N682FE
Service difficulty reports · 299
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 = 'N682FE' 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.
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 = 'N682FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201610133600Floor Panel · brokenMAIN CABIN FLOOR PANEL 231CF BROKEN. FABRICATED FLOOR PANEL 231CF IAW SRZ-25-005. CAT "A" MAJOR.SDR FDEA201610133599Floor Panel · brokenMAIN CABIN FLOOR PANEL 232FF BROKEN. FABRICATED FLOOR PANEL 232FF IAW SRZ-25-005. CAT "A" MAJOR.SDR FDEA201610133597Floor Panel · brokenMAIN CABIN FLOOR PANEL 232DF BROKEN. FABRICATED FLOOR PANEL 232DF IAW SRZ-25-005. CAT "A" MAJOR.SDR FDEA201610133596Floor Panel · brokenMAIN CABIN FLOOR PANEL 232RG BROKEN. FABRICATED FLOOR PANEL 232RG IAW SRZ-25-005. CAT "A" MAJOR.SDR FDEA201610133595Floor Panel · brokenMAIN CABIN FLOOR PANEL 232TG BROKEN. FABRICATED FLOOR PANEL 232TG IAW SRZ-25-005. CAT"A" MAJOR.SDR FDEA201610133593Floor Panel · brokenMAIN CABIN FLOOR PANEL 242GJ BROKEN. FABRICATED FLOOR PANEL 242GJ IAW SRZ-25-005. CAT "A" MAJOR.SDR FDEA201610133591Floor Panel · damagedMAIN CABIN FLOOR PANEL 241GJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133590Floor Panel · damagedMAIN CABIN FLOOR PANEL 241MJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133589Floor Panel · damagedMAIN CABIN FLOOR PANEL 241WJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133588Floor Panel · damagedMAIN CABIN FLOOR PANEL 241ZJ FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133587Floor Panel · damagedMAIN CABIN FLOOR PANEL 241VH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
SDR FDEA201610133586Floor Panel · damagedMAIN CABIN FLOOR PANEL 241TH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133583Floor Panel · crackedFWD CARGO FLOOR PANEL 132PG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133582Floor Panel · crackedFWD CARGO FLOOR PANEL 131MG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610133581Floor Panel · crackedFWD CARGO FLOOR PANEL 132NG IS CRACKED.. FABRICATED A NEW FLOOR PANEL IAW SRZ- 25-005. MAJOR REPAIR.SDR FDEA201610133580Floor Panel · crackedFWD CARGO FLOOR PANEL 132LG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRSDR FDEA201610133579Floor Panel · crackedFWD CARGO FLOOR PANEL 131QG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123570Floor Panel · crackedFWD CARGO FLOOR PANEL 131NG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123569Floor Panel · crackedAFT CARGO FLOOR PANEL 151TF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123568Floor Panel · crackedAFT CARGO FLOOR PANEL 151UF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123567Floor Panel · crackedAFT CAGO FLOOR PANEL 152RF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123566Floor Panel · crackedAFT CARGO FLOOR PANEL 151SF FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123565Floor Panel · crackedFWD CARGO FLOOR PANEL 132RG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123564Floor