We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Aerospatiale
Model
AS355F2 ECUREUIL
Year
1991
Serial number
5489
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
7
Engines
2
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H11EU
Mode S code
A3F7BE
Engine
Make and model
Allison 250-C20 Ser
Type
Turbo-shaft
Power
420 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
1993 – 2003Duke UniversityDurham, NC
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · destroyed
Oct 17, 2000 · Burlington, NC
The mechanics failure to comply with manufacturers instructions for correction of a illuminated main rotor gearbox oil pressure warning light resulting in the helicopter being dispatched on a ferry flight with a failed main rotor gearbox oil pump, failure of the main rotor gearbox combining gearbox gears due to oil starvation, loss of main rotor RPM, and the helicopter colliding with trees and…
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
Engine (250-C20 SER)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, installed.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Fire protection · fire wire · brokenFeb 17, 1996
DURING APPROACH, NR 1 FIRE LIGHT DIMLY ILLUMINATED THEN EXTINGUISHED. DURING HOVER, NR 1 FIRE LIGHT DIMLY ILLUMINATED ONCE MORE AND ON ENGINE SHUT-DOWN, CAME ON FULL BRIGHT. NO FIRE WITNESSED. FOUND/REPAIRED BROKEN WIRE TO FIRE DETECTOR TO FUEL PUMP STATION.
From FAA Service Difficulty Reports; matched by N-number and serial number.