2024 Bell 407 GXI
Single Turbine Helicopter
Aircraft Details
Seller reportedAvionics & Equipment
VFRproviding Primary Flight Display (PFD) and Multi-Function Display (MFD) functionalities Two Integrated Avionics Units
each consisting of a 16-watt VHF communication transceiver with 8.33 kHz spacing
VHF navigation WAAS GPS navigationand glideslope receiver One audio control panel with clearance recording and Automatic Speech Recognition (ASR) capability One digital Air Data Computer (ADC) with Outside Air Temperature (OAT) probe One Air Data and Attitude Heading Reference System (ADAHRS) and magnetometer One mode S transponder with extended squitter
including Traffic Information Service (TIS)with ADS-B "Out" capability One engine and airframe interface unit One engine signal conditioner Tail rotor video camera system with capability to view approximately 25 feet in complete darkness Synthetic Vision System (SVS)
and Helicopter Terrain Awareness and Warning System (HTAWS) features Integrated Engine Indication and Crew Alerting System (EICAS)
including Power Situation Indicator (PSI) that provides an integrated display presentation of all critical engine parameters into a single indicator to present the power "margin" remaining Fuel flow indication with range ring display capability Flight Data Recording of 60 standard aircraft and engine parameters 28 volt DC system Battery
17 amp-hour nickel cadmium External power and grounding receptacle Starter-generator (180 ampere) Solid state voltage regulator 28 volt outlet in cockpit Heated pitot tube and Static ports LED lighting: Anti-collision strobe Cockpit / map Instrument Landing Position
Description
Fresh 24 month inspection to be completed July 1st 2026. TT 215 HOURS. The optional 2-axis autopilot is a Bell 407GXi specific kit. It features greater capabilities at a lower cost and is the only kit that is fully-integrated with the Garmin G1000H™ avionics suite to display autopilot modes, hold references, audio alerts and CAS messages. This kit provides enhanced lateral and longitudinal stability in low-speed flight and a cyclic force trim release switch, a beep reference switch, pitch/roll/yaw hands-on stability augmentation, and pilot-initiated automatic recovery. The modes and annunciations of the Bell 407GXi autopilot include: * Autopilot (AP) Modes - Attitude hold - Heading hold • Coupled AP Roll Axis Modes - Altitude hold - Altitude preselect - Airspeed hold - Glideslope capture and track (with Radar Altimeter installed) • Coupled AP Pitch Axis Modes - Heading select - FMS flight plan following - VOR capture and track (with Radar Altimeter installed) - Localizer capture and track • PFD Annunciations - Pitch/Roll mode indications - Beep/Hold references - Out-of-Detent indications - AFCS-related CAS messages The Bell 407GXi autopilot Stability and Control Augmentation System (SCAS) significantly reduces pilot workload by providing precise control during all modes of flight, regardless of wind conditions or the aircraft's center of gravity. It also features a recovery mode which allows the aircraft to safely exit inadvertent IMC or unusual attitudes if a pilot loses visual reference due to limited visibility conditions. Upon initiating the autopilot "Go Around" mode using the collective or mode panel switch, the Bell 407GXi autopilot system will level the pitch and roll attitude of the aircraft. The pilot can then apply power using the collective for a wings-level climb at best climb rate airspeed (70 KIAS) to safely navigate through the appropriate emergency or initiate a go-around procedure.
Engine
Powered by the Rolls-Royce M250-C47E/4 engine
Propeller
Cabin; bonded aluminum honeycomb, and semimonocoque structure with composite side panels and aft fuselage skins Doors (five), one hinged double door and copilot door on left side, pilot and passengers on right side, all doors are composite material. Landing gear, tubular skid type with replaceable skid shoes. Locks for cabin doors and luggage compartment Luggage compartment with composite door Provisions for mooring, jacking and single point lifting Tail boom, monocoque structure with vertical fin and fixed stabilizer Tail skid (tail rotor guard) Windows (except windshield), gray tinted plexiglass Three color exterior paint schemes
Interior
Corporate/VIP: Features rich leather, noise-reduction soundproofing, and a spacious 7-place cabin. Always Hangared Remarkably maintained 10/10
Exterior
Three color exterior paint schemes
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 |
|---|---|---|---|---|---|---|
|
Charlie Berichi
trade-a-plane.com
|
$5,100,000
|
Fort Lauderdale, FL | Jun 13, 2026 | 10 days | Active |
Estimate Monthly Payment
Bell 407 GXI loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Bell 407 GXI
This 2024 Bell 407 GXI (N305CB) is a 7-seat single turbine helicopter with 215 hours on the airframe. This aircraft is listed at the market average at $5,100,000.
The 407 GXI cruises at 133 kts (246 km/h) with a range of 330 nm (611 km) — ideal for short hops and local flights. Service ceiling of 18,500 ft allows operation above most weather.
Operating costs: Fuel burn is 40 GPH (151 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $220/hr in fuel alone. Total variable cost including maintenance reserves is approximately $550/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $100,000. With 215 hours on the airframe, this aircraft has 3,285 hours remaining to engine TBO .
NTSB records show 0 incidents for this airframe — a clean safety record.
Pre-Purchase Checklist
Bell 407 GXI — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateBELL 407
AeroGurus estimates based on industry averages for the BELL 407. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N305CB.
Location & Ownership
Title 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 N305CB against the NTSB accident database.