Aircraft Finder

MD HELICOPTERS (MCDONNELL DOUGLAS) 500E(1989)

Specifications

Year1989
Serial Number0350E
RegistrationN915LY
Total Hours9,941.3
LocationHILLSBORO, OREGON
RegionNORTH AMERICA

Broker

HILLSBORO AVIATION

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AI Description

  • Model: 500E
  • Condition: Used
  • Location: Hillsboro, Oregon
  • Engine: RR 250-C20R/2
  • Engine Total Time: 9,064.3 hours
  • Engine Time Since Overhaul (TSO): 876.7 hours
  • Airframe Total Time: 9,941.3 hours
  • Dual Cargo Hook System (Onboard Systems STC SR02693LA)
  • Inlet Barrier Filter (IBF) Kit – Donaldson STC SR01394LA
  • Avionics:
  • Garmin GTR 255H Comm #1 & #2
  • Garmin GMA 340 Audio Panel
  • Garmin GTX 345 ADS-B Transponder (In / Out)
  • Garmin GA-35 WAAS GPS Antenna
  • Garmin Aera 760 Portable GPS (panel mounted)
  • Flight Instruments:
  • Airspeed Indicator
  • Altimeter
  • Vertical Speed Indicator (VSI)
  • Attitude Indicator
  • Turn Coordinator
  • Dual Tachometer
  • Interior Features:
  • Dual Controls
  • Aft Seat Belt / Shoulder Harness
  • First Aid Kit
  • Fire Extinguisher
  • Flashlight

About this Model

Overview

The MD 500E is an evolution of the Hughes/MD 500 series that emphasizes a compact footprint, responsive handling, and mission flexibility. Buyers typically consider it for utility roles where quick turns, confined-area operations, and good visibility matter more than cabin volume. The 500E’s airframe and rotor system are widely associated with training, patrol/observation, and light utility work, with numerous configuration options depending on prior operator use.

Mission Fit

Mission fit is strongest for short-to-medium stage lengths with frequent landings and repositioning. The type’s compact size supports confined landing zones and rooftop/urban operations when permitted. For buyers focused on carrying multiple adult passengers plus baggage in comfort, larger cabin helicopters tend to be a better match.

Cabin

Cabin experience is typically functional rather than spacious. Seating and interior finish vary widely by configuration and prior mission (e.g., utility, police, training), and noise/vibration expectations align with a light single-turbine helicopter. Visibility from the cockpit and forward cabin area is a common operational advantage for observation and approach/landing tasks.