2010 Bell 429
Delivery Position

Standard Equipped Aircraft
Optional Equipment Not Selected
 

The Bell 429 is "quite possibly the most advanced light twin IFR helicopter ever created.
Fast, impeccably appointed and more spacious than any helicopter in its class.
Intelligently designed and highly adaptable to address an array of individual needs.
It's how those who have arrived choose to travel." (Source: Bell Helicopter)

Bell 429 Features (Please refer to the Bell 429 Production Brochure for More Details)
  • Intermediate-class cabin at light twin price and operating cost
  • Seats 8 occupants in a variety of seating arrangements
  • Basic aircraft is Single Pilot IFR, Category "A" certified
  • MSG-3 Maintenance
  • Open cabin and flat floor
  • Damage tolerant hub and rotor system
  • Energy attenuating crew and passenger seats
  • Crash worthy fuel system
  • Cabin can be quickly reconfigured for a variety of mission configurations
  • Spacious 74 cu. ft. baggage compartment with access from side
  • Composite tail boom, fatigue tolerant
  • Dual Digital 3-axis autopilot with SCAS
  • Extremely low fly-over noise signature far exceeding current and anticipated ICAO standards
  • Composite tail rotor driveshaft
  • 2575 lb payload capability
  • Certified to latest airworthiness requirements (Enhanced occupant safety factor)
  • Large doors sliding/hinged combination doors on both sides of cabin for ease of access and oversize cargo
  • Superb cockpit and cabin visibility
Standard Features: (Highlights)

  • 2 Pratt & Whitney 207D1 Engines w/ Electronic Engine Controls (EEC) & Fuel Management Module (FMM)
  • 216.9 Gal (820 liters) Fuel
  • Inlet Barrier Filter & Electrical Provisions
  • Engine Fire Detector
  • Dual Bottle Fire Extinguisher System
  • Wire Strike Protection Fixed Provisions
  • Air Conditioning Fixed Provisions
  • Bleed Air Heater Fixed Provisions
  • 3 Color Paint Scheme
Standard Avionics: (Highlights)
  • EFIS/EICAS (Electronic Flight Instruments System / Engine Indicating & Crew Alerting System)
  • Two 6" x 8" LCD Displays
  • 3-Axis Autopilot
  • Dual Channel Aircraft Data Interface Unit
  • Dual Channel SCAS & Trim Actuators
  • Dual Channel AD/AHRS (Air Data/Attitude Heading Reference System)
  • Standby Instruments (Attitude, Altitude, Heading & Airspeed)
  • Electronic Data Recorder (Non-Crashworthy)
  • Dual Garmin 430 VOR/ILS/GS/Comm/GPS (WAAS Capable)
  • Garmin GTX-330 Mode S Transponder
  • Honeywell KRA-405B Radar Altimeter
  • Artex C406-N-HM ELT



SPECIFICATION SUBJECT TO VERIFICATION UPON INSPECTION
AIRCRAFT SUBJECT TO PRIOR SALE OR WITHDRAWAL FROM THE MARKET


For more information contact us at info@baliaircraft.com
615.361.3781 or fax us at 615.367.1226

 

 

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