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Aircraft record

N300EWCessna 210L

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Sep 1998)4 ADs may apply3 service difficulty reports

Registration
Valid
expires Dec 31, 2028
Based in
Collinsville, TX
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
since 2021
NTSB events
2
substantial, 1998
ADs may apply
4
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
2F Trade LLC
Owner type
LLC
City, state
Collinsville, TX
Certificate issued
Dec 13, 2021
Expires
Dec 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Feb 20, 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
210L
Serial number
21061219
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
A31FCB

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. 2021 – now2F Trade LLCCollinsville, TX · current

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 (2)

Accident · substantial damage

Sep 26, 1998 · Orlando, FL

A 6-8 inch crack on the right main landing gear strut, which allowed the hydraulic fluid to escape from the system, along with a power pack sequencing valve failure which allowed the main landing gear to fold on landing. A factor in the accident was the pilots execution of a night landing without her prescribed eye glasses.

Damage
Substantial
Injuries
None
Report
ATL98LA130

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL98LA130)

Accident · substantial damage

Jun 30, 1995 · Truckee, CA

fuel exhaustion due to the pilot's inadequate preflight fuel planning, and his failure to refuel the aircraft while en route.

Damage
Substantial
Injuries
Minor
Report
LAX95LA234

From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX95LA234)

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 (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 · cylinder · crackedJul 20, 2011

    DURING A 100 HR INSPECTION FOUND THE CYLINDER HEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM COOLING FINS ABOVE EXHAUST PORT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder · crackedJul 20, 2011

    DURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM COOLING FINS ABOVE EXHAUST PORT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder · crackedJul 20, 2011

    DURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM COOLING FINS ABOVE EXHAUST PORT.

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

Related aircraft

Show all 8 related aircraft
All 234 registered Cessna 210L aircraft

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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