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Aircraft record

N682RC1980 Cessna TU206G

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 4, 2009.

Safety record in brief:1 NTSB accident (substantial damage, Aug 2009)3 ADs may apply2 service difficulty reports

Registration
Deregistered
Last based in
Woodinville, WA
owner city / state
Engine
TSIO-520 SER · 300 hp
Cont Motor
Owners
1
since 2007
NTSB events
1
substantial, 2009
ADs may apply
3
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Woodinville, WA
Certificate issued
Aug 7, 2007
Canceled
Nov 4, 2009
Airworthiness
Standard · Normal
Airworthiness date
Feb 12, 1980

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
Cessna
Model
TU206G
Year
1980
Serial number
U20605537
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
A90C1F

Engine

Make and model
Cont Motor Tsio-520 Ser
Type
Reciprocating
Power
300 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. 2007 – 2009Individual ownerWoodinville, WA

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

Aug 28, 2009 · Ballard, WA

The pilot's precautionary water landing with partially extended landing gear. Contributing to the accident was the unidentified anomaly with the airplane's electrical system, which rendered the gear position indicator system inoperative.

Damage
Substantial
Injuries
Minor
Report
WPR09LA423

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR09LA423)

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
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (TU206G)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.
2008-10-02Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…May 12, 2008Airframe (TU206G)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007.

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.

  • Wings · bracket · crackedMar 5, 1999

    THIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROTATION CAUSED THIS CONDITION. THESE PARTS SHOULD BE INSPECTED ON ALL ROBERTSON EQUPPED AIRCRAFT. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · bracket · crackedMar 5, 1999

    THIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROBERTSON CAUSED THIS CONDITON. ALL ROBERTSON STOL EQUIPPED AIRCRAFT SHOULD HAVE THIS BRACKET INSPECTED. (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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