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Aircraft record

N2437S1976 Cessna 210L

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 6, 2020.

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply7 service difficulty reports

Registration
Deregistered
Last based in
Lees Summit, MO
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Aviasol LLC
Owner type
LLC
City, state
Lees Summit, MO
Canceled
May 6, 2020
Airworthiness
Standard

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
210L
Year
1976
Serial number
21061281
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
A23E82

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. until 2020Aviasol LLCLees Summit, MO

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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
2020-03-16Fuselage Main, StructureMar 9, 2020Airframe (210L)
2012-10-04WingsJun 5, 2012Airframe (210L)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 (210L)
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 (7)

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.

  • Reciprocating engine · cylinder · leakingJun 29, 2012

    DURING A 100 HOUR INSPECTION, COMPRESSION TEST LEAK CHECK WITH SOAPY WATER, A CRACK WAS FOUND AT FIRST FIN, INTO COMBUSTION CHAMBER. REPLACED WITH NEW CYLINDER ASSY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder head · crackedJun 29, 2012

    DURING 100 HR INSPECTION, COMPRESSION TEST, LEAK CHECK WITH SOAPY WATER FOUND A CRACK IN CYLINDER HEAD FROM TOP OF SPARK PLUG HOLE TO INTAKE VALVE. REPLACED WITH NEW CYLINDER ASSY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder · crackedMar 2, 2012

    DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LONG. REPLACED PROT 4 TO 6 INCHES LONG. REPLACED BOTH WITH NEW CYLINDER ASSY. NR 3 CYLINDER, SN 61105-24. NR 5 CYLINDER, SN 61105-22.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Reciprocating engine · cylinder · crackedMar 2, 2012

    DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LONG. REPLACED PROT 4 TO 6 INCHES LONG. REPLACED BOTH WITH NEW CYLINDER ASSY. NR 3 CYLINDER, SN 61105-24. NR 5 CYLINDER, SN 61105-22.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder · crackedJan 10, 2006

    CRACKED AT BARREL AND HEAD. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder head · crackedJan 10, 2006

    CRACKED AT BARREL AND HEAD. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · mount · defectiveJul 27, 2000

    PART LABELLED/MANUFACTURED WRONG. NOTICED LT FORWARD ENGINE MOUNT SAGGING. UPON FURTHER INSPECTION, FOUND PART LABELLED ''TOP FORWARD MTG'', BUT DID NOT HAVE REINFORCEMENT WASHER BUILT IN. CHECKED ALL OTHER P/N J-12453-2 MOUNTS IN STOCK, ALL LABELLED ''TOP FORWARD MOUNTING'' AND HAVE REINFORCEMENT…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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