Boeing 737-201
Service difficulty reports · 2,471
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 = '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.
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
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 USAA001364Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED, STATION 639 STRINGER 4R. INSTALLED PART PER EO 5393G227. (M)SDR USAA001363Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 827 AT STRINGER 10L. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAASB00233Wire · brokenTPA - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 5 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 5. OPERATIONAL CHECK GOOD. (M)SDR USAASB00225Valve · dirtyIAD - FLT 2753 - ON CLIMB-OUT FROM IAD, AT FL220, THE NR 1 ENGINE FUEL HEAT VALVE OPEN LIGHT ILLUMINATED AND THE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND. CAPTAIN ACCOMPLISHED SPECIAL PROCEDURES, SHUT DOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCSDR USAA001280Skin · crackedTPA - FOUND SKIN CRACKED 1.5 INCH, BETWEEN 727A AND 727B STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)SDR USAASB00217Light · failedBWI - MAINTENANCE FOUND THE PORTABLE FORWARD EMERGENCY LIGHT INSIDE THE FLIGHT COMPARTMENT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPS CHECK NORMAL. (M)SDR USAASB00214Handle · failedBOS - FLT 2602 - CAPTAIN REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION TO RETRACT THE LANDING GEAR. CREW ACCOMPLISHED ABNORMAL PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMSDR USAA001205Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, LEFT FUSE EXT SKIN STATION 766, STRINGER 18L. INSTALLED DOUBLER PER EA 67770. (M)SDR USAASB00208Light · failedPVD - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB00198Adc · failedTPA - FLT 2674 - ON CLIMB-OUT, NR 2 MACH METER OFF FLAG DISPLAYED, NR 2 ALTIMETER STANDBY FLAG APPEARED, TCAS BECAME INOPERATIVE, ALT REPORTING ON THE XSPONDER BECAME INOP, NR 2 V-SPEED SHOWED A DESCENT DURING CLIMB. CREW UNABLE TO PULL ANY CB'S ON PANEL TO RSDR USAA001015Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, AT FS 747 AND STRINGER 17L LT EXTERIOR SKIN. REPAIRED DOUBLER PER SRM 53-30-3 FIG 1, 17 AND EA 67683. (M)SDR USAA000998Skin · crackedTPA - FOUND SKIN CRACKED 2.5 INCHES, FUSELAGE SKIN FORWARD CORNER OF AFT ENTRY DOOR CUTOUT. INSTALLED PLATES AND FASTENERS PER SRM 53-30-3 FIG 24. (M)SDR USAASB00188Line · leakingMCO - FLT 2670 - UPON APPROACH INTO MCO, AFTER SETTING FLAPS, FLIGHT ENCOUNTERED SYSTEM A HYDRAULIC FLUID LOSS. BOTH A PUMP LOW PRESSURE LIGHTS ILLUMINATED. CREW ACCOMPLISHED ALTERNATE FLAP EXTENSION AND MANUAL GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER SDR USAA000954Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 986.5, LBL 38. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1. (M)SDR USAA000953Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 20R. INSTALLED TIE CLIP PER EO 5393G227. (M)SDR USAA000950Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 3 INCHES AND 2 INCHES BY 2 INCHES, BS 986.5 4 INCHES, RBL AND 4 INCHES THROUGH 12 INCHES LBL. FABRICATED NEW T-CAP AND ANGLE DOUBLER PER TR 53-60-01. (M)SDR USAA000949Strap · crackedCLT - FOUND STRAP CRACKED .750 INCH, S-5A STRAP STATION 1138 LT SIDE. INSTALLED INTERIM REPAIR PER EA 67518 AND SRM 53-00-01 FIG 221. (M)SDR USAA000948Stringer · crackedCLT - FOUND STRINGER CRACKED 3 INCHES, STATION 1006 TO 1009, STRINGER 27R. REPAIRED PER BOEING DWG 65-46558. (M)SDR USAA000947Skin · crackedCLT - FOUND AFT SKIN CRACKED .350 INCH, BS 951 AFT GALLEY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA000946Skin · crackedCLT - FOUND SKIN CRACKED .3 INCHES, STATION 948 SKIN UPPER END SERVICE DOOR HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)SDR USAA000945Frame · crackedCLT - FOUND FRAME .125 INCH CRACKED, STATION 887, STRINGER 19L. REMOVED AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 9. (M)SDR USAA000944Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787, STRINGER 3R. INSTALED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA000943Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 764.5 AT STRINGER 19L. INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 6. (M)SDR USAA000942Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 727A PLUS 17 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)SDR USAA000941Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727A PLUS 8 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)SDR