N701SE

CESSNA 208B · 1998 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: FLORIDA AIR CARGO INC, FL (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Florida Air Cargo Inc (P3EA)Certificate holderMatched by certificate designator
Florida Air Cargo Inc (P3EA)Operatoron 2007-11-06Operator named in NTSB report

Accident & incident history

Accident · 2007-11-06 Operator named in NTSB report
CESSNA C208B No injuries Part 135Florida Air Cargo Inc

Operated by Florida Air Cargo, Inc (per NTSB report)

Source: NTSB case MIA08LA014

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.

4 reports on file, 2002-04-22 – 2009-01-24.

OTHER · 2009-01-24 Matched by certificate designator
ATA 5530

Part: HINGE — CORRODED (VERTICAL STAB)

DURING THE REMOVAL OF THE RUDDER, LWR STABILIZER HINGE ASSY WAS FOUND WITH HEAVY CORROSION. THIS CORROSION WAS NOT VISIBLE WITHOUT REMOVING THE RUDDER. (K)

Source: SDR 2009FA0000085
OTHER · 2005-10-10 Matched by certificate designator
ATA 7230

Part: PLENUM — DAMAGED (ENGINE)

WHILE REMOVING THE ENGINE FOR A SCHEDULED OVERHAUL, WE NOTICED 5 RIVETS SHEARED OFF THE TOP HALF OF THE INDUCTION AIR PLENUM BAND ASSEMBLY. A SHEARED RIVET HEAD CAN EASILY FIT THRU THE ENGINE INLET SCREEN AND COULD BE INGESTED BY THE ENGINE CAUSING GREAT DAMAGE OR TOTAL ENGINE FAILURE. (K)

Source: SDR 2005FA0001427
OTHER · 2005-10-10 Matched by certificate designator
ATA 7230

Part: PLENUM — CORRODED (ENGINE)

WHILE REMOVING THE ENGINE FOR A SCHEDULED OVERHAUL, WE NOTICED 5 RIVETS SHEARED OF THE TOP HALF OF THE INDUCTION AIR PLENUM BAND ASSY. A SHEARED RIVET HEAD CAN EASILY FIT THRU THE ENGINE INLET SCREEN AND COULD BE INGESTED BY THE ENGINE CAUSING GREAT DAMAGE OR TOTAL ENGINE FAILURE. (K)

Source: SDR 2005FA0001428
OTHER · 2002-04-22 Matched by certificate designator
ATA 6114

Part: HUB — CRACKED (PROPELLER)

PROPELLER WAS DISASSEMBLED AND INSPECTED FOR OVERHAUL. PROPELLER HUB WAS STRIPPED, ETCHED AND DYE PENETRANT INSPECTED. INDICATIONS OF CRACKS WERE APPEARANT AT 5 LOCATIONS ON THE REAR HALF OF THE HUB NEXT TO THE REAR BETA ROD BUSHING SOCKETS. EDDY CURRENT INSPECTION VERIFIED ALL LOCATIONS WERE CRACKED. PART WAS RETIRED FROM SERVICE.

Source: SDR 2002FA0000550