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Aircraft record

N8660K1947 Universal Stinson 108

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 13, 2017.

Safety record in brief:1 NTSB accident (substantial damage, Apr 2016)No ADs since 1998 matched1 service difficulty report

Registration
Deregistered
Last based in
Centerport, NY
owner city / state
Owners
1
since 2015
NTSB events
1
substantial, 2016
ADs may apply
0
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Centerport, NY
Certificate issued
Jul 16, 2015
Canceled
Mar 13, 2017
Airworthiness
Standard · Normal, Utility
Airworthiness date
Apr 15, 1971

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
Universal Stinson
Model
108
Year
1947
Serial number
108-1660
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
ABE783

Engine

Make and model
Franklin 6a4150 Series
Type
Reciprocating
Power
150 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 – 2017Individual ownerCenterport, NY

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

Apr 30, 2016 · Calverton, NY

The pilot's failure to maintain directional control during the landing roll.

Damage
Substantial
Injuries
None
Report
ERA16LA173

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA16LA173)

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.

  • Wings · spar · corrodedNov 20, 1998

    AIRCRAFT WAS METALIZED IN 1960'S. NO INSPECTION PROVISIONS IN WINGS. FRONT SPAR ON RT WING WAS/IS SEVERELY CORRODED FROM STA 40 TO STA 80. CORROSION IS ON LEADING EDGE SIDE OF SPAR. FOUR LEADING EDGE FORMERS ALSO SEVERELY CORRODED.

    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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