Boeing 737-490
Service difficulty reports · 3,288
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 = '737490' 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 = '737490' 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 FL2420260515321Plate · corrodedPLATE CORRODED BETWEEN FS. 559-578 LBL 45.64-70.88SDR 202604150001Floorbeam · crackedWHILE ACCOMPLISHING PEMCO SB 737-57-0001 REV 5 AND SB 737-57-1210 REV 2 OF AD 2008-04-21 FOUND CRACK INDICATIONS WERE NOTED AT BBL .07 FLOOR BEAM BETWEEN BS 705-715 BETWEEN THE LOWER WEB FLOOR BEAM #1-#4 HOLES AND #6-#7 HOLES. CRACKS WERE ALSO NOTED AT THE UPPSDR TSAA2026032700002Skin · damagedFELT TAIL STRIKE ON ROTATIONSDR TSAA2026021200001Indicator · failedFIRST OFFICER'S AIRSPEED INDICATOR FAILED WITH A RED FLAG. NEEDLE FROZEN AT 296 KTS.SDR I5EA2023011700002Battery Pack · no testRH OWEE LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK AT M1479 POWER SUPPLY AT STA. 598R IAW B737-400 AMM 33-51-51. OPS CHECK GOOD.SDR I5EA2021121100004Power Supply · no testEMERGENCY LIGHT POWER SUPPLY FOUND BAD AT STA. 747R. REMOVED AND REPLACED POWER SUPPLY M1435 AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-51. STA. 747R.SDR I5EA2021121100003Battery Pack · no testEMERGENCY EXIT LIGHT INOP AT R/H BULL NOSE ROW 10. REMOVED AND REPLACED BATTERY PACK ON M1435 POWER SUPPLY AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-51. STA. 747RSDR I5EA2021121100002Battery Pack · no testEMERGENCY EXIT LIGHT INOP AT L 2 DOOR. REMOVED AND REPLACED BATTERY PACK ON M1197 POWER SUPPLY AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-51. STA. 960L.SDR I5EA2021121100001Battery Pack · no testEMERGENCY EXIT LIGHT IS INOP AT L/H OVER WING EXIT. REMOVED AND REPLACE BATTERY PACK ON M1134 POWER SUPPLY AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-51. STA. 634L.SDR I5EA2021022200006Charger · inoperativeLEFT AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACES BATTERY CHARGER AT M1197 WITH SERVICEABLE UNIT IAW B737-400 AMM 33-51-51, TESTS OK.SDR EE4Y2020111911959Skin · crackedUPPER FUSELAGE, RT AFT GALLEY DOOR, LOWER INNER SKIN CUTOUT WITH CRACK. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF JOB: A1J185 NRI: 2-59).SDR EE4Y2020111911958Floor Support · corrodedUPPER FUSELAGE, FROM BODY STATION 947 TO 967 AT RBL 50 FLOOR SUPPORT INTERCOSTAL WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 2-57).SDR EE4Y2020111911957Rib · crackedLT HORIZONTAL STABILIZER, LEADING EDGE STATION 95 RIB WITH CRACK. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 3-23).SDR EE4Y2020111911956Floor Support · corrodedUPPER FUSELAGE, FROM BODY STATION 986.5 TO 996 AT RBL 46, FLOOR SUPPORT ANGLE WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 2-56).SDR EE4Y2020111911955Angle · corrodedUPPER FUSELAGE, AFT GALLEY SERVICE DOOR, FWD FRAME LOWER HINGE AREA ANGLE WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 2-15).SDR EE4Y2020111911954Shear Tie · corrodedLOWER FUSELAGE BODY STATION 500G BEWTEEN STRINGER 27LH AND