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Aircraft record

N18JC1974 Helio HT-295

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jan 2025)No ADs since 1998 matched1 service difficulty report

Registration
Valid
expires Apr 30, 2028
Based in
Gaithersburg, MD
owner city / state
Owners
1
since 1998
NTSB events
1
substantial, 2025
ADs may apply
0
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Winged Vision Incorporated
Owner type
Corporation
City, state
Gaithersburg, MD
Certificate issued
Sep 9, 1998
Expires
Apr 30, 2028
Airworthiness
Standard · Normal
Airworthiness date
Nov 25, 1998

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
Helio
Model
HT-295
Year
1974
Serial number
1719
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A13F1E

Engine

Make and model
Lycoming Go-480 Series
Type
Reciprocating
Power
295 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. 1998 – nowWinged Vision IncorporatedGaithersburg, MD · current

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 (1)

Accident · substantial damage

Jan 5, 2025 · Marion, OH

The failure of the right main landing gear spring due to intergranular stress-corrosion cracking that progressed into fatigue. Contributing to the accident was the improper rework of the spring at an undetermined time.

Damage
Substantial
Injuries
None
Report
ERA25LA091

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA25LA091)

Accident history for this model

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 (1)

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.

  • Fuselage · saddle · crackedApr 19, 2013

    RIGHT MAIN GEAR ATTACH AREA (STEEL TUBE STRUCTURE) FOUND CRACKED AT THE REAR INBD SIDE OF THE GEAR SADDLE. WEDGES WERE LOOSE, POSSIBLY CONTRIBUTING TO GEAR MOVEMENT.

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

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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