Boeing 737-401
Service difficulty reports · 2,961
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737401' 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 aircraft_model_key = '737401' 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 USAA991350Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 480 INBOARD RIVET.. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991349Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 907 INBOARD RIVET. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991348Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 867 INBOARD RIVET. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991312Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 380 INBOARD RIVET. FABRICATED DOUBLER PER SRM 53-00-07 FIG 201. (M)SDR USAA991311Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUDN TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 380 OUTBOARD RIVET. FABRICATED DOUBLER PER SRM 53-00-07 FIG 201. (M)SDR USAA991310Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8R AND 9R STATION 440 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991309Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 440 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991308Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 867 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991307Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUDN A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R STATION 867 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991306Frame · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 400 INBOARD RIVET FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA991305Frame · crackedCLT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 907. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991304Sill · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AT BS 947-1006, WL 208, RBL 55 LOWER SILL ASSEMBLY. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)SDR USAA991303Crease Beam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION RIGHT CREASE BEAM INNER CHORD UPPER SURFACE FROM BS 294.5 TO 338. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 53-10-51. (M)SDR USAA991302Angle · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH AREA OF CORROSION AFT ENTRY DOOR CREASE BEAM INNER CHORD Z-ANGLE. CORROSION LEVEL 1. CORROSION TASK C 53-107-02. INSTALLED NEW CREASE BEAM INNER CHORD PER SRM 51-10-02. (M)SDR USAA991283Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION IN NUT PLATE HOLES BL 0 TO RBL 56, 12 EACH 1 INCH BY 1 INCH FLOORBEAM. CORROSINLEVEL 2. REPLACED T-CAP PER SRM 53-10-51. (M)SDR USAA991282Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA991281Bulkhead · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..750 INCH CRACK AT STATION 178, LBL 4.75, WL 198 BULKHEAD. INSTALLED REPAIR DOUBLER PER TR 53-10-07 REV A. (M)SDR USAA991280Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK AT STATION 380 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED DOUBLER PER EA 66083 AND TR 53-10-14. (M)SDR USAA991279Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727D RIGHT, BETWEEN STRINGER 8 AND 9 FRAME. INSTALLED DOUBLER PER EA66083 AND TR 53-10-14. (M)SDR USAA991278Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 747 LEFT, BETWEEN STRINGE R8 AND 9 FRAME. INSTALLED DOUBLER PER EA 66083 AND TR 53-10-14. (M)SDR USAA991277Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 747 RIGHT, BETWEEN STRINGER 8 AND 9 FRAME. INSTALLED DOUBLER PER EA 66083 AND TR 53-10-14. (M)SDR USAA991259Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND ONE INCH AREA OF CORROSION TOP SURFACE AROUND CLIPNUT HOLE STATION 967 RBL 30 FLOORBEAM. CORROSION LEVEL 2. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-30-51. (M)SDR USAASB99276Socket · failedTPA - MAINTENANCE FOUND THE RIGHT FUSELAGE EMERGENCY EGRESS LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (X)SDR USAA991258Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK THROUGH 2 FASTENER HOLES ON INNER CHORD OF FRAME BS 601, WL 208 LEFT SIDE. INSTALLED CHORD ANGLE REPAIR PER EA 66021. (M)SDR USAA991257Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 665, LBL 31 PRESSURE DECK BELOW CABIN FLOOR BULKHEAD. INSTALLED DOUBLER PER TR 53-60-04. (M)SDR USAA991256Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT INBOARD LOWER T/E NR 2 SLAT SKIN. INSTALLED DOUBLER PER BOEING DWG 65C30133. (M)SDR USAA991255Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991254Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991253Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991252Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991251Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION FOUND CORROSION AT CLIPNUT HOLES UPPER FLANGE BS 947, RBL 16. CORROSION LEVEL 1. INSTALLED FLOORBEAM REPAIR PER TR 53-60-02. (M)SDR USAA991250Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION NUMEROUS AREAS .500 INCH FLOORBEAM BS 986 UPPER SURFACE OF T-CAP UPPER CHORD. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED REPLACEMENT T-CAP PER TR 53-60-01. (M)SDR USAA991244Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIRED ANGLE PER TR 53-10-14 AND EA 66040 AND SRM 53-60-07. (M)SDR USAA991243Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66040 AND SRM 53-60-07. (M)SDR USAA991242Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991241Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991240Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 199, LBL 4.5 BULKHEAD WEB. INSTALLED DOUBLER PER EA 66072. (M)SDR USAA991239Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 480 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED LARGER FASTENER PER SRM 51-40-2. (M)SDR USAA991238Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 500A BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIR DOUBLER PER EA 66037 AND TR 53-10-14. (M)SDR USAA991236Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 747 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M)SDR USAA991235Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727D BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FRAME REPAIR PER TR 53-10-14. (M)SDR USAA991234Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION FOUND 3 AREAS OF CORROSION 2 INCH BY 4 INCH AT STATION 294.5, RBL 54 Z ANGLE. CORROSION LEVEL 2. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M)SDR USAA991232Frame · corrodedCLT - DURIGN Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH BS 344, LBBL 50 - RBBL 24 EXTRUSION UPPER CHORD. CORROSION LEVEL 2. CORROSON TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51. (M)SDR USAA991231Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIPNUT HOLE ON TOP OF FLOORBEAM 1 INCH BY 1 INCH BS 967, RBL 15, WL 208. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-30-51. (M)SDR USAA991230Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 199, RBL 4.5 BULKHEAD WEB. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA991229Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A . 5 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. INSTALLED NEW CLIP PER SRM 51-10-02. (M)SDR USAA991228Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727D BETWEEN STRINGER 8 AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991227Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT T-CAP 1 INCH BY 1 INCH 12 PLACES STATION 294.3, RBL 0-52. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51. (M)SDR USAA991203Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLE ON FLOORBEAM T-CAP BS 312, LBL 26, WL 208. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED T-CAP PER SRM 53-10-51 FIG 205. (X)SDR USAA991276Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 10 INCH AREA OF CORROSION RIGHT CREASEBEAM INNER CHORD 1.5 INCH AFT OF STATION 294.5 TO 3.25 INCH FORWARD OF 360 CHORD. CORROSION LEVEL 1. INSTALLED NEW PART PER SRM 53-10-15. (M)
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