N675FE
Service difficulty reports · 248
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 = 'N675FE' 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 = 'N675FE' 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 FDEA201708232325Dummy Rail · crackedDUMMY SEAT TRACK LT NR 5 AT FR 54 TO FR54.2 FAILED GAP CHECK. UPON REMOVAL OF LT NR 5 DUMMY SEAT TRACK AND 3EA FLOOR SUPPORTS FOUND DUMMY SEAT TRACK CRACKED. REMOVED AND REPLACED LT NR 5 DUMMY SEAT TRACK FR 54 TO FR54.2 AND REINSTALLED 3EA FLOOR SUPPORTS IAWSDR FDEA201708222296Dummy Rail · crackedDUMMY SEAT TRACK RT NR 5 AT FR38.2 TO FR40 FAILED GAP CHECK. UPON REMOVAL OF RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 FOUND CRACKED. NO ESTABLISHED LIMITS PER SRM. REMOVED AND REPLACED RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 IAW SRM 51-40-21. MAJOR REPSDR FDEA201708222295Seat Track · gougedMAIN DECK BETWEEN FRAME 57 TO FRAME 57.1 Y 1959. SEAT TRACK HAS GOUGE ON CROWN. CLS ATTACHED AT DAMAGE LOCATION FR57 - FR57.1 Y1959 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 204. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201 USING A53274005-SFS-. MAJOR RESDR FDEA201703230982Door · unknownR1 DOOR SLIDE WILL NOT ARM. RAN A R1 DOOR SLIDE ARMING TEST AND TEST OF THE ASPSU IAW MM 25-61-20-06-01 AND 52-73-00-05-02. ALL CHECKS WERE NORMAL.SDR FDEA201612164475Switch · stickingL1 DOOR EMERGENCY TEST SWITCH (25WL) STICKS IN THE TEST POSITION. REMOVED AND REPLACED THE SWITCH IAW SMP. SYSTEM OPS CHECKED GOOD IAW MM 33-51-00-05. ACFT OK FOR SERVICE.SDR FDEA201605031444Not Reported · malfunctionedAS WE LOST A/S THE RUDDER STARTED PULSING LT & RT. NO RUDDER LIMIT LIGHTS ILLUMINATED. IT DAMPED AS WE SLOWED & DESCENDED. NR 2 YAW DAMPER WAS ENGAGED. WE HAD KICKED AUTOPILOT OFF AT THIS POINT, SIGNIFICANT YAWING LT & RT. PRECAUTIONARY R & R NR 2 FAC IAWSDR FDEA201603100893Gcu · malfunctionedDUE TO NR 2 GEN FAULT, STARTED APU & THEN APU GEN FAULTED. INFO ONLY, MASSIVE AMOUNT OF RAIN & LIGHTNING STRIKE TWO LEGS PRIOR. APU HAD FAULTED FIRE TRIP ON GND POWER CONTROL UNIT. R & R THE APU GEN CONTROL UNIT IAW A & B AMM CHPT 24-22-12-04. RAN APU GENSDR FDEA201603100887Gcu · failedAT FL300 NR 2 GEN FAULTED, RESET FAULTED AGAIN. COMPLIED IN ECAM & QRH & PAW. FOUND NR 2 GEN GCU FAILED ON THE GPCU. R & R THE NR 2 ENG GEN GCU IAW A & B AMM CHPT 24-22-12-04. RAN THE NR 2 ENG IAW A & B JRH, NR 2 GEN. OPERATIONS CHECKED SATISFACTORY. ACFSDR FDEA201506242014Stator · failedAFTER TAKEOFF NR 1 BRAKE INDICATOR ROSE TO 300. DROPPED GEAR TO COOL THE BRAKES. AFTER BRAKES WHERE COOL, CONTINUED FLIGHT TO DESTINATION. REMOVED TIRE & FOUND THAT STATOR DISK HAS COME APART & WEDGED BETWEEN THE TWO ROTOR DISK. R & R BRAKE IAW 32-42-27-SDR FDEA201504111214Spar · damagedLEFT WING ROOT REAR SPAR SPOT FACE DAMAGED. REPAIRED IAW SRM 51-71-80. COMPLIED WITH EA 6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201504111213Spar · damagedLEFT WING ROOT REAR SPAR 47, RIB 1 HOLE U SPOT FACE DAMAGED. SPOTPACED THE HOLE U AT LT WING ROOT SPAR IAW SRM 51-71-80. COMPLIED WITH EA :6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503271093Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 26 - 38.2, Y0. REMOVED THE CORROSION IAW SRM 51-74-10 EXCEEDED THE ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-16-101 FIG 102. CUT OUT THE DAMAGED SEAT TRACK SECTION AT FRAME 26 - 28 IAW SRM 53-10-16-201 PARA 4. WETSDR FDEA201503271092Skin · damagedLOWER FUSELAGE, FRAME 36 - 37, STRINGER 43R - 44R,SEVERAL LIGHTING STRIKE BURN MARKS ON SKIN. REPAIRED THE SKIN IAW SRM 53-10-12 FIG 208. INSTALLED THE DOUBLER & FASTENERS ON REPAIRED PART IAW SRM 53-10-12 FIG 208. