2017 BELL 407 GXP

2017 Bell 407GXP

The 2017 Bell 407GXP, with serial number 54707, is a single-engine, light utility helicopter distinguished by its vibrant orange exterior. Currently registered as TBD, this helicopter has logged approximately 620 total hours since new. It is powered by the reliable Rolls-Royce 250-C47B/8 turboshaft engine, featuring Full Authority Digital Engine Control (FADEC). The combination of modern avionics, proven performance, and a versatile cabin layout makes this aircraft ideal for both utility and executive operations.

Aircraft Highlights:
This Bell 407GXP is equipped with the advanced Garmin G1000H Integrated Avionics Suite, providing
pilots with a modern glass cockpit environment. One of the standout features is the 2-Axis Bell AutoPilot Flight Control System, which enhances stability, precision, and reduces pilot workload during all
phases of flight. To further ensure passenger comfort, the Dual Forward Evaporators Air Conditioner
delivers superior cooling performance, particularly in hot and humid environments. The helicopter
integrates crash-resistant fuel systems and seating, accommodates up to six passengers, and is powered
by the renowned Rolls-Royce 250-C47B/8 engine with FADEC for efficiency and reliability. a two-blade, semi-rigid composite unit. Both rotor systems utilize elastomeric bearings and allow for individual blade replacement, simplifying maintenance and reducing operating costs.

Controls:
The flight control system is supported by
dual redundant hydraulics, ensuring both
reliability and safety. Features such as
force trim and artificial feel systems
enhance pilot comfort, while adjustable
cyclic, collective, and directional pedals
provide for precise handling.
Additionally, droop and flapping restraint
mechanisms contribute to stable and
predictable flight performance.

Powerplant and Fuel System:
At the heart of the Bell 407GXP is the Rolls-Royce 250-C47B/8 turboshaft engine equipped with FADEC,
ensuring optimized performance and efficiency. The engine delivers 862 shaft horsepower (shp) for
takeoff and 813 shp continuously. Fuel is stored in crash-resistant bladder tanks with a total capacity of
approximately 127 US gallons.
Transmission and Drive
The main transmission is rated for 862 shaft horsepower at takeoff and features a two-stage planetary
gearbox with an integrated freewheeling unit. Power is transmitted to the tail rotor via a driveshaft
system, incorporating intermediate and tail rotor gearboxes to ensure smooth and efficient operation.
Avionics:
The cockpit of the Bell 407GXP is centered around the Garmin G1000H Integrated Avionics Suite, which
features dual 10.4-inch LCD displays for both primary flight and multifunction data. Enhanced situational
awareness and safety are provided by Synthetic Vision Technology, a Helicopter Terrain Awareness and
Warning System, and an integrated Flight Management System. Standard avionics include VHF
communication and navigation radios, GPS, and a Mode-S transponder. The 2-Axis Bell Auto-Pilot Flight
Control System further augments safety by offering stability enhancement and automatic pitch and roll
control.
awareness for the pilot.

Safety and Warning Systems:
Safety features include a master caution and warning system, supported by aural alerts and advisory
messages. An engine fire detection and extinguisher system provides additional protection, while an
Emergency Locator Transmitter (ELT) ensures rapid location in the event of an emergency.
 

Interior and Cabin:
The cockpit is fitted with crash-resistant pilot and co-pilot seats equipped with lap belts and shoulder
harnesses. An anti-reflection instrument panel enhances visibility, and a portable fire extinguisher is
installed for added safety. The passenger cabin seats up to six passengers and features intercom and
loudspeaker systems, reading lights, ventilation outlets, and large windows, offering excellent visibility
and a comfortable travel experience.

Environmental and Utility Equipment:
Passenger comfort is further enhanced by the Dual Forward Evaporators Air Conditioner, providing
superior cooling performance. Additional equipment includes a rotor brake, and provisions for external
cargo hook, making the aircraft highly adaptable for a wide range of missions.

Aircraft Equipment List, Standard
1 28 Amph Battery
2 Aux Fuel Tank Provisions (19Gal)
3 Doors-Jettisonable (Crew Only)
4 Dual Controls
5 Glass Cockpit-G1000 (Garmin) G1000NXi
6 High Skid Gear with Flight Steps
7 LED Lighting (Interior/Exterior)
8 Main Rotor Blades - High Visibility
9 Rotor Brake
10 Tail Rotor Camera
11 Wire Strike Protection System
12 Artex C406-NHM ELT with PGM Adaptor
13 Artex C406-NHM ELT Provisions
14 Standard 3 Color Paint Scheme
15 Door Openers for Baggage Door (AA)
16 Door Openers for Jettisonable Crew Doors (AA)
17 Door Openers for Cabin Door (AA)
18 Pre-Flight Kit - 4 Handles & 2 Maintenance Steps (AA)
19 Inlet Barrier Filter 20 Aft Cabin ICS - 5 Place
21 Bleed Air Heater with Windshield & Chin Bubble Defrost (Air Comm)

Installed Optional Equipment:
1 Headliner – Standard with AC Ducting
2 Litter Provisions
3 Litter Ski Provisions
4 Cargo Hook Provisions Kit (P/N 206-706-341-111)
5 Radar Altimeter #2
6 Expanded Avionics Shelf
7 Snow Baffles
8 AirComm Air Conditioner with Dual Forward Evaporators
9 Spacemaker and Cover (AA)
10 Dual Controls Hanger Kit in Baggage Compartment
11 Cut Out/Blank Plate in Avionics Panel for Onboard Systems Load Weighing System Indicator
12 Autopilot – 2-Axis Bell Auto Pilot Flight Control System
13 Ground Handling Wheels (1) Set

Engine & Mods