Boeing 737-401

Service difficulty reports · 2,961

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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.

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)Jun 30, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR USAA990628Frame · crackedCLT - DURING Q-5 CHECK, VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 867 BETWEEN STR 8R AND STR 9R FRAME. (X)Jun 30, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 30, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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 Jun 29, 1999 · N407US · Boeing 737401 · Engine EGT/TIT Indicating SystemSDR 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 Jun 26, 1999 · N406US · Boeing 737401 · Hydraulic Pump (Electric/Engine), MainSDR USAA990613unknownCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Miscellaneous StructureSDR 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.Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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 STRAJun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, FrameSDR 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)Jun 21, 1999 · N404US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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)Jun 16, 1999 · N422US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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 ALIJun 11, 1999 · N411US · Boeing 737401 · Inertial Guidance SystemSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, BulkheadSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Floor PanelSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, FrameSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Miscellaneous StructureSDR 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)May 22, 1999 · N419US · Boeing 737401 · Fuselage Main, Floor BeamSDR 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. May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR 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)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR 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)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR 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)May 19, 1999 · N407US · Boeing 737401 · Trailing Edge FlapsSDR 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. May 17, 1999 · N413US · Boeing 737401 · Emergency Lighting
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