Boeing 737-230
Service difficulty reports · 466
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 = '737230' 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 = '737230' 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 TSAA0251248Window Frame · crackedTRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OSDR TSAA0233230Battery Pack · dischargedREPLACED NR 2 FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0253242Web · crackedREMOVED EXISTING FASTENERS, STIFENERS, FILLERS, AND DAMAGED SECTION OF WEB AS SHOWN ON FIGURE 5. FABRICATED A .050 INCH THICK REINFORCING DOUBLER FROM 7075-T6. ALODINE AND APPLIED BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES. INSTALLED RE-ENFORCING DOUBLER,SDR TSAA0233220Battery Pack · dischargedREPLACED LEFT OVERWING IDENTICAL POWER PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0253216Stiffener · crackedREPAIRED CRACK AT BS 178, WI 184 LBL 5.7 VERTICAL CHORD. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN AREA. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0233211Battery Pack · dischargedREPLACED AFT ENTRY EMERGENCY IDENT LIGHT, INOPERATIVE. AIRCRAFT OK FOR SERVICE.SDR TSAA0233210Battery Pack · dischargedREPLACED LEFT OVERWING EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE.SDR TSAA0233208Battery Pack · dischargedREPLACED CENTER EMERGENCY CONTROL MODULE BATTERY PACK DUE TO LOW VOLTAGE. OP CHECK, OK. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0233209Battery Pack · dischargedREPLACED NR 1 THRU 6 FLOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE.SDR TSAA0278199Bracket · crackedTHE NUMBER ONE REVERSER UNLOCK LIGHT ILLUMINATED IN-FLIGHT. THE AIRCRAFT RETURNED TO AND LANDED AT AIRPORT WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE UPPER LOCK ACTUATOR SENSOR BRACKET CRACKED. MAINTENANCE REPLACED THE SENSOR BRACKET AND AS A PRECAUTIOSDR TSAA0253204Skin · gouged23 INCH LONG GOUGE AND .5000 INCH TO 3 INCH DEEP DENT NOTED ON FUSELAGE EXISTING REPAIR AT BS344 - BS360+7. INSTALLED REPAIR PARTS REPAIR COMPLETED IAW SRM. AIRCRAFT OF FOR SERVICE.SDR TSAA0253195Skin · crackedTRIMMED OUT DAMAGE SKIN AT BS 749 STRINGER 18R. HFEC EDGE OF TRIMMED AREA, NO DEFECTS NOTED.SDR TSAA0221175Controller · malfunctionedON CLIMB OUT, AIRCRAFT WAS UNABLE TO MAINTAIN PRESSURIZATION. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. BITE AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR TSAA0257184Skin · corrodedLEFT LOWER OUTBOARD WING TRAILING EDGE CORRODED AT WSL 453. BLENDOUT TO REMOVE ALL CORROSION CONFIRMED USING 10X VISUAL INSPECTION NO DEFECTS NOTED, OBTAINED A SURFACE FINISH OF 125 MICROINCHES RADIUS OR SMOOTHER, FLAT PEENED REWORKED AREA, ALODINED AND PRIMESDR P2EA2002M047Lens · missingROW 4 EMERGENCY TRACK LIGHTING MISSING LENS. REMOVED AND REPLACED LENS IAW MM 33-53-0. OPERATIONAL CHECK NORMAL.SDR TSAA0233160Battery Pack · dischargedREPLACED NR FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR P2EA2002M046Skin · crackedSKIN CRACK ON L1 DOOR AT LOWER AFT CORNER. REPAIRED SKIN IAW SRM 52-00-3.SDR TSAA0233158Battery Pack · dischargedREPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0233159Light · inoperativeREPLACED FORWARD SERVICE DOOR IDENT LIGHT ASSEMBLY DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE.SDR P2EA2002M042Tailpipe · crackedDURING TRANSIT CHECK FOUND THE NR 2 ENGINE TAIL PIPE EXTENSION WITH CRACK. REMOVED AND REPLACED THE NR 2 ENGINE TAIL PIPE EXTENSION WITH SERVICEABLE EXTENSION IAW 78-32-211.SDR