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Aircraft record

N9592F1974 Hughes 269C

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 23, 2013.

Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Nov 1989)5 ADs may apply

Registration
Deregistered
Last based in
Hillsboro, OR
owner city / state
Engine
HIO-360 SER · 205 hp
Lycoming
Owners
1
since 1993
NTSB events
2
destroyed, 1989
ADs may apply
5
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Helicopter Speacialties INC
Owner type
Corporation
City, state
Hillsboro, OR
Certificate issued
May 14, 1993
Canceled
May 23, 2013
Airworthiness
Standard · Normal
Airworthiness date
Jun 11, 1974

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
Hughes
Model
269C
Year
1974
Serial number
440296
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
4H12
Mode S code
AD58BA

Engine

Make and model
Lycoming Hio-360 Ser
Type
Reciprocating
Power
205 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1993 – 2013Helicopter Speacialties INCHillsboro, 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 (2)

Accident · destroyed

Nov 15, 1989 · Estacada, OR

THE PILOT MISJUDGED CLEARANCE BETWEEN HER EXTERNAL LOAD AND THE OBSTRUCTION. FACTORS RELATED TO THE ACCIDENT WERE: THE OBSTRUCTION, IMPROPER MAINTENANCE AND MODIFICATION OF THE EXTERNAL LOAD LINE/HOOK BY THE OPERATOR, FAILURE OF THE PILOT TO JETTISON THE EXTERNAL LOAD, AND A FAILURE OF THE OPERATOR MANAGEMENT TO ASSURE THE PILOT HAD RECEIVED ADEQUATE TRAINING/CERTIFICATION.

Damage
Destroyed
Injuries
Fatal
Report
SEA90LA016

From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA90LA016)

Accident · substantial damage

Mar 20, 1985 · Elma, WA

JUST PRIOR TO LIFT-OFF A VIBRATION ACCOMPANIED BY LATERAL ROCKING OCCURRED. ALTHOUGH THE PLT BROUGHT THE POWER TO IDLE. THE HELICOPTER HAD ALREADY STARTED TO COME APART. DURING ENGINE EXAMINATION IT WAS FOUND THAT THE GROUND RESONANCE OCCURRED DUE TO UNDER TO RQ WING OF THE MAIN ROTOR DAMPNERS. THE DAMPNERS HAD BEEN SERVICED JUST 1.5 HOURS PRIOR TO THIS ACCIDENT.

Damage
Substantial
Injuries
None
Report
SEA85LA079

From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA85LA079)

Accident history for this model

ADs published since 1998 that may apply (5)

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.

ADSubjectEffectiveApplies to
2017-14-06Sikorsky Aircraft Corporation Helicopters (Type Certificate Previously Held by Schweizer…Aug 25, 2017Airframe (269C)Only with: Lower coupling driveshaft P/N 269-5412, 269A5504, 269A5504-003, 269A5504-005, 269A5559, or 269A5559-003 installed.
2015-23-01Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft…Dec 15, 2015Airframe (269C)
2001-25-52Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A HelicoptersMay 8, 2002Airframe (269C)Only with: With tailboom support strut assemblies P/N 269A2015 or 269A2015-5, tailboom center attach fitting P/N 269A2324, or center frame aft cluster fitting P/N 269A2234 or 269A2235 installed.
99-17-10Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D…Sep 2, 1999Airframe (269C)Only with: Tail rotor swashplate shaft P/N 269A6049-3 installed.
95-21-02Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B…Nov 17, 1995Airframe (269C)Only with: Main rotor drive shaft P/N 269A5305-3 or 269A5305-11 installed, except drive shafts with serial number prefix "SZ" or "ZS".

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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