2025 Bell 505
Single Turbine Helicopter
Aircraft Details
Seller reportedAvionics & Equipment
Description
Brand New Airconditioning Dual Controls Equipped With High Skids
Interior
BLACK LEATHER INTERIOR
Exterior
WHITE
Modifications / STCs
• ELECTRONIC STANDBY INSTRUMENTS (REQUIRED)
• INLET BARRIER FILTER (REQUIRED)
• DUAL PILOT CONTROLS
• ROTOR BRAKE
• SLIDING WINDOWS (PILOT & CO-PILOT)
• AUTOMATIC DOOR OPENERS FOR CO-PILOT DOOR
• AUTOMATIC DOOR OPENERS FOR PILOT DOOR
• WIRE STRIKE PROTECTION SYSTEM
• CARGO MIRROR R/H
• OPERATOR ACCESSORY PACKAGE
• MECHANICAL GROUND HANDLING WHEELS (STANDARD SKID GEAR ONLY)
• BOSE HEADSET ADAPTER
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 |
|---|---|---|---|---|---|---|
|
Cornell Grove
avbuyer.com
|
Contact for price
|
Switzerland | Mar 16, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Bell 505
This 2025 Bell 505 is a 5-seat single turbine helicopter . There are currently 27 505 aircraft listed for sale with asking prices ranging from $1,300,000 to $2,681,652.
The 505 cruises at 125 kts (232 km/h) with a range of 340 nm (630 km) — ideal for short hops and local flights. Service ceiling of 20,000 ft allows operation above most weather.
Operating costs: Fuel burn is 30 GPH (114 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $165/hr in fuel alone. Total variable cost including maintenance reserves is approximately $400/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $80,000.
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
Bell 505 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateBELL 505
AeroGurus estimates based on industry averages for the BELL 505. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Switzerland
CH
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.
Service Difficulty Reports — Bell 505
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
SKID TUBE FOUND BROKEN ALL THE WAY THROUGH DURING POST FLIGHT INSPECTION.
LEFT HAND SKID TUBE FOUND BROKEN ALL THE WAY THROUGH DURING POST FLIGHT INSPECTION.
LEFT HAND SKID TUBE FOUND BROKEN COMPLETELY THROUGH DURING POST FLIGHT INSPECTION.
SUPPORT BEARINGS IN TRANSMISSION RESTRAINT P/N SLS-030-910-109, HAVE BECOME "UN-STAKED" RESULTING IN A 1TO 1 VERTICAL VIBRATION.
NR SENSOR FAILURE. NR WENT TO ZERO IN FLIGHT. CAUSED TRANSPONDER TO GO OFF LINE AS AIRCRAFT THOUGHT IT WAS ON THE GROUND DUE TO ZERO ROTOR RPM.
APRIL 29, 2022. APROX. 10:00 AM. S WESTVIEW DR, CEDAR CITY, UT 84720 SHORTLY AFTER TAKEOFF, ROUGHLY 5 MILES SOUTH OF CDC AIRPORT THE MGT STARTED TO RISE. PILOT TURNED BACK TOWARD THE AIRFIELD WHILE MGT AND TOT CONTINUED TO RISE. DROPPING COLLECTI...
MINIMAL SPLINE ENGAGEMENT BETWEEN THE HYDRAULIC PUMP ADAPTER ASSY AND THE MAIN GEARBOX OIL PUMP SPLINES. THE PUMP ADAPTER ASSY HAD MOVED IN THE DIRECTION OF THE HYDRAULIC PUMP AND BOTTOMED OUT ON THE LARGER DIAMETER TAPERED AREA OF THE HYDRAULIC PUMP...
HYDRAULIC SYSTEM FAILED IN FLIGHT. DRIVESHAFT ASSEMBLY BETWEEN HYDRAULIC PUMP AND TRANSMISSION OIL PUMP SPLINES FAILED. DRIVESHAFT ASSEMBLY PART NUMBER P/N M206-204026-041.
ENGINE WAS SENT TO THE REPAIR STATION FOR REPAIR AFTER METAL PARTICLES WERE FOUND ON THE ACCESSORY GEARBOX MAGNETIC PLUG. DURING DISASSEMBLY IT WAS NOTED THAT TWO TABS FROM THE INTERMEDIATE GEAR BEARING CAGE WERE MISSING AND MATCHED THE TWO METAL PA...
(CAN) AFTER PERFORMED MAINTENANCE BY (CSF) AND INITIATED A GROUND RUN FOR A LEAK CHECK. START TEMPERATURES WERE NORMAL AT IDLE AND WHEN THE PILOT SWITCHED TO FLY MODE MGT AND OIL TEMPERATURE ROSE TO A POINT THAT THE OIL TEMPERATURE CEASED TO REGISTE...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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