEW BOLTS P/N AN4-10A AND NEW 4EA NEW WASHERS P/N 140-009C16S48.
DURING 12 MONTH INSPECTION FOUND CRACKS RADIATING FROM WHERE THE RIVETS ARE INSTALLED ON EITHER END ON ONE OF THE SEGMENTED RIVETED DRIVE SHAFT ASSEMBLY. THIS WAS DETECTED WITH A 10X MAGNIFYING GLASS. THE OTHER SEGMENTED SHAFTS CHECKED OUT OK. PART W...
THE FREEWHEELING UNIT WAS FAILING CAUSING THE MAIN GEARBOX CHIP LIGHT TO INTERMITTENTLY ILLUMINATE. WHEN THE CHIP DETECTORS WERE INSPECTED THERE WAS NO METAL NOTED. NOTHING APPEARED IN THE OIL FILTER OR SCREEN DURING THE SERVICEABILITY CHECK.
THROTTLE CABLE FAILED ON STARTUP CAUSING ENGINE OVER-TEMP.
IN PERFORMING BEL HELICOPTER 100HR PERIODIC INSPECTION A CRACK WAS IDENTIFIED ON THE FORWARD SEGMENT OF THE TAIL ROTOR DRIVE SHAFT AT FLANGE. THE CRACK IS LOCATED AT THE AFT FLEX COUPLING MOUNTING FLANGE. THE CRACK TRAVELS LONGITUDINALLY ACROSS A SEC...
DURING SCHEDULED AIR FRAME INSPECTION, DISCOVERED A CRACK IN THE UPPER LEFT HAND TAIL BOOM ATTACH FITTING. (AIR-FRAME SIDE OF TAIL BOOM.) PERFORMED DYE PENETRATE TEST THAT CONFIRMED CRACK LOCATION BETWEEN THE TWO AFT OUTBOARD RIVET LOCATIONS.
THE LH UPPER AFT LONGERON WAS FOUND CRACKED. THE CRACK EXTENDED DOWNWARD FROM THE UPPER FLANGES FREE EDGE AT BS 130. THE LONGERON WAS REPLACED.
THE LT BS 130 FRAME WAS FOUND CRACKED DURING A PHASE VISUAL INSPECTION. THE CRACK EXTENDED OUTBOARD 5.0 INCH FROM THE INBOARD FLANGE FREE EDGE AT LBL 67. THE FRAME WAS REPLACED.
DURING CLIMB 850 FEET, LATERAL VIBRATION CAME. LANDING PROCEDURES, AFTER VISUAL INSPECTION MAIN ROTOR BLADE TIP CAME OUT. AFTER DEEP INSPECTION AT HOME BASE, TELL-TALE WEIGHT SHEARED OFF INSIDE THE SPAR. CAUSING BLADE UNSERVICEABLE AFTER THIS EVENT.
INITIATED A NORMAL TAKEOFF TO THE SOUTH FROM TB-45. APPROXIMATELY 3-5 SECONDS AFTER INITIATION, A LOUD BANG WAS HEARD WITH ACCOMPANING AIRFRAME SHUTTER. ABORTED TAKE OFF. SECOND BANG AND SHUTTER FOLLOWED AS ACFT SETTLED TO THE GROUND.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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