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503251074Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 54.3 - 58, Y-450. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503231056Rivet · corrodedAGEING INSPECTION, EXISTING REPAIR ON MDCC SEAT TRACK BETWEEN FRAME 65 - 69, Y0 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND THE REPAIR CONFORMED TO SRM 53-10-16 FIG 201 EXCEPT MINOR DEVIATION. NO CHAMFER EDGES, MOREOVER, SOME RIVETS SDR FDEA201503221047Fitting · looseRIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND INBD LUG BUSHING LOOSE. REPAIRED IAW AMM 54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503221046Fitting · looseRIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REPAIRED IAW SRM 51-72-20, AND AMM54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503221045Fitting · looseLEFT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REMOVED THE BUSHING IN REPAIR AREA IAW SRM 51-72-20. RE-BORED THE RIB 12 FITTING WITHOUT EXCEED 62.23MM IAW AMM 54-51-72-08-02. INSTALLED THE BUSH IAW AMM 54-51-72-08-02. SDR FDEA201503221044Seat Track · crackedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED FRAME 26 - 38.2, Y-1959. REMOVED THE CORROSION IAW SRM 51-74-10. CRACK WAS FOUND AND WAS OUT OF ALLOWABLE IAW SRM 53-10-16-101. CUT OUT SEAT TRACK. REPAIRED IAW SRM 53-10-16 FIG 201. THIS REPAIR WAS CATEGORY "A". SDR FDEA201503201029Skin · damagedAGEING INSPECTION, EXISTING REPAIR ON RT WING INBD FLAP UPPER SKIN RIB 11 - RIB 13 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 206. WORN MARKS WERE ALSO FOUND ON EXISTING REPAIR DOUBLER, REPORTSDR FDEA201503201028Skin · damagedAGEING INSPECTION, EXISTING REPAIR ON LT WING MID FLAP UPPER SKIN RIB 13 - 15 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 205. MOREOVER WORN MARKS WERE ALSO ON EXISTING REPAIR DOUBLER, REPORTEDSDR FDEA201503201025Repair · crackedAGEING INSPECTION, EXISTING REPAIR ON MDCC FLOORBEAM BETWEEN FRAME 28, Y-450 TO Y-953 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH EA 6-5310-101017. MOREOVER, THE EXISTING REPAIR FITTING FOUND CRACKED. REPORSDR FDEA201503201024Repair · damagedAGEING INSPECTION, EXISTING REPAIR ON RT INBD FLAP LE SKIN RIB 12A - 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 57-50-00 FIG 208. HOWEVER, DENTS & NICKS WERE FOUND ON EXISTING REPAIR INSERT. REPORTED TO SDR FDEA201503201023Adapter · wornMDCC FLOORBEAM ADAPTOR WORN, FRAME 32 BETWEEN Y1456 & Y1959. REMOVED THE DAMAGED ADAPTER IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201022Adapter · wornMDCC FLOOR STRUCTURE CROSSBEAM ADAPTOR WORN, FRAME 30 BETWEEN Y1456 & Y1959. REPLACED THE DAMAGE ADAPTOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201021Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 40 - 45, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED THE SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201020Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 44 - 48, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10. THE REMOVAL WAS WITHIN ALLOWABLE IAW SRM 53-10-16 101. MINOR REPAIR IAW GMM6-2-100.SDR FDEA201503201019Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 38.2 - 40, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED THE NEW SEAT SDR FDEA201503201018Seat Track · corrodedMDCC FRAME 74 - 75, Y-45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201017Seat Track · corrodedMDCC FRAME 65 - 66, -Y95.