Panel · crackedFWD CARGO FLOOR PANEL 131SG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123563Floor Panel · crackedFWD CARGO FLOOR PANEL 131RG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123562Floor Panel · crackedFWD CARGO FLOOR PANEL 132SG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123560Floor Panel · crackedFWD CARGO FLOOR PANEL 131LG IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123559Floor Panel · crackedFWD CARGO FLOOR PANEL 131KG IS CRACKED FABRICATED FWD CARGO FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201610123556Deck Plate · corrodedMAIN CARGO DECK BETWEEN SEAT TRACKS 1 AND 2R AT FRAME 25, HAS CORROSION ON MAIN DECK PANEL. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS ON DECK PLATE IAW SRM 53-13-15. REMOVED PANEL IAW SRM 51-40-21 AND STIFFNER. FABRICATED PANE IAW SRM 53-SDR FDEA201609023104Smoke Detector · false activationMAIN DECK CARGO SMOKE, AFT COMPARTMENT INDICATION. COMPLIED WITH ECAM AND WARNING EXTINGUISHED. NO EXCESSIVE TEMPS ON ECAM AIR CONDITION PAGE. VISUAL INSPECTION REVEALED NO SMOKE ON MAIN DECK. ACCESSED AFT MAIN CARGO DECK. NO EVIDENCE OF SMOKE WAS PRESENTSDR FDEA201510153232Computer · faultedON APPROACH ON SLAT EXTENSION 1 & 2 SLATS & FLAPS FAULT, CYCLED NO HELP. WHILE PERFORMING QRH PROCEDURE SLAT & FLAPS EXTENDED NORMALLY. DURING POST FLIGHT CHECKS FOUND FAULTS ON BOTH SFCC'S. SFCC 1 & SFCC 2, BOTH INDICATED SLAT JAM. RESET BOTH SFCC'S & CYSDR FDEA201504051155Rib · corrodedLEFT MLG FWD LUG HAS CORROSION ON BOTH FACES & BORE COMPLIED WITH EA 6-5710-T0316549, REPAIR OF RIB 5 FWD LUG LT.SDR FDEA201504021142Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0316574 REV NO POS P1.SDR FDEA201503251082Hose · crackedDG EXTINGUISHER HOSES NR 1 & 3, CRACKED & COLLAPSING WHERE HOOKED TO DG CAN & NEED TO BE REPLACED. R & R HOSES NR 1 & 3 IAW AMM 26-28-00, OK FOR SVC.SDR FDEA201407151778Skin · delaminatedRIGHT WING AILERON UPPER SURFACE HAS ONE DENT 5.5 INCHES FROM AFT SIDE & 6 INCHES FROM INBD SIDE. IAW NTM 51-10-08 CHECK FOR CRACK & NO CRACK FOUND. TAP TEST INSPECT THE DENT & FOUND DELAMINATION 20MMX20MM IAW SRM 57-61-11 & SRM 51-77-12 PARA 4 D REMOVE THE SDR FDEA201407111704Skin · damagedLEFT PYLON AFT FAIRING LOWER BLUE HYD TUBE CONNECTOR LOOSED AT WING SKIN POS. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORKSDR FDEA201407111703Skin · damagedLEFT PYLON AFT FAIRING LOWER GREEN HYD TUBE CONNECTOR LOOSED AT WING SKIN POS. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORSDR FDEA201407111702Skin · damagedRIGHT ENG PYLON AFT FIRING ONE HYD TUBE LOOSED. CLEAN THE RELATED AREA PER A300-600 AMM51-78-00 AND FOUND THE WING SKIN HOLE DAMAGED. OVERSIZE THE HOLE CONCENTRICALLY TO REMOVE THE DAMAGE. PERFORM HFEC INSPECTIONS TO THE REWORKED AREA AND NO CRACK FOUND PERSDR FDEA201405141020Gcu · failedLOST AC BUS NR 2 IN FLIGHT 5 MIN AFTER T/O AT 8,000'. RETURNED TO KMEM. R & R NR 1 ENG GCU IAW AMM ATA 