Boeing 737-201

Service difficulty reports · 2,471

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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 = '737201'
  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 USAA010080Bulkhead · crackedCLT - FOUND BULKHEAD .250 INCH CRACK, STATION 178, BULKHEAD, WL 214, LBL 6.5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010079Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 214, RBL 5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010078Bulkhead · crackedCLT - FOUND BULKHEAD .250 INCH CRACKED, STATION 178, WL 214, LBL 5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010077Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD WL 207, RBL 1.5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010075Angle · corrodedCLT - FOUND Z-ANGLE CORRODED, 8 PLACES 1 INCH BY 1 INCH, FORWARD ENTRY DOOR Z-ANGLE. CORROSION LEVEL 1 C53-107-01. REPLACED Z-ANGLE PER SRM 51-10-1. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010076Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES, STRINGER 28R OUTBOARD SIDE OF STRINGER 8 AFT OF FRAME 312. CORROSION LEVEL 1. REMOVED AND REPLACED AND INSTALLED DOUBLER PER SRM 51-40-2. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB01026Duct · leakingFLL - FLT 2626 - ON CLIMB-OUT FROM FLL, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED PROCEDURES, REDUCED POWER TO IDLE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY Jan 28, 2001 · N263AU · Boeing 737201 · Air Intake Anti/De-Ice SystemSDR USAASB01022Accessory Unit · failedBWI - FLT 2735 - UPON GEAR EXTENSION INTO BWI, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS. CREW ENSURED GEAR HANDLE WAS IN DOWN DETENT. AFTER RECYCLING GEAR, CREW RECEIVED NORMAL THREE GREEN GEAR LIGHTS AND NO RED LIGHTS. FLIGHT LANDED AT BWI WITHOJan 26, 2001 · N245US · Boeing 737201 · Landing Gear Position and WarningSDR USAA010059Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 24 INCHES, STATION 312, LBL 12 TO RBL 12. CORROSION LEVEL 2 C53-107-01. SPLICED IN NEW T-CAP SECTION PER TR 53-10-13. (M)Jan 22, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010054Angle · crackedCLT - FOUND UPPER CHORD ANGLE CRACKED 2 INCHES, 727 BULKHEAD AT RBL 25. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M)Jan 22, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010053Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, BS 597 LEFT JUST ABOVE CENTER WING. INSTALLED NEW FRAME PER SRM 51-10-1. (M)Jan 22, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAASB01016Proximity Switch · out of adjBWI - FLT 2679 - ON APPROACH TO BWI, THE LEADING EDGE TRANSIT LIGHT ILLUMINATED, ALONG WITH A BAD VIBRATION, DURING FLAP EXTENSION. THE NR 3 AND NR 4 LEADING EDGE SLATS WOULD NOT EXTEND. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEJan 22, 2001 · N259AU · Boeing 737201 · Leading Edge Slat Position Indicating SystemSDR USAA010052Fitting · corrodedCLT - FOUND FITTINGS SPAR CORRODED 4 INCHES, REAR SPAR HINGE FITTING LT CLEVIS AND LUG. CORROSION LEVEL 1 C53-701-02. SPOT FACED LUG PER EA 68689. (M)Jan 22, 2001 · N245US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA010051Fitting · corrodedCLT - FOUND REAR SPAR FITTING CORRODED 4 INCHES, RT HINGE ATTACH CLEVIS. CORROSION LEVEL 1 C53-701-02. SPOT FACED INBOARD/OUTBOARD CLEVIS PER EA 68752. (M)Jan 22, 2001 · N245US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAASB01011Engine · failedLGA - FLT 2990 - ON CLIMB-OUT FROM LGA, AFTER FL120, CREW REPORTED LOSS OF NR 1 ENGINE OIL AND THE LOW OIL PRESSURE LIGHT ILLUMINATING. OIL PRESSURE DROPPED BELOW THE RED LINE AND HELD AT ABOUT 20 PSI. CREW SHUT DOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY ANJan 19, 2001 · N247US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA010164Skin · crackedBOS - FOUND SKIN CRACKED 2 INCHES, BS 727A STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 PP 2E, FIG 1. (M)Jan 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010001AStiffener · corrodedCLT - FOUND STIFFENER CORRODED 7 INCHES BY 1 INCH, BS 235, RBL 10, WL 195 FORWARD UPPER ACCESS PANEL. INSTALLED ANGLE AND STIFFENER PER SRM 53-10-2 AND 53-30-0. (M)Jan 15, 2001 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010002AFrame · crackedCLT - FOUND FRAME CRACKED 3 INCHES, FORWARD ENTRY DOOR BOTTOM FRAME. REPLACED FRAME PER SRM 51-10-1. (M)Jan 15, 2001 · N245US · Boeing 737201 · Passenger/Crew DoorsSDR USAA010003AIntercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 178, WL 195, RBL 26 AND LBL 26. REPLACED INTERCOSTAL PER SRM 53-10-1. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010019Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 827 STRINGER 2L, 6L AND 10L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010018Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 2R AND STRINGER 4L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010017Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 10R. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010016Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 5R. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010015Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 767, STRINGER 5L, 6L. INSTALLED MODIFIED TIE CLIP PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010014Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 767, STRINGER 4R. