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 USAASB99214Circuit Card · failedIND - FLT 696 - AS LANDING GEAR WAS LOWERED IN PREPARATION FOR LANDING AT IND, THE CREW RECEIVED A NOSE GEAR UNSAFE LIGHT. CREW RECYCLED THE LANDING GEAR THREE TIMES AND ACCOMPLISHED A TOWER FLYBY. TOWER STATED NOSE WHEEL LOOKED DOWN BUT CAPTAIN CHECKED SCOPSDR USAA990857Skin · crackedCLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK LOWER SKIN RIGHT HORIZ STAB STATION 96 TO 97.5, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. SDR USAA990856Skin · crackedCLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.625 INCH CRACK LOWER SKIN RIGHT HORIZ STABILIZER STATION 124 TO STATION 125.6, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER TRSDR USAASB99188Wire Harness · failedPIT - FLT 8574 - FLIGHT RETURNED TO FIELD AT PIT TWO TIMES FOR A NR 2 ENGINE OVERHEAT LIGHT ILLUMINATING DURING CLIMB-OUT. BOTH TIMES THE LIGHT EXTINGUISHED WHEN POWER WAS REDUCED TO IDLE. BOTH FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH THE NR 2 ENGINE AT ISDR USAA990866Z-Angle · corrosionCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION AT NUTPLATE STATION 947-986.5, LBL 45 Z-ANGLE. CORROSION LEVEL 2. REPAIRED PER SRM 51-10-02. (M)SDR USAA990865Floorbeam · corrosionCLT - DURING Q-3 VISUAL INSPECTION, FOUND A AREA OF CORROSION IN CLIPNUT HOLES T-CAP OF FLOORBEAM STATION 294.5, RBL 15-52. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-40-02. (M)SDR USAA990778Skin · crackedCLT - DURING Q-3 CHECK, FOUND .25 INCH SKIN CRACK IN AFT CARGO DOOR HANDLE FLAP CUT OUT. INSTALLED DOUBLER PER SRM 52-00-01. (M)SDR USAA990777Angle · crackedCLT - DURING Q-3 CHECK, FOUND CRACK AT STATION 294.5 JUST AHEAD OF Z-ANGLE AT RT ENTRY. REPLACED ANGLE PER SRM 51-10-02. (M)SDR USAA990776Intercostal · crackedCLT - DURING Q-3 CHECK, FOUND 1 INCH CRACK AT STATION 397 B/O 0 INTERCOSTAL UPPER CHORD. REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M)SDR USAA990775Bulkhead · crackedCLT - DURING Q-3 CHECK, FOUND .25 INCH CRACK AT 178 BULKHEAD AFT SIDE RBL 2, 4 INCHES UP FROM BASE OF BULKHEAD. DOUBLER REPAIR PER SRM 53-10-008 FIG 203. (M)SDR USAA990774Angle · corrodedCLT - DURING Q-3 CHECK, FOUND CORROSION ENTIRE UPPER SURFACE OF FORWARD ENTRY DOOR Z-ANGLE STATION 320-344. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M)SDR USAA990773Floorbeam · corrodedCLT - DURING Q-3 CHECK, FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM T-CAP AT STATION 947 BETWEEN LBL 14 TO RBL 16, CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED T-CAP SECTION/DOUBLERS PER SRM 53-00-51 FIG 202. (M)SDR USAA990748Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 907 LEFT SIDE STRINGER 8-9 IN FRAME. REPAIRED DOUBLER PER EA 65076. (M)SDR USAA990747Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 727B BETWEEN STRINGER 9L AND STRINGER 8L FRAME. REPAIRED DOUBLER PER EA 65076. (M)SDR USAA990746Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 291 MINUS 2, 4 INCH BELOW STRINGER 12R AT OUTBOARD FLANGE SHEAR WEB ANGLE. REPAIRED PER SRM 53-10-02. (M)SDR USAA990745Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 291.5, 4 INCHES ABOVE STRINGER 10R ANGLE. REPAIRED PER BOEING 737-400 SRM 51-10-02. (M)SDR USAA990730Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FRAME AT STATION 867 LEFT BETWEEN STRINGER 8/9. REPAIRED DOUBLER PER EA 65076. (M)SDR USAASB99176Connector · failedPHL - FLT 1429 - DURING TAKEOFF, THE CAPTAIN'S SLIDING WINDOW WIRING STARTED SPARKING AND BURNING AT THE CONNECTOR STRAIN RELIEF. CAPTAIN TURNED THE WINDOW HEAT OFF AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENSDR USAA990710Channel · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD OUTBOARD ACCESS CUTOUT PYLON CHANNEL. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR USAA990705Web · crackedCLT - DURING A Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN UPPER CHORD RADIUS AT BS 380-400, BLO WL 208 SHEAR WEB. REPLACED UPPER CHORD PER SRM 53-30-51. (M)SDR USAA990656Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 360 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR CHANNEL PER SRM 53-00-07 AND EA 64815. (M)SDR USAA990655Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 827 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED FRAME REPAIR PER SRM 53-00-07 AND EA 64916 AND EA 64815. (M)SDR USAA990654Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER EA 64815. (M)SDR USAA990653Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 747 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (M)SDR USAA990652Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 747 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER EA 64815 AND SRM 53-00-07. (M)SDR USAA990651Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER EA 64815. (M)SDR USAA990650Frame · crackedCLT - DURIGN Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIRE ANGLE PER EA 64815. (M)SDR USAA990649Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 727D BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER EA 64815. (M)SDR USAA990648Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 727B BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR ANGLE PER SRM 53-00-53. (M)SDR USAA990647Frame · crackedCLT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND A .25 INCH CRACK AROUND RIVET AT BS 500D BETWEEN STR 8R AND STR 9R FRAME. INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (X)SDR USAA990646Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 500C BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (M)SDR USAA990645Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 440 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR ANGLE PER EA 64815. (M)SDR USAA990644Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 400 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FILLER AND REPAIR ANGLE PER EA 64815 AND SRM 53-00-07 FIG 202. (M)SDR USAA990643Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 907 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER EA 64815. (M)SDR USAA990642Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK AROUND RIVET AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIR ANGLE PER SRM 53-00-07 AND EA 64815. (M)SDR USAA990641Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 727F BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR ANGLE PER SRM 53-00-07 AND EA 64815. (M)SDR USAA990614Frame · crackedCLT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND A .25 INCH CRACK AT BS 787 BETWEEN STR 8 AND STR 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64815. (X)SDR USAA990667Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 45 INCH AREA OF CORROSION AROUND SCREW HOLE AT STATION 344 LBL 28 FLOORBEAM. CORROSION TASK NR C53-107-02 AND LEVEL 2. REPLACED DAMAGED AREA PER SRM 53-00-51. (M)SDR USAA990666Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND SCREW HOLE AT STATION 344 LBL 28 FLOORBEAM. CORROSION TASK NR C53-107-02 AND LEVEL 2. REPLACED DAMAGED AREA PER SRM 53-00-51. (M)SDR USAA990640Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT FORWARD SERVICE DOOR CUT-OUT FRAME AT UPPER FORWARD STOP FITTING. REPLACED DOOR FRAME SKIN AND STOP FITTING PER SRM 51-10-02. (X)SDR USAA990639Frame · crackedCLT - DURING Q-T CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 747 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990638Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 747 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990637Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 787 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990636Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 787 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990635Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .3750 INCH CRACK AT STA 440 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990634Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 440 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990633Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 727G BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990632Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 727G BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990631Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECITON, FOUND A.3750 INCH CRACK AT STA 500A BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990630Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 480 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)
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