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201503201016Seat Track · corrodedMDCC FRAME 70 - 71, Y0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201015Seat Track · corrodedMDCC FRAME 70 - 71, -Y45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21, FRAME 68 - 73, -450. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201014Seat Track · corrodedMDCC FRAME 71 - 72, Y124.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 ,CRACK FOUND .CUT AND REMOVED THE CORROSION ON SEAT TRACK SECTION FOR FR68-FR69 .PER SRM 53-10-16 FIG 201. MADE THE REPAIR SPLICE AND SEAT .TRACK PER SRM 53-10-16SDR FDEA201503201013Seat Track · corrodedMDCC FRAME 71 - 72, Y88.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FR 69-72 Y852.4. PER SRM 51-40-21.THIS REPAIR CATEGORY IS "A" .MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201012Seat Track · corrodedMDCC FRAMES 76 - 77, Y79.0 SEAT TRACK CORRODED. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FRAME 73 - 77 IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100. .SDR FDEA201503201011Floor Support · corrodedMAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y1959 FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND DELAMINATION & REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW FLOOR SUSDR FDEA201503201010Floor Support · corrodedMAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y-1959 FLOOR SUPPORT CORRODED. REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW SUPPORT IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIRSDR FDEA201503201008Floorbeam · crackedMDCC FRAME 31, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 21SDR FDEA201503201007Floorbeam · crackedMDCC FRAME 32, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 21SDR FDEA201503201006Floorbeam · crackedMDCC FRAME 64 Y-112 FLOORBEAM CRACKED. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211, NO CRACK FOUND. REPAIRED THE FLOORBEAM IAW SRM 53-10-15 FIG 211. WET INSTALLED THE REPAIR PARTS IAW SRM 53-10-15 FIG 211. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMMSDR FDEA201503201005Seat Track · corrodedMDCC SEAT TRACK CORRODED ,FRAMES 40 - 42, Y-1456. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-1SDR FDEA201503201004Adapter · crackedMDCC FLOORBEAM CRACKED, FRAME 67 BETWEEN Y1456 & Y1959. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211. PERFORMED HFEC INSPECTION TO THE CUT OUT IAW NTM 51-10-08. NO CRACK FOUND. FABRICATED THE REPAIR ANGLE & FILLER SRM 53-10-15 FIG 211. WET INSTALLED TSDR FDEA201503201003Adapter · crackedMDCC FLOORBEAM ADAPTOR CRACKED, FRAME 59 BETWEEN Y-953 & Y-1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GSDR FDEA201503201002Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE LOWER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201001Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503201000Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503200999Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE LOWER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503200998Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503200997Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE UPPER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0316343 PT1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201503200996Adapter · crackedMDCC FLOORBEAM ADAPTOR CRACKED, FRAME 62 BETWEEN Y953 & Y1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. FABRICATED THE NEW ADAPTER IAW DWG A53278288. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM6-2-100.
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