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010013Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 747, STRINGER 5L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010012Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 4R, 6R, 8L AND 9L. INSTALLED MODIFIED TIE CLIP PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010011Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 2L, 6L AND 7L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010010Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATIN 727A, STRINGER 1. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010009Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 685, STRINGER 2L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010008Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663-675, STRINGER 10L. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010007Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH STATION 643, STRINGER 4R. REPAIRED PER EO 5393G227. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010006Web · crackedCLT - FOUND WEB CRACKED 1 INCH, LT CREASE BEAM WEB STATION 616-639, STRINGER 18L. INSTALLED NEW WEB PER SRM 51-10-1 AND 51-30-3. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010005Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .75 INCH, BS 520, STRINGER 19L. INSTALLED NEW STRINGER TIE CLIP PER SRM 51-10-1. (M)Jan 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB01006Battery Pack · dischargedTPA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 1 THROUGH 8 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT 8A AND REMOVED AND REPLACED THE BATTERY PACK AT SEAT 17A. OPERATIONAL CHECK GOOD. (M)Jan 14, 2001 · N245US · Boeing 737201 · Emergency LightingSDR USAASB00364Oil Cooler · malfunctionedEWR - FLT 2995 - ON CLIMB-OUT FROM LGA, BETWEEN FL120 TO FL150, THE NR 1 ENGINE OIL PRESSURE APPROACHED THE RED RADIAL. THRUST WAS REDUCED BUT OIL TEMPERATURE ROSE THROUGH YELLOW BANK. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO EWR.Dec 31, 2000 · N247US · Boeing 737201 · Engine Oil CoolerSDR USAASB00366Duct · crackedBWI - FLT 2631 - EN ROUTE FROM FLL TO LGA, THE RIGHT WING-TO-BODY OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND CONTINUED FLIGHT ON ONE PACK, WHEREAS LIGHT EXTINGUISHED. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INDec 31, 2000 · N248US · Boeing 737201 · Air Distribution SystemSDR USAASB00365Battery Pack · dischargedBWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. (M)Dec 30, 2000 · N248US · Boeing 737201 · Emergency LightingSDR USAA002218Stringer · corrodedCLT - FOUND STRINGER CORRODED 3 INCHES, BS 990, STRINGER 25R INSIDE STRINGER. SPLICED REPAIR PER SRM 53-10-3. CORROSION LEVEL 1 C53-202-01. (M)Dec 29, 2000 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA002217Stringer · corrodedCLT - FOUND 2 INCHES OF CORROSION, BS 962, STRINGER 25R INSIDE STRINGER. CORROSION LEVEL 1 C 53-202-01. STRINGER STRAP REPLACED PER SRM 51-30-2. (M)Dec 29, 2000 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA002214Web · crackedCLT - FOUND WEB FLANGE CRACKED 4 INCHES, STATION 727 AFT SIDE LBL 12, 26 INCHES ABOVE STRINGER 26L. REPLACED CRACKED INTERCOSTAL PER SRM 51-10-01. (M)Dec 28, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB00361Charger · dischargedLGA - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY PATH LIGHTS FROM SEAT ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Dec 27, 2000 · N252AU · Boeing 737201 · Emergency LightingSDR USAA002210Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, STRINGER 27R PLUS 909. REMOVED AND REPLACED DAMAGED PART SPLICE AND FILLER PER EA 68674A. (M)Dec 27, 2000 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB00359Transmitter · malfunctionedBOS - FLT 2610 - WHILE SELECTING FLAPS 5 ON APPROACH AT MHT, THE FLAPS JAMMED BETWEEN THE 2 AND 5 POSITION. DUE TO THE SHORT RUNWAYS AT MHT, CREW DECIDED TO DIVERT TO BOS. DURING FINAL APPROACH TO BOS, CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHDec 26, 2000 · N265AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAA002196Structure · corrodedFOUND CORROSION ON T-CAP .250 INCH BY .250 INCH, BS 947, RBL 36 - RBL 52. INSTALLED FILLER AND DOUBLER PER EA 68715. (M)Dec 26, 2000 · N245US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002186Stringer · corrodedCLT - FOUND STRINGER CORRODED 3 INCHES, STATION 907, STRINGER 20R. CORROSION LEVEL 1 C53-107-02. INSTALLED STRINGER SPLICE PER SRM 51-10-02 AND 51-10-1. (M)Dec 21, 2000 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA002185Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED .5 INCH BY 5 INCHES, BS 767 BETWEEN STRINGER 26R-27R. CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-10-4 9A. (M)Dec 21, 2000 · N245US · Boeing 737201 · Fuselage Main, StructureSDR USAA002183Stiffener · crackedCLT - FOUND HORIZONTAL STIFFENER CRACKED 4 INCHES, 727 BULKHEAD, LBL 11 - LBL 12, UP FROM CARGO FLOOR. FABRICATED NEW PART AND INSTALLED PER SRM 51-10-01. (M)Dec 21, 2000 · N245US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA002182Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BELLY AT STATION 767, BL 0. INSTALLED DOUBLER PER EA 68722. (M)Dec 21, 2000 · N245US · Boeing 737201 · Fuselage Main, FrameSDR USAASB00353Seal · failedBWI - FLT 2637 - ON CLIMB-OUT FROM BWI, AT FL230, A LOUD SQUEAL BEGAN COMING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD MAIN Dec 21, 2000 · N252AU · Boeing 737201 · Passenger/Crew Doors
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