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Aircraft record

N117P1976 Cessna T210L

Registration validUnclaimedSource: FAA, updated Oct 16, 2026

Safety record in brief:1 NTSB accident (substantial damage, Mar 1983)5 ADs may apply1 service difficulty report

Registration
Valid
expires Nov 30, 2029
Based in
Wichita, KS
owner city / state
Engine
TSIO-520 SER · 300 hp
Cont Motor
Owners
1
since 2022
NTSB events
1
substantial, 1983
ADs may apply
5
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Registered owner
Co-owners
City, state
Wichita, KS
Certificate issued
Nov 17, 2022
Expires
Nov 30, 2029
Airworthiness
Standard · Normal
Airworthiness date
Jun 26, 1976

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
T210L
Year
1976
Serial number
21061407
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
A04779

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. 2022 – nowCo-ownersWichita, KS · current
  2. Date unknownIndividual ownerdifferent airframe: Beechcraft 35 S/N D1210

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Mar 7, 1983 · Farmington, MN

DURING AN IFR FLIGHT, THE ENGINE LOST POWER AT 4000 FT MSL AND THE PILOT WAS UNABLE TO RESTART THE ENGINE. HE BROKE OUT OF THE CLOUDS AT A LOW ALTITUDE IN THE VICINITY OF A LAKE THAT WAS COVERED WITH ICE. THE PILOT DID NOT KNOW THE CONDITION OF THE ICE, SO HE LANDED WITH THE GEAR UP FOR BETTER DISTRIBUTION OF THE WEIGHT. THE AIRCRAFT SKIDDED OVER THE ICE FOR SEVERAL HUNDRED FEET, THEN BROKE…

Damage
Substantial
Injuries
None
Report
CHI83LA130

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI83LA130)

Accident history for this model

ADs published since 1998 that may apply (5)

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 (T210L)
2012-10-04WingsJun 5, 2012Airframe (T210L)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 (T210L)
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 (T210L)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 (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.

  • Landing gear · wheel · crackedAug 1, 1997

    BOTH MAIN WHEELS CRACKED. THESE ARE 3-PIECE WHEELS USED ON VARIOUS CESSNA SINGLES IN THE 1970'S. THIS SUBMITTER FEELS A MORE LIKELY CAUSE (OTHER THAN OVERTORQUING) IS STRESS CAUSED BY PULLING SMALL AMOUNTS OF ALUMINUM THROUGH THE THREADS EACH TIME THE BOLTS ARE REMOVED WHICH TENDS TO SPREAD THE…

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

Sources

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

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