N529FE
Service difficulty reports · 240
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 = 'N529FE' 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 = 'N529FE' 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 06FDEA04168Seat Track · corrodedCABIN, SEAT TRACK STA 1179 TO STA 1301 X=75.5 (LT) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04140Frame · damagedAFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 FOUND EXISTING REPAIR DOUBLER AT RBL 27.5. SNRM N01258: REFER TO SNRM N00806 AND SRM 51-31-01 VOL II FOR WORK CARRIED OUT. AFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 REMOVED AS PER SRSDR 06FDEA04142Web · crackedAFT FUSELAGE COMPT UPPER TORQUE BOX WEB AT STA 2007 FOUND WITH CRACK. STOP DRILLED AS PER SRM 53-40-00 FIG.23 VOL.I. REPAIR FILLER AND DOUBLER FABRICATED AS PER SRM 53-40-00 FIG.23 VOL.I USING MATERIAL 7075T6-.032" AND MIL-T-9046-0.032". REPAIR FILLER AND DSDR 06FDEA04141Seat Track · corrodedCABIN SEAT TRACK AT STA 990 TO STA 1079 X=-8.5 (RT) FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04126Seat Track · corrodedCABIN SEAT TRACK AT STA 6-0 TO STA 6-30 X=27.5 (LT) FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04125Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 30 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04124Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 28 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04120Seat Track · corrodedCABIN SEAT TRACK AT STA 824 TO STA 840 X=8.5 LT FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04119Seat Track · corrodedCABIN SEAT TRACK AT STA 808 TO STA 859 X=27.5 LT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04118Seat Track · corrodedCABIN SEAT TRACK AT STA 6-100 TO STA 1199 X=27.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04117Seat Track · corrodedFOUND CABIN SEAT TRACK AT STA 845 TO STA 899 X=75.25 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04109Bulkhead · damagedAFT CABIN, AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007 FOUND EXISTING REPAIR DOUBLER AT LBL 27.5. SNRM N00806: AFT CABIN AFT PRESSURE BULKHEAD LOWER T-CHORD AT STA 2007. REMOVED AS PER SRM 51-31-01 VOL II. NEW T-CHORD HOLES PICKED-UP AND REPROTECTED SDR 06FDEA04116Seat Track · corrodedCABIN SEAT TRACK AT STA 899 TO STA 1099 X=27.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL. I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04115Seat Track · corrodedCABIN SEAT TRACK AT STA 899 TO STA 962 X=8.5 RT FOUND WITH CORROSION. REPAIR CARRIED OUT PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04114Seat Track · corrodedFOUND CABIN SEAT TRACK AT STA 935 TO STA 1025 X=8.5 LT FOUND WITH CORROSION. CORROSION CRACK REMOVED AND SECTIONAL REPAIR PERFORMED AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04113Seat Track · corrodedCABIN SEAT TRACK AT STA 890 TO STA 979 X=27.5 LT FOUND WITH CORROSION. REPAIR CARRIED OUT PER SRM 53-70-00 FIG.1 VOL. I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04112Skin · damagedHORIZONTAL STAB CONSTANT SECTION LT BARREL NUT HOLE NR 17 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A. 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04111Skin · damagedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 6 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A.1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04110Spar · damagedHORIZONTAL STAB CONSTANT SECTION RT SIDE BARREL NUT HOLE NR 1 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT.1. HORIZONTAL STAB CONSTANT SECTION R/H BARREL NUT HOLE NR 1 REPAIRED AS PER E.A.1-5510-106546 ATTACHMENT 1. REPAIR CLASSIFIED MAJOR AS PESDR 06FDEA04108Rib · crackedLT WING NR 16 SLAT TRACK CUTOUT I/B RIB SUSPECT CRACK. LT WING NR 16 SLAT TRACK CUTOUT I/B CRACK RIB REMOVED AND INSTALLED NEW RIB AS PER SRM 51-31-01 VOL.II REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA04107Nut Plate · damagedLOWER ANTI-COLLISION STROBE LIGHT 14 MOUNTING NUT PLATE FOUND DAMAGED. REPAIRED IAW EA 1-5330-106553. