N300EW

CESSNA 210L · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: 2F TRADE LLC, TX (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
FLIGHT EXPRESS INCOperatoron 1998-09-25Operator named in NTSB report
FALLON AEROMOTIVE, INC.Operatoron 1995-06-29Operator named in NTSB report

Accident & incident history

Accident · 1998-09-25 Operator named in NTSB report
Cessna 210L No injuries Part 135FLIGHT EXPRESS INC

Operated by FLIGHT EXPRESS (per NTSB report)

Source: NTSB case ATL98LA130
Accident · 1995-06-29 Operator named in NTSB report
CESSNA 210L Minor injury Part 91FALLON AEROMOTIVE, INC.

Operated by FALLON AEROMOTIVE (per NTSB report)

Source: NTSB case LAX95LA234

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2011-07-20.

OTHER · 2011-07-20 Unresolved
ATA 8530

Part: CYLINDER — CRACKED (NR 3)

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.

Source: SDR FPI2011F00003
OTHER · 2011-07-20 Unresolved
ATA 8530

Part: CYLINDER — CRACKED (NR 4)

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.

Source: SDR FPI2011F00004
OTHER · 2011-07-20 Unresolved
ATA 8530

Part: CYLINDER — CRACKED (NR 2)

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.

Source: SDR FPI2011F00002