N685FE

Service difficulty reports · 276

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 = 'N685FE' 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 FDEA200911023786Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 241 WH IS BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4. INSTALLED PANEL IAW AMM 53-10-23.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023784Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 YG IS BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4. INSTALLED FLOOR PANEL IAW AMM 53-10-23-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023779Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 VG IS BROKEN. REMOVED PANEL, FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023778Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 RG IS BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023777Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS BROKEN. REMOVED FLOOR BOARD; FABRICATED NEW BOARD USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023776Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 ZJ IS BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4. INSTALLED FLOOR PANEL IAW AMM 53-10-23.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023774Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 SF IS BROKEN. REMOVED PANEL, FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023773Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 MF IS BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200911023771Floor Panel · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 BF BROKEN. REMOVED PANEL; FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H" AND AMM 53-10-25-4.Nov 2, 2009 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908092959Hose · damagedDURING CLIMBOUT PASSING 15000' LOST BLUE SYSTEM HYD SYSTEM QTY FOUND HYD PRESSURE LINE ON ENG NR 1 BLUE SYS WORN THROUGH AT CLAMP. PART NIS AT LCK ORDERED PART. REPLACED BROKEN CLAMP. HOSE ASSY SECURE. NR 1 ENGINE FAN AND REVERSER COWLS CLOSED AND SECUREDAug 9, 2009 · N685FE · Airbus A300F4605R · Hydraulic System, MainSDR 08FDEA02735Smoke Detector · malfunctionedON SHORT FINAL TO KMEM RWY 36L, GOT AVIONICS SMOKE WARNING AND CRC. DECLARED EMERGENCY AND STOPPED ON RWY. RAN QRH PROCEDURES. NO SMOKE NOTED, SHUTDOWN ENGINES STARTED APU AND ASKED FOR TOW-IN TO PARKING. T/S AVIONICS COMPARTMENT SMOKE DETECTION USING TSMJul 8, 2008 · N685FE · Airbus A300F4605R · Smoke DetectionSDR 08FDEA02734Smoke Detector · failedON SHORT FINAL TO KMEM RWY 36L, GOT AVIONICS SMOKE WARNING AND CRC. DECLARED EMERGENCY AND STOPPED ON RWY. RAN QRH PROCEDURES. NO SMOKE NOTED, SHUTDOWN ENGINES STARTED APU AND ASKED FOR TOW-IN TO PARKING. T/S AVIONICS COMPARTMENT SMOKE DETECTION USING TSMJul 8, 2008 · N685FE · Airbus A300F4605R · Smoke DetectionSDR 08FDEA02168Fire Detector · malfunctionedABOUT 80 MILES OUT OF KEWR HAD A LOWER CARGO FIRE INDICATION AND FOLLOWED PROCEDURES AND FIRE BOTH FWD CARGO BOTTLES, FOLLOWED ON GROUND EVACUATION CHECKLIST, L1 DOOR SLIDE DEPLOYED NORMAL STOP AND ROLLOUT. REMOVED AND REPLACED BOTH FWD CARGO COMPT SMOKE DET Jun 5, 2008 · N685FE · Airbus A300F4605R · Fire DetectionSDR 08FDEA00275Mount · corrodedNR 1 ENGINE FWD MOUNT FITTING AFT UPPER I/B AND O/B HOLES HAVE A 2.5 SQ INCH AREA OF CORROSION EACH AT RECESS DIAMETERS AND AROUND UPPER SURFACE WORKED LEVEL 1 CORROSION ON NR 1 ENGINE FWD MOUNT HOLES AND REMOVED CORROSION AND REPAIRED IAW FED-EX EA NR 6-54Jan 25, 2008 · N685FE · Airbus A300F4605R · Engine Mount SectionSDR 08FDEA00117Seat Track · gougedMAIN DECK CARGO COMPARTMENT FR 