Description

Bell 407 – 2003

AIRFRAME:
TTSN: 4295 hrs

ENGINE:
Engine TTSN: 4295 Hrs
Engine Type: Rolls Royce 250
Engine Cycles: 7710

FEATURES:
Dual Pilot Controls
Air Comm Dual Evap Air Conditioning Kit
Air Comm Bleed Air Heater w/Chin Bubble Defrost
Aux Fuel Tank Provisions installed
Bristol Wire Strike Protection System

AVIONICS:
Garmin G1000NXi
Garmin GTX-345R Transponder
Garmin GMA-350Hc Audio Panel
Garmin GRA-55 Radar Altimeter
Artex ME406HM 406Mhz ELT
Garmin GDL-69AH XM Wx
Mid-Continent MD302
Garmin Flight stream 510
Onboard Systems E-87

The Bell 407 is a four-blade, single-engine, civil utility helicopter; a derivative of the Bell 206L-4 Long Ranger.
The 407 uses the four-blade, soft-in-plane design rotor with composite hub developed for the United States Army’s OH-58D Kiowa Warrior instead of the two-blade, semi-rigid, teetering rotor of the 206L-4

Bell 407 Speed Performance

• Maximum speed: 140 kn (160 mph, 260 km/h)
• Cruise speed: 133 kn (153 mph, 246 km/h)
• Range: 324 nmi (373 mi, 600 km)
• Service ceiling: 18,690 ft (5,700 m)

For detailed specs, please visit this page: BELL SPECS
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