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Aircraft record

N961CC1981 Cessna 210N

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 4, 2020.

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply4 service difficulty reports

Registration
Deregistered
Last based in
San Diego, CA
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
since 2016
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
San Diego, CA
Certificate issued
Feb 18, 2016
Canceled
Aug 4, 2020
Airworthiness
Standard · Normal
Airworthiness date
Jan 5, 1982

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
210N
Year
1981
Serial number
21064620
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
AD6012

Engine

Make and model
Cont Motor Io 520 Series
Type
Reciprocating
Power
285 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. 2016 – 2020Individual ownerSan Diego, CA

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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (4)

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
2023-02-17Fuselage Main, StructureMar 20, 2023Airframe (210N)
2012-10-04WingsJun 5, 2012Airframe (210N)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; …
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (210N)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (IO 520 SERIES)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.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (4)

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.

  • Engine fuel and control · fcu · malfunctionedMay 21, 1999

    DURING FLIGHT, THE FUEL PRESSURE WAS NOTED TO FLUCTUATE ERRATICALLY. REPLACING THE FUEL CONTROL UNIT RESOLVED THE PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · camshaft · chippedMay 10, 1999

    DURING A ROUTINE 100-HOUR INSPECTION EXCESSIVE METAL WAS FOUND IN THE ENGINE OIL FILTER. FURTHER INVESTIGATION REVEALED A CHIPPED CAM LOBE AND LIFTER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · valve guide · wornOct 21, 1997

    DURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND PAST THE INTAKE VALVE ON THE NR 6 CYLINDER. THE REMOVED CYLINDER, INTAKE VALVE AND GUIDE WERE FOUND WORN OUT. THE VALVE LASH WAS ALSO FOUND TO BE EXCESSIVE ON THE NR'S 2, 4, AND 6 CYLINDERS. THE PUSH RODS WERE REPLACED WITH .030 INCH OVERSIZE.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Reciprocating engine · valve guide · wornMar 21, 1997

    DURING A ROUTINE COMPRESSION CHECK, EXCESSIVE LEAKAGE PAST THE PISTON RINGS WAS FOUND ON THE THE NR 2 CYLINDER. THE REMOVED CLYINDER WAS FOUND WORN OUT AND THE PISTON RINGS STUCK IN THE RING GROOVES. SUBMITTER SUGGESTED POSSIBLE CAUSE AS EXCESSIVE LEAD SLUDGE BUILD-UP FROM THE USE OF TCM APPROVED…

    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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