Description
Bell 407 GX – 2012 White
- TT: 385 HRS
- June Model 2012
- Auto Pilot
- Executive Full House Option
- Dual Controls with safety covers
- High Skid Gear with flite step
- Rotor Brake
- AFS Inlet Barrier Filter
- High Visibility main rotor blades
- Blade folding kit
- Tail Rotor Camera
- Wire Strike Protection System
- 19Gal Aux Fuel tank
- Aircomm Air conditioner w/ dual forward evaporators
- Artic Bleed Air Heater w/ Defroster
- Cargo Hook Provisions
- Litter Provisions
- Jettinsonable Crew doors
- Preflight kit w/ folding steps & Dual step handles
- Pneumatic door openers
- Co-pilot Tail rotor pedal lockout kit
- Cabin & baggage floor protectors
- Spacemaker baggage extender
- Baggage compartment edge protector
- 5250lbs Gross weight kit
- Locking fuel cap
- Pulse landing light kit
- Snow baffles
- Power plus STC
- Hat Rack safety net
- Bear Paws
- 28 amp battery
AVIONICS
- Garmin G1000H System w/ Dual GDU 10.4” LCD PFD & MFD Interchangeable displays w/ Synthetic Vision System (SVS) & initial HTAWS & NAV databases
- 2-Axis HeliSAS Auto Pilot w/ Heading, NAV, ALT & Auto Recovery modes
- Garmin AERA 796 Touch screen w/ Gizmo panel mount
- Dual GIA 63H Integrated Avionics unit
- GPS: Dual WAAS
- VHF COMM: Dual – 16 Watt / 8.33 kHz spacing
- VHF, Nav & Glideslope: Dual
- Audio Control panel: Garmin GMA 350H
- Garmin GTX 33 H Mode S Transponder w/ extended Squitter & ADS-B Out capability w/ TIS
- TAS: Garmin GTS 800
- Garmin GDL 69A XM Satellite Weather & Radio
- GEA 71H Engine & Airframe Unit
- GDC 74H Air Data Computer
- GRS 77H Altitude & Heading reference system (AHRS)
- Standby air speed, Altimeter & Compass
- Artex C406-NHM ELT w/ NAV Interface & Transmit on 406, 243.0, 121.5
- 2 Bose A20 Headsets
*Sold*
History
In 1993, Bell began the development of a new light Aircraft in order to replace its Model 206 series. The program resulted in the 407, a development of Bell’s LongRanger. Bell modified a 206L-3 LongRanger to serve as a 407 demonstrator. The demonstrator used hardware for the 407… and added moulded fairings for wider fuselage representation. The demonstrator was first flown in April 1994. The first 407 prototype accomplished its maiden flight in June 1995. The second prototype followed in July 1995. The first production 407 flew in November 1995. TCAA granted certification for the 407 on February 9 1996 and the FAA followed shortly after on February 23 1996.
Design
The Bell 407 features a four blade main rotor. In addition, the blades and hub use composite construction without life limits. Hence this provides better performance and a more comfortable ride. The 407’s fuselage is 8 inches wider… therefore increasing internal cabin space. Additionally included are 35% larger main cabin windows. Not only is the Rolls-Royce/Allison 250-C47 turboshaft engine powerful.. but also allows an increase in Maximum take off Weight. Hence it improves performance at hotter temperatures and higher altitudes. The air-frame is similar to the LongRanger. Also included is a carbon fibre composite tail boom. The helicopter has standard seating for two crew and five cabin seats.
Bell 407 GX – 2012 White
The Bell 407 is a civil utility helicopter. Moreover it combines reliability, speed and performance… coupled with manoeuvrability. The aircraft also includes a cabin configuration for an array of missions and pay loads. The engine delivers not only exceptional performance… but also has the ability to cruise at 140 259 km/hr. The Bell 407 also provides a quiet and smooth ride in most weather conditions. The Bell 407 GX version of the 407 that features the new Garmin G1000 H-model glass cockpit along with superior avionics and improved flight controls.
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