N643FE
Service difficulty reports · 351
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 = 'N643FE' 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 = 'N643FE' 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 FDEA201108293547Hinge Bracket · corrodedRT WING OTBD FLAP INBD HINGE (WING SIDE) WING STA XW 486.403, LOWER MOUNT OTBD HOLE FOUND CORRODED HOLE EXCEEDED CMM 57-44-08 LIMITS ARC 0502-14. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750-154210, & EO 1-5750-7-5002. REPAIR CLASSIFIED AS MAJOR SDR FDEA201108293548Spar Cap · corrodedRT WING REAR SPAR CAP FOUND CORRODED. EXCEEDED LIMITS AT XORS 1040. CORROSION REMOVED IAW SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.148"; MATERIAL, REMOVED = 0.034"; MATERIAL REMAINED = 0.114" - FOUND EXCEEDED LIMIT IAW SRM 57-00-00, REV 47, FIGSDR FDEA201108293546Longeron · corrodedLONGERON 19R BS 1219-1239. FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. MATERIAL ORIGINAL THICKNESS = 0.100 INCH; MATERIAL REMOVED= 0.037 IN; MATERIAL REMAINED = 0.063 IN FOUND EXCEEDED LIMIT IAW SRM 53-00-00, REV 47, FIGURE 205. ACCOMPLISHSDR FDEA201108293545Longeron · corrodedLONGERON 16L BS 1199-1219 CORRODED. CORROSION EXCEEDED SRM LIMITS IAW SRM 53-00-00 REV 47, FIG 205. LONGERON REMOVED IAW SRM 51-31-01, REV 47. NEW LONGERON FABRICATED IAW DWG AEA7063, REV G AND INSTALLED SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR SDR FDEA201108293544Longeron · corrodedLONGERON 16L BS 1179-1199 CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORGINAL THICKNESS = 0.125"; MATERIAL REMOVED = 0.065"; MATERIAL REMAINED = 0.060 INCH, FOUND EXEEDED LIMIT IAW SRM 53-00-00, REV 47, FIG 205. NEW LONGERON FABRICATED IAW DWG ASDR FDEA201108293543Longeron · corrodedLONGERON 16L, BS 1179-1199 CORROSION EXCEEDED SRM LIMITS. NEW LONGERON FABRICATED IAW DWG AEA7065, REV B AND INSTALLED IAW SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201108293542Skin · crackedLT WING FIXED L/E LOWER SURFACE AT OTBD SLAT MECHANISM ACCESS DOOR 518FB STA, XOS 542. FWD CORNER FOUND SKIN WITH 1.0" CRACK. REPAIRED IAW SRM 57-40-02 REV 47, FIG 201, REPAIR 7. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.SDR FDEA201108293541Seat Track · corrodedMAIN DECK - CORROSION ON SEAT TRACK FLANGE AT STA 5-0 TO STA 5-53, X =75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS =0.080"; MATERIAL REMOVED =0.040"; MATERIAL REMAINED = 0.040", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRSDR FDEA201108293540Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1159 TO STA 1219, X =107. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.038"; MATERIAL REMAINED =0.042", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECSDR FDEA201108263512Longeron · corrodedCENTER CARGO COMPARTMENT STA 5-83 TO STA 5-93, RT LONGERON NR33R CORRODED. LONGERON REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS= 0.060"; MATERIAL REMOVED = 0.040"; MATERIAL REMAINED = 0.030" - FOUND EXCEEDED LIMITS IAW SRM 53-00-00 REV 47, SDR FDEA201108263511Access Door · crackedRT WING FIXED L/E LOWER SURFACE AT REFUELING ACCESS DOOR INBD SIDE AREA FOUND WITH 1.2" CRACKED. CRACK TRIMMED OUT IAW SRM 57-40-02, REV 47, FIG 201, REPAIR 7. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-02, REV 47, FIG 201, REPAIR 7. RSDR FDEA201108253477Longeron · corrodedCORROSION ON LONGERON 12R AT BS 1239-1299. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.173 INCH; MATERIAL REMOVED = 0.055 IN; MATERIAL REMAINED = 0.118 IN AND FOUND EXCEEDED LIMITS SRM 53-22-00, REV 47, FIG 205. LONGERON SECTION REMOVSDR FDEA201108253476Longeron · corrodedLONGERON 18R, STA 1481-1501 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 REV 47 AND FOUND CRACKED. NEW LONGERON FABRICATED IAW DWG AEA0220, REV R. CRACKED LONGERON R & R SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201108253474Doubler · crackedCENTER WHEEL WELL RT SIDE FWD SPOILER MIXER CONTROL ROD CUT-OUT DOUBLER FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01, REV 47. NEW DOUBLER FABRICATED IAW DWG AEA0526 AND INSTALLED IAW SRM 51-33-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 1SDR FDEA201108253473Doubler · crackedCENTER WHEEL WELL, LT SIDE FWD SPOILER MIXER CONTROL ROD CUT-OUT DOUBLER FOUND CRACKED. REMOVED DOUBLER IAW SRM 51-31-01, REV 47. NEW DOUBLER FABRICATED IAW DWG AEA0526 AND INSTALLED IAW SRM 51-33-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100,SDR FDEA20110823341AWindow Frame · corrodedCOCKPIT- L2 SLIDING WINDOW CUT-OUT AT LOWER AFT FRAME SUPPORT FOUND CORRODED FOUND CORROSION EXCEEDED SRM LIMITS. COMPLIED WITH EA 1-5320-149869. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.SDR FDEA201108233422Longeron · corrodedLONGERON 16R STA 1361 TO 1381 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01, REV 47. ORGINAL THICKNESS = 0.100 INCH; MATERIAL REMOVED = 0.050 INCH; MATERIAL REMAINED = 0.050 INCH, FOUND EXEEDED LIMIT IAW SRM 53-00-00 REV 47, FIGURE 205. LONGERON SSDR FDEA201108233421Longeron · corrodedLONGERON 25R BS 1381-1401. FOUND WITH CORROSION. REMOVED SRM 51-21-01, REV 47. ORIGINAL THICKNESS =0.100 INCH; MATERIAL REMOVED = 0.060 IN; MATERIAL REMAINED = 0.040 IN, AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 47, FIG 205. NEW LONGERON FABRICATED SDR FDEA201108233419Longeron · corrodedLONGERON 20R STA 1401 TO STA 1421 FOUND WITH CORROSION. REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.040 IN; MATERIAL REMAINED = 0.040 IN, AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 47, FIG 205. NEW LONGERON SDR FDEA201108233417Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 6-30 TO 6-100 1661, X = 27.5. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRSDR FDEA201108233416Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1561 TO 1661, X = -75, EXCEEDED SRM LIMITS.SDR FDEA201108233415Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1561 TO 1661, X = -75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECSDR FDEA201108233413Floor Support · corrodedFLOOR SUPPORT AT RT STA 595, X = -75.25 CORRODED BEYOND SRM LIMITS. CORROSION REMOVED IAW SRM 51-21-01, REV 47. MATERIAL ORIGINAL THICKNESS = 0.075"; MATERIAL REMOVED = 0.050"; MATERIAL REMAINED = 0.025" FOUND EXCEEDED LIMIT IAW SRM 53-00-00, REV 47, FIG 20SDR FDEA201108193381Longeron · corrodedCENTER CARGO COMPARTMENT - ALONG LEFT STA 1722 LONGERON 46L, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS = 0.100 INCH; MATERIAL REMOVED = 0.090"; MATERIAL REMAINED = 0.010" - FOUND EXCEEDED LIMIT IAW SRM 53-00-SDR FDEA201108193380Seat Track · corrodedCORROSION ON SEAT TRACK AT RT STA 595 TO 615, X = -107.25 EXCEEDED SRM LIMITS. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.060 INCH; MATERIAL REMAINED = 0.020 INCH FOUND EXCEEDED LIMITS IAW SRM 53-00-SDR FDEA201108193379Finger Doubler · crackedLEFT WING L/E COMPARTMENT FROM ST XORS 506 TO STA XORS 545 FOUND SEVERAL LOCATION OF FINGER DOUBLER WITH 0.375 INCH CRACKS. FINGER DOUBLER TRIMMED-OUT IAW SRM 57-40-02, REV 47, FIG 203. REPAIR 9. FILLERS DOUBLERS AND ANGLES FABRICATED AND INSTALLED IAW SRM SDR FDEA201108193378Finger Doubler · crackedLEFT WING L/E COMPARTMENT AT STA XORS 595 FOUND FINGER DOUBLER WITH 0.375 INCH CRACK. TRIMMED-OUT AND REPAIR CARRIED-OUT SRM 57-40-02, REV 47, FIG 203, REPAIR 9. CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201108193377Finger Doubler · crackedLT WING L/E COMPARTMENT AT STA XORS 665 FINGER FOUND DOUBLER WITH 0.375 INCH CRACKED. REPAIR CARRIED-OUT IAW SRM 57-40-02, REV 47, FIG 203 REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 113.SDR FDEA201108193376Finger Doubler · crackedLT WING L/E COMPARTMENT AT STA XORS 625 FINGER DOUBLER FOUND WITH A 0.375 INCH CRACK. FINGER DOUBLER TRIMMED-OUT AND REPAIR CARRIED-OUT IAW SRM 57-40-02, REV 47, FIGURE 203, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201108183339Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1159 - 1219, X = 75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.045 INCH; MATERIAL REMAINED = 0.035 INCH, FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. SEASDR FDEA201108183358Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1561 TO 1621, X = 107. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECSDR FDEA201108183357Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1461 TO 5.0, X = 107. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS=0.080 INCH; MATERIAL REMOVED=0.050 INCH; MATERIAL REMAINED =0.030 INCH, FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODSDR FDEA201108183355Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1761 TO 1821, X = -8. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS=0.080"; MATERIAL REMOVED=0.045"; MATERIAL REMAINED=0.035 INCH, FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECTIONSDR FDEA201108183354Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 5-53 TO 1531, X = -8. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.052"; MATERIAL REMAINED = 0.028", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECSDR FDEA201108183353Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 5-32 TO 5-53, X = 8. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.020"; MATERIAL REMAINED = 0.060", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SECSDR FDEA201108183350Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1821 TO 1887, X = 75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.050 INCH; MATERIAL REMAINED = 0.050", FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRSDR FDEA201108183349Skin · crackedLT WING FIXED L/E NR 3 SLAT TELESCOPIC DUCT CUT-OUT AREA FOUND CRACKED APPROX 0.250" SKIN. REPAIR FABRICATED IAW SRM 57-40-01, REV 47 AND INSTALLED IAW SRM 57-40-01, REV 47, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.SDR FDEA201108183348Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1561 TO 1661, X = -8. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.045 INCH; MATERIAL REMAINED = 0.035 INCH, FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CSDR FDEA201108183347Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1561 TO 1661, X = 8. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035 INCH, FOUND EXCEEDED SRM 53-00-52 REV 47, FIG 101LIMITS. SEAT TRACK SSDR FDEA201108183346Rib · crackedLT WING L/E COMPARTMENT AT NR 16 SLAT TRACK AREA INBD SUPPORT RIB SUSPECTED CRACKED APPROX 0.187 INCH. R & R IAW SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201108183344Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 5.0 TO 5-53, X =107 EXCEEDED SRM LIMITS. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED =0.050 INCH; MATERIAL REMAINED = 0.030 INCH FOUND EXCEEDED LIMITS IAW SRM 53-00-52,SDR FDEA201108183343Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1441, 5.0, X = 75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035 INCH, FOUND EXCEEDED SRM 53-00-52, REV 47, FIG 101 LIMITS. CORRODED SSDR FDEA201108183342Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AT STA 1361 TO 1401, X = 75. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.035 INCH; MATERIAL REMAINED = 0.045 INCH, FOUND EXCEEDED IAW SRM 53-00-52, REV 47, FIG 101 LIMISDR FDEA201108183341Seat Track · corrodedSEAT TRACK AT MAIN DECK STA 1229 TO 1331, X = 27.5 LT, FOUND WITH CORROSION THAT EXCEEDED SRM LIMITS. CORRODED AREA REMOVED: MATERIAL THICKNESS = 0.0890 INCH, MATERIAL REMOVED = 0.040", MATERIAL REMAINED = 0.040". EXCEEDED LIMITS IAW SRM 53-02-52, REV 47, SDR FDEA201108183340Seat Track · corrodedSEAT TRACK AT MAIN DECK STA 1229 TO 1331, X = -8.5 RT, FOUND WITH CORROSION THAT EXCEEDED SRM LIMITS AEA7325-23. CORRODED AREA REMOVED: MATERIAL THICKNESS = 0.080 INCH, MATERIAL REMOVED = 0.040 INCH, MATERIAL REMAINED = 0.040 INCH. EXCEEDED LIMITS IAW SRM SDR FDEA201108183338Skin · crackedRT WING TELESCOPIC DUCT CUT-OUT FOUND CRACKED SKIN. REMOVED IAW AMM 27-80-30-4, REV 70.1. EXTERNAL REPAIR DOUBLER AND REPAIR FILLER FABRICATED IAW SRM 57-40-01, REV 47 AND INSTALLED IAW SRM 57-40-01, REV 47, FIG 201. RT WING L/E NR 3 SLAT ASSY RE-INSTALLEDSDR FDEA201108183335Seat Track · corrodedSEAT TRACK AT MAIN DECK STA 1331 TO 1531, X = -8.5 RT. FOUND WITH CORROSION THAT EXCEEDED SRM LIMITS. CORRODED AREA REMOVED, ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.055 INCH; MATERIAL REMAINED = 0.025 INCH AND EXCEEDED LIMITS IAW SRM 53-00-5SDR FDEA201108183333Seat Track · corrodedSEAT TRACK AT MAIN DECK STA 1331 TO 1531, X = 8.5 LT FOUND WITH CORRODED. CORROSION REMOVED, ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.045"; MATERIAL REMAINED = 0.035" AND EXCEEDED LIMITS IAW SRM 53-00-52, REV 47, FIG 101. NEW SEAT TRACK REPAIR SDR FDEA201108183331Seat Track · corrodedSEAT TRACK AT MAIN DECK BS 745 TO 1119, X = -8.5 RT FOUND CORRODED. CORROSION REMOVED, ORIGINAL THICKNESS = 0.100 INCH; MATERIAL REMOVED = 0.050"; MATERIAL REMAINED = 0.050" AND EXCEEDED LIMITS IAW SRM 53-00-52, REV 47, FIG 101. NEW SEAT TRACK REPAIR CARRISDR FDEA201108183330Seat Track · corrodedSEAT TRACK AT MAIN DECK STA 1831 TO 1887, X = 8.5 LT FLANGE. CORROSION REMOVED, ORIGINAL THICKNESS = 0.080"; MATERIAL REMOVED = 0.040"; MATERIAL REMAINED = 0.040" AND EXCEEDED LIMITS IAW SRM 53-00-52, REV 47, FIG 101. REPAIR CARRIED OUT IAW SRM 53-00-52, R
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