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Aircraft record

N902701966 Hughes 269A

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Jun 2023)5 ADs may apply

Registration
Valid
expires Apr 30, 2028
Based in
Anderson, SC
owner city / state
Engine
HIO-360 SER · 205 hp
Lycoming
Owners
1
since 2015
NTSB events
3
substantial, 2023
ADs may apply
5
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Co-owners
City, state
Anderson, SC
Certificate issued
Apr 21, 2015
Expires
Apr 30, 2028
Airworthiness
Standard · Normal
Airworthiness date
Apr 5, 1979

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
269A
Year
1966
Serial number
66-18283
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
4H12
Mode S code
AC7A00

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. 2015 – nowCo-ownersAnderson, SC · current
  2. 1966Intermountain Aviation INCdifferent airframe: Beechcraft Snb-5 S/N 39777

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (3)

Accident · substantial damage

Jun 27, 2023 · Anderson, SC

The mechanics’ improper torquing of the main rotor blade dampers, which resulted in a ground resonance event during landing.

Damage
Substantial
Injuries
None
Report
ERA23LA289

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA23LA289)

Accident · substantial damage

Dec 26, 1990 · Sellersburg, IN

A PILOT INDUCED LOSS OF ENGINE POWER BY INADVERTENT DEACTIVATION OF THE FUEL MIXTURE CONTROL.

Damage
Substantial
Injuries
None
Report
CHI91LA048

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI91LA048)

Accident · substantial damage

Feb 20, 1987 · Jacksonville, FL

THE INSTRUCTOR PLT WAS DEMONSTRATING A HOVERING AUTOROTATION LANDING WITH FORWARD MOVEMENT, WHEN, AFTER THE THROTTLE WAS CLOSED, THE HELICOPTER HUNG IN THE AIR. FORWARD CYCLIC WAS THEN APPLIED WHEN HE REALIZED THAT THE ROTOR RPM BEGAN TO DETERIORATE. THE HELICOPTER THEN CONTACTED THE GROUND IN A SLIGHT NOSE LOW ATTITUDE, AFTER WHICH, REAR CYCLIC WAS APPLIED. THE MAIN ROTOR BLADES THEN SEVERED…

Damage
Substantial
Injuries
None
Report
MIA87LA089

From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA87LA089)

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 (269A)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 (269A)
2001-25-52Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A HelicoptersMay 8, 2002Airframe (269A)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 (269A)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 (269A)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 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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