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 FDEA201407091912Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241ZJ CRACKED. FABRICATED FLOOR PANEL 241ZJ ON T14 1080636 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091911Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 242GF UPPER SURFACE SKIN BULGING & DELAMINATED. FABRICATED NEW FLOOR PANEL 242GF ON T14 1080334 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091910Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL BETWEEN FRAME 30 - 37, -Y450 & -Y953 UPPER SURFACE HAS SKIN BULGING & DELAMINATED. FABRICATED NEW FLOOR PANEL 242BF ON T14 1080335 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091909Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL BETWEEN FRAME 60 - 62, -Y450 & -Y953 UPPER SURFACE HAS SKIN BULGING & DELAMINATION. FABRICATED NEW FLOOR PANEL 252UH ON T14 1079958 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091908Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL FROM FRAME 62 - 65, Y1959 & Y1456 UPPER SURFACE SKIN HAS BULGING & DELAMINATED. FABRICATED NEW FLOOR PANEL 251YG ON T14 1080331 IAW DWG SRZ-25-001. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091906Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242QJ CRACKED. FABRICATED NEW FLOOR PANEL 242QJ ON T14 1080642 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091905Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242EK CRACKED. FABRICATED NEW FLOOR PANEL 242EK ON T14 1080643 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091904Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 252BF UPPER SURFACE SKIN BULGING & DELAMINATED. FABRICATED NEW FLOOR PANEL 252BF ON T14 1080332 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091903Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UJ CRACKED. FABRICATED NEW FLOOR PANEL 242UJ ON T14 1080644 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091902Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242WH CRACKED. FABRICATED NEW FLOOR PANEL 242WH ON T14 1080645 IAW DWG SRZ- 25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091901Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241UJ CRACKED. FABRICATED NEW FLOOR PANEL 241UJ ON T14 1080647 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091900Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241GK CRACKED. FABRICATED FLOOR PANEL 241GK ON T14 108063 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091899Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241AJ CRACKED. FABRICATED FLOOR PANEL 241AJ ON T14 1080638 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091898Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241WH CRACKED. FABRICATED FLOOR PANEL 241WH ON T14/1080639 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407091897Floor Panel · crackedMAIN CABIN FLOOR PANEL 242ZJ CRACKED. FABRICATED NEW PANEL 242ZJ ON T14/1080635 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.Jul 9, 2014 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201407081953Skin · gougedLEFT WING INNER FLAP SKIN UPPER SURFACE HAS GOUGE. BLENDED AREA IAW SRM 51-73-10, L=3.0 INCHES, W=1.3 INCHES & D=.020 INCHES, FOUND OUT OF LIMITS IAW SRM 57-50-00 FIG 101. PERFORMED SKIN PATCH REPAIR BY FABRICATED REPAIR DOUBLER FROM MATERIAL 2024T3-056C BATJul 8, 2014 · N685FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201407031921Skin · dentedFORWARD RT EXTERNAL FUSELAGE AT FRAME 2 BELOW FLOOR LINE, SKIN IS DENTED. DENT MEASURES A=1.5 INCHES, B=0 INCHES, D=.125 INCHES & T=.047 INCHES, FOUND TO BE OUT OF NEARNESS IAW SRM 53-11-12. REPAIRED AREA IAW SRM 53-11-12 FIG 201. PAINTED AREA IAW SRM 51-75Jul 3, 2014 · N685FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201309052123Filter · failedNR 2 ENGINE GENERATOR FAULTED DURING CLIMBOUT AT ABOUT 4500 FT. ATTEMPTED RESET IAW ECAM. DRAINED NR 2 IDG OIL, INSTALLED NEW IDG OIL FILTER, RAN ENGINE NR 2 GENERATOR. OPS CHECKED GOOD. IAW MM 24-11-00-03-01, & MM 12-13-24-00-01.Sep 5, 2013 · N685FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201211294202Smoke Detector · malfunctionedPASSING APPROX FL300, RECEIVED A AFT & BULK SMOKE INDICATION. COMPLIED WITH ECAM CHECKLIST AND RETURN TO DEPARTURE. NO SMOKE INDICATION INSIDE ACFT. FIRE CREW HAD NO HEAT INDICATIONS ON AFT END OF ACFT. REPLACED AFT CARGO BAY SMOKE DETECTORS 9WH AND 44WH, Nov 29, 2012 · N685FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201205181849Skin · dentedLT WING OUTER FLAP L/E DENTED APPROX L=12" X W = 4" X D =.46" BETWEEN RIB 17 AND 18 DENT MEASURING L =12" X W = 4" X D =.79" FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, FIG 101. REPAIRED LT WING OUTER FLAP L/E IAW SRM 57-50-00, FIG 208. OPS CHECKED GOOD IAW May 18, 2012 · N685FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201205161821Crossbeam · gougedMAIN DECK CARGO CROSSBEAM FR 57 BETWEEN SEAT TRACK 2R AND 3R AFT SIDE OF CROSSBEAM HAS ONE GOUGE AT VERTICAL STIFFENER, ONE GOUGE ON RADIUS OF RISER, NINE GOUGES ON AFT FACE OF CROSSBEAM AT FASTENER HOLES. SMOOTHED DAMAGED AREA IAW SRM 51-73-10 PG 209, STEP May 16, 2012 · N685FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201205131807Adapter · gougedFLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R - 3R GOUGED AT FR 57 APPROX L = 0.5". R & R CLEVIS ADAPTER AT FR 57, SEAT TRACK 2R TO 3R IAW FSRM 51-72-10, PARA 6, PG 2.May 13, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205111790Seat Track · wornBETWEEN FR 60 AND 61, SEAT TRACK 4L HAS A BROKEN AND WORN SCALLOP. FOUND DAMAGED SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 201. REPAIRED DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 102.May 11, 2012 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205091774Skin · dentedRIGHT WING AILERON DENTED AT LOWER SURFACE 3 INCHES FROM T/E AND 28 INCHES FROM OTBD SIDE 2 SQUARE INCHES X .020 INCHES. REPAIRED IAW SRM 51-77-12 PAR 4C. RESTORED SURFACE PROTECTION IAW SRM 51-75-10, PAR 5 AND COMPLIED WITH EA6-5750-157845 PT 1.May 9, 2012 · N685FE · Airbus A300F4605R · AileronsSDR FDEA201205041741Skin · gougedLEFT WING CENTER FLAP UPPER SURFACE MID SECTION BETWEEN RIBS 13 TO RIBS 15 AND BETWEEN STRINGERS 2.5 & 2.7 HAS SIX GOUGES. REPAIRED IAW FSRM 57-50-00, FIG 205, PAGE 216-219.May 4, 2012 · N685FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201205011694Floor Support · corrodedMAIN DECK CARGO, FR13 TO 17 BELOW FLOOR PANEL 221FF FLOOR SUPPORT TEE UPPER FLANGE HAS THREE AREAS WITH CORROSION. REMOVED LEVEL 1 CORROSION , R & R FLOOR SUPPORT IAW SRM 51-74-10 AND 51-72-10.May 1, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205011690Thrust Plate · corrodedTHRUST PLATE FROM FR 25 TO FR 26 BETWEEN SEAT TRACKS 5L & 6L HAS 3 EA. AREAS OF CORROSION (MARKED). APPROX 3 SQ IN TOTAL. REMOVED CORROSION FROM THRUST PLATE AT FRAME 25-26 BETWEEN 5L AND 6L IAW FSRM 51-74-10. FOUND TO BE OUT OF TOLERANCE MFG DWG A53781984 May 1, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204301685Floorboard · damagedAFT CARGO FLOORBOARD 151VF 18 EA AREA IMPACT DAMAGE BOTTOM AND IS BROKEN. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 30, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204291671Stiffener · crackedFWD CARGO COMPPARTMENT UPPER CEILING FR 32 BETWEEN SEAT TRACKS 2R & 3R BEAM VERTICAL STIFFENER CRACKED. REPAIRED FWD CARGO COMPT UPPER CEILING FR 32 BETWEEN 2R & 3R IAW FSRM 53-10-15, FIG 212 SHEETS 1 & 2 PAGES 393-400.Apr 29, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204291670Adapter · gougedMAIN DECK CARGO, CLEVIS ADAPTER GOUGED AT FRAME 57.1 BETWEEN SEAT TRACKS 2R AND 3R. REMOVED AND REPLACED CLS ADAPTER AT FRAME 57.1 BETWEEN SEAT TRACKS 2R AND 3R IAW FSRM 51-40-21 PAR. 7.Apr 29, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204291669Adapter · gougedMAIN DECK CARGO, CLEVIS ADAPTER AT FRAME 57.2 BETWEEN TRACKS 2R AND 3R GOUGED. R & R CLEVIS ADAPTER AT FRAME 57.2, BETWEEN TRACKS 2R AND 3R IN MDCC, IAW FSRM 51-40-21, PAR 7.Apr 29, 2012 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204271658Floor Panel · delaminatedAC COMPARTMENT FLOOR PANEL 147AF UPPER SURFACE, DISBONDED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271652Floor Panel · crackedFLOOR PANEL 242ZJ HAS EIGHT CRACKS AT CLEVIS CUTOUTS FROM 3" TO 9 " LENGTH. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271650Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241AJ HAS 7 EACH CRACKS AROUND CLEVIS ADAPTER CUTOUTS FROM 4" TO 9" LENGTH. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271649Floorboard · crackedFLOORBOARD 242QJ HAS SEVEN CRACKS AROUND CLEVIS CUTOUTS FROM FOUR TO NINE INCHES. LENGTH FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271648Floorboard · crackedFLOORBOARD 232YG HAS THREE, NINE INCH CRACKS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271647Floorboard · damagedAFT CARGO FLOORBOARD 151MF HAS TWELVE AREAS OF IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV JApr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271646Floorboard · damagedFWD CARGO FLOORBOARD 131QF HAS TEN AREAS OF IMPACT DAMAGE AND EDGE DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204271645Floorboard · delaminatedFWD CARGO BAY FLOORBOARD 132QF BOTTOM SIDE HAS SIX PUNCTURES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 27, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261623Floorboard · damagedFLOORBOARD 242 RG BROKEN, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261622Floor Panel · crackedFLOOR PANEL 242MF HAS SIX CRACKS FROM 2 TO 8 INCHES, AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261621Floor Panel · crackedFLOOR PANEL 251YG HAS TWO CRACKS ON TOP SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261620Floor Panel · crackedFLOOR PANEL 242GF HAS SIX CRACKS FROM 2 TO 9 INCHES, AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261619Floor Panel · crackedMAIN DECK CARGO, FLOOR PANEL 242UJ HAS EIGHT CRACKS AROUND CLEVIS CUTOUTS FROM 3 TO 9 INCHES IN LENGTH FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261618Floor Panel · damagedFWD CARGO FLOOR PANEL 131PG HAS TWO BROKEN AREAS AND EDGE DAMAGE. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261617Floor Panel · crackedFLOOR PANEL 232NG HAS TWO 9 INCH CRACKS. FABRICATED FLOOR PANEL DWG NR SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204261616Floor Panel · crackedFLOOR PANEL 242BF HAS THREE CRACKS IN TOP SKIN FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Apr 26, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204251584Floorboard · crackedMAIN DECK CARGO FLOORBOARD 241GH HAS TWO CRACKS AT CLEVIS CUTOUTS APPROX 9 INCHES LENGTH. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Apr 25, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204251583Floorboard · crackedMAIN DECK CARGO FLOORBOARD 241TH HAS TOP SIDE CRACKED 20 INCHES. TOTAL LENGTH FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005. REV J.Apr 25, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204251582Floorboard · crackedMAIN DECK CARGO FLOORBOARD 251NG HAS TWO CRACKS FROM 6-8 INCHES LONG AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOORBOARD DWG SRZ 25-005, REV J.Apr 25, 2012 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
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