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Aircraft record

N6628K1993 Windler Socoy Steven TRI Q2

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 25, 2018.

Safety record in brief:1 NTSB accident (destroyed damage, Sep 2006)No ADs since 1998 matched

Registration
Deregistered
Last based in
New Port Richey, FL
owner city / state
Engine
C85 SERIES · 85 hp
Cont Motor
Owners
1
since 1999
NTSB events
1
destroyed, 2006
ADs may apply
0
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
New Port Richey, FL
Certificate issued
Feb 8, 1999
Canceled
Jan 25, 2018
Airworthiness
Experimental · Amateur Built
Airworthiness date
May 18, 1993

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
Windler Socoy Steven
Model
TRI Q2
Year
1993
Serial number
1969SW
Aircraft type
Fixed wing single engine
Category
Land
Certification
Not Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A8BF21

Engine

Make and model
Cont Motor C85 Series
Type
Reciprocating
Power
85 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. 1999 – 2018Individual ownerNew Port Richey, FL
  2. 1979Grumman American Aviation CorpElmira, NY · different airframe: Grumman Acft Eng Cor-Schweizer G-164c S/N 10c
  3. 1947 – 1956Bellingham Air Service INCBellingham, WA · different airframe: Republic Rc-3 S/N 901

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 · destroyed

Sep 22, 2006 · Branson, MO

Fatigue failure, originating in an area of surface corrosion, of the right elevator mid span hinge pin and the subsequent failure of the elevator torque tube. Additional causes are the separation of the elevator from the airframe due to the hinge pin and torque tube failures, and the pilot's inability to maintain control of the airplane after separation of the control surface.

Damage
Destroyed
Injuries
Fatal
Report
CHI06LA268

From NTSB records; matched by N-number.Read NTSB report (search CAROL for CHI06LA268)

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 (0)

No Service Difficulty Reports found for this airframe since 1995.

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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