N907FX
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
12 reports on file, 2005-03-12 – 2024-06-20.
Part: WINDSHIELD — FAILED (COCKPIT) · airframe 29,280 hrs · 31,431 cycles
DURING CRUISE OF FLIGHT, THE PICâS FRONT WINDSHIELD PANE SHATTERED. DUE TO THE CONDITION OF THE WINDSHIELD AND A SLIGHT BURNING SMELL IN THE COCKPIT, THE CREW DESCENDED TO 10,000 FEET, DECLARED AN EMERGENCY, AND DIVERTED TO PTP. CORRECTIVE ACTION IN WORK.
Part: ATTACH FITTING — CRACKED (MLG ACTUATOR) · airframe 27,826 hrs · 30,065 cycles
DURING CRUISE FLIGHT, HEARD A LOUD BANG, WITH LEFT LANDING GEAR SHOWING RED UNSAFE INDICATIONS ON BOTH PRIMARY AND SECONDARY INDICATIONS. PERFORMED CHECKLIST AND COMPLETED FLIGHT WITH THE LANDING GEAR DOWN. MAINTENANCE FOUND THE LT MLG ACTUATOR ATTACH BRACKET CRACKED LOOSE FROM THE AIRFRAME.
Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 25,546 hrs · 26,906 cycles
FOUND PITTING CORROSION OUT OF LIMITS ON CAPTAINS FLOOR PANEL P/N S53173206200. REPLACED FLOOR PANEL IAW ATR SRM.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 25,546 hrs · 26,906 cycles
FLOOR PANEL 214BF UNDER 90VU RACK FOUND TO HAVE PITTING CORROSION OUT OF LIMITS. REPLACED FLOOR PANEL P/N S53173102202.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,546 hrs · 26,906 cycles
LEFT OUTBOARD SEAT TRACK HAS PITTING CORROSION OUT OF LIMITS. REPLACED SEAT TRACK P/N S53375001204.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 25,546 hrs · 26,906 cycles
FLOOR PANEL 213BF UNDER 80VU ELECTRONICS RACK FOUND TO HAVE PITTING CORROSION OUT OF LIMITS. REPLACED FLOOR PANEL P/N S53173111200.
Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 25,546 hrs · 26,906 cycles
FOUND PITTING CORROSION OUT OF LIMITS ON FIRST OFFICERS FLOOR STRUCTURE P/N S53173111200. REPLACED FLOOR STRUCTURE IAW ATR SRM.
Part: HINGE — CRACKED (CARGO DOOR) · airframe 24,514 hrs · 26,050 cycles
FOUND CRACK ON AFT CARGO DOOR DURING SCHEDULED INSPECTION.
Part: RETAINER — CORRODED (WING) · corrosion level 2 · airframe 23,729 hrs · 25,060 cycles
DURING A GENERAL VISUAL INSPECTION, NOTICED THERE IS EXFOLIATION CORROSION OF THE WING PRESSURE DECK SEAL RETAINER LOCATED AT REAR SPAR (FUSELAGE FRAME 27) BETWEEN RIBS 1LT - 1RT.
Part: PUMP — INOPERATIVE (HYD SYSTEM)
AFTER DEPARTURE, THE BLUE HYDR SYS PRESSURE WENT TO -0-PSI. THE FLAPS WOULD NOT RETRACT, AFTER COMPLETING THE APPROPRIATE CHECKLIST, THE CREW DECIDED TO RETURN TO DEPARTURE. AFTER TROUBLESHOOTING THE MECHANIC FOUND A BAD HYDR PUMP. (K)
Part: CAP — UNSECURE (OIL FILLER) · airframe 22,796 hrs · 24,166 cycles
DURING TAXI, THE NR 1 ENG OIL PRESSURE LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THE OIL FILLER CAP WAS FOUND UNSECURED. THE ENGINE OIL WAS SERVICED, THE CAP SECURED, AND RETURNED THE A/C TO SERVICE. NO FURTHER PROBLEMS NOTED.
Part: LINE — CRACKED (HYDRAULIC SYS)
DURING TAXI, NORMAL BRAKING ACTION WAS LOST. AFTER TROUBLESHOOTING A TUBE TO THE BRAKE METERING VALVE WAS FOUND TO BE BROKEN. THE TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.