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Aircraft record

N1078T1958 Sikorsky S-58HT

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 19, 2026.

Safety record in brief:1 NTSB accident (substantial damage, Mar 2008)No ADs since 1998 matched2 service difficulty reports

Registration
Deregistered
Last based in
Winder, GA
owner city / state
Engine
PT6T-3 · 900 hp
P&W Canada
Owners
1
on record
NTSB events
1
substantial, 2008
ADs may apply
0
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Winder, GA
Canceled
Jun 19, 2026
Airworthiness
Standard · Transport
Airworthiness date
Jun 4, 1991

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
Sikorsky
Model
S-58HT
Year
1958
Serial number
581016
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
14
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
1H11
Mode S code
A02237

Engine

Make and model
P&W Canada Pt6t-3
Type
Turbo-shaft
Power
900 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. until 1988Individual ownerdifferent airframe: Bell 206b S/N 2920
  2. until 2026Individual ownerWinder, GA

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

Mar 9, 2008 · Belmont, WV

The fatigue failure of a tail rotor blade during an external load lift.

Damage
Substantial
Injuries
Serious
Report
NYC08LA129

From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC08LA129)

ADs published since 1998 that may apply (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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.

  • Main rotor · shaft · crackedMay 19, 1995

    TRANSMISSION DISASSEMBLED TO INSPECT MAST (ASB 58B35-33) (234.9 HRS SINCE LAST COMPLIANCE), .25 INCH CRACK INDICATION FOUND BEGINNING AT TRAILING DOWEL PIN HOLE TOWARDS UNDERCUT IN MAST BASE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · shaft · crackedMar 7, 1995

    TRANSMISSION DISASSEMBLED FOR OVERHAUL. PERFORMED MAGNAFLUX INSPECTION OF MAST FOLLOWING STRUCTURAL FAILURE OF ANOTHER MAST IN ANOTHER AIRCRAFT. FOUR INCH CRACK INDICATION FOUND BEGINNING AT DOWEL PIN HOLE TO UNDERCUT IN MAST BASE THEN UP MAST THROUGH BEARING MOUNT AREA. AIRCRAFT HAS BEEN LOGGING…

    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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