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 USAA991275Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25INCH CRACK STATION 827, BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-10-14 AND SRM 53-00-07. (M)SDR USAA991274Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 787, BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-10-14. (M)SDR USAA991273Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 727F, BETWEEN STRINGER 8L AND STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-10-14. (M)SDR USAA991272Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK LOWER INNER RADIUS OF FORWARD SERVICE DOOR FORWARD FRAME STATION 294.5, RBL 54.25 DOOR CUTOUT FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA991268Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 907 AT RIVET IN PSU SUPPORT AT STRINGER 8R FRAME. DAMAGED REMOVED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M)SDR USAA991267Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 907 AT RIVET IN PSU SUPPORT AT STRINGER 8L FRAME. DAMAGED REMOVED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M0SDR USAA991266Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 706 AT TIE CLIP STRINGER 10R STRINGER TIE CLIP. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-10-02. (M)SDR USAA991265Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 520 AT PSU SUPPORT STRINGER 8R FRAME. INSTALLED REPAIR DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M)SDR USAA991264Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME STATION 616, RBL 54 INNER CHORD ANGLE. INSTALLED REPAIR ANGLE AND FILLER PER TR 53-62-01. (M)SDR USAA991263Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME STATION 616, LBL 54 INNER CHORD ANGLE. INSTALLED REPAIR ANGLE AND FILLER PER TR 53-62-01. (M)SDR USAA991226Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 827 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991225Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 787 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991224Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 727F BETWEEN STRINGER 8L AND 9L INSTALLED DOUBLER PER SRM 53-10-14. (M)SDR USAA991223Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK IN ANGLE RADIUS .5 INCH AFT OF STATION 294.5, RBL 54.25 ANGLE.. INSTALLED DOUBLER AND FILLER PER SRM 51-70-11. (M)SDR USAA991222Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R AT BS 867 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND TR 53-10-14. (M)SDR USAA991221Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 827 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND TR 53-10-14. (M)SDR USAA991220Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 907 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND TR 53-10-14. (M)SDR USAA991219Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R AT BS 907 FRAME. INSTALLED DOUBLER AND FILLER PER SRM 53-00-07. (M)SDR USAA991237Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FRAME REPAIR PER EA 66032. (M)SDR USAA991163Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 1.250 INCH SKIN CRACK JUST BELOW STRINGER 23L AND 3 INCH AFT OF STATION 727D. INSTALLED REPAIR DOUBLER PER EA 65983 AND TR 53-60-03. (M)SDR USAASB99251Battery Charger · failedCLT - MAINTENANCE FOUND THE LEFT AISLE EMERGENCY LIGHT ABOVE THE LEFT AFT EMERGENCY EXIT WINDOW INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. (X)SDR USAASB99250Turbine · failedGSO - FLT 1046 - DURING CRUISE AT APPROXIMATELY FL 290, THE CREW HEARD A LOUD BANG FROM THE LEFT SIDE OF THE ACFT WITH FLUCTUATIONS OF THE LT ENGINE GAUGES. ENGINE INDICATIONS RETURNED TO NORMAL AND THE CREW CONTINUED FLIGHT. SHORTLY THEREAFTER, ANOTHER LOUDSDR USAASB99242Modular Assembly · failedEWR - FLT 1056 - AFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. WITH HANDLE IN 'OFF' POSITION, THE LEFT MAIN GEAR EXTENDED DOWN AND LOCKED. CREW RECYCLED GEAR AND SAME PROBLEM OCURRED. FLIGHT RETURNED TO FIELD AT EWR AND LANDEDSDR USAASB99233Sensor · out of adjustCLT - FLT 731 - EN ROUTE FROM PHL TO MSY, THE NLG UNSAFE ILLUMINATED AND REMAINED ON. CREW RECYCLED GEAR AT 230 KNOTS BUT LIGHT REMAINED ON. CAPTAIN ACCOMPLISHED VISUAL CHECK AND DETERMINED GEAR WAS STOWED AND DOORS WERE CLOSED. SINCE THERE WAS NO MAINTENANSDR USAA990977Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK