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
Eurocopter
Model
AS 350 B2
Year
1993
Serial number
2759
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H9EU
Mode S code
ACB186
Engine
Make and model
Turbomeca Arriel 1ser
Type
Turbo-shaft
Power
681 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
1998 – 2013Individual ownerMcminnville, OR
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 · substantial damage
Apr 11, 2002 · Valdez, AK
The pilot's failure to disengage the hydraulic system, and maintain forward airspeed during landing as delineated in the emergency procedures section of the helicopter's operations manual, which resulted in a loss of control while hovering. Factors contributing to the accident were the separation of the hydraulic pump drive belt, and the subsequent lockup of the flight control system.
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.
Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and…
Sep 2, 2010
Airframe (AS 350 B2)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N 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.
Tail rotor · blade · looseJun 15, 1999
DELAMINATION OF SS LEADING EDGE BOTH SIDES OF ONE BLADE. SUBMITTER STATED THIS BLADE HAD JUST HAD THE SAME PROBLEM 86.1 HOURS AGO. INSPECTION OF RECORDS REVEALED THIS PARTICULAR SIDE WAS FACTORY ORIGINAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.