Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA991055Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT UPPER OUTBOARD CORNER OF CO-PILOTS NR 1 WINDOW SKIN. INSTALLED DOUBLER PER EA65643 AND SRM 53-30-3 FIG 11. (M)SDR USAA991054Splice · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 907 STRINGER 4L, AT FASTENER HOLE STRINGER SPLICE. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-02. (M)SDR USAA991053Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 887, STRINGER 9R AT FASTENER HOLE FRAME. INSTALLED DOUBLER AND FILLER PER EA 65542, SRM 53-00-07 AND SRM 53-30-07. (M)SDR USAA991052Shear Beam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT BS 726, LBL 61, WL 188 STRINGER 18A SHEAR BEAM WEB. FABRICATED REPAIR ANGLES, AND INSTALLED PER EA 65576, SRM 51-40-05 AND SB 737-53-1170. (M)SDR USAA991051Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 312, BL 0 UPPER CHORD BEAM. CORROSION LEVEL 2, CORROSION TASK C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR SPLICES PER SRM 53-10-51. (M)SDR USAA991050Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 294, LBL 12 BEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M)SDR USAA991049Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 294, RBL 12 BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR SPLICES PER SRM 53-10-51. (M)SDR USAA991033Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 108 INCH SPAN OF CORROSION ALL NUTPLATE HOLES STATION 967 FLOORBEAM CAP LBL 54 TO RBL 54. CORROSION LEVEL 2. REPLACED DAMAGED CAP SECTION PER TR 53-10-05 AND SRM 51-30-01. (M)SDR USAA991014Crease Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION LEFT SERVICE DOOR Z-ANGLE INNER CHORD OF CREASE BEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-202-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)SDR USAA991005Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 28 INCH AREA OF CORROSION AT BS 986 FLOORBEAM UPPER SURFACE RBL 13 - LBL 15. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. SPLICED IN NEW T-CAP SECTION PER TR 53-10-05. (M)SDR USAA991003Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 907 STRINGER 9R AT FASTENER HOLE FRAME. INSTALLED FILLER AND REPAIR ANGLE PER EA 65542. (M)SDR USAA990998Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP AT BS 597 AT , S-1, S-8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA990997Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP AT BS 616, S-1, S-5L, S-8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (X)SDR USAA990996Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 312, STR 5L FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (X)SDR USAA990995Lug · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION LEFT LOWER FRONT HORIZ STAB TO LTR SECTION ATTACH LUG. CORROSION LEVEL 1. REPAIRED SPOTFACE AND SHOTPEEN SURFACES PER EA 65596. (M)SDR USAA990994Crease Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT RIGHT SERV DOOR Z-ANGLE INNER CHORD OF CREASE BEAM. CORROSION LEVEL 2. REPLACED DOOR SILL PER SRM 51-10-02. (M)SDR USAA990990Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 827, SR 9L FRAME. INSTALLED FILLER AND REPAIR ANGLE PER EA 65542. (X)SDR USAA990989Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE OF INNER CHORD BS 616, FUSELAGE FRAME WL 203 LEFT SIDE. INSTALLED FILLER AND DOUBLER PER SRM 3-10-23 AND EA 65562. (X)SDR USAA990988Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 616 RBL 62, WL 202, INBOARD CHORD ANGLE. INSTALLED REPAIR ANGLES PER EA 65562. (X)SDR USAA990987Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 887, STR 9L FRAME. INSTALLED DOUBLER PER EA 65542 AND SRM 53-00-07. (X)SDR USAA990986Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STA 480 STR 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND E 65542. (X)SDR USAA990985Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 400 STR 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65542. (X)SDR USAA990984Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 STR 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65542. (X)SDR USAA990978Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS OF CORROSION 1 INCH BY 1 INCH AT BS 328, RBL 25-35. CORROSION LEVEL 2, CORROSON TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP PER SRM 53-10-51. (M)SDR USAA990952Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FRAME AT BS 1006 BETWEEN STRINGER 18L AND 19L. CORROSION LEVEL 2, CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990951Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 663 STR 10R TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (X)SDR USAA990948Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STA 616 STR 4R TIE CLIP. REPAIRED PER SRM 51-10-02. (X)SDR USAA990940Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 663 STR 10L TIE CLIP. REPAIRED PER SRM 51-10-02. (X)SDR USAA990939Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 639 STR 4R TIE CLIP. REPAIRED PER SRM 51-10-02. (X)SDR USAA991096Floorbeam · corrodedCLT - DURING A DROP IN VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT FLOORBEAM STATIN 967, LBL 5, LBL 17 AND RBL 18. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. FABRICATED NEW T-CAP AND ANGLES PER SRM 53-00-51 FIG 202. (M)SDR USAA991095Floorbeam · corrodedCLT - DURING A DROP-IN VISUAL INSPECTINO, FOUND A 1 INCH AREA OF CORROSION AT NUTPLATE HOLES ON UPPER CHORD FLOORBEAM T-CAP STATION 986.5 BETWEEN LBL 45 AND RBL 45. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP PER SRM 53-00-51. (M)SDR USAA991031Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 59 INCH AREA OF CORROSION AT STATION 285-344, WL 208.1 Z-ANGLE. CORROSION LEVEL 2. REMOVED AND REPLACED Z-ANGLE EPR SRM 51-10-02. (M)SDR USAA991032Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER T-CAP AT NUTPLATE HOLES 10 INCH AT BS 294.5, LBL 22 TO RBL 22, BEAM CAP. CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M)SDR USAA991022Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM UPPER CHORD STATION 986 FROM BL 3.5 TO RBL 9.5, CORROSION LEVEL 1. INSTALLED DOUBLER PER TR 53-10-05. (M)SDR USAA991023Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION FLOORBEAM BETWEEN STATION 986.5 BY 1016 DIAGONALLY FROM RBL 19 TO RBL 5. CORROSION LEVEL 1. REPAIRED WITH IDENTICAL PART PER SRM 51-10-02. (M)SDR USAA991002Floorbeam · corrodedCLT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH AREA OF CORROSION FLOORBEAM 967 UPPER CHORD AT LBL 27.5, CORROSION LEVEL 1. REPAIRED DOUBLER PER SRM 53-00-51. (M)SDR USAA991102Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)SDR USAA991090Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 EACH .50 INCH CRACKS AT BS 5332, RBBL 60, WL 21.5 SKIN ASSEMBLY. INSTALLED REPAIR PLATES PER SRM 53-10-01 FIG 202. (X)SDR USAA991081Fitting · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEMBLY. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (X)SDR USAA991057Keel Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CORRODED AREA KEEL BEAM AT BS 500C PLUS 9.5 INCH LBL 5. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER EA 65730. (M)SDR USAA991047Keel Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY 5 INCH AT STATIN 532, RLB 6.5 STRINGER 28R KEEL BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED REPAIR STRAP AND ANGLE PER EA 65811. (M)SDR USAA991029Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT BS 907, STR 9L STRINGER TIE CLIP. REPAIRED WITH IDENTICAL PART PER SRM 51-10-2. (X)SDR USAA991021Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X)SDR USAA991020Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 887, BETWEEN STR 8L AND STR 9L FRAME. INTALLED DOUBLER ANGLE PER EA 65618. (X)SDR USAASB99247Tire · failedLAS - FLT 606 - AFTER T/O AND GEAR ACTUATION, THE 'A' HYD SYS LOW PRESSURE LIGHTS ILLUMINATED AND THE HYD QTY WENT TO ZERO. CREW COULD NOT GET THE GEAR TO RETRACT. AN EMERGENCY WAS DECLACED. FLIGHT RETURNED TO FIELD AT LAS AND LANDED WITHOUT FURTHER INCIDENSDR SWAA991694Angle · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED, BS 360, LBL 68, WL 230. REMOVED AND REPLACED ANGLE PER SRM.SDR USAASB99245Harness · failedORD - FLT 1817 - EN ROUTE FROM PHL/MSP, CAPTAIN REPORTED THE NR 2 AND NR 3 TRANSFORMER RECTIFIERS HAD TRIPPED AND THE CAPTAIN'S WINDOW OVERHEAT LIGHT WAS ON. CAPTAIN RESET T/R'S, BUT THEY BOTH TRIPPED AGAIN. LOSS OF ELECTRIC TRIM, AUTOSPEED BRAKE AND RIGHT SDR SWAA991681Beam · crackedDURING SCHEDULED 1/2D CHECK, FOUND CENTER SECTION LONGITUDINAL BEAM CRACKED ON UPPER SURFACE BS 707-710, RBL 24.5. REPAIRED BEAM PER SRM.SDR SWAA991667Floorbeam · corrodedDURING SCHEDULED 1/2D CHECK, FOUND CORROSION BS 328 FLOORBEAM UPPER FACE LBL 28. REPAIRED BEAM PER SRM.SDR DL733992230Skin · gougedFUSELAGE SKIN FS 807-907, STRINGER 25L-27R, SKIN GOUGE REPAIR. THE FUSELAGE SKIN WAS BADLY SCRATCHED AND GOUGED FROM FS 807 TO FS 907 BETWEEN STRINGERS 25L AND 27R DUE TO IMPACT WITH GROUND EQUIPMENT. THE SKIN WAS CUT AT FS 807 BETWEEN STRINGER 25L AND 2
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