N569FE
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.
16 reports on file, 2004-02-03 – 2012-08-07.
Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 80,647 hrs · 27,490 cycles
CRACK IN LT SIDEWALL 10 INCHES AFT OF BS 1381 AND 4 INCHES DOWN FROM UPPER BULKHEAD. CRACK EMANATE'S OUT OF LIGHTNING HOLE AND ENDS AT FASTENER. REPAIRED LT WW SIDEWALL IAW SRM 53-00-01, FIG 10.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,535 hrs · 27,416 cycles
ON PRE FLIGHT RECEIVED AN EMERGENCY BATTERY LOW ALERT. R & R EMERGENCY POWER BATTERY PACK IAW MM 33-51-01-4. OPS CHECKS NORMAL.
Earlier reports · 2004–2011 · 14 reports
2011
Part: INDICATOR — FALSE ACTIVATION (CARGO FIRE DETEC) · airframe 78,681 hrs · 26,426 cycles
AFTER MIN 0149 MIN ENROUTE FWD LOWER CARGO FIRE AGENT DISCHARGE SWITCH STARTED TO FLASH. DISCHARGED AGENT PER PHASE ONE/QRH. DIVERTED TO PHX, LANDED UNEVENTFULLY. EVIDENCE OF LEAK, REMOVED AND REPLACED NR 2 FIRE EXTINGUISHER CONTAINER PER MM 26-22-01-4.. ELECTRICAL CONNECTOR FOR BOTH SQUIBS NOT CONNECTED. REMOVED AND REPLACED FWD DISCHARGE CARTRIDGE PER MM 26-22-04-4-0. CONNECTED ELECTRICAL CONNECTOR TO SQUIB AND FINISHED INSTALLATION PER MM 26-22-01-4 AND PERFOMED ADJUSTEMNT TEST PER 26-22-01-5.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,673 hrs · 26,420 cycles
LOWER FUSELAGE AT STA 1821, CORROSION EMMITING FROM FASTENERS AND SKIN BETWEEN LONGERON 46R THRU 48R. REMOVED AREA OF CORROSION, FABRICATED REPAIR PARTS REF SRM 53-20-00, FIG 6. INSTALLED FILLER, DOUBLER, AND TRIPLER REF SRM 53-20-00, FIG 6. ALODINED, PRIMED, AND PAINTED REPAIR AREA REF SRM 51-21-01, VOL II.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,673 hrs · 26,420 cycles
HEAVY CORROSION FOUND AT STA 1701, L44 TO L45, CUT OUT DAMAGE AND REMOVED CORROSION, REF SRM 51-21-01. FABRICATED REPAIR PARTS REF SRM 51-21-01, VOL II AND SRM 53-20-00. INSTALLED REPAIR REF SRM 53-20-00, FIG 6. ALODINED REPAIR AREA REF SRM 51-21-01, VOL II. PREP AND PAINTED REPAIR AREA REF SRM 51-21-02.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,673 hrs · 26,420 cycles
TEAR STRIP BULGING & CORROSION PRESENT AT STA 1884, LONGERON 45R. CUT OUT DAMAGE AND REMOVED CORROSION REF SRM 51-21-01 & SRM 53-20-00. FABRICATED FILLERS, DOUBLERS, AND TRIPPLERS REF SRM 53-20-00, FIG 5, SH. 6. INSTALLED FILLERS, DOUBLERS, AND TRIPPLERS REF SRM 51-35-01. ALODINED, PRIMED, AND PAINT REPAIR SRM 51-21-02.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,673 hrs · 26,420 cycles
LOWER FUSELAGE AT STA 1801, CORROSION EMMITING FROM FASTERNER AND SKIN BETWEEN L46R THRU L48R. REMOVED AREA OF CORROSION, FABRICATED REPAIR PARTS REF SRM 53-20-00, FIG 6. INSTALLED FILLER, DOUBLER, AND TRIPLER REF SRM 53-20-00, FIG 6 ALODINED, PRIMED, AND PAINTED REPAIR AREA REF SRM 51-21-01, VOL II.
Part: SPAR CAP — CRACKED (LT WING) · airframe 78,673 hrs · 26,420 cycles
LT WING AFT LWR SPAR CAP, FOUND 3 CRACKED HOLES ON THE OTBD ROW AND 1 CRACKED HOLE ON THE FWD MOST INBD LT WING AFT LOWER SPAR HAS BEEN REPAIRED AND COMPLIES WITH EA NR 8-5710-142566.
