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ROBINSON R44 RAVEN II(2008)

Specifications

Year2008
Serial Number--
Registration--
Total Hours1,150
LocationSOUTHERN AFRICA, SOUTH AFRICA
RegionAFRICA

Broker

PACIFIC AIRHUB AIRCRAFT SALES

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AI Description

  • Model: R44 Raven II
  • Year: 2008
  • Configuration: Passenger / Corporate
  • Airframe Hours: 1,150
  • Engine Hours Remaining: 1,050 (of 2,200 total)
  • Airframe Hours Remaining: 1,050 (of 2,200 total)
  • 12-Year Airframe Inspection: 7 years remaining
  • 12-Year Engine Inspection: 7 years remaining
  • Avionics:
  • Nine Hole Panel
  • Artificial Horizon
  • Direction Indicator
  • Altimeter
  • Vertical Speed Indicator
  • Bendix King Transponder and Comm
  • Garmin 420 GPS
  • Additional Features:
  • Air-Conditioning
  • Bubble Windows
  • Leather Seats
  • All Service Bulletins (SBs) and Airworthiness Directives (ADs) completed

About this Model

Overview

The Robinson R44 Raven II is a single-engine, four-seat light helicopter commonly used for primary/advanced training, personal transport, utility support, and aerial observation. It emphasizes straightforward systems, a relatively low cockpit workload for its class, and broad parts/service availability in many regions. Typical missions center on short to moderate legs with payload managed around fuel, passengers, and environmental conditions (heat/high altitude).

Mission Fit

The R44 Raven II fits operations that prioritize flexible point-to-point access and time-on-task over long range or high payload. It is well suited to mixed use—training plus personal travel—where dispatch reliability depends on disciplined weight-and-balance planning and realistic hot-and-high performance margins.

Cabin

The cabin is compact but practical for four occupants, typically arranged as two front seats and a rear bench. Large windows support outward visibility for training and observation. Noise and vibration are typical of a piston helicopter, so passenger comfort improves with quality headsets and thoughtful loading. Baggage capability is modest and sensitive to fuel load and density altitude.