N680FE

Service difficulty reports · 219

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 = 'N680FE' 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 FDEA201608263011Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL 252RG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608263001Floor Panel · damagedMAIN DECK FLOOR PANEL 242DF DAMAGED FABRICATED FLOOR PANEL 242DF ON T16/1225111 IAW SRZ 25-005. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262999Floor Panel · damagedMDCC FLOOR PANEL 241TH PUNCTURED, CRACKED 91-078. FABRICATED PANEL 241TH ON T16/1225470 IAW SRZ-25-005. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262998Floor Panel · delaminatedDELAMINATION, CRACK ON FLOOR PANEL 242AK IN MD CARGO COMPARTMENT FRAME 47, RT SIDE, DOT 139-010. FABRICATED PANEL 242AK ON T16/1225628 IAW SRZ 25-005. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262997Panel · wornAGING REPAIR ASSESSMENT: RIGHT HORIZONTAL STABILIZER L/E PANEL 341AB FOUND HOLE ELONGATED. COMPLY WITH ATTACHMENT-B OF EO 6-5100-7-5000, PART 1. COMPLIED WITH ATTACHMENT-B OF EO 6-5100-7-5000 P1 INSPECTION OF REPAIR, DETERMINED IT TO BE CURRENT WITH FAA APPRAug 26, 2016 · N680FE · Airbus A300F4605R · Horizontal Stabilizer, Plate/SkinSDR FDEA201608262996Mount · corrodedNR 1 ENGINE FORWARD PYRAMID MOUNT INBD AFT HOLE HAS A SIGN OF CORROSION AND HAS GOUGE ON TOP 91-097. REMOVED CORROSION IAW SRM 51-74-10 & GOUGE IAW SRM 51-73-10. BORE DIAMETER AFTER REMOVAL IS 0.964", FOUND TO BE WITHIN REPAIRABLE LIMITS IAW SRM 54-51-81, FIAug 26, 2016 · N680FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA201608262992Floor Panel · damagedFORWARD CARGO FLOOR PANEL 131KG BROKEN DAMAGED. PANEL RACK, FABRICATED FLOOR PANEL 131KG ON T16/1225127 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262991Floor Panel · damagedFWD CARGO FLOOR PANEL 132KG BROKEN, DAMAGED. PANEL RACK, FABRICATED FLOOR PANEL 132KG ON T16/1225128 IAW SRZ 25-005, CAT-A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262990Floor Panel · crackedAFT CARGO FLOOR PANEL 152PF CRACKED. FABRICATED FLOOR PANEL 152PF ON T16/1225224 IAW SRZ 25-005, CAT A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262989Floor Panel · crackedAFT CARGO FLOOR PANEL 152RF CRACKED. FABRICATED FLOOR PANEL 152RF ON T16/1225120 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262988Floor Panel · damagedFORWARD CARGO FLOOR PANEL 132SG BROKEN, DAMAGED. FABRICATED FLOOR PANEL 132SG ON T16/1225126 IAW SRZ 25-005 CAT-A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262987Floor Panel · crackedAFT CARGO FLOOR PANEL 151WF CRACKED. FABRICATED FLOOR PANEL 151WF ON T16/1225119 IAW SRZ 25-005. CAT-A. MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262986Floor Panel · crackedAFT CARGO FLOOR PANEL 152WF CRACKED. FABRICATED FLOOR PANEL 152WF ON T16/1225384 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262985Floor Panel · crackedAFT CARGO FLOOR PANEL 151PF CRACKED. FABRICATED FLOOR PANEL 151PF ON T16/1225376 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262984Floor Panel · crackedAFT CARGO FLOOR PANEL 151MF CRACKED. FABRICATED FLOOR PANEL 151MF ON T16/1225374 IAW SRZ 25-005, CAT-A MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608262983Floor Panel · crackedAFT CARGO FLOOR PANEL 152VF CRACKED. FABRICATED FLOOR PANEL 152VF ON T16/1225401 IAW SRZ 25-005. CAT-A, MAJOR REPAIR.Aug 26, 2016 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201511203727Computer · faultedWHEN FLYING ILS 26L, AT 3000 MSL & ON INTERCEPT HEADING TO FINAL, WHILE SLOWING FROM 170 KIAS TO 160, FLAPS STUCK AT 15. RECYCLED HANDLE & FLAPS STAYED STUCK AT 15. SLATS WORKED NORMALLY, LANDED WITH FLAPS 15. CHECKED FLAP TORQUE INDICATORS, NOT SET. CHECKNov 20, 2015 · N680FE · Airbus A300F4605R · Trailing Flap Position Indicating SystemSDR FDEA201503281110Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION ON FWD FACE & IN BORE. COMPLIED WITH EA 6-5710-T0316490 REV NO POS P1. WINGS, BASIC WING STRUCTURE CORROSION REPAIR OF RIB 5 FWD LUG. MAJOR REPAIR.Mar 28, 2015 · N680FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201412024038Rib · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & BOTH FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0313802 WINGS BASIC WING STRUCTURE TERMINATING ACTION OF MLG SUPPORT RIB 5 FWD LUG LT. MAJOR REPAIR.Dec 2, 2014 · N680FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406031287Fitting · crackedFOUND FRAME 12A RT FITTING CRACKED 5/8 INCH. R & R FITTING IAW EO 6-5340-7- 5002 PT 7.Jun 3, 2014 · N680FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201406031286Fitting · crackedONE CRACK 5/8 INCH, WAS FOUND AT FRAME 12A RT FITTING AREA. R & R FITTING IAW EO 6-5340-7-5002 PT8. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 3, 2014 · N680FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201405281210Attach Angle · crackedFORWARD MAIN DECK UTILITY AREA FOUND ONE ATTACHED ANGLE CRACKED. CUT OUT DAMAGED ATTACH ANGLE. FABRICATED REPLACEMENT SECTION OF ANGLE AND REPAIR SPLICE ANGLE. INSTALLED REPAIR WET WITH SEALANT IAW EA 6-5310-T0308363. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2May 28, 2014 · N680FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201405271201Skin · scratchedLOWER FUSELAGE EXTERNAL SKIN SCRATCHED, LOCATION BETWEEN FRAME 66 & 67 FROM STRING 49 RT TO 52 RT. DURING PRELIMINARY INSPECTION WAS FOUND, BLEND OUT THE SCRATCHED ARE & MEASURE THE MAX DEPTH 0.036"X2.7"X1.7" DXLXW OVER ALLOWABLE LIMIT IAW AB6F SRM 53-17-12 &May 27, 2014 · N680FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201305311147A/C Pack · overheatedON CLIMBOUT, RECEIVED ECAM ADV FOR PACK 2 AT 95 DEGREES & CLIMBING. PACK NR 2 MODE SELECTED TO MAN AND MODUALATED VALVE POSITION TO KEEP PACK FROM OVERHEATING. COULD NOT GET COCKPIT TEMP BELOW 96 DEGREES AND RISING. R & R FAN BYPASS CHECK VALVE IAW AMM 2May 31, 2013 · N680FE · Airbus A300F4605R · Cabin Cooling SystemSDR FDEA201207042482Warning Light · false activationLANDING GEAR AIR GROUND POSITION DISAGREE AT ROTATION, SWITCHED TO POSITION NR 2. CREW DEBRIEF INDICATES THAT FAULT WAS ECAM ALERT - FLT/GND DISAG. FURTHER DEBRIEF INDICATES THAT FAULT CLEARED WHEN L/G POS NR 2 WAS SELECTED.Jul 4, 2012 · N680FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201203080822Skin · damagedRIGHT HORIZ STABILIZER L/E PANEL NR 341AB FOUND HOLE ELONGATED. REPAIRED IAW EA 6-5510-150443 PART1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Horizontal Stabilizer, Plate/SkinSDR FDEA201203080815Floor Panel · damagedCARGO BAY FLOOR PANEL 162HF FOUND DAMAGED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-35 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-011 REVISION E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203080814Floor Panel · corrodedBULK CARGO COMPARTMENT FLOOR PANEL 162EF LOWER SURFACE FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-35 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-011 REVISION E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203080811Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241JF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203080810Floor Panel · delaminatedMAIN DECK FLOOR PANEL NR 242KF FOUND DELAMINATED. MAIN DECK FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REV. 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REV. J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203080813Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241PF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203080809Floor Panel · delaminatedCOCKPIT FLOOR PANEL NR 211HF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-21 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SR30-53-005. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201203080812Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242MF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 8, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203060789Floor Panel · brokenMAIN DECK FLOOR PANEL 241LK FOUND BROKEN. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 6, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203060788Seat Track · wornMAIN DECK SEAT TRACK AT FRAME 54 TO FRAME 54.2 LT NR 5 FOUND DIMENSION "B". GAP VALUE EXCEEDED LIMITS. REPAIRED IAW SRM 53-15-16 FIGURE 201 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 6, 2012 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203030766Seat Track · crackedMAIN DECK SEAT TRACK AT FRAME 54 - 54.2, LEFT NR 3 FOUND CRACKED AT CROWN AREA. DAMAGED SEAT TRACK REMOVED AND NEW SEAT TRACK INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201203030762Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241GJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030755Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242ZJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030754Floor Panel · delaminatedMAIN DECK FLOOR PANEL 232YG FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23, REV 52.2. NEW FLOOR PANEL 232YG FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030752Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241WH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030751Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241AJ FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030750Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241TH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030746Floor Panel · delaminatedMAIN DECK FLOOR PANEL 251XG FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030745Floor Panel · delaminatedMAIN DECK FLOOR PANEL 241QH FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL NR 241QH FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030744Floor Panel · delaminatedMAIN DECK FLOOR PANEL 251VF FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 53-10-25, REV 52.2. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030764Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242SF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030759Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242BF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030757Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242UJ FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. NEW FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030756Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242QJ FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-25 REVISION 52.2. FLOOR PANEL FABRICATED IAW DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201203030753Floor Panel · delaminatedMAIN DECK FLOOR PANEL 242GF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-10-23 REVISION 52.2. NEW FLOOR PANEL FABRICATED AS PER DRAWING SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Mar 3, 2012 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
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