Boeing 737-301

Service difficulty reports · 4,797

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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.

SDR USAA950301Pump · failedCLT - FLT 731 - FLIGHT EN ROUTE PHL TO MSY WHEN FORWARD NR 2 MAIN TANK FUEL BOOST PUMP LOW PRESSURE LIGHT CAME ON. FLIGHT DIVERETED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 FORWARD BOOST PUMP PER MM 28-22-41. NO LEAKS NOTMar 25, 1995 · N577US · Boeing 737301 · Fuel Boost PumpSDR USAA950246Door · missingTPA - FLT 60 - ON CLIMB-OUT FROM TPA, LEFT ENGINE PYLON PANEL CAME OFF. FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED PANEL ON CDL 54-20-1 AND RELEASED AIRCRAFT. REPLACED NACELLE STRUT ACCESS DOOR ON LEFT ENGINE PYLONMar 15, 1995 · N563AU · Boeing 737301 · Service DoorsSDR USAA950243Eel · inoperativeDCA - LEFT SEAT EMERGENCY LIGHT ON ROW 10 INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (W)Mar 12, 1995 · N353US · Boeing 737301 · Emergency LightingSDR USAA950214Bulb · failedIAH - FLT 1439 - FLIGHT EN ROUTE SAT TO PIT WHEN NR 2 ENGINE OIL TEMPERATURE EXCEEDED RED LINE. CREW SHUT DOWN ENGINE AND DIVERTED TO IAH WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE OIL TEMPERATURE BULB. (Z)Mar 6, 1995 · N353US · Boeing 737301 · Engine Oil TemperatureSDR USAA950157Fan Blades · bird strikeLGA - FLT 488 - AT 500 FEET ON CLIMB-OUT, HAD A SUDDEN LOUD RUMBLE AND HIGH VIBRATION IN NR 2 ENGINE. WHEN POWER HAS REDUCED AT LEVEL OFF, NOISE DECREASED AND VIBRATION DECREASED TO NORMAL LEVELS. SUSPECTED BIRDSTRIKE. FLIGHT RETURNED TO LGA WHERE LANDING WFeb 23, 1995 · N589US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAA950187Intercostal · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 10 INCH TOTAL OF CORRODED AREA ON INTERCOSTAL AT BS 986.5 THROUGH BS 1016. REPAIRED PER SRM 53-60-51 AND SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (Z)Feb 20, 1995 · N335US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950186Floor Beam · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .625 INCH BY 10 INCH TOTAL CORROSION IN SEVERAL PLACES, ON FLOOR BEAM AT BS 847 THROUGH BS 787.7. REPAIRED PER SRM 53-00-53 FIG 202. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (Z)Feb 20, 1995 · N335US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950099Mix Valve · failedPIT - FLT 576 - ON CLIMB-OUT, CREW HAD NO CONTROL OVER RT AIR MIX VALVE. VALVE WENT FULL COLD AND WAS NOT CONTROLLABLE IN MANUAL OR AUTO. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED RT PACK AIR MIX VALVE. OPS CHECK, LEAFeb 12, 1995 · N560AU · Boeing 737301 · Cabin Temperature Control SystemSDR USAA950183Skin · chaf wearINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND APPROX .5 INCH BY 4 INCH LONG CHAF WEAR DEEP INTO FUSELAGE SKIN, BETWEEN STRINGER 1 AND 2 LEFT AT STATION 867 TO 887. REPAIRED PER SRM 53-00-01 AND TR 53-30-01 AND TR 53-30-03 AND EA 38864. (Z)Feb 10, 1995 · N335US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA950185Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON AFT CARGO FLOOR STRINGERS, BS 775 AT LBL 2, 7, AND 12 RBL 2, 7, (5 PLACES). REPAIRED PER TR 53-10-06. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Z)Feb 8, 1995 · N335US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA950190Floor Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH BY .028 INCH SPOT OF CORROSION BS 1006 RBL 10. REPAIRED PER EA 38836. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (Z)Feb 7, 1995 · N335US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950189Blkhd Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 36 INCH CORRODED AREA, STATION 947 BULKHEAD LOWER ATTACH ANGLE S-26 R TO S-26L. REPAIRED PER BOEING DRAWING NR PL 65-49616 REV LTR AND SHT 13 OF 73 ID NR 12. CORROSION TASK NR C53-208-01, CORROSION LEFeb 6, 1995 · N335US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA950188Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 200 INCH CORRODED AREA STATION 727 TO 767 AND 847 TO 947 RIGHT ANGLE IN AFT CARGO. REPAIRED PER SRM 51-10-02 AND 51-40-02. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Z)Feb 6, 1995 · N335US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950184Beam · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 31 INCH BY 2 INCH CORRODED AREA ON BEAM AT BS 986.5. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-00-51. CORROSION LEVEL 2. (Z)Feb 3, 1995 · N335US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950182Bulkhead Skin · crackedINT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN BS 178, BS 178 RBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z)Feb 1, 1995 · N335US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA950181Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .375 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN (BS 178) BS 178, LBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z)Feb 1, 1995 · N335US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA950137Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH IN LENGTH CORROSION SEVERAL AREAS, BS 947 TO BS 1006 'Z' ANGLE RT AFT SERVICE DOOR. REPAIRED PER SRM 51-70-11. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 26, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950133Hat Channel · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 30 INCH CORRODED AREA LT LAVATORY AFT FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 26, 1995 · N301AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA950128Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24 INCH BY 1.3 INCH CORROSION ON INTERCOSTAL BS 1006 TO BS 1016 RBL 18 INCHES. REPAIRED PER SRM 51-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 24, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950127Cap Strip · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24.6 INCH BY 1.3 INCH CORROSION BS 1006 TO BS 1016 LBL 28 INCHES. REPAIRED PER SRM 51-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 24, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950121Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION WIDTH OF FLOORBEAM, FLOORBEAM HOLES CORRODE AT BS 1016. REPAIRED PER TYPICAL