N522FE
Service difficulty reports · 338
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 = 'N522FE' 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 = 'N522FE' 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 06FDEA02961Stringer · crackedCRACK FOUND AT THE END OF STRINGER 44 APPROX .7500 INCH AT RT WING TANK XORS 523. DURING HFEC INSPECTION. SNRM N00814: RT TANK END OF STRINGER 44 CRACK AT XORS 523 REPAIRED IAW EA1-5720-102162. WINGS, OUTER WING, RT WING STRINGER REPAIR IAW SRM. REPAIR CLASDR 06FDEA02957Stringer · crackedCRACK FOUND AT THE END OF STRINGER 11 APPROX 12" AT RT WING TANK XORS 704 DURING HFEC INSPECTION. RT WING TANK END OF STRINGER 11 CRACK AT XORS 704 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I AND STRINGER CLIP REPLACED AS PER EA 1-5720-102164. REPAIR CLSDR 06FDEA02945Floor Panel · damagedCOCKPIT, RIGHT OBSERVER STATION BASE STRUCTURE FOUND DAMAGED. COCKPIT RIGHT OBSERVER BASE STRUCTURE WEB AREA TRIMMED OUT AS PER SRM 53-00-01 VOL I. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REV 12 06-10-01-001 ON TRIMMED OUT AREA AND FOUND NO CRACK EVSDR 06FDEA02942Floor Panel · damagedCOCKPIT, FLOOR PANEL NR 215BF FOUND DAMAGED. COCKPIT FLOOR PANEL REMOVED AS PER AMM 53-21-01. NEW FLOOR PANEL FABRICATED AS PER DWG ABA7411 AND INSTALLED AS PER AMM 53-21-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.SDR 06FDEA02941Seat Track · corrodedMAIN DECK AFT, RBL 78 O/B CURVED SEAT TRACK FOUND CORRODED AT STA 1964. MAIN DECK AFT AT LBL 78 STA 1964 CORROSION MATERIAL REMOVED 0.060" ORIGINAL THK 0.100" REMAINING 0.040" AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL I FIG 3. CORRODED SEAT TRACK REMOVESDR 06FDEA02960Stringer · crackedCRACK FOUND AT THE END OF STRINGER 13 APPROX 6.5" AT RT WING TANK XORS 577 DURING HFEC INSPECTION. RHW TANK END OF STRINGER 13 CRACK AT XORS 577 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I AND STRINGER CLIP REPLACED AS PER EA1-5720-102158 TITLE: WINGS-OUTSDR 06FDEA02959Stringer · crackedCRACK FOUND AT THE END OF STRINGER 42 APPROX 1/2 INCH AT RT WING TANK XORS 629 DURING HFEC INSPECTION. RHW TANK END OF STRINGER 42 CRACK AT XORS 629 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02958Stringer · crackedCRACK FOUND AT THE END OF STRINGER 12 APPROX 12.5" AT RT WING TANK XORS 642 DURING HFEC INSPECTION. RHW TANK END OF STRINGER 12 CRACK AT XORS 642 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02956Stringer · crackedCRACK FOUND AT THE END OF STRINGER 10 APPROX 11.5" AT RT WING TANK XORS 760 DURING HFEC INSPECTION. RHW TANK END OF STRINGER 10 CRACK AT XORS 760 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02955Stringer · crackedCRACK FOUND AT THE END OF STRINGER 41 APPROX 1/2" AT LT WING TANK XORS 685 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 41 CRACK AT APPROX XORS 685 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02954Stringer · crackedCRACK FOUND AT THE END OF STRINGER 11 APPROX 8.5" AT LT WING TANK XORS 704 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 11 CRACK AT XORS 704 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02953Stringer · crackedCRACK FOUND AT THE END OF STRINGER 10 APPROX 10.5" AT LT WING TANK XORS 760 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 10 CRACK AT XORS 760 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA02952Stringer · crackedCRACK FOUND AT THE END OF STRINGER 9, APPROX 12" AT LT WING TANK XORS 819 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 9 CRACK AT XORS 819 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 3 VOL 1. