N904FE

CESSNA 208B · Valid Registration

Registered owner: FEDERAL EXPRESS CORPORATION, TN (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
CORPORATE AIR (HSYA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

K J · 2017-09-19 Matched by certificate designator
ATA 7930

MIDWAY THROUGH FLIGHT, ON THE EMPTY STAGE LEG, THE PILOT NOTICED OIL APPEARING IN THE OIL PRESSURE GAUGE. ALL ENGINE INDICATIONS WERE NORMAL THE FLIGHT CONTINUED TO DESTINATION, WHEN THE STAGE FLIGHT GOT CLOSER TO THE AIRPORT, THE PILOT SAW THAT OIL HAD FILLED THE GAUGE AND WAS ALSO COMING OUT OF THE CO-PILOTS YOKE AND DRIPPING. DECLARED AN EMERGENCY AND WAS GIVIEN DIRECT CLEARANCE TO LAND. ON LANDING THE LOW OIL PRESSURE GAUGE BEGAN FLASHING AND THEN CAME ON SOLID, THE ACFT WAS SHUTDOWN.

Source: SDR HSYA201709200001 · FAA SDRS
J · 2012-12-31 Matched by certificate designator
ATA 3417

PILOT REPORTED AN ADC FAILURE, LOSS OF AIRSPEED, ALTIMETER, VERTICAL SPEED, TAS AND OAT DISPLAYS DURING CRUISE. AIRCRAFT LANDED WITHOUT INCIDENT. MX TROUBLESHOOT AND INSPECTED ACFT AHRS 1 TAS ALERT IAW STC ICAW A0-01080-05, REV 1 AND REFERENCING FLIGHT-LINE MM A0-00601-05, REV A, PAGE 3-13. MX RESET GTP-59 AND GDC-74 CONNECTOR PLUGS AND PERFORMED GROUND OPS AND FUNCTIONAL CHECKS AND SELF-TESTS. ALL CHECKS WERE GOOD. ACFT RETURNED TO SERVICE - THREE FLIGHTS HAVE BEEN COMPLETED WITH NO FURTHER DEFECTS NOTED.

Source: SDR HSYA201212310002 · FAA SDRS
C B · 2012-02-23 Matched by certificate designator
ATA 7200

PILOT REPORTED DURING TAXI, A STRONG CHEMICAL ODOR IN COCKPIT. TAXIED ACFT BACK TO THE BLOCKS. FREIGHT INSPECTED AND NO DISCREPANCIES FOUND. MX TROUBLESHOT AND FOUND THAT THE APPARENT CAUSE TO BE RESIDUAL RECOVERY WASH FLUID FROM A COMPLETED COMPRESSOR TURBINE WASH. MX COMPLETED A DESALINATION WASH AND RAN ACFT ENGINE AT 80 PERCENT NG FOR 3 MINUTES TO CLEAN OUT ANY RESIDUAL FLUID THAT COULD BE LEFT IN THE COMPRESSOR TURBINE SECTION OF ENGINE. NO FURTHER ODORS COULD BE NOTED. PERFORMED IAW MM 71-00-00.

Source: SDR HSYA2012022312412 · FAA SDRS
O · 2000-10-22 Matched by certificate designator
ATA 5330

HNL - MAINTENANCE FOUND FUSELAGE SKIN PANEL, UPPER CENTER FORWARD, CORRODED. PANEL CORRODED BEYOND LIMITS FOR 2024T3, .032 INCH THICK. REMOVED AND REPLACED PANEL ASSEMBLY IAW C208 SRM 53-10-10 AND SRM 51-40-00. (X)

Source: SDR 20001109SH038 · FAA SDRS