N684FE

Service difficulty reports · 190

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N684FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201611013789Floor Panel · damagedAFT CARGO FLOOR PANEL 151TF DAMAGED/BROKEN. AFT CARGO FLOOR PNL 151TF FABRICATED ON T16/1237003 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.Nov 1, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201611013788Floor Panel · damagedFWD CARGO FLOOR PANEL 132SG DAMAGED/BROKEN. FWD CARGO FLOOR PNL 132SG FABRICATED ON T16/1237567 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.Nov 1, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201611013786Floor Panel · damagedFWD CARGO FLOOR PANEL 131LG DAMAGED/BROKEN. FWD CARGO FLOOR PANEL 131LG FABRICATED ON T16/1237562 IAW SRZ 25-005. CAT A REPAIR. MAJOR REPAIR.Nov 1, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313778Floor Panel · brokenMAIN CARGO FLOOR PANEL 252BH BROKEN AROUND CUT-OUT. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313777Floor Panel · crackedMAIN CARGO FLOOR PANEL 251RH HAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313776Floor Panel · crackedMAIN CARGO FLOOR PANEL 252VF CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313773Floor Panel · crackedMAIN CARGO FLOOR PANEL 241WH CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313772Floor Panel · crackedMAIN CARGO FLOOR PANEL 241TH CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313771Floor Panel · crackedMAIN CABIN FLOOR PANEL 242MF CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313767Floor Panel · damagedMAIN CARGO FLOOR PANEL 252UH HAS SEVERAL ELONGATED FASTENER HOLES. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313766Floor Panel · crackedMAIN CARGO FLOOR PANEL 232YG HAS A CRACK. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313765Floor Panel · crackedMAIN CARGO FLOOR PANEL 241MJ HAS A CRACK. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610313764Floor Panel · crackedMAIN CABIN FLOOR PANEL 241HK CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Oct 31, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608072833Leg Assy · defectiveLANDING GEAR WOULD NOT RETRACT IN SYS 1 OR SYS 2. FOLLOWED ECAM AND QRH PROCEDURES. GEAR HANDLE WOULD NOT GO PAST MID-POINT. PERFORMED BITE CHECK ON PROXIMITY DETECTOR UNIT REF MM 32-61-00, FAULT BL IS DISPLAYED. R&R LT MLG LEG ASSEMBLY PER WORK CARD 32110Aug 7, 2016 · N684FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201608062827Landing Gear · lack of lubeLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, IN POSITION DETECTOR, SYSTEM 1, SWITCHED TO POSITION DETECTOR 2 AND ATTEMPTED TO RETRACT WITH NO SUCCESS. REF TSM 32-61-00, CHECK PROXIMITY BOX FOR FAULTS, FOUND BL, FAULT. CLEARED FAULT AND TESTED PROXIMITY SENSAug 6, 2016 · N684FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201605201686Lever · excess playHARMONIC VIBRATION LASTED FOR 1 MIN WENT AWAY FOR 10 SECONDS & THEN CAME BACK. VIBRATION WAS WORSE AT HIGHER SPEEDS, LEAST AT 290 KNOTS & BELOW. VIBRATION FREQUENCY WAS MEDIUM & ENTIRE AIRFRAME WAS SHAKING. DID NOT FEEL VIBE IN CONTROL COLUMN, NOR THROTTLESMay 20, 2016 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201602160605Smoke Warning · false activationDURING TAXI, IN HEAVY THUNDERSTORM CONDITIONS, REC'D MAIN DECK CARGO SMOKE WARNING OF MID-2, LOOP B, WITH LOOP A MEL'D OFF. DONNED O2 MASKS & RAN ECAM CHECKLIST, SHUTTING DOWN RT PACK & ISOLATING HOT AIR. SMOKE WARNINGS & INDICATIONS CEASED. DID NOT EVACUATFeb 16, 2016 · N684FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201512103970Hmu · malfunctionedCRUISE FLIGHT AT FL 350L, ENG NR 2 N 1, EGT & FUEL FLOW BECAME UNSTABLE, CONTINUOUSLY FLUCTUATING. ENG STABILIZED ONCE ON DESCENT BEGAN & WAS NORMAL THROUGH LANDING & TAXI. REPLACED HMU & FUEL PUMP.Dec 10, 2015 · N684FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR FDEA201506262094Moisture Trap · leakingREVIEWED QRH ON TAXI OFF ROLL, HAD ABOUT 5 KTS SPLIT BETWEEN CAPTAINS PFD & STBY, FOR UNRELIABLE AT 80 KTS, SPLIT GOT GREATER AS AIRSPEED NEVER CALLED INCREASED. ROTATED ON FIRST OFFICERS CALL, 144 WITH 144 ON STBY AIRSPEED. NEVER GOT ADC FAULT. INFLIGHT 23Jun 26, 2015 · N684FE · Airbus A300F4605R · High Speed WarningSDR FDEA201504171251Pressure Switch · faultedDURING TAKEOFF ROLL APPROX 80 KTS, MASTER CAUTION LIGHT & CHIME CAME ON INDICATING GREEN, 1 & 2, HYD PRESSURE INOPERATIVE. PERFORMED REJECT & QRH. REMOVED AND REPLACED GREEN HP MANIFOLD PRESSURE SWITCH 30WW AS A