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02944Floor Panel · damagedCOCKPIT, FLOOR PANEL NR 215AF FOUND WITH PUNCH MARK. COCKPIT FLOOR PANEL NR 215AF REMOVED AS PER AMM 53-21-01. NEW FLOOR PANEL FABRICATED AS PER DWG ABA 7146 AND INSTALLED AS PER AMM 53-21-01. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA02943Floor Panel · damagedCOCKPIT, FLOOR PANEL NR 215DF FOUND DAMAGED. COCKPIT FLOOR PANEL REMOVED AS PER AMM 53-21-02. NEW FLOOR PANEL FABRICATED AS PER DWG ABA 7415 AND INSTALLED AS PER AMM 53-21-02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02930Seat Track · corrodedMAIN DECK AFT, LBL 78 O/B CURVED SEAT TRACK FOUND CORRODED AT STA 1964. CORROSION REMOVED ON SEAT TRACK BASE AS PER SRM 51-21-01 VOL II. MATERIAL REMOVED 0.065" ORIGINAL THK 0.100" MATERIAL REMAIN 0.035" AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL.ISDR 06FDEA2951Beam · damagedSNRM N00757: EXISTING REPAIR AT RT WING FIXED TRAILING EDGE BEAM XW 286.SDR 06FDEA2950Skin · damagedSNRM N00696: EXISTING REPAIR AT LT WING IB TRAILING EDGE LOWER SKIN.SDR 06FDEA2949Skin · damagedSNRM N00695: EXISTING REPAIR FOUND AT LT IB TRAILING EDGE FLAP UPPER SKIN.SDR 06FDEA2948Skin · damagedSNRM N00693: EXISTING DOUBLER REPAIR AT FUSELAGE SKIN, STA 2033, LONGERON 39R TO 40R.SDR 06FDEA2947Cap · damagedSNRM N00691: EXISTING REPAIR AT VERTICAL STABILIZER NR 4, BANJO FITTING CARRY THROUGH CAP.SDR 06FDEA2946Web · damagedSNRM N00690: EXISTING REPAIR FOUND AT UPPER TORQUE BOX PLANE WEB STA 2010 RT.SDR 06FDEA2945Structure · damagedSNRM N00658: COCKPIT: RT OBSERVER STATION BASE STRUCTURE FOUND DAMAGED.SDR 06FDEA2944Floor Panel · damagedSNRM N00657: COCKPIT: FLOOR PANEL NR 215AF FOUND WITH PUNCH MARK.SDR 06FDEA2943Floor Panel · damagedSNRM N00656: COCKPIT: FLOOR PANEL NR 215DF FOUND DAMAGED.SDR 06FDEA2942Floor Panel · damagedCOCKPIT: FLOOR PANEL NR 215BF FOUND DAMAGED.SDR 06FDEA2941Seat Track · corrodedMAIN DECK AFT, RBL 78 O/B CURVED SEAT TRACK FOUND CORRODED AT STA 1964.SDR 06FDEA2930Seat Track · corrodedSNRM N00598: MAIN DECK AFT, LBL 78 OB CURVED SEAT TRACK FOUND CORRODED AT STA 1964.SDR 06FDEA2961Stringer · crackedSNRM N00814: CRACK FOUND AT THE END OF STRINGER 44 APPROX .7500 INCH AT RT WING TANK, XORS 523, DURING HFEC INSPECTION.SDR 06FDEA2960Stringer · crackedSNRM N00813: CRACK FOUND AT THE END OF STRINGER 13 APPROX 6.5 INCHES AT RT WING TANK, XORS 577, DURING HFEC INSPECTION.SDR 06FDEA2959Stringer · crackedSNRM N00812: CRACK FOUND AT THE END OF STRINGER 42 APPROX .5 INCH AT RT WING TANK, XORS 629, DURING HFEC INSPECTION.SDR 06FDEA2958Stringer · crackedSNRM N00811: CRACK FOUND AT THE END OF STRINGER 12 APPROX 12.5" AT RT WING TANK XORS 642 DURING HFEC INSPECTION.SDR 06FDEA2957Stringer · crackedSNRM N00810: CRACK FOUND AT THE END OF STRINGER 11 APPROX 12 INCHES AT RT WING TANK, XORS 704, DURING HFEC INSPECTION.SDR 06FDEA2956Stringer · crackedSNRM N00809: CRACK FOUND AT THE END OF STRINGER 10 APPROX 11.5 INCH AT RT WING TANK, XORS 760, DURING HFEC INSPECTION.SDR 06FDEA2955Stringer · crackedSNRM N00792: CRACK FOUND AT THE END OF STRINGER 41 APPROX .5 INCH AT LT WING TANK, XORS 685, DURING HFEC INSPECTION.SDR 06FDEA2954Stringer · crackedSNRM N00791: CRACK FOUND AT THE END OF STRINGER 11 APPROX 8.5 INCHES AT LT WING TANK, XORS 704, DURING HFEC INSPECTION.SDR 06FDEA2953Stringer · crackedSNRM N00789: CRACK FOUND AT THE END OF STRINGER 10 APPROX. 10.5 INCHES AT LT WING TANK, XORS 760, DURING HFEC INSPECTION.SDR 06FDEA2952Stringer · crackedSNRM N00788: CRACK FOUND AT THE END OF STRINGER 9, APPROX 12 INCHES AT LT WING TANK. XORS 819 DURING HFEC INSPECTION.
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