USAA000940Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706, STRINGER 3R. REMOVED AND REPLACED PER SRM 51-10-1. (M)SDR USAA000939Floorbeam · crackedCLT - FOUND 2 CRACKS IN FLOORBEAM .100 INCH, BS 663, WL 208 UPPER T-CAP. INSTALLED REPAIR PER TR 57-10-04. (M)SDR USAA000938Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .250 INCH, STATION 520, RBL 45 UPPER CHORD RADIUS. INSTALLED REPAIR PER EA 67455. (M)SDR USAA000937Floorbeam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, BS 520, RBL 24, WL 208. INSTALLED REPAIR ANGLE PER EA 67455. (M)SDR USAA000936Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED, BS 520, LBL 45 UPPER CHORD AFT RADIUS. INSTALLED DOUBLER PER EA 67455. (M)SDR USAA000935Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .500 INCH, BS 520, LBL 24 UPPER CHORD AFT RADIUS. REPAIRED PER EA 67455. (M)SDR USAA000934Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 520, STRINGER 19L. INSTALLED DOUBLER PER SRM 51-40-03. (M)SDR USAA000933Web · crackedCLT - FOUND WEB CRACKED .5 INCH, STRINGER 10L SUPPORT WEB BS 350. REPLACED WEB PER SRM 51-10-02. (M)SDR USAA000932Angle · crackedCLT - FOUND ANGLE CRACKED 1.5 INCHES, BS 350, STRINGER 16L. REPLACED SUPPORT ANGLE PER SRM 51-10-2. (M)SDR USAA000931Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES, BS 350, STRINGER 15L. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND SRM 51-40-02. (M)SDR USAA000930Frame · crackedCLT - FOUND FRAME CRACKED 1.5 INCH, BS 350, AT STRINGER 15L DOOR STOP FITTING. REPAIRED PER SRM 51-10-2. (M)SDR USAA000929Skin · crackedCLT - FOUND OUTER SKIN CRACKED 3 INCHES, AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER STATION 947. INSTALLED EXTERNAL SKIN TRIPLER PER SRM 53-30-3. (M)SDR USAA000928Skin · crackedCLT - FOUND INNER SKIN PLATE CRACKED 1 INCH, AFT SERVICE DOOR FUSE. CUTOUT TORQUE BOX INBOARD SIDE. INSTALLED DOUBLER AND FILLER PER TR 53-30-07A. (M)SDR USAA000927Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .200 INCH, RT WING LANDING GEAR BEAM. ACCOMPLISHED PART A PER TR 57-40-10. (M)SDR USAA000951Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 24 INCHES BY 1 INCH, AFT SERVICE DOOR BS 947 TO BS 986 RT. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)SDR USAASB00182Transmitter · failedMIA - FLT 2781 - ON FINAL APPROACH INTO MIA, THE FLAPS BECAME ASYMMETRIC AND WOULD NOT EXTEND BEYOND FIVE DEGREES. CREW ACCOMPLISHED GO-AROUND AND THEN PROCEEDED TO USE THE ALTERNATE FLAP EXTENSION PROCEDURES. PROCEDURE WAS SUCCESSFUL AND THE AIRCRAFT LANDEDSDR USAA000889Skin · crackedBOS - FOUND SKIN CRACKED 1.75 INCH, STATION 767 ON STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGE 11-12B, SHTS 1-4. (M)SDR USAASB00177Indicator · failedCLE - FLT 1231 - ON APPROACH TO CLE, CREW WAS UNABLE TO EXTEND FLAPS. CREW ACCOMPLISHED GO AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. CREW RECEIVED PARTIAL FLAPS USING ALTERNATE FLAP METHOD. HAD FULL LEADING EDGE DEVICES AND 15 DEGREES FLAPS ON TRAILINSDR USAASB00176Csd · failedCRW - FLT 2704 - EN ROUTE FROM BWI TO CLE, THE NR 1 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED CSD AND THEN THE APU QUIT. WITH ONLY ONE POWER SOURCE REMAINING, THE FLIGHT DIVERTED TO CRW. FLIGHT LANDED WITHOUT FURTHER SDR USAASB00175Csd · overservicedCHS - FLT 2634 - DURING CRUISE, ENROUTE FROM MCO TO BWI, THE NR 1 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 1 ENGINE CSD. A SHORT TIME LATER, THE APU HIGH OIL TEMPERATURE LIGHT ILLUMINATED RESULTING IN APU AUTO SDR USAASB00174Charger · failedPBI - PILOT REPORTED THAT THE FLOOR PROXIMITY EMERGENCY PATH LIGHT, AT SEAT 5C, REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY BENEATH SEAT 5ABC. OPERATIONAL CHECK GOOD. (M)SDR USAA000879Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, AFT ENTRY DOOR SILL Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-10-1 AND 51-30-0. CORROSION LEVEL 1. (M)SDR USAA000873Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES, STATION 947 STRINGER 27L. REMOVED AND REPLACED PER SRM 53-10-03. (M)SDR USAA000872Fitting · crackedCLT - FOUND BULKHEAD FITTING CRACKED .750 AND .375 INCH, BS 663.75 BULKHEAD FITTING RT SIDE WL 191.5 POCKET. REMOVED AND REPLACED BULKHEAD FITTING PER EA 67452, 67457 AND 67412. (M)SDR USAASB00172Csd · failedLGA - FLT 2653 - CREW REPORTED THAT DURING CLIMB-OUT FROM BOS, EN ROUTE TO MCO, NUMEROUS COMPONENTS ASSOCIATED WITH THE AC BUS NR 1 FAILED OR BEAME INTERMITTENT. FOUND THE NR 1 GENERATOR FREQUENCY WAS OFF SCALE LOW. CREW STARTED THE APU AND PLACED IT ON THE
Back to Boeing 737-201