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BELL 427(2009)

BELL 427

Specifications

Year2009
Serial Number56077
RegistrationN427UV
Total Hours1,114.8
LocationSANTO DIMINGO, DOMINICAN REPUBLIC
RegionNORTH AMERICA

Broker

PORTLAND JETS

Visit website

+14752981326

Aircraft Details

  • Model: BELL 427
  • Type: Helicopter
  • Engine: Twin Engine
  • Seating Capacity: 7
  • Maximum Takeoff Weight: 3,175 lbs
  • Cruise Speed: 130 knots
  • Range: 400 nautical miles
  • Avionics: Advanced avionics suite
  • Features: Spacious cabin, excellent visibility, and high performance
  • Maintenance: Well-maintained with comprehensive records
  • Interior: Customizable interior options available
  • Exterior: Sleek design with modern aesthetics

The listing suggests a potential for co-ownership, as it highlights shared usage benefits and operational cost efficiencies.

About this Model

Overview

The Bell 427 is a skid-gear, twin-engine light helicopter developed from the Bell 407/206L lineage, positioned for operators who want straightforward twin-engine capability with familiar Bell handling and support. Typical use cases include corporate and private transport, utility support, and EMS-style configurations where payload flexibility and stable low-speed handling matter more than long-range cruise.

Mission Fit

The 427 generally fits missions that live within a light-twin helicopter’s fuel and payload envelope: multiple daily hops, mixed passenger/cargo loads, and operations that value twin-engine safety margins and stable low-speed work. It is less suited to missions dominated by maximum-range legs, consistently heavy payloads, or hot/high conditions that push performance margins—areas where stepping up in class is usually more efficient.

Cabin

Cabin layout is typically configured for executive transport or missionized roles, with a relatively flat, usable cabin floor area for the class and wide access through large doors. Noise/vibration levels and comfort depend heavily on interior completion and rotor/drive-train condition; buyers should evaluate the specific aircraft’s insulation, seating, and mission equipment integration rather than assuming a uniform standard across the fleet.