PRECAUTION IAW AMM 29-11-12-04. REPLACED GApr 17, 2015 · N684FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201408282340Door Frame · dentedFWD CARGO COMPARTMENT CUT OUT FWD FRAME FRAME 20A STRINGER 39R - 41R FOUND 1 EACH DENT. COMPLIED WITH EA 6-5310-T0310888 PART1, TITLE: FUSELAGE - MAINFRAME. ONE DENT ON FRAME FR20A WEB AT STRINGER 39R-41R. REPAIRED THE FWD CARGO COMPARTMENT CUTOUT FWD FRAMEAug 28, 2014 · N684FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201408212272Hook · chafedAFT CARGO DOOR NR 2 LOCKING HOOK WORN. PER AMM52-30-21-01-01 REPLACED THE HOOK OF AFT CARGO DOOR NR 2 LOCKING, TEST OF THE LOCKING MECHANISM FOR INSTALLATION,TEST OK.Aug 21, 2014 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201408212271Hook · chafedAFT CARGO DOOR NR 1 LOCKING HOOK WORN. PER AMM 52-30-21-04-01 REPLACED THE AFT CARGO DOOR NR 1 LOCKING HOOK. PERFORM INSTALLATION TEST OF THE LOCKING MECHANISM ,TEST OK.Aug 21, 2014 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201408202228Frame · crackedFUSELAGE CTR SECTION LT FRAME 44 STRINGER 24 TO 28, HOLE B WITH CRACK SIGNAL. COMPLIED REPAIR PER EO 6-5310-7-5006 B PART1, TITLE: FUSELAGE - CENTER SECTION - AD 2004-23-20 - INSPECT BETWEEN FR41 TO FR46 FROM STGR 24 TO STGR 28 ON LT & RT. SB A300-53-6122, Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201408202227Structure · crackedCENTER WING JOINT AT FRAME 40 LT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. REAMED THE HOLE OF CENTER WING JOINT FRAME 40 LT SIDE UPPER FASTENER TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5710-T0310695APT1 TITLE:WING-BASIC WING STRUCTURE -CRACK HOLE IN CENTEAug 20, 2014 · N684FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201408202226Structure · crackedCENTER WING JOINT AT FRAME 40 RT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. REAMED THE HOLE OF CENTER WING JOINT FRAME 40 RT SIDE UPPER FASTENER TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5710-T0310695APT1 TITLE:WING-BASIC WING STRUCTURE -CRACK HOLE IN CENTEAug 20, 2014 · N684FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201408202225Crossbeam · crackedMDCC FRAME 39 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACE THE CRACKED CROSSBEAM AT MDCC FR39 B/W Y-450 TO Y-953 PER AMM 20-21-12- 00,MAJOR REPAIR IAW GMM 6-2-100.Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202232Adapter · corrodedMDCC FRAME 38.1 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR38.1 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202231Adapter · corrodedMDCC FRAME 38.2 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR38.2 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202229Crossbeam · corrodedMDCC FRAME 49 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACE THE CORRODED CROSSBEAM PER A300-600F SRM51-40-21,(MDCC FR49 B/W Y-1959 TO Y-2462 CROSSBEAM) ,THIS REPAIR CATEGORY IS "A",MAJOR REPAIR IAW GMM 6-2-100.Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202224Crossbeam · crackedMDCC FRAME 41 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACED THE MDCC FR41 B/W Y-450 TO Y-953 CROSSBEAM PER AMM20-21-12-00. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202222Crossbeam · crackedMDCC FRAME 42 BETWEEN Y-450 TO Y-953 CROSSBEAM CRACKED. REPLACED THE MDCC FR42 B/W Y-450 TO Y-953 CROSSBEAM PER AMM20-21-12-00. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202234Adapter · corrodedMDCC FRAME 34 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR34 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTER PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100.Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202233Adapter · corrodedMDCC FRAME 39 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR39 B/W Y-1959 TO Y-2462 CROSSBEAM ADAPTATOR PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408202230Crossbeam · corrodedMDCC FRAME 48 BETWEEN Y-1959 TO Y-2462 CROSSBEAM CORRODED. REPLACED THE MDCC FR48 B/W Y-1959 TO Y-2462 CROSSBEAM PER A300-600F SRM51-40-21. MAJOR REPAIR IAW GMM6-2-100Aug 20, 2014 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201407241955Line · leakingAFTER DEPARTURE, ECAM & OVERHEAD SHOWED LOSS OF GREEN HYD PRESSURE & QTY. COMPLIED WITH ECAM & QRH. CONFIGURED FOR LANDING WITH GRAVITY EXTENSION. DURING APPROACH, GREEN HYD QTY SHOWED SOME FLUID REMAINING. PUMPS OFF LESS THAN ONE MINUTE AFTER ECAM. CONJul 24, 2014 · N684FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201407241944Transmitter · faultyIN DESCENT HAD ECAM & OVERHEAD SHOWED LOSS OF FLUID & LOSS OF PRESS IN GREEN SYS. COMPLIED WITH ECAM FOR LOSS OF PRESS IN GREEN SYS. FULLY CONFIGURED FOR LANDING HYD FLUID LEVEL INDICATION CAME BACK TO NORMAL, LANDED UNEVENTFUL. R & R GREEN SYS RESERVOIR TRJul 24, 2014 · N684FE · Airbus A300F4605R · Hydraulic Quantity SensorSDR FDEA201401130091Window · crackedFL340, LT WINDOW HEAT CAME ON, TURNED HEAT OFF. OUTER WINDOW SCREEN CRACKED. FOLLOWED ECAM PROCEDURES & LANDED. REMOVED AND REPLACED L1 WINDOW IAW MM 56-11-11-04.Jan 13, 2014 · N684FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201310032381Transmitter · failedPRIOR TO TOP OF DESCENT, RECEIVED AN ECAM "HYD BLUE LO QTY" WARNING. BOTH OVERHEAD BLUE SYS QUANTITY AND ON ECAM WAS AT REDLINE. WARNING CAME AND WENT NUMEROUS TIMES. TURNED OFF BLUE SYS PUMP AND DIVERTED TO LAX. AFTER PUMP TURNED OFF, BLUE SYS QTY WENT UP Oct 3, 2013 · N684FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA201206192258Skin · dentedFRAME 1, STRINGER 25 + 10" FOUND ONE DENT 4.25"X5.5". FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-11-12. 2. NDI WAS COMPLETED. NO CRACK WAS FOUND REF. TO AB6 NTM PART 6 51-10-07 PAGE 601. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 19, 2012 · N684FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201206112180Floor Panel · puncturedAFT CARGO FLOOR PANEL HAS A 1 INCH PUNCTURE OF THE UPPER SURFACE AT FR 54.1 AND -Y1400.Jun 11, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206112178Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 152PF HAS EDGE AREA WITH IMPACT DAMAGE. REMOVED AFT CARGO BAY FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20, DWG 16 A53279902. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM Jun 11, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206072121Floor Panel · damagedNR 241TH FLOOR PANEL UPPER SURFACE HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-25-4. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, MC. INSTALLED FLOOR PANEL IAW AMM 53-10-25-4. THE REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS MINOR.Jun 7, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201205312024Floor Panel · damagedAFT CARGO COMPARTMENT 152XF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL AND INSTALLED INSERTS WITH ADHESIVE IAW SRM 53-10-20, IRM 9701 AND DWG 17 A53279913. INSTALLED FLOOR PANEL TO NORMAL CONDITMay 31, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201205312023Floor Panel · damagedAFT CARGO COMPARTMENT 151WF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED A NEW PANEL AND INSTALLED INSERTS WITH ADHESIVE IAW SRM 53-10-20, AND DWG 17 A53279913. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMay 31, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201205312022Floor Panel · damagedAFT CARGO COMPARTMENT 151XF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. FABRICATED THE NEW FLOOR PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20, NSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-33-04 IAW GMM 6-May 31, 2012 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201205312019Seat Track · wornMAIN DECK FLOOR AREA, FOUND SEAT TRACK, IS EXCESSIVELY WORN AT FR44 AND Y1456 POSITION . R & R THE SEAT TRACK IAW SRM 51-40-21. THE REPAIR EVLUATED IAW GMM 6-2-100 AND CLASSIFIED AS MAJOR.May 31, 2012 · N684FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201106242405Unknown · odorF/O SMELLED SOMETHING ABNORMAL JUST A MOMENT PRIOR TO AVIONICS SMOKE INDICATION DURING TAXI-OUT. SUBSEQUENT CHECK OF SNIFFER FAN WAS NEGATIVE FOR SMOKE OR FUMES. WARNING EXTINGUISHED AFTER APPROX 2 MINUTES. CHECKED AVIONICS AREA WITH SEVERAL SYSTEMS ON, COJun 24, 2011 · N684FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA201009073306Coalescer Bag · odorAPROX 50 MINUTES INTO FLIGHT HAD MAIN DECK AFT LOOP A FAULT. FOLLOWED QRH WITH GOOD TEST. BUT THEN LATER REPEATED SMOKE WARNING FROM MAIN DECK AFT. FOLLOWED BY VISIBLE BLUE SMOKE HAZE IN COCKPIT AND LATERBY SMOKE WARNING FROM MAIN DECK MID 1 AND MID 2 ACCSep 7, 2010 · N684FE · Airbus A300F4605R · Humidity Control SystemSDR FDEA201009043275Unknown · odorAFTER 45 MINUTE GOT MAIN DECK LOOP FAULT AND ALMOST IMMEDIATELY MAIN CARGO SMOKE. DONNED O2 MASKS. AFTER A FEW SECONDS GOT AVIONICS SMOKE. ENROUTE WE HAD DETECTED WHAT SEEMED LIKE HOT AIR COMING FROM THE AIR CONDITIONING, EVEN THOUGH THE TEMPERATURES WERE SHOSep 4, 2010 · N684FE · Airbus A300F4605R · Air Distribution System
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