2001 Bell 412
Twin Turbine Helicopter
Aircraft Details
Seller reportedAvionics & Equipment
Description
JetHQ is pleased to showcase this 2001 Bell 412EP. This low-hour, well-maintained helicopter features advanced avionics fit, a large, configurable cabin, and robust utility gear, delivering reliability and performance for multiple missions. HIGHLIGHTS: Thirteen (13) Passenger + Two (2) Crew Configuration Low Flight Hours Air Conditioning Heavy Duty High Skid Gear Generator Capacity and Engine Upgrades ADDITIONAL FEATURES: Rotor Brake Dual Controls 82 gal Aux Fuel Tank L/H Dual ELT Setup Cargo Hook Suspension System
Engine
Pratt & Whitney PT6T-3D Total Cycles: 2,244
Propeller
Main Rotor Type: 412-015-300-109 Total Hours: 2,785.5 Tail Rotor Type: 212-010-750-105 Total Hours: 2,785.5 Gearbox 1 Type: 412-706-029-103 Total Hours: 1,147.5 Gearbox 2 Type: 412-706-029-103 Total Hours: 377.5
Interior
AESTHETICS: Colors: Grey & Beige Condition: Original 2001 LAYOUT: Configuration: Thirteen (13) Passengers + Two (2) Crew Seating: Nine (9) Forward-Facing Seats Four (4) Side Seats AIR CONDITION / HEATING: Air Conditioner
Exterior
AESTHETICS: Base Paint: White Accent Colors: Blue and Red Stripes, Yellow Trim Condition: Original 2001
Inspection
INSPECTION - COMPLIED WITH - NEXT DUE 300 HR / 12 M 29 May 2026 28 May 2027 600 HR / 12 M 29 May 2026 28 May 2027 5,000 HR / 5 Y 16 Jul 2021 15 Jul 2026 Engine 150 HR / 12 M 29 May 2026 28 May 2027 Engine 300 HR / 12 M 29 May 2026 28 May 2027 Engine 900 HR / 12 M 29 May 2026 28 May 2027 Engine Overhaul - 4,000 HR
Modifications / STCs
• Cargo Hook Suspension System
• Aux Fuel Provisions (82 gal Aux Fuel Tank L/H)
• VHF COM #2
• Heated Windshield Kit
• Rotor Brake
• Dual Controls
• Heavy Duty High Skid Gear
• Vertical Sliding Window L & R
• Remote Battery Pack
• Waterproof Flightlights
• Additional ELT
• EGPWS
• Anti-Slip Link
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 |
|---|---|---|---|---|---|---|
|
JetHQ
controller.com
|
Price on request
|
Hubei, China | Jul 26, 2026 | 0 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Bell 412
This 2001 Bell 412 is a 15-seat twin turbine helicopter with 2,785 hours on the airframe. There are currently 11 412 aircraft listed for sale with asking prices ranging from $5,200,000 to $5,200,000.
The 412 cruises at 122 kts (226 km/h) with a range of 360 nm (667 km) — ideal for short hops and local flights. Service ceiling of 20,000 ft allows operation above most weather.
Operating costs: Fuel burn is 100 GPH (378 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $550/hr in fuel alone.
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 412 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateBELL 412
AeroGurus estimates based on industry averages for the BELL 412. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Hubei, China
CN
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 412
ADs are mandatory safety instructions issued by the FAA. 10 recent ADs found for this aircraft type.
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 Inc. Model 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 205A, 205A-1, 205B, 212, 412, 412EP, and 412CF Helicopters
View full AD →Bell Helicopter Textron, Inc. Model 205A-1, 205B, 212, 412, 412EP, and 412CF Helicopters
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Bell 412
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
THE CREW CAME OUT FOR A TRAINING FLIGHT, STARTED THE AIRCRAFT JUST FINE AND IDLED ON DECK FOR A FEW MINUTES. UPON TAKE OFF THE #1 INVERTER SWITCH TURNED ITSELF OFF AND SUBSEQUENTLY LOST AUTOPILOT. WHEN THE INVERTER SWITCH WAS SWITCHED BACK TO ON THAT...