STRINGER 28RH, FRAME-SHEAR TIE WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 1-22).SDR EE4Y2020111911953Angle · crackedRT ELEVATOR HINGE NUMBER 4, ANGLE WITH CRACK. IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 3-8).SDR EE4Y2020111911951Channel · corrodedLOWER FUSELAGE BODY STATION 540 STRINGER 26L CHANNEL WITH CORROSION. NOTE: IT WILL BE REPLACED BY B737-400 SRM INSTRUCTION (REF: JOB: A1J185 NRI: 1-81).SDR EE4Y2020111911950Skin · crackedRT WING TRAILING EDGE AT WBL 204, FLAP LEADING EDGE SKIN WITH CRACK. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 6-54).SDR EE4Y20201119Skin · corrodedWING CENTER SECTION, BETWEEN LBL 45.61 AND LBL 70.85, BETWEEN REAR SPAR AND STIFFENER S-2C UPPER SKIN WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER AW AVIATION TECH SERVICES ENGINEERING ORDER NUMBER 2020-1012 (REF: JOB: A1J185 NRI: 2-17).SDR EE4Y2020111811942Spar · crackedLT WING REAR SPAR UPPER CHORD AT RSS 224 OPEN HOLE WITH CRACK INDICATION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 5-43).SDR EE4Y2020111811945Floorbeam · corrodedUPPER FUSELAGE BODY STATION 986, FLOOR BEAM UPPER CHORD WITH CORROSION AT SEVERAL PLACES. NOTE: THE FLOOR BEAM UPPER CHORD WAS REPAIRED, AS PER PEMCO ENGINEERING AUTHORIZATION NUMBER PD37-53-3198 INSTRUCTION (REF: JOB: A1J184 NRI: 2-32).SDR I5EA2020062418003Light · inoperativeEMERGENCY LIGHT INOP R/H FWD CABIN.SDR I5EA2020062418002Light · inoperativeEMERGENCY LIGHT INOP FWD EMERGENCY EXIT R/HSDR I5EA2020062370003Light · inoperativeEMERGENCY LIGHT INOP R/H FWD CABIN.SDR I5EA2020061700002Light · inoperativeEMERGENCY LIGHT INOP FWD EMERGENCY EXIT R/HSDR I5EA202001220003Power Supply · inoperativeL1 DOOR INDICATOR INOPERATIVE. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED M1133 POWER SUPPLY ASSY IAW AMM 33-51-51, OPS CHECK GOOD.SDR FOTR20180830005Fitting · crackedDURING HFEC OPEN HOLE INSPECTION OF MCD LATCH ASSY. FASTENER HOLES, INDICATION NPTED AT STA 420 FASTENER HOLE NR 2F.SDR FOTR201808209004Skin · bulgedLOWER FUSELAGE SKIN BULGING AT BS 538 BETWEEN STRINGERS 27R - 28R.SDR FOTR201808209003Spar · crackedRT WING REAR SPAR RSS 218 CRACKED AT INBD SIDE OF MLG SUPPORT FITTING.SDR FOTR201808209002Support Angle · corrodedBS 540 BETWEEN STRINGERS 27R - 28R SUPPORT ANGLE HAD CORROSION.SDR FOTR2018080800001Frame · crackedFORWARD CARGO BAY, BS 500B FRAME WAS CRACKED AT THE INBD SIDE OF WIRE PENETRATION HOLE.SDR I5EA2018022100003Battery Pack · weakEMERGENCY LIGHT AT 14DEF INOPERATIVE. TROUBLESHOOT IAW WDM 33-51-14, AND FOUND THE BATTERY PACK M1435 WEAK. REMOVED AND REPLACED THE BATTERY PACK. OPS TESTED GOOD IAW AMM 33-51-51.SDR ASAA2018020123399Screw · shearedCREW COULD NOT OPEN L1 DOOR AFTER LANDING. GROUNDED - YES. FOUND SCREW SHEARED ON LOWER RADIUS LINK OF L1 DOOR GUIDE ARM. REMOVED RADIUS LINK OUT OF THE WAY AND WAS ABLE TO OPEN DOOR. REMOVED AND REPLACED RADIUS LINK ATTACHING HARDWARE ON GUIDE ARM REF CMM 52-SDR ASAA2017111022533Sign · brokenEXIT SIGN ABOVE THE ENTRY TO FLIGHT DECK IS BROKEN. