Boeing 737-232

Service difficulty reports · 1,700

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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 = '737232'
  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 DL73S050135Engine · odorFRONT LAV SMOKE ALARM CAME ON SHORTLY AFTER TAKEOFF AND SMOKE THIN AND WISPY, CAME FROM LAV. SMOKE SMELL EVIDENT THROUGHOUT ENTIRE AIRCRAFT. WASHED NR 1 ENGINE AND RAN ENGINE WITH PACKS. NO SMELL NOTEDFeb 26, 2005 · N327DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73S050111Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 764 RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 19L. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUT OUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER Feb 13, 2005 · N305DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S050109Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 18R RUNNING ALONG THE MILL LINE OF THE BONDED INTERNAL DOUBLER. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT TO THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DFeb 13, 2005 · N305DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S050097Frame · crackedA FASTENER HOLE COMMON TO THE OUTER CHORD OF THE AFT FRAME OF THE L2 DOOR CUTOUT (FS 992, BETWEEN STRINGERS 7L & 8L) WAS FOUND CRACKED. THE HOLE WAS OVERSIZED AND AN INSURANCE CUT MADE TO REMOVE THE CRACK. THE OVERSIZED HOLE WAS REPAIRED WITH AN ALUMINUM BUSFeb 8, 2005 · N330DL · Boeing 737232 · Fuselage Main, FrameSDR DL73S050091Engine · malfunctionedFLT 7000 FT CLIMB EPR 250 - CLIMBING CLEAN HEARD LOUD BOOM WITH A/C SHUDDER ONCE. ALL ENG IND NORM AND STEADY. PNEU NORM. NO VISIBLE DAMAGE FROM CABIN F/A'S. ATB CVG UNEVENTFUL. DECLARED EMERGENCY WITH CVG DEPT CONTROL. BORO BOTH ENGINES, OK. FOUND LEFTFeb 8, 2005 · N319DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73S050060Engine · malfunctionedAFTER TAKEOFF WHEN THROTTLES RETARDED NR 2 ENGINE REMAINED AT 1.6 EPR. REPLACED FUEL CONTROL.Jan 26, 2005 · N308DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73S050032Proximity Switch · out of adjustSELECTED FLAPS AND L/E TRANSIT AMBER LIGHT ILLUMINATED. CONFIRMED BY L/E AMBER LIGHTT ON OVERHEAD PNL. FOLLOWED QRH PROCEDURES AND PLANNED FLAP 15 LANDING. ON SHORT FINAL L/E FLAP GREEN LIGHT ILLUMINATED AND SELECTED FLAPS 30. RIGGED NR 1 L/E FLAP EXTENDEDJan 14, 2005 · N314DA · Boeing 737232 · Leading Edge Slat Control SystemSDR DL73S050029Shaft · failedFUEL PUMP SHAFT SHEARED AT ROTATION. RUNWAY EXCURSION ON RETURN IN BAD WEATHER. REPLACING NR 2 ENGINE FUEL PUMP AND CONTROL.Jan 13, 2005 · N311DL · Boeing 737232 · Engine Fuel and ControlSDR DL73S050026Ballast · inoperativeCREW REPORTED ACRID SMELL THROUGHTOUT CABIN. INSP E/E COMP, CARGO BAYS, CABIN BALLAST. FOUND BALLAST OF SEAT 2CD BAD. REPLACED BALLAST. A/C OK FOR SERVICE.Jan 13, 2005 · N319DL · Boeing 737232 · Passenger Compartment LightingSDR DL73S050011Fairing · looseAFTER T/O EXP VIBRATION, LIGHT TO MODERATE, APPROX 12,000 AND 300 KTS. SLOWED TO 250 VIBRATION SUBSIDED SOMEWHAT. EXPERIENCED VIBRATION THRU 210 KTS LIGHT. FOUND E/E DOOR SEAL OUT OF POSITION. REPAIRED SAME. FOUND 2 FLAP FAIRINGS LOOSE. TIGHTENED SAME.Jan 9, 2005 · N320DL · Boeing 737232 · Trailing Edge FlapsSDR DL73S041136Adc · contaminatedAFTER DE-ICING AUTOTHROTTLES DISARMED DURING T/O, NO RE-ENGAGE AT ACCEL PDC CADC FAIL MSG, MACH TRIM FAIL LIGHT. DURING CLIMB CAPTS A/S AND ALTM OFF MSG AFTER LVL OFF. AT FL 290 APPROX 5 MIN CABIN ALT WARN HORN DIFF PRESS 6 PSI, CABIN ALT 10K. FOLLOWED QRH Dec 24, 2004 · N304DL · Boeing 737232 · Air Data ComputerSDR DL73S041118Bulkhead · crackedINSPECTION OF THE FS 1016 P-DOME BULKHEAD WEB PER AD 99-08- 23 REVEALED 3 CRACKED CHORD ATTACH FASTENER HOLES BETWEEN STRINGERS 5L & 7L. THE CRACKS WERE REMOVED BY TRIMMING THE WEB. