N565FE
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.
7 reports on file, 2004-05-12 – 2008-02-21.
Part: RELAY — MALFUNCTIONED (MLG) · airframe 79,951 hrs · 25,412 cycles
ON ARRIVAL AFTER GEAR DOWN GOT LVL 2 LT ANTI-SKID FAIL. IT DID NOT REAPPEAR AFTER DROPPING GEAR ON SECOND APPROACH. REPLACED RELAY R2-105 PER SMP. OP CHECKED SYSTEM PER MD10-10 MM 32-45-00-5. OP CHECK OK. OK FOR SERVICE.
Part: FEEDER CABLE — CHAFED (ZONE 100) · airframe 79,471 hrs · 25,166 cycles
FOUND FWD CARGO POWER FEEDER CABLES CHAFED THROUGH BETWEEN 875-950. TEMP SPLICED IN NEW FEEDER CABLE, PERMANENT FIX TO FOLLOW. REPLACED DAMAGED FEEDER CABLE FROM EXT PWR CONNECTION AT STA 635 TO 1099 ELECT CONTROL PANEL LT PANEL, OPS CHECK GOOD PER AMM 20-30-01, AMM 20-30-07. NEED TO STRING TIE FEEDER CABLE FOR EXT PWR STA 635 TO 1099. STRING TIED FEEDER CABLE FROM STA 635 TO STA 1099 AMM 20-30-07. NEED TO INSTALL SPIRAL WRAP ON FEEDER CABLES IN SUMP AREA STA 635 TO 1099. INSTALLD SPIRAL WRAP IAW EO 8-2450-7-5000-4 PER SEQ 953.
Part: ENGINE — FAILED (NR 1) · airframe 75,108 hrs · 23,244 cycles
AFTER TAKEOFF AT SMF NR 1 ENG RPM ROLLED BACK TO 42 PERCENT EGT TO 992 AN HAD SEVERE VIBRATION. SHUTDOWN NR 1 IAW QRH. NOTE HAD NO FIRE WARNING IND. 1 FIRE BOTTLE USED- GND WITNESS OBS FLAMES FROM CENTER OF ENG. EXHAUST REMOVED AND REPLACED #1 ENG NR 1 FIRE EXTINGUISHER BOTTLE, PERFORMED STALL INSPECTIONS, OVERTEMP INSPECTIONS, FAIL TO RESPOND TO THROTTLE MOVEMENT TROUBLESHOOTING FOUND VSV OUT OF RIG ,CORRECTED, ALSO UPON ENGINE RUN FOUND BAD CIT SENSOR, REPLACED. OK FOR SERVICE.
Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 75,102 hrs · 23,241 cycles
NR 1 ENGINE REMAINED AT FLIGHT IDLE DURING DESCENT AND WOULD NOT FOLLOW THROTTLE. N1 AND N2 SLOWLY STARTED DECAYING UNTIL GEN, AIR, HYDRAULIC ALERTS STARTED COMING ON. EGT WAS BELOW OTHER ENGINES 150-200 DEG FF WAS APPROX 500 PPH. FIRST NOTED PROBLEM FL220, RPM LOW AT FL180. MOTORIZED NR 1 ENG AS PER FEC MD-10 JRH AND NO FOG FROM TAILPIPE. TRIED STARTING ENG AND ENG WOULD FLAME OUT AT APPROX 41 PERCENT. FF WOULD DECREASE AND ENG WOULD SPIN DOWN.
Part: THROTTLE CABLE — CONTAMINATED (ENGINE) · airframe 74,188 hrs · 22,829 cycles
ON DESCENT NR 2 ENGINE THROTTLE WOULD NOT RETARD. ENGINE STUCK AT 85 PERCENT N2, FUEL FLOW WAS INOP. PERFORMED PRECAUTIONARY SHUTDOWN. PURGED CABLE OF MOISTURE PER MM SUPPLEMENT 76-11-01 -2 / 5A STEP 6, ALL TEST PAST PER MM 76-11-01-2 PARAGRAPH 4.
Part: RIB — CRACKED (ZONE 500) · airframe 74,124 hrs · 22,800 cycles
WING - LT WING RIB XORS 372 UPPER CAP CRACKED. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-78165.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,124 hrs · 22,800 cycles
FUSELAGE - RT CENTRAL CARGO DOOR SILL RAIL CORROSION AT STA 1681, LONGERON 43. CORROSION REMOVAL AND REPAIR ANGLE INSTALLATION IAW FEDEX EA 8-5315-75701.