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.SDR 06FDEA04056Floor Panel · dentedCOCKPIT, DENT MARKS ON FLOOR PANEL 216BF. COCKPIT FLOOR PANEL #216BF REMOVED AS PER AMM 53-21-02. FLOOR PANEL FABRICATED AS PER DRAWING ABA 8675, NEW FLOOR PANEL PAINTED AS PER SRM 51-21-01 AND INSTALLED AS PER AMM 53-21-02. REPAIR CLASSIFIED MAJOR ASSDR 06FDEA04024Stringer · crackedCRACK FOUND APPROX 10" IN LENGTH DURING HFEC INSPECTION ON RT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04005Stringer · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 44 XORS 523. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 2 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04004Stringer · crackedCRACK FOUND APPROX 10" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 14 XORS 521. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 1 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04003Stringer · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 43 XORS 565. REPAIRED AS PER E.A.1-5720-106552.SDR 06FDEA04002Stringer · crackedCRACK FOUND APPROX 13" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 1 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA04001Stringer · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 42 XORS 642. LT WING TANK AT THE END OF STRINGER 42 XORS 642 CRACK REPAIRED AS PER E.A.1-5720-106551 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04000Stringer · crackedCRACK FOUND APPROX 4" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 38 XORS 877. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 2 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03999Stringer · crackedCRACK FOUND APPROX 0.25" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 9 XORS 819. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 1 VOL.I. THIS REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA03998Stringer · crackedCRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 10 XORS 760. REPAIRED AS PER SRM 57-20-00 FIG. 10 OPT 3 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03997Stringer · crackedCRACK FOUND APPROX 0.25" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 41 XORS 685. REPAIRED AS PER SRM 57-20- 00 FIG. 10 OPT 2 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03996Stringer · crackedCRACK FOUND APPROX 8.5 IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 11 XORS 704. REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03960Skin · damagedREMOVED AND REPLACED FUSELAGE SKIN AND DOUBLERS PER DIRECTION OF AIRCRAFT ACQUISITION ENGINEERING. SKIN REPLACEMENT IS TO ELIMINATE PREVIOUS REPAIR AT STATIC PORT; RT FUSELAGE, FWD OF FWD LOWER CARGO COMPT DOOR. SNRM S00005: REFER TO EA 1-5330-104764 FOR WOSDR 06FDEA03955Bulkhead · damagedEXISTING REPAIR FOUND AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT SNRM N00405: EXISTING REPAIR AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 381015-14, EO 1-5100-7-5001ASDR 06FDEA03959Skin · unknownEXISTING REPAIR FOUND AT AFT CARGO DOOR LWR FWD CORNER, SNRM N00411: AFT CARGO DOOR LOWER FWD CORNER FASTENERS REMOVED AS PER SRM 51-35-01 VOL.II. DAMAGED AREA TRIMMED OFF AS PER SRM 52-10-00 FIG 17 VOL I. NEW REPAIR DOUBLER AND FILLER REWORKED AS PER SRM 5SDR 06FDEA03954Skin · damagedEXISTING REPAIR FOUND AT FUSELAGE SKIN AFT LAVATORY EXHAUST PORT STA 1937 AND STA 1959. REWORK CARRIED OUT AS PER E.A.1-5330-105642.SDR 06FDEA03952Skin · damagedEXISTING REPAIR FOUND AT RT WING NR 1 SLAT UPPER SKIN LOWER AFT EDGE STA XIS 349.035.SDR 06FDEA03951Skin · damagedEXISTING REPAIR FOUND AT LT WING NR 2 SLAT LOWER SKIN STA XIS 349.035. EXISTING REPAIR FOUND AT LT WING NR 2 SLAT LOWER SKIN STA XIS 349.035 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 10 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA03949Skin · damagedEXISTING REPAIR FOUND AT LT WING NR 1 SLAT LOWER SKIN STA XIS200. EXISTING REPAIR AT L/H WING NR 1 SLAT LOWER SKIN STA XIS 200, NEW SKIN REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
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