Part: SPAR — CRACKED (ZONE 500) · airframe 78,673 hrs · 26,420 cycles
LEFT WING REAR SPAR LOWER CHORD ANGLE AT STA.XORS 345 HAS A CRACK INDICATION THROUGH 3 FWD FWD HOLES AND CAN BE SEEN ON THE AFT SIDE EXTENDING OUT OF THE RADIUS APPROX.1" AFT AND UP THE VERTICAL LEG UNDER THE FITTING. (VERIFIED BY N.D.T) REPAIRED AND COMPLIED WITH E.A. 8-5710-142566.
2009
Part: TUBE — DAMAGED (FUEL SYSTEM) · airframe 76,712 hrs · 25,449 cycles
FUEL ALERT. LEVEL 2 FUEL QTY/USED CHECK AIRBORNE. FOLLOWED QRH, FUEL SYS MANUAL, ISOLATED TANKS. TANK NR 1 SUSPECT. WERE ON DESCENT TO SLC SO LANDED AND SHUT NR 1 ENG DOWN. LEAK CONFIRMED ON GROUND. FACT: FOUND ROD END HOSE BLOWN ON NR 1 ENG MEC. REPLACED VSV ROD END TUBE AT MEC IAW MM 73-20-01-2. RAN NR 1 ENG IAW JRH CH 5. ENGINE RUN AND LEAK CHECK WAS NORMAL. ACFT OK FOR SERVICE.
Part: FIREWALL — CORRODED (NR 3 NACELLE) · airframe 75,719 hrs · 24,994 cycles
NR 3 PYLON, AFT MOUNT FIREWALL ATTACH HOLES HAVE CORROSION. NR 3 ENGINE PYLON AFT MOUNT FIREWALL ATTACH HOLES REPAIRED PER EA 8-5450-126149 SEQ 923 W/O 43105.
2007
Part: LINE — RUPTURED (HYD SYSTEM) · airframe 73,262 hrs · 23,834 cycles
PDIS: AT ROTATION LOSS OF HYD "SYS 1", 0.0. FOUND INLET HOSE ON LOWER HYDRAULIC PUMP RUPTURED. NEEDS NEW HOSE, PUMPS, FILTERS. FOUND HYD LINE NR 1 ENGINE DRIVEN PUMP LINE RUPTURED, REPLACED LINE,BOTH ENG DRIVEN PUMPS, ALL RELATED FILTERS AND LEAK CHECKED PER MM 29-11-01, AND MM 29-11-02, OPS GOOD.
Part: TRANSPONDER — FAILED (NR 2) · airframe 73,095 hrs · 23,750 cycles
IN CRUISE FLIGHT FL 340 TOWER REPORTED US 400' LOW THEN 600' HIGH WITHIN 3 SECONDS ON XPDR NR 1. SWITCHED TO TRANSPONDER NR 2, CENTER REPORTED US AS STABLE AT FL 340. REMOVED AND REPLACED NR 1 TRANSPONDER PER EO REF 8-3454-7-5001 AND MM REF 34-54-00-5.
2004
Part: ANGLE — CRACKED (ZONE 500) · airframe 67,606 hrs · 21,316 cycles
EXISTING REPAIR SPLICE ON LEFT WING STRINGER 4 CRACKED AT XORS 930. CRACKED REPAIR ANGLE REPLACED BY A NEW REPAIR ANGLE MADE FROM 7075-73511 THAT ARE MORE FATIGUE RESISTANT IAW FEDEX EA 8-5710-73240.
Part: CAP — CRACKED (RT & LT WING) · airframe 67,606 hrs · 21,316 cycles
RIGHT AND LEFT WING UPPER CAP CRACKED AT XORS 372. THE CRACKS ARE AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED. REPAIR ANGLE AND DOUBLERS HAVE BEEN INSTALLED IAW FEDEX EA 8-5710-73236.
Part: SKIN — CRACKED (ZONE 300) · airframe 67,606 hrs · 21,316 cycles
HORIZONTAL STABILIZER - UPPER COSTANT SECTION AND OUTBOARD SKINS CRACKS WITHIN FLYABLE LIMITS. PANELS INVOLVED: ALC7436-1, ALC7437-1, ALC7207-1 AND ALC7208-1. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73235.