RT HORIZONTAL STAB TORQUE BOX LOWER SKIN ACCESS. INSTALLED REPAIR DOUBLER ACCESS PANEL PER EA 65418. (M)SDR USAA990975Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 601, WL 203 LEFT SIDE CHORD ANGLE. REPAIRED STIFFENER ANGLE PER EA 65335 ADN TR 53-10-23. (M)SDR USAA990974Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK LOWER OUTBOARD CORNER OF FORWARD SERVICE DOOR UPPER FORWARD STOP PAN FITTING FRAME. REPLACED DEFECTIVE PART PER DRAWING 65-45807. (M)SDR USAA990973Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE INNER CHORD ANGLE BS 616 FUSELAGE FRAME WL 200 LEFT SIDE. INSTALLED DOUBLER PER EA 65335. (M)SDR USAA990972Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480R BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990971Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990967Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990965Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 31 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED PER EA 65407. (M)SDR USAA990932Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK FUSELAGE SKIN STATION 727D PLUS 10, CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202 AND EA 65488. (M)SDR USAA990922Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440R BETWEEN STRINGER 8 AND 9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990921Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH CORRODED AREA FORWARD SERVICE DOOR CUTOUT FRAME FWD INBOARD CHORD AT BOTTOM END JUST ABOVE CREASE BEAM INNER CHORD ANGLE, CORROSION LEVEL 1. REMOVED MINOR CORROSION PER SRM 51-10-02. (M)SDR USAA990912Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLES ON UPPER T-CAP OF FLOORBEAM AT BS 947, LBL 14 TO RBL 14, WL 208. CORROSION LEVEL 1. SPLICED NEW UPPER CHORD/DOUBLERS PER SRM 53-00-51 AND TR 53-60-02. (M)SDR USAA990911Frame · crackedC.T - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827L, STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990894Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP Z-ANGLE FORWARD ENTRY. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)SDR USAA990893Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP ANGLE FORWARD SERV, CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M)SDR USAA990889Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601 FUSELAGE FRAME, WL 203 LEFT SIDE. INSTALLED DOUBLER PER EA 65335 AND TR 53-10-23. (M)SDR USAA990888Intercostal · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 328-344 RBL 10.5 INTERCOSTAL. CORROSION LEVEL 1. REPAIRED PER SRM 53-10-02. (M)SDR USAA990887Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RT HORIZONTAL STABILIZER STAB AFT SPAR STAB STATION 128 LOWER SKIN. REPAIRED PER SRM 55-10-01 FIG 206 AND TR 55-10-07 REV A. (M)SDR USAA990886Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601, FUSELAGE FRAME, WL 203 RT SIDE. INSTALLED REPAIR DOUBLER AND HI-LOCKS PER TR 53-10-23, EA 65335 AND SRM 53-60-07. (M)SDR USAA990881unknownCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 321 UPPR CHORD AT LBL 12.5 T-CAP. CORROSION LEVEL 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-51. (M)SDR USAA990874Intercostal · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AT STATION 312-328, RBL 30 UPPER CHORD INTERCOSTAL. CORROSION LEVEL 1. REPAIRED PER SRM 51-40-02. (M)SDR USAA990873Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUT PLATE HOLES ON T-CAP FLOORBEAM STATION 328, LBL 28, AND LBL 11. CORROSION LEVEL 1. REPLACED T-CAP. INSTALLED PER SRM 53-10-51 FIG 205. (M)SDR USAA990847Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 400L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990846Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 380L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA991008Skin · crackedPHL/PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT IN PHL FOUND 1.125 INCH LONG CRACK IN SKIN AT STATION 727D AT STRINGER 25 RT. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01, FIG L02, SH 3 AND EA 52813. (M)SDR USAASB99220Printed Circuit · failedPHL - FLT 973 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A LEFT MAIN LANDING GEAR UNSAFE LIGHT INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'LEFT GEAR UP AND LOCK SWITCH' PRINTED CIRCUIT C
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