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 USAA990629Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 827 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAA990628Frame · crackedCLT - DURING Q-5 CHECK, VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 867 BETWEEN STR 8R AND STR 9R FRAME. (X)SDR USAA990627Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 907 BETWEEN STR 8R AND STR 9R FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X)SDR USAASB99158Egt Light · illuminatedCLT - FLT 932 - UPON CLIMB-OUT FROM CLT, AP APPROX 18,000 FT, THE NR 1 ENGINE EGT LIGHT ILLUMINATED AS THE NR 1 ENGINE EXCEEDED LIMITS. CAPTAIN PULLED THE THROTTLE BACK OT IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT. NO ENGINE SHUTDOWN SDR USAASB99155Pump · leakingPIT - FLT 268 - APPROXIMATELY 30 MILES OUT FROM PIT, THE FLIGHT LOST SYSTEM A-HYDRAULIC QUANTITY. CREW SHUT OFF SYSTEM 'A' ELECTRIC HYDRAULIC PUMP AND FOLLOWED PROCEDURES. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED SDR USAA990613unknownCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .SDR USAA990612Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500D BETWEEN STRINGER 8R AND 9R FRAME. REPAIRED DOUBLER PER EA 64832 AND SRM 53-00-07. (M)SDR USAA990611Angle · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK IN RADIUS INBOARD SUPPORT ANGLE AT STATION 540 RAM AIR DUCT INLET. REPAIRED DOUBLER AND ANGLE PER TR 53-50-03. (M)SDR USAA990605Floorbeam · corrodedCLT - DURING Q-5 CHECK, VISUAL INSPECTION FOUND AN AREA OF CORROSION APPROXIMATELY 2 INCHES BY 6 INCHES UPPER T-CAP AT STA 967, LBL 30, LBL 5, AND RBL 18 FLOORBEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REPAIRED PER TR-53-15-01A AND SRM 53-60-51.SDR USAA990604Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION APPROXIMATELY 20 INCH BY 2 INCH UPPER T-CAP AT STA 947, LBL 12 TO RBL 12 FLOORBEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. INSTALLED REPLACEMENT T-CAP WITH SPLICE ANGLES AND STRASDR USAA990603Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500A BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07 FIG 202. (M)SDR USAA990602Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FUOND A .375 INCH CRACK AT STATION 787 BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832. (M)SDR USAA990594Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK AT STATION 867 BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832. (M)SDR USAA990593Frame · crackedCLT - DURNG Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 480 BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (M)SDR USAA990592Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 827 BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832. (M)SDR USAA990591Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500C BETWEEN STRINGER 8L AND 9L ON FRAME. INSTALLED DOUBLER PER EA 64832. (M)SDR USAA990590Floorbeam · corrosionCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BY 72 INCH AREA OF SURFACE CORROSION UPPER T-CAP OF FLOORBEAM AT STATION 986.5. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED NEW FABRICATED T-CAP PER TR 53-60-01. (M)SDR USAA990599Floorbeam · corrodedTPA - DURNIG CX-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AFT CARGO DOOR THRESHOLD STATION 807 TO 847, RBBL 13.8. INSTALLED DOUBLER PER EA 64280. (M)SDR USAASB99141Irs · failedROC - FLT 1886 - AFTER TAKEOFF, CREW REPORTED LOSING HEADING INDICATOR. CREW ACCOMPLISHED SPECIAL PROCEDURES, BUT FAILED TO REST. CAPTAIN ELECTED TO RETURN TO FIELD AT ROC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ALISDR USAA990530Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)SDR USAA990529Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)SDR USAA990528Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 7 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)SDR USAA990527Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, LBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)SDR USAA990526Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, LBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)SDR USAA990525Frame · crackedCLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 787, BETWEEN STRINGER 8 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990524Frame · crackedCLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 827, BETWEEN STRINGER 