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Aircraft record

N502CH1978 Hughes HUGHES 369D

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply5 service difficulty reports

Registration
Valid
expires Apr 30, 2027
Based in
Destin, FL
owner city / state
Owners
1
since 2008
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Vertol Systems Co INC
Owner type
Corporation
City, state
Destin, FL
Certificate issued
Apr 2, 2008
Expires
Apr 30, 2027
Airworthiness
Standard · Normal
Airworthiness date
Apr 12, 1995

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
HUGHES 369D
Year
1978
Serial number
180252D
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H3WE
Mode S code
A64198

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
  1. 2008 – nowVertol Systems Co INCDestin, FL · 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 (3)

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
2006-16-04Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Sep 7, 2006Engine (250-C20 SER)
2006-13-06Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Jul 26, 2006Engine (250-C20 SER)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed.
2005-10-13Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E…Jun 22, 2005Engine (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 (5)

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.

  • Main rotor · mast · corrodedSep 13, 2004

    DURING 100 HR INSPECTION, THE MAIN ROTOR DRIVESHAFT WAS REMOVED FOR INSPECTION. THE MECHANIC LOOKED DOWN THE MAST AND FOUND THE PAINT ON THE INSIDE DIAMETER WAS BLISTERED AND PEELING. THE MECHANIC ALSO NOTICED PAINT ON THE TOP OF THE MAIN TRANSMISSION SPLINES. THE MAIN ROTOR MAST WAS REMOVED AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Rotor flight controls · bracket · crackedJan 18, 2002

    LT TORQUE PEDAL BRACKET FAILED PRIOR TO ENG START ON GROUND. FAILED BRKT ASSY WAS SENT TO LOCAL LAB FOR FRACTOGRAPHIC EXAMINATION. -7 (RT) BRACKET FROM SAME HELICOPTER AND BOTH -8 AND -7 BRACKETS FROM SECOND HELICOPTER WERE REMOVED FOR VISUAL AND NDT INSP. EVIDENCE OF FATIGUE CRACK IN A RADIUS AT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · pin · brokenJul 7, 2000

    VISUAL INSPECTION REVEALED BROKEN PIN. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Engine oil · sender · failedJun 18, 1998

    AFTER 14.2 HOURS, THE OIL TEMPERATURE STARTED READING HIGH. AFTER TROUBLESHOOTING, THE SENDER WAS CHANGED AND THE PROBLEM WAS CORRECTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · blade pin · failedSep 4, 1996

    DURING THE 100-HOUR INSPECTION WHILE BLADES WERE BEING REMOVED FOR INSPECTION, THE MAIN ROTOR BLADE PIN S/N 09884-6097 FELL APART. THE BLADE PIN SHANK BROKE AT THE POINT WHERE THE THREADS START. PART TT: 4667.2. PART HAS A LIFE LIMIT OF 7600 HRS. (X)

    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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