DURING CRUISE FLIGHT EXPERIENCED A TOTAL LOSS OF ALL MAIN ROTOR TRANSMISSION FLUID DUE TO FAILURE OF 1 ELBOW FITTING (P/N: AS1040W0404). EMERGENCY LANDING PERFORMED WITH NO DAMAGE TO AIRCRAFT OR INJURY TO ANY OCCUPANTS. DURING CONVERSATIONS WITH THE ...
COMPLETE SEPERATION OF THE PIVOT BEARING ELASTOMER FROM THE BASE. NOT VISABLE WITH THE BLADES INSTALLED, TOTAL FAIURE HAD NOT TAKEN PLACE 7.0 HOURS AGO.THIS ITEM HAS A FIRST INSPECTION INTERVAL AT 2500 HOURS, AIRCRAFT ONLY HAS 1800 BUT IS 13 + YEARS ...
FAILED ELASTOMER FOUND DURING REMOVAL FOR MAST SEAL REPLACEMENT. THIS PART CAN ONLY BE INSPECTED WITH MR HUB DISASSEMBLED AND THE ONLY REQUIREMENT FOR THIS INSPECTION IS LOCATED IN THE 2500 HOUR AIRFRAME INSPECTION. THE AIRCRAFT IN QUESTION ONLY HA...
THE HELICOPTER EXPERIENCED A TORQUE AND RPM FLUCTUATION SHORTLY AFTER TAKE-OFF. A FAULTY AUTOMATIC FUEL CONTROL UNIT WAS REPLACED. DURING THE ENGINE RIGGING PROCESS, EXCESSIVE PLAY WAS NOTED IN THE DROOP COMPENSATOR ROD ASSEMBLY. FURTHER INSPECTIO...
(CAN) DURING FLIGHT TEST. CHSP CASS MESSAGE APPEARED IN FLIGHT. TROUBLESHOOT FOUND 1 WIRE MISSING (BUT NOT RELATED) (TC# 20190715012)
(CAN) ON INSPECTION, FACTORY LEAD SEAL BROKEN AND LIFE RAFT ACTUATING CABLES WERE FOUND TO BE OUT OF RIG I.A.W. MANUFACTURES ICA DIMENSIONS (PARA 4.4.6 & 4.4.7) AT THE MULTI CABLE BOX. EXCESSIVE FREE PLAY FOUND IN CONSOLE TO BOX CABLE WHICH WOULD HAV...
(CAN) AFTER A SUCCESSFUL FLOAT DEPLOYMENT AND INFLATION FROM COCKPIT DURING THE 36 MONTH INSPECTION, THE LIFE RAFT DEPLOYMENT HANDLE WAS CYCLED NUMEROUS TIMES BUT FAILED TO DEPLOY/INFLATE THE LIFE RAFTS. LIFE RAFTS WERE SUCCESSFULLY DEPLOYED USING TH...
R/H TAILBOOM PANEL P/N 205 032 811 077 OUTER SKIN DELAMINATED APPROX. 24” X 3.5” BETWEEN BOOM STATIONS 77-101 WL 72.L/H TAILBOOM PANEL P/N H205 032 813 67 OUTER SKIN DELAMINATED APPROX. 15” X 2.75” BETWEEN BOOM STATIONS 73-88. ALSO PANEL HAS CORROSIO...
DURING ROUTINE MAINTENANCE / MODIFICATION IT WAS VISUALLY NOTED THAT THERE WAS AN ABNORMAL WEAR PATTERN ON THE SPIRAL BEVEL GEAR INSIDE THE MAIN ROTOR TRANSMISSION ASSY P/N 412-040-007-101 S/N BH282157. TECHNICAL SUPPORT WAS CONTACTED, AND VERIFIED T...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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