REPAIR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 24, 1995 · N301AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950119Support Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION , FOUND .75 INCH BY .75 INCH 6 AREAS CORROSION 4 INCHES AFT OF BS 727 D FROM BL 0 TO S-28 L BL 0 TO S-28 R UNDERSIDE OF ANGLES WHERE NUTPLATE ATTACHES. REPLACED PER T/R 53-10-06, SRM 53-00-53, AND BAC DRW. CORROSION TJan 23, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950032Gcu · failedIND - FLIGHT EN ROUTE PIT TO PHX WHEN NR 1 GENERATOR DROPPED OFF LINE, FOLLOWED BY APU OPERATING INTERMITTENTLY THE SHUTTING DOWN. FLIGHT DIVERTED TO IND WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BENT PIN NR 2213 ON NR 1 ENGINE GCU. REPLJan 22, 1995 · N563AU · Boeing 737301 · AC Generation SystemSDR USAA950139Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION FOUND 8 SQUARE INCHES OF CORROSION 'Z' ANGLE FWD ENTRY DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 20, 1995 · N301AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA950141Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 L. REPAIRED PER SRM 53-00-03. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA950140Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 R. REPAIRED PER SRM 53-00-03. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA950136Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 SQUARE INCHES OF CORROSION BS 947 TO BS 1006. REPAIRED PER SRM 51-10-2 AND SRM 51-10-11. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950135Angle · corrosionINT - DURING Q-6 VISUAL INSPECTION, FOUND 3 INCH BY 59 INCH CORRODED AREA, BS 947 TO 1006 LT SIDE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-2. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950134Hat Channel · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 30 INCH CORRODED AREA RT AFT LAVATORY FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA950124Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 19 INCH CORRODED AREA ON INTERCOSTAL AT BS 967 TO BS 986 RBL 18 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950118Seat Track · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND .25 INCH BY .5 INCH GOUGE STA 887 LBL 25. REPAIRED PER SRM 53-00-52 FIG 204. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950115Girt Bracket · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORRODED AREAS ON GIRT BRACKETS 2 PLACES. FWD ENTRY STA 312 AND STA 244. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 19, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950126Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18 TO RBL 24 TO RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REF 95ZZZW195.Jan 18, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950125Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 18, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR 95ZZZW195Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18 TO RBL 24 TO RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REF USAA950126.Jan 18, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950129Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES CORROSION ON INTERCOSTAL AT BS 947 TO BS 967 AT LBL 30. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 17, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950028Door · not lockedMCO - FLT 682 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FOUND FWD ELECTRICS BY DOOR UNLATCHED. CLOSED AND SECURED DOOR. SYSTEM CHECKS NORMAL. (W)Jan 14, 1995 · N334US · Boeing 737301 · Electrical/Electronic Compartment DoorsSDR USAA950026Eel Batt Charger · inoperativePHL - COCKPIT EMERGENCY EXIT DOES NOT LIGHT WHEN TESTED. MAINTENANCE REPLACED CHARGER ASSEMBLY. EMERGENCY LIGHTS CHECK GOOD. (Z)Jan 13, 1995 · N573US · Boeing 737301 · Emergency LightingSDR USAA950138Angle · corrosionINT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND CORROSION TWO AREAS 2 INCH BY 2 INCH, 54.0 INCH BY 1 INCH 'Z' ANGLE FWD GALLEY SERVICE DOOR BS 294.5 TO BS 344. REPAIRED PER BOEING DRAWING 65-45875 AND SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSJan 11, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950132Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUMEROUS SCREW HOLES .500 INCH BY 500 INCH, INTERCOSTAL BETWEEN BS 312 AND BS 328, 11.5 INCHES FROM BBL 0. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950131Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .500 INCH CORROSION ON INTERCOSTAL BETWEEN BS 328 AND BS 344, 25 FROM BBL 0. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950130Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION ON INTERCOSTAL AT BS 312 TO BS 328 AT LBL 12 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950123Floorbeam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 31.0 INCH BY 2 INCH BS 328 FLOORBEAM T-CAP. REPAIRED PER SRM 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950122Floorbeam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORROSION ON FLOORBEAM AT BS 344 FROM BL 0 TO LBL 24 INCHES. REPAIRED PER TR 53-10-03. CORROSION TASK NR. C53-107-02. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA950120Seat Track · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND TWO CORROSION AREAS 1.0 INCH BY 1.0 INCH AND .500 BY 1.0 INCH, BETWEEN FWD GALLEY BULKHEAD AND BS 294.5, 42.0 INCHES FROM BBL 0. REPAIRED PER BOEING DRAWING 69-40352-6. CORROSION TASK NR C53-107-0Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950117Floor Support · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION OF FLOOR SUPPORT, FOUND SURFACE CORROSION AROUND NUTPLATES 1 INCH BY 1 INCH SEVERAL PLACES 20 INCHES RBL BETWEEN STA 807 AND STA 907. REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W)Jan 11, 1995 · N301AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA950116Frame · corrodedINT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 4 INCH BY 2 INCH CORRODED AREA STA 500 D STR 27 LT. REPAIRED PER SRM 53-00-07 FIG 204. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W)Jan 10, 1995 · N301AU · Boeing 737301 · Fuselage Main, Frame
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