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 095482-14AD.Dec 16, 2004 · N310DA · Boeing 737232 · Fuselage Main, BulkheadSDR DL73S041111Bulb · inoperativeEMERGENCY LIGHT BELOW OVERHEAD BIN AT ROW 1 ABC INOP. RELAMPED EMERGENCY LIGHT.Dec 16, 2004 · N334DL · Boeing 737232 · Emergency LightingSDR DL73S041110Wire · pulledSEAT ROW EMERGENCY LIGHT AT 18DEF INOP, HAS WIRED PULLED OUT OF CONNECTOR. REPLACED EMERGENCY LIGHT ON 18DEF SEAT ROW.Dec 16, 2004 · N334DL · Boeing 737232 · Light System WiringSDR DL73S041117Skin · crackedINSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK AT FS 380. THE CRACK WAS REMOVED WITH A 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095527-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041116Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT REVEALED A CRACK AT FS 411. THE CRACK WAS REMOVED WITH A 7 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095530-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041115Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 512. THE CRACK WAS REMOVED WITH A 14 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095529-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041114Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 432. THE CRACK WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND ER/A 095531-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041113Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED CRACKS AT FS 470. THE CRACKS WERE REMOVED WITH A 17 INCH LONG SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095528-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041105Skin · crackedNUMEROUS SKIN CRACKS FOUND ALONG STRINGER 4L BETWEEN STATION 540 AND 727. REPAIRED IAW ERA 095481-14AD.Dec 15, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041100Skin · crackedFUSELAGE SKIN CRACKED AT MULTIPLE LOCATIONS ALONG STRINGER 4R BETWEEN STA 540 AND 727. REPAIR IAW ER/A 095480-14AD.Dec 14, 2004 · N310DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041091Shuttle Valve · leakingB-SYSTEM HYD LEAK FOUND AT PUSHBACK. REPLACED BRAKE SHUTTLE VLV IAW M/M.Dec 9, 2004 · N313DL · Boeing 737232 · Master Cylinder/Brake ValveSDR DL73S041081Power Supply · inoperativeON L/O CHECK, FOUND FWD CABIN EMERGENCY PATH LIGHTS INOP. REPLACED FWD CABIN EMERGENCY LIGHTS POWER SUPPLY. CHECKS GOOD.Dec 4, 2004 · N304DL · Boeing 737232 · Emergency LightingSDR DL73S041071Skin · crackedA 1 INCH CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP AT THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER B737 SRM AND ER/A 095399-14, REV A.Nov 30, 2004 · N331DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041063Outflow Valve · failedACFT UNABLE TO PRESSURIZE IN STBY MODE. REMOVED AFT OUTFLOW VALVE. INSTALLED NEW VALVE PER MAINTENANCE MANUAL. ALSO REPLACED CONTROLLER AND PANEL TEST SYS PER MAINTENANCE MANUAL.Nov 26, 2004 · N309DL · Boeing 737232 · Pressure Regulator/Outflow ValveSDR DL73S041060Frame · crackedA 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAME LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14.Nov 23, 2004 · N332DL · Boeing 737232 · Cargo/Baggage DoorsSDR DL73S041051Module · malfunctionedON CLIMBOUT AT 14,000 FEET NR 1 ENG OVERHEAT LIGHT ILLUM. IAW CK LIST THRUST LEVER RETARDED. LIGHT WENT OUT. REPLACED ENG FIRE/OVERHEAT MODULE. RAN ENGS AT T/O AND CLIMB PWR, ALL TEST NORMAL.Nov 22, 2004 · N302DL · Boeing 737232 · Fire DetectionSDR DL73S041055Skin · crackedA 1.5 INCH CRACK WAS FOUND IN THE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18L AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 095229-14AD.Nov 20, 2004 · N326DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041053Skin · crackedTHE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 2.5 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 39Nov 20, 2004 · N316DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041038Skin · crackedA 1 INCH CRACK WAS FOUND IN THE CORNER OF THE LOWER HINGE CUTOUT OF THE L2 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE UNDERLYING BEARSTRAP INSPECTED TO ENSURE IT WAS CRACK FREE. THE SKIN CRACK CUTOUT WAS REPAIRED WITH AN EXTERNAL STEEL DOUBLERNov 16, 2004 · N301DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S041012Shear Beam · crackedA 1 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE AT THE AFT END OF THE STRINGER 18A SHEAR BEAM WEB AT FS 727 ON THE LT SIDE OF THE AIRCRAFT. THE CRACK EXTENDED TO THE AFT EDGE OF THE PART AND FWD OF THE END FASTENER HOLE. THE CRACK WAS REPAIRED WITH ANov 2, 2004 · N329DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR DL73S040999Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK RUNNING ALONG THE BONDED DOUBLER EDGE JUST BELOW STRINGER 23R BETWEEN FS 927 & 947. AN EXISTING SKIN DOUBLER WAS IN AN ADJACENT FRAME BAY. