Specifications
Broker
CHARLIE BERICHI
CHARLIE
1-800-337-5263
Aircraft Details
- Fresh 24-month inspection to be completed by July 1st, 2026
- Total time: 215 hours
- Equipped with a Bell 407GXi-specific 2-axis autopilot fully integrated with Garmin G1000H avionics
- Autopilot includes attitude/heading hold, altitude preselect, airspeed hold, glideslope/localizer/VOR capture (with radar altimeter), FMS flight plan following, and recovery mode
- Two 10.4" high definition display units (PFD/MFD)
- Dual integrated avionics units with VHF comm/nav, WAAS GPS, and glideslope receiver
- Audio control panel with clearance recording and automatic speech recognition
- Digital air data computer, ADAHRS, Mode S transponder with ADS-B Out, engine/airframe interface unit
- Tail rotor video camera for night vision (approx. 25 feet)
- Synthetic Vision System (SVS) and Helicopter Terrain Awareness and Warning System (HTAWS)
- Integrated engine indication and crew alerting system (EICAS)
- Flight data recording of 60 parameters
- 28V DC system, NiCad battery, external power, starter-generator, heated pitot/static ports, LED lighting
- Skid-type landing gear, composite doors, mooring/jacking/lifting provisions, tinted windows
- Powered by Rolls-Royce M250-C47E/4 engine
- Corporate/VIP interior: rich leather, noise-reduction soundproofing, 7-place spacious cabin, always hangared, 10/10 condition
About this Model
Overview
The Bell 407GXi is an evolution of the 407 line aimed at operators who want a familiar, proven airframe paired with updated cockpit integration and improved powerplant performance margins. It is commonly selected for utility, corporate, public safety, and training missions where speed, payload flexibility, and straightforward single-engine operations matter more than all-weather, multi-engine redundancy.
Mission Fit
Typical missions center on short-to-medium sectors with frequent stops, operating from helipads, confined areas, or unimproved sites. The platform’s power and rotor system support productive performance in high density altitude environments, but payload-range tradeoffs remain central: additional fuel can quickly reduce available cabin load, particularly with mission equipment installed.
Cabin
Cabin layout is oriented around a single-pilot cockpit with club-style rear seating and good visibility. Noise and vibration levels are consistent with the light single-engine class; passenger comfort is generally strong for shorter legs and sightseeing, while longer legs depend on seating configuration, headset use, and installed options. Access and loading benefit from the wide doors and a cabin that can be configured for passenger, utility, or specialized missions.