N5545A1985 Cessna P210R
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply3 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Individual owner
- City, state
- Kettering, OH
- Certificate issued
- Jul 23, 2020
- Expires
- Jul 31, 2027
- Airworthiness
- Standard · Normal
- Airworthiness date
- Sep 30, 1985
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 dataAirframe
- Manufacturer
- Cessna
- Model
- P210R
- Year
- 1985
- Serial number
- P21000864
- 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
- A7114F
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- 2020 – nowIndividual ownerKettering, OH · current
- 1967 – 1968Individual ownerHuntsville, TX · different airframe: Cessna 170 S/N 19657
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs 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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-02-17 | Fuselage Main, Structure | Mar 20, 2023 | Airframe (P210R) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (P210R)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; … |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (P210R) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (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. |
| 98-05-14 R1 | Cessna Aircraft Company Models T210N, P210N, and P210R Airplanes | Sep 22, 1998 | Airframe (P210R)Certain serial numbers: T210N 21063641–21064897; P210N P21000386–P21000834 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
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 · exhaust valve · wornJul 20, 2000
CYLINDER NR 1 WAS RUNNING TOO COOL. WEAK COMPRESSION WAS NOTED PULLING PROPELLER THROUGH. COMPRESSION TEST RESULTS 65/80. FERROUS METAL NOTED IN FILTER ELEMENT. ROCKER COVER WAS REMOVED. ROCKER ARM FOR EXHAUST WAS HITTING ON SPRING RETAINER. END OF EXHAUST VALVE WAS WORN DOWN TO KEEPER. CONTINUED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · keeper · wornJul 20, 2000
CYLINDER NR 1 WAS RUNNING TOO COOL. WEAK COMPRESSION WAS NOTED PULLING PROPELLER THROUGH. COMPRESSION TEST RESULTS 65/80. FERROUS METAL NOTED IN FILTER ELEMENT. ROCKER COVER WAS REMOVED. ROCKER ARM FOR EXHAUST WAS HITTING ON SPRING RETAINER. END OF EXHAUST VALVE WAS WORN DOWN TO KEEPER. CONTINUED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · rod end · wornApr 16, 1999
DURING AN ENGINE CHANGE, PLAY WAS NOTED IN ROD ASSEMBLY LINKING VAPC WITH THE THROTTLE BODY. UPON DISASSEMBLY OF THE LINK ROD UNIT, NOTED THE ROD END 632557 WAS WORN WHERE IT CONNECTED TO THEVAPC LINKAGE. APPROXIMATELY 20 PERCENT REDUCTION IN DIAMETER WAS NOTED. INSTALLATION OF A NEW ROD END CURED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026