38.2 TO FR 39 SEAT TRACK R-2 HAS GOUGES AT SCALLOPS IN 1 AREA, .250" DEEP REMOVED AND REPLACED R-2 SEAT TRACK ASSEMBLY FROM FR 38.2 TO 39 IAW A300-600 SRM 51-72-10 AND SRM 53-15-16.Jan 12, 2008 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00116Seat Track · gougedMAIN DECK CARGO COMPARTMENT FR 44 SEAT TRACK L-2 IS GOUGED ON SCALLOP .250" DEEP REMOVED AND REPLACED DAMAGED SEAT TRACK L-2 SECTION FROM FRAME 40 TO 44.5 IAW A300-600 SRM 51-72-10 AND SRM 53-15-16.Jan 12, 2008 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00115Seat Track · bentMDCC, BETWEEN FRAMES 20 AND 21, SEAT TRACK L-5 IS BENT. REMOVED AND REPLACED SEAT TRACK NR 5 LT BETWEEN FRAMES 18 TO 26 IAW A300-600 SRM 51-75-10 AND SRM 53-13-16.Jan 12, 2008 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04794Generator · inoperativeREJECTED T/O ON 18L KMEM DUE TO F/O'S PFD AND NAV DISPLAY SHOWING DIAGONAL LINES. ABORTED AT 60 KTS. ALL CHECKLISTS COMPLETED AND PERFORMED SECOND UNEVENTFUL TAKEOFF. PERFORMED EFIS BITE AND DISPLAYS TEST ON SYSTEM, ALL CHECKS NORMAL. SWAPPED NR 3 SGU ANov 14, 2007 · N685FE · Airbus A300F4605R · AC Generation SystemSDR 07FDEA03874Shutoff Valve · malfunctionedON TAKEOFF, NR 2 THRUST REVERSER PRESSURIZED-REJECT AT 50 KNOTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 24SEP07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD TSep 18, 2007 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA03775Shutoff Valve · malfunctionedON TAKEOFF, GOT ENG NR 2 REVERSER PRESSURIZED-REJECT SAME ON SECOND TRY. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITIONSep 14, 2007 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA00015Spring · detachedCAPT SEAT SLIPPED BACK AT 80 KTS REJECTED TAKEOFF, SEAT CHECKED AND LOCKED INTO POSITION. INSPECTED SEAT LOCK MECHANISM, FOUND LEVER SPRING OFF, LEVER-REATTACHED SAME PER SMP-SEAT LOCKS NORMAL. OK FOR SERVICE. INSPECTED SEAT IAW MM 25-11-11-06-1. FOUND RELJan 3, 2007 · N685FE · Airbus A300F4605R · Flight Compartment EquipmentSDR 06FDEA03964Pitot Tube · obstructedFO NO AIRSPEED, RTO AT 50 KTS. REMOVED DEBRIS FROM FO PITOT PROBE, BLEW NITROGEN THRU 2 LINES SECTIONS AFT OF PROBE. NO DEBRIS NOTED. USING HAND PUMP, WAS ABLE TO READ 260KTS AT INDICATOR PER MM 34-10-00-5, OK FOR SERVICE.Nov 12, 2006 · N685FE · Airbus A300F4605R · Pitot/Static SystemSDR 06FDEA2824Hose · rupturedAFTER T/O Y-SYSTEM LO PRESS ECAM RSVR SHOWED FLUID LOSS. LANDED, TAXIED BACK. SVCD Y-HYD SYSTEM TO FULL, PRESS Y-HYD, FOUND 1 HOSE RUPTURED IN RT WHEEL WELL AFT OUTBOARD CORNER. MARKED WITH SPEED TAPE AND A RAG, NEED HOSE MFG AE712686-1. ALSO FOUND ANOTHEAug 2, 2006 · N685FE · Airbus A300F4605R · Hydraulic System, MainSDR 02FDEA00882Thrust Reverser · malfunctionedNR 2 REVERSER PRESSURIZED AT 60KTS ON TAKEOFF MSP. ACN RELEASED FOR SERVICE PER MEL/CDL. ENGINE NR 2 THRUST REVERSER INOP. THRUST (1 OR 2) REVERSER DEACTIVATED IN FORWARD THRUST POSITION.Nov 27, 2002 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR 01FDEA00237Landing Gear · failedLANDING GEAR WOULD NOT RETRACT AFT DEPART IAH. WHEEL WELL DOORS OPENED. PERF SYS BITE, NO FAULTS FOUND, DEFERRED NR 1 POS IND SYS ON MEL 32-2.Mar 29, 2001 · N685FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 99FDEA00515Indicator · leaking99-298 - NR 2 ENG OIL QTY BEFORE START WAS 17 QTS, AFT START AND T/C WAS 13 QTS. AFTER 1 HR CR 10 QT. THEN LOSS OF A QT 20 MIN 7 QTS. SWAPPED OIL QUAN IND PER MEM MOCC. RAN ENGINE, FOUND NO LEAKS. ENG IND 17 QTS.Dec 30, 1999 · N685FE · Airbus A300F4605R · Engine Oil Quantity
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