8R/9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990523Frame · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 380, BETWEEN STRINGER 8R/9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990522Frame · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 380, BETWEEN STRINGER 8 AND STRINGER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990521Frame · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990520Frame · crackedCLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990519Frame · crackedCLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK AT FUSELAGE FRAME AT FASTENER HOLE AT BS 747 BETWEEN STRINGER 8 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990518Frame · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 480, BETWEEN STRINGER 8 AND STRINGER 9L INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990517Frame · crackedCLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 440, BETWEEN STRINGER 8 STRINGER 9. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990516Frame · crackedCLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 500A, BETWEEN STRINGER 87 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M)SDR USAA990515Frame · crackedCLT - DURING Q-2 CHECK, FOUND .125 INCH CRCK AT FUSELAGE FRAME AT FASTENER HOLE AT BS 440 BETWEEN STRINGER 8 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M)SDR USAA990513Frame · crackedCLT - DURING Q-2 CHECK, FOUND 1.5 INCH CRACK AT FASTENER HOLE OF INBOARD CHORD OF FUSELAGE FRAME AT BS 597, WL 203, RBL 64. INSTALLED DOUBLER PER EA 64518 AND EA 64594. (M)SDR USAA990512Frame · crackedCLT - DURING Q-2 CHECK, FOUND 1 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 827, BETWEEN STRINGER 8 AND STRINGER 9L. DOUBLER AND FILLER INSTALLED PER SRM 53-00-07. (M)SDR USAA990511Bulkhead Web · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH VERTICAL CRACK ON BULKHEAD WEB AT STATION 178, LBL 4.5, WL 198. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M)SDR USAA990509Frame · crackedCLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 787 BETWEEN STRINGER 8 AND STRINGER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA990508Floor · crackedCLT - DURING Q-2 CHECK, FOUND TWO .75 INCH CRACKS AT FORWARD END OF BEAD IN PRESSURE DECK/FLOOR AT STTION 6635 LBL 33. INSTALLED DOUBLER PER EA 64506 AND REV EA 64506A. (M)SDR USAA990507Frame · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 867 BETWEEN STRINGER 8 AND STRINGER 9L. INSTALLED DOUBLER PER EA 64536. (M)SDR USAA990462Frame · crackedCLT - DURING Q-2 CHECK, FOUND .75 INCH IN FUSELAGE FRAME AT FAST HOLE AT BS 747 BETWEEN STRINGER 8/STRINGER 9L. REMOVED CRACKED AND INSTALLED DOUBLER PER SRM 53-00-07 AND EA 54536. (M)SDR USAA990461Floorbeam · corrodedCLT - DURING Q-2 CHECK, FOUND .250 INCH BY .250 INCH AREAS OF CORROSION ON FLOORBEAM AT BS 986.5 AT LBL 45.5-RBL 45.5. CORROSION LEVEL 2. INSTALLED NEW 'T' CAP PER TR 53-60-01. (M)SDR USAA990458Angle · crackedCLT - DURING Q-2 CHECK, FOUND 1 INCH CRACK AT DRAG ANGLE AT STATION 540 STRINGER 22L. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-50-03. (M)SDR USAA990457Floorbeam · corrodedCLT - DURING Q-2 CHECK, FOUND 1 INCH BY 1 INCH CORRODED AREA ON FLOORBEAM AT BS 312 RBL 37, WL 208.1. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM 53-10-51. (M)SDR USAA990376Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION ON CARRIAGES SUPPORT ARM INBOARD MID FLAP, INBOARD CARRIAGE, OUTBOARD ARM AT BEARING MOUNT HOLE FOR ECCENTRIC BUSHING. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. SDR USAA990375Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, INBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSION TASK C57-306-04. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA990374Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP INBOARD CARRIAGE, INBOARD SUPPORT ARM, AT ECCENTIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA990373Support · corrodedCLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, OUTBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAASB99130Connector · looseTPA - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTING AT SEAT ROW 6A AND THE FIRST CLASS CABINET, LEFT SIDE INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG AT THE FIRST CLASS CABINET, LEFT SIDE, DISCONNECTED. RECONNECTED CANNON PLUG. OPERATIONAL CHECK GOOD.
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