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN COVER THAT WAS BROKEN.SDR ASAA2017092523694Gate · crackedCRACK FOUND ON L2 DOOR LOWER GATE, AFT END. ACFT GROUNDED. REPLACED THE DOOR GATE.SDR ASAA2017091322121Frame · crackedRIGHT OTBD BS 727 FRAME CRACKED, STRINGER 18A. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW AD20122304-400-53-011R, AND AD20122304-400-53-8.SDR ASAA2017091322063Tee Fitting · crackedFWD GALLEY DOOR CUTOUT NR 1 DOOR STOP TEE CRACKED IN RADIUS BS 333, STRINGER 8. ACFT GROUNDED. REMOVED AND REPLACED THE TEE IAW SRM 51-40-02.SDR ASAA2017080321547Guide Arm · damagedRAMP REPORTED UNABLE TO OPEN THE L1 DOOR. ACFT GROUNDED. ATTEMPTED TO OPEN DOOR, NO LUCK. DOOR UNLATCHES, CRACKS OPEN MAKING A CRACKLING NOISE AND BINDS. FOUND BOTTOM RADIUS LINK KEY WASHER AND SCREW MISSING WHICH CAUSED BINDING ON L1 DOOR GUIDE ARM. REMOVSDR ASAA2017073123693Skin · crackedFORWARD CARGO DOOR SKIN CRACKED, UPPER AFT CORNER OF HANDLE CUT OUT. ACFT GROUNDED. INSTALLED A REPAIR DOUBLER IAW SRM 52-00-01-2R-2.SDR ASAA2017053020919Battery Pack · failedEMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 1 - 11ABC FOUND INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS NORMAL IAW AMM 33-51-06-960-805.SDR ASAA2017052220920Stop Fitting · gougedFWD CARGO DOOR FWD LOWER FITTING DAMAGE IN PREVIOUS BLENDED AREA OUT OF LIMITS OF IAW SRM 52-30-02-1A-1. ACFT GROUNDED. REPLACED FWD LOWER STOP FITTING IAW SRM 51-40-02, AND DWG 65-46921.SDR ASAA2017040720427Doubler · corrodedNR 3 SLAT TAI DUCT NOSE BEAM DOUBLER CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE SLAT TAI DUCT NOSE BEAM DOUBLER IAW SRM 51-40-02-0G-0.SDR ASAA2017033120403Fitting · corrodedNLG DOWNLOCK ACTUATOR LT AND RT ATTACH FITTINGS HAVE CORR IN BUSHING LUGS. GROUNDED - YES. REMOVED AND REPLACED LT AND RT FITTINGS IAW SRM 51-40-02-0G-0.SDR ASAA2017033020377Support · corrodedAT FWD SIDE OF BS 227 BULKHEAD LOWER LT DOOR STOP BACKUP SUPPORT FITTING EXFOLIATED PANEL RACK. ACFT GROUNDED. FABRICATED A NEW SUPPORT IAW SRM 51-40-06-0G-0 AND BDWG 65-45801.SDR ASAA2017032920341Attach Angle · crackedSTRINGER 10R ATTACH ANGLE CRACKED AT BS 277. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER ATTACH ANGLE IAW SRM 51-40-02-0G-0.SDR ASAA2017032720402Frame · corrodedFWD SIDE OF BS 227 BULKHEAD LOWER FRAME IS CORRODED AT BL0 TO RBL5. ACFT GROUNDED. REPAIRED IAW SRM 53-10-08-2R-13.SDR ASAA2017032720343Fitting · crackedRIGHT INBD NR 5 GROUND SPOILER INBD ACTUATOR HINGE FITTING LUG IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW SRM 51-10-02.SDR ASAA2017032720342Intercostal · crackedINTERCOSTAL IS CRACKED AT BS 277, STRINGER 14R, APPROXIMATELY .050 INCHES AT FORWARD RADIUS TRIMOUT. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR ASAA2017032620378Stiffener · corrodedFRAME AFT OF FWD ACCESSORY DOOR CUTOUT HAS CORROSION. ACFT GROUNDED. REMOVED, FABRICATED, AND INSTALLED A NEW VERTICAL STIFFENER IAW SRM 51-40-05-0G-0 AND DWG AND10137.
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