N811FX
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.
18 reports on file, 2008-04-11 – 2025-12-11.
Part: ENGINE — POWER LOSS (ZONE 500) · airframe 35,050 hrs · 35,874 cycles
IN-FLIGHT ENGINE SHUTDOWN, FLIGHT 8850, TLH-MEM. ON THE VISUAL APPROACH TO RUNWAY 27 AT KMEM, THE CREW OBSERVED THE NO. 1 ENGINE TORQUE INDICATION BECOME ERRATIC, THEN DROP TO ZERO, ACCOMPANIED BY AN UNCOMMANDED LEFT ROLL. MEMORY ITEMS WERE ACCOMPLISHED, AND THE CREW SHUT DOWN THE NO. 1 ENGINE AND FEATHERED THE PROPELLER. AN EMERGENCY WAS DECLARED WITH ATC. THE CREW CONTINUED FOR THE LANDING AND COMPLETED A SINGLE-ENGINE LANDING ON RUNWAY 27 WITHOUT FURTHER INCIDENT. ONCE CLEAR OF THE RUNWAY, THE ENGINE WAS SECURED USING THE QRC/QRH. AIRPORT RESCUE/FIRE PERSONNEL REPORTED NO FIRE OR SMOKE OBSERVED, AND THE AIRCRAFT TAXIED IN AND PARKED.
Earlier reports · 2008–2023 · 17 reports
2023
Part: UNKNOWN — LEAKING (CABIN) · airframe 33,907 hrs · 34,894 cycles
DUE TO O2 LEAK, CREW O2 CYLINDER PRESSURE DROPPED TO "0" PSI, REQUIRED REPLACEMENT. REMOVED AND REPLACED O2 CYLINDER. PERFORMED LEAK CHECK WITH NO DEFECTS NOTED.
2022
Part: HMU — FAULTED (ENGINE) · airframe 33,404 hrs · 34,541 cycles
TORQUE SPLIT WITH POWER LEVERS IN NOTCH. RIGHT ENGINE TORQUE MATCHED FADU. LEFT ENGINE WAS 10% LOW. REQUIRES 3/4 KNOB MISS MATCH TO MATCH TORQUE. REPLACED LEFT HAND ENGINE HMU. OPS CHECK GOOD.
2014
Part: LINE — FAILED (HYD SYSTEM) · airframe 29,113 hrs · 31,160 cycles
AFTER BLOCK OUT OF FLIGHT THE COPILOTS BRAKE WAS FOUND TO BE INOPERATIVE. REPLACED HYDRAULIC LINES. CHECKED GOOD & ACFT RETURN TO SERVICE.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 29,112 hrs · 31,157 cycles
DURING BRAKE CHECK FOR TAXI, THE LT BRAKE PEDAL ON THE COPILOTS SIDE WAS INOPERATIVE. TROUBLESHOT & A HYD LEAK WAS FOUND. THE LINE WAS REPAIRED IAW AMM 20-23-13. LEAK & OPERATIONS CHECKED GOOD IAW JIC 32-42-00 OPT 10000.
Part: FILTER — LEAKING (BRAKE SYS) · airframe 29,110 hrs · 31,155 cycles
DURING TAXI OUT, COPILOTS LEFT BRAKE PRESSURE WAS INSUFFICIENT. THE CREW TAXIED THE ACFT BACK TO THE RAMP. REPLACED THE HYD ACOUSTIC FILTER AT 9GXA IAW ATR-72JIC 29-10-00 RAI 10080. THE SYS CHECKED GOOD. THE BRAKE LOW PRESSURE LINE WAS BLEED IAW JIC 32-42-00 BLD 10000. THE NORMAL BRAKE SYS CHECKED GOOD.
Part: SKIN PANEL — CORRODED (LT WING) · airframe 29,104 hrs · 31,151 cycles
FOUND LT WING LOWER SKIN PANEL INTERNAL CORROSION AT JET PUMP SUPPORT SEATING BETWEEN RIBS 4 & 5, STIFFENERS 8 - 9. REPAIRED IAW SRI DT S-2157 14-21832 DATED 4/11/2014. APPROVED DATA IS SHEET DO TS-2644 10 5790.
Part: PANEL — CORRODED (LT WING) · airframe 29,104 hrs · 31,151 cycles
FOUND PANEL 521DT & 522CT HOUSINGS CORRODED OUT OF LIMITS ON REMOVABLE PANEL PN S57112322200. REPAIRED IAW SRI DT S-2001 14-21784 ISSUE A DATED 4/5/2014. APPROVED DATA IS SRAS DT S-2001 14 8440.
Part: HOUSING — CORRODED (RT WING) · airframe 29,104 hrs · 31,151 cycles
FOUND PANEL 622CT HOUSING CORRODED OUT OF LIMITS ON REMOVABLE PANEL PN S57112322201. REPAIRED IAW SRI DT S-2001 14-21784 ISSUE A DATED 4/5/2014. APPROVED DATA IS SRAS DT S-200114 8440.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,104 hrs · 31,151 cycles
FOUND CREASE BEAM WEB PN S53374000204 CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,104 hrs · 31,151 cycles
FOUND CREASE BEAM WEB PN S53374000228 CORRODED BEYOND LIMITS. REPLACED WEB IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,104 hrs · 31,151 cycles
FOUND CREASE BEAM PN S53373000226 CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.
Part: PAN — DENTED (CARGO DOOR) · airframe 29,104 hrs · 31,151 cycles
FOUND DENTS IN AFT CARGO DOOR FRAME PANS PN S52176204202, S52176204206 & S51276204208 TO BE OUT OF LIMITS. REPAIRED IAW DWG 72R47000-07 DATED 3/31/2014.
2013
Part: DOOR — OUT OF TOLERANCE (AFT CARGO) · airframe 29,070 hrs · 21,116 cycles
DISCOVERED FORWARD GAP ON AFT CARGO DOOR TO BE OUT OF TOLERANCE. MAJOR REPAIR.
2009
Part: DOOR — SEPARATED (LT MLG) · airframe 27,443 hrs · 29,820 cycles
WHILE EN ROUTE ON FLIGHT 7499 CRW-MEM, THE LEFT LANDING GEAR DOOR AND FOLDING DOOR DETACHED FROM THE AIRCRAFT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 27,218 hrs · 29,626 cycles
LONGITUDINAL FLOORBEAM CRACKED BETWEEN FRAME 28 AND 28C LEFT SIDE. REPAIRED CRACK BY ACCOMPLISHING REPAIR IAW M7 AEROSPACE LONGITUDINAL SPLICE REPAIR DRAWING NUMBER 42-7000 DATED 02/02/2007 AND LAR 0903001 DATED 03/12/2009.
2008
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,009 hrs · 29,469 cycles
DURING CLIMBOUT THE COPILOTS WINDSHIELD DEVELOPED A CRACK. THE PILOT DECLARED AN EMERGENCY AND MADE A SAFE LANDING IN MIA. THE WINDSHIELD WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
Part: PUMP — CRACKED (NR 2 ENGINE) · airframe 26,211 hrs · 28,844 cycles
DURING FLT (MIA-KIN) 5NM FROM KIN THE NR 2 ENG OIL PRESSURE DROPPED TO ZERO WITH CAP WARNING "ENG OIL" AND CRC. THE ENG WAS SHUTDOWN AND THE PIC DECLARED AN EMERGENCY. UPON INSP AFTER LANDING, THE COWLING WAS COVERED WITH OIL. AN OVERSPEED HYDRAULIC PUMP HAS BEEN DETERMINED TO BE THE CAUSE FOR THE LOSS OF ENG OIL.