1978 Bell 212
Turbine Helicopters
Aircraft Details
Seller reportedAvionics & Equipment
IFRDescription
•Cargo sling provisions •Cargo mirrors provisions •Floats provisions •Hoist provisions
Engine
Engine 1 46,412 cycles
Modifications / STCs
• •Fire extinguisher x2
• •First aid kit x2
• •Cargo sling provisions
• •DART landing gear
• •Hoist provisions
• •Search light
• •Cargo mirrors provisions
• •Floats provisions
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Rotortrade
controller.com
|
Contact for price
|
Kuala Lumpur, Malaysia | Mar 25, 2026 | — | Active | |
|
Rotortrade
controlleremea.co.uk
|
Contact for price *
Contact for price
|
Kuala Lumpur, Malaysia | Apr 04, 2026 | — | Active |
* Converted to USD at daily European Central Bank (ECB) exchange rates
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Bell 212
This 1978 Bell 212 is a 15-seat turbine helicopters with 17,380 hours on the airframe. There are currently 10 212 aircraft listed for sale with asking prices ranging from $1,870,000 to $3,675,000.
Operating costs: Fuel burn is 80 GPH (303 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $440/hr in fuel alone. Total variable cost including maintenance reserves is approximately $900/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $180,000. With 17,380 hours on the airframe, this aircraft has exceeded TBO (3,500 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 10 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Bell 212 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateBELL 212
AeroGurus estimates based on industry averages for the BELL 212. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Kuala Lumpur, Malaysia
MY
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.
Airworthiness Directives — Bell 212
ADs are mandatory safety instructions issued by the FAA. 10 recent ADs found for this aircraft type.
Bell Helicopter Textron, Inc. (Bell), Model 205A-1, 205B, 210, and 212 Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, 412EP Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters
View full AD →Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412EP, and 412CF Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 204B, 205A, 205A-1, 205B and 212 Helicopters
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Bell 212
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
HOSE ASSEMBLY CHAFING DAMAGE RESULTING IN LOSS OF FLUID.
UPON VISUAL INSPECTION OF FRICTION DAMPERS AND TRANSMISSION MOUNTS, FOUND LIFT LINK FITTING CRACK ON THE AFT LUG BUSHING AREA COVERING THE ENTIRE LATERAL (SIDE). TRANSMISSION MOUNTS WERE REMOVED AND INSPECTED FOUND PRESSURE REQUIRED TO DEFLECT MOUNT ...
(CAN) PILOT REPORTED HEARING NOISE AT LEFT REAR OF AIRCRAFT AND CHANGE IN FLIGHT REGIME LIKE SMALL WIND GUST. NO ABMORMAL INSTRUMENT INDICATIONS. AIRCRAFT LANDED AND DISTINCT WHINE NOISE HEARD PRIOR TO SHUT DOWN. ENGINES SHUT DOWN AND BASIC VISUAL IN...
(CAN) TORQUE GAUGE FAILED AND POPPED CIRCUIT BREAKER. (TC# 20190725007)
(CAN) IT WAS REPORTED TO BELL:DURING BUCKETING OPERATIONS AT APPROX 300 FEET ABOVE GROUND LEVEL, THE PILOT OBSERVED THAT THE #2 ENGINE FIRE LIGHT HAD ILLUMINATED. HE PILOT FOLLOWED THE EMERGENCY PROCEDURES FOR AN ENGINE FIRE INDICATION AND SUBSEQUENT...
(CAN) THE #2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. POST LANDING INSPECTION REVEALED THERE WAS NO FIRE. MAINTENANCE PERSONNEL DISCOVERED THE #2 SIDE FIRE DETECTION AMPLIFIER HAD CAUSED A FALSE FIRE WARNING INDICATION. THE FIRE DETECTION...
(CAN) PILOT WAS LIFTING A WATER BUCKET FROM A SWAMP NEAR LAC LA BICHE WHEN THE AIRCRAFT KICKED TO THE LEFT AND HE LOOKED OVER AT HIS GUAGES AND NOTICED THAT ENGINE 1 WAS OFFLINE. HE PROCEEDED TO RELEASE THE LONGLINE AND BUCKET, LEAVING THEM IN THE SW...
(CAN) DURING THE ANNUAL INSPECTION OF THE ELT, UPON OPENING THE UNIT, IT APPEARED EVIDENT AN INTERNAL BATTERY CELL HAD RUPTURED, WAS BULGING AND LEAKING ELECTROLYTE. THE BATTERIES ARE OF LITHIUM ION TECHNOLOGY. THE ELT BATTERY WAS REPLACED WITH A NEW...
(CAN) NEW TAIL ROTOR COUPLING FROM MANUFACTURER PART NUMBER 204040604005S HAS SCORING MARKS IN VALLEY BETWEEN TEETH. MACHINE MARKS THREE COUPLINGS WITH SAME DEFECT
(CAN) TRD OUTER COUPLING FOUND WITH POSSIBLE MACHINING MARKING/GOUGES.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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