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Aircraft record

N9623F1970 Hughes 269C

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply2 service difficulty reports

Registration
Valid
expires Feb 29, 2028
Based in
Pompton Plains, NJ
owner city / state
Engine
I0360 SER · 180 hp
Lycoming
Owners
1
since 1988
NTSB events
None
since 1982
ADs may apply
5
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Pompton Plains, NJ
Certificate issued
Aug 17, 1988
Expires
Feb 29, 2028
Airworthiness
Standard · Normal
Airworthiness date
May 29, 1986

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
1970
Serial number
800031
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
AD665B

Engine

Make and model
Lycoming I0360 Ser
Type
Reciprocating
Power
180 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. 1988 – nowIndividual ownerPompton Plains, NJ · current

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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

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 (2)

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.

  • Electrical power · pulley · damagedMay 12, 1999

    ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. PROBLEM HAS NOT RECURRED. POSSIBLE CAUSE IS FATIGUE OF COOLING FINS. SUBMITTER SUGGESTED INSPECTION OF FINS EACH 100 HOURS FOR CRACKS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · alternator · damagedMay 1, 1999

    ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. PROBLEM HAS NOT RECURRED. POSSIBLE CAUSE IS FATIGUE OF COOLING FINS. SUGGEST INSPECTION OF FINS EACH 100 HOURS FOR CRACKS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

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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