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS CUT OUT OF THE SKIN, ANDOct 28, 2004 · N319DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040993Fuse · failedEMERGENCY LIGHTS AT R2 DOOR AND AFT AISLE EXIT INOPERATIVE. REPLACED BLOWN FUSES IN POWER SUPPLY FOR LIGHTS.Oct 26, 2004 · N309DL · Boeing 737232 · Emergency EquipmentSDR DL73S040985Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED MULTIPLE CRACKS BETWEEN FS 560 & 620. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 094301-14AD.Oct 19, 2004 · N323DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040958Actuator · failedAFTER LANDING A-SYS HYD QTY DROPPED TO 0. REPLACED NR 1 SPOILER ACTUATOR FOR LEAKING.Oct 10, 2004 · N302DL · Boeing 737232 · Drag Control ActuatorSDR DL73S040954Wire · brokenWHILE TURNING NR 1 ENG START SWITCH TO START ENG GOT LOUD POP ALONG WITH SPARK FROM BEHIND OVERHEAD PANEL. MTC FOUND 2 BROKEN WIRES BEHIND PANEL THAT CHAFED FROM RUBBING WHISKEY COMPASS EACH TIME IT IS STOWED. REPAIRED WIRES AND REPLACED SWITCH AS PRECAUTIONOct 9, 2004 · N309DL · Boeing 737232 · Engine Starting System WiringSDR DL73S040953Floorbeam · crackedINSPECTION OF THE LBL AND RBL 24.82 LONGITUDINAL FLOORBEAMS OVER THE CENTER WING REVEALED CRACKS IN THE BEAM WEB AND CAP AT THE AILERON QUADRANT CUTOUTS AT FS 679. THE CRACKS ARE TYPICAL OF AD 2001-17-18. THE CRACKED AREA WAS REPAIRED BY REPLACING THE BEAMOct 7, 2004 · N301DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S040951Skin · crackedTHE LOWER AFT CORNER OF THE RIGHT WING SCANNING LIGHT CUTOUT AT FS 530 WAS FOUND WITH A .5 INCH CRACK IN THE SKIN. THE CRACK WAS REMOVED WITH A SMALL CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094021-14.Oct 7, 2004 · N301DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040949Skin · crackedFOUND ON X-2 LETTER CK, 3.5 INCH CRACK IN FUSELAGE SKIN STA 944 AND STR 25 RIGHT. REPAIRED PER SRM 53-30-3 FIG 48.Oct 5, 2004 · N315DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040939Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 16L AT FS 525. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 093927-Sep 30, 2004 · N334DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040938Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2.7 INCH CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE THE STRINGER 25R SKIN LAP JOINT AT FS 930. THE CRACKED AREA WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM ASep 30, 2004 · N334DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040932Skin · crackedTHE FUSELAGE SKIN AT THE L1 DOOR OPENING WAS FOUND CRACKED AT THE CUTOUT EDGE JUST ABOVE THE LOWER AFT CORNER. THE CRACKS WERE SMALL AND TYPICAL OF BAC S/B 737-53-1083. THE CRACKS WERE TRIMMED OUT OF THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLESep 27, 2004 · N314DA · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040931Door Frame · crackedINSPECTION OF THE C2 DOOR OPENING FRAME AT FS 794 PER AD 93-14-10 REVEALED CRACK IN THE DOOR FRAME WEB AND FLANGE JUST BELOW THE NR 5 DOOR STOP FITTING. THE CRACKS WERE REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND AN EXTERNAL ALUMINUMSep 27, 2004 · N314DA · Boeing 737232 · Fuselage Main, StructureSDR DL73S040925Skin · gougedFUSELAGE SKIN GOUGED AT STATION 827 AND STR 26R. REPAIRED IAW ERA 093263-14.Sep 27, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040924Skin · crackedFUSELAGE SKIN CRACKED AT NUMEROUS LOCATIONS ALONG STRINGER 4L FROM STATION 540 - 727. REPAIRED IAW ERA 093294-14AD.Sep 27, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040916Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A CRACKED FASTENER HOLE AT FS 807. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093396-14AD.Sep 24, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040918Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 390. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093394-14AD.Sep 23, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040915Skin · crackedA 1.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 20L AND FS 765. THE CRACK WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE B737 SRM AND ER/A 093792-14.Sep 23, 2004 · N317DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040912Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER 4R AND STATION 390 & 400. REPAIRED IAW ERA 093395-14AD.Sep 23, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S040911Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER 4L AND STATION 727A +10. REPAIRED IAW ERA 093401-14AD.Sep 23, 2004 · N306DL · Boeing 737232 · Fuselage Main, Plate/Skin
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