24-22-12-04. OPERATIONS CHECKED GOOD ON ENG RUN IAW A300-600 JRH. .SDR FDEA201405130997Unknown · unknownON ARRIVAL, LOST AC BUSS 2 AND ALL ASSOCIATED EQUIPMENT & FLIGHT CONTROLS. NOT ABLE TO RESET ANYTHING. ACFT FLOWN ON GEN 1 & APU GEN ENTIRE FLT IAW MEL 24-11-01-A. SUGGEST GEN 2 IS NOT THE PROBLEM. PERFORMED TROUBLESHOOTING PROCEDURES TO AC BUSS NR 2, FOUNSDR FDEA201403270593Pressure Switch · failedNR 2 FUEL FILTER CLOG ECAM & AMBER FUEL CLOG LIGHT ILLUMINATED ON CTR ENGINE PANEL. FOLLOWED ECAM, QRH & LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-11-04. OPS AND LEAK CHECKED GOOD IAW AMM 71-00-00-SDR FDEA201402040258Tru · failedON FINAL APPROACH TO KMEM, FIRST OFFICER`S INSTRUMENTS LOST ALONG WITH SPOILERS, NR 2 PITCH TRIM, NR 2 YAW DAMPER, FIRST OFFICER`S WINDOW HEAT LOSS WAS ONLY MOMENTARY. SHORTLY FOLLOWED BY ELEC ODOR IN THE COCKPIT. DECLARED EMERGENCY & LANDED. DURING FLIGHT SDR FDEA201308031755Transducer · failedCONFIGURED FOR LANDING, AT MED AUTOBRAKES SELECTION, ECAM AUTO BRAKE FAULT ILLUMINATED. DESELECTED AND RESELECTED WITH SAME RESULT., GO AROUND AND DIVERTED FOR TROUBLESHOOTING. AT GEAR EXTENSION, SAME RESULT. ACCOMPLISHED BITE CHECK OF BSCU IAW TSM 32-42-SDR FDEA201203020770Line · leakingON ARRIVAL, FOUND LARGE AMOUNT OF FUEL DRAINING FROM DRAIN MAST OF NR 1 ENGINE. OPENED NR 1 ENGINE CORE COWL AND FOUND MAIN FUEL LINE SPRAYING FUEL AT THE FIREWALL CONNECTION. PULLED FIRE HANDLE AND DISCONNECTED FUEL LINE AT THE FIREWALL AND FOUND RETAINER SDR FDEA201202090532Skin · damagedRT WING ALL SPEED AILERON LOWER SURFACE PUNCTURED AT T/E 23" FROM OTBD EGDE 0.10 DEEP, REF AMM 27-10-00-06M, REPAIRED PUNCTURE ON LOWER SURFACE OF R/T WING ALL SPEED AILERON, ALODINED PRIMED, AND TOP COAT REPAIR IAW SRM 51-77-12 4C, 51-21-10 AND 51-75-10 ANDSDR FDEA201202040474Door Frame · gougedFWD CARGO COMPT DOOR FRAME AT FR20A, 6 IN LONG GOUGE APPROX 1 INCH WIDE. COMPLIED WITH EA 6-5310-156091 PART 1.SDR FDEA201202030467Thrust Plate · corrodedMDCC FLOOR THRUST PLATE BETWEEN FR 26 AND FR27 AND -Y450 TO -Y 953 (SEAT TRACK 2R AND 3R), HAS .5 INCH OF CORROSION. THRUST PLATE FOUND TO BE OUT OF LIMITS IAW DWG A53781984. R & R THRUSTPLATE IAW SRM 51-40-21, PARA 5 AND DWG A53781984.SDR FDEA201202030466Seat Track · damagedUPON REMOVAL OF THRUST PLATE BETWEEN FR26-27, SEAT TRACK 4R AND 3R, FOUND 3 ELONGATED HOLES ON OTBD FLANGE OF SEAT TRACK AT SPLICE POINT, 1 EA DRILL START, AND REPAIR SPLICE UPPER FLANGE IS BENT. REPAIR SPLICE AND SEAT TRACK FOUND TO BE OUT OF LIMITS IASDR FDEA201202030450Structure · corrodedRIGHT WINGLET T/E INBD STATIC DISCHARGER HAS CORROSION EXTENDING FROM UNDERNEATH THE BASE ESTIMATED DEFECT MEASURES 4 SQ IN, REMOVED LEVEL 1 CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-30-11. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR IAW SRM 5SDR FDEA201202010425Seat Track · distortedMDCC SEAT TRACK 5L DISTORTED BELOW INBD FLANGE FR 20 DEFECT MEASURES 10" LONG. REPAIRED IAW EA6-5310-157810 PT 1.
Back to N682FE