2024 Bell 407 GXITurbine Helicopter • Fort Lauderdale, FL, USA

PFD

Two 10.4 inch High Definition Display Units, Providing Primary Flight Display (PFD) And Multi-Function Display (MFD) Functionalities

MFD

Two 10.4 Inch High Definition Display Units, Providing Primary Flight Display (PFD) And Multi-Function Display (MFD) Functionalities

Comms

Two Integrated Avionics Units, Each Consisting Of A 16-Watt VHF Communication Transceiver With 8.33 KHz Spacing, VHF Navigation, WAAS GPS Navigation, And Glideslope Receiver

Audio

One Audio Control Panel With Clearance Recording And Automatic Speech Recognition (ASR) Capability

GPS

WAAS GPS Navigation

AP

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.

ADSB

One Mode S Transponder With Extended Squitter, Including Traffic Information Service (TIS), With ADS-B Out Capability

Traffic

Traffic Information Service (TIS)

EMS

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

Air Data Computer

One Digital Air Data Computer (ADC) With Outside Air Temperature (OAT) Probe

ADAHRS

One Air Data And Attitude Heading Reference System (ADAHRS) And Magnetometer

Synthetic Vision System

Synthetic Vision System (SVS)

Terrain Awareness and Warning System

Helicopter Terrain Awareness And Warning System (HTAWS) Features

Fuel Flow Indication

Fuel Flow Indication With Range Ring Display Capability

Flight Data Recording

Flight Data Recording Of 60 Standard Aircraft And Engine Parameters

Electrical System

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

Pitot Heat

Heated Pitot Tube And Static Ports

Lighting

LED Lighting: Anti-Collision Strobe

Tail Rotor Video Camera

Tail Rotor Video Camera System With Capability To View Approximately 25 Feet In Complete Darkness