P2EA2002M041Tailpipe · crackedDURING TRANSIT CHECK FOUND THE NR 1 ENGINE TAIL PIPE EXTENSION WITH CRACK. REMOVED AND REPLACED THE NR 1 ENGINE TAIL PIPE EXTENSION WITH SERVICEABLE TAIL PIPE EXTENSION IAW 78-32-211.SDR P2EA2002MO38Indicator · failedT/E FLAPS WOULD NOT EXTEND FROM FULL UP POSITION UPON DEPARTURE FROM GATE. REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41, OPS CHECK GOOD AT ALL POSITION SETTINGS.SDR TSAA0233129Battery Pack · dischargedREPLACED FORWARD ENTRY DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE.SDR TSAA0233122Battery Pack · dischargedREPLACED FORWARD SERVICE DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0233123Battery Pack · dischargedREPLACED FORWARD ENTRY DOOR EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0233121Battery Pack · dischargedREPLACED NR 2 EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0233120Battery Pack · dischargedREPLACED NR 6 EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0233119Battery Pack · dischargedREPLACED AFT ENTRY IDENT EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0251107Floorbeam · crackedFOUND A 2.5 INCH CRACK AT BS 710 FLOORBEAM BBL .07 ON THE WEB. CUT OUT DAMAGED AREA ON THE WEB. FABRICATED A REPAIR DOUBLER IAW FIGURE 6. INSTALLED DOUBLER, STIFFENERS AND FILLERS. REPAIR COMPLETED IAW ECO 2223 R1. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251111Fitting · corrodedFOUND CORROSION ON THE FORWARD LOWER EXTRUSION, LOWER FRAME SECTION IN THE RIGHT WHEEL WELL BETWEEN BS 680 AND BS 690. CUT OUT DAMAGED SECTION OF WEB. FABRICATED AND INSTALLED NEW WEB SECTION IAW SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251110Fitting · corrodedFOUND CORROSION ON THE FORWARD LOWER EXTRUSION ON THE FRAME IN THE LEFT WHEEL WELL AT BS 680. REMOVED THE FORWARD LOWER EXTRUSION. INSTALLED NEW EXTRUSION SECTION IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251109Keelbeam · corrodedFOUND CORROSION ON THE KEEL BEAM LOCATED IN THE MAIN WHEEL WELL AT BS 685 LEFT CHORD AT THE MOUNT SCREW HOLES. REPAIRED BY REMOVING CORROSION IAW DETAIL VII, VIII AND IX. REPAIR COMPLETED IAW SRM 53-10-1, FIGURE 7, BS 685. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251108Keelbeam · crackedFOUND CRACK ON THE LOWER CHORD IN THE LEFT MAIN WHEEL WELL AT BS 652 KEEL BEAM FUSELAGE SKIN AREA. TRIMMED OUT CRACK AND VERIFIED REMOVED USING HFEC METHOD. FABRICATED A REPAIR ANGLE AND FILLER. REPAIR COMPLETED IAW ECO 2726R3 PART II. AIRCRAFT RETURNED TOSDR TSAA0253112Stringer · corrodedFOUND EXFOLIATION CORROSION ON STRINGER 27L AT BS 967. REMOVED THE DAMAGED SECTION OF THE STRINGER. FABRICATED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 PAGE 10. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251106Floorbeam · crackedFOUND A CRACK AT FUSELAGE STATION 665 FLOORBEAM BL 0 ON THE UPPER CHORD. FABRICATED AND INSTALLED REINFORCING DOUBLER, STIFFENERS, FILLERS, SPLICE PLATE AND ANGLE. REPAIR COMPLETED IAW ECO 2223 R1 PART II DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0253116Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 867 RIGHT WINDOW BOTTOM FORWARD CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE SDR TSAA0253115Window Frame · crackedPERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 787 RIGHT WINDOW UPPER AFT CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE EDGE SDR TSAA0253114Structure · crackedPERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDCIATION AT BS 440 RT WINDOW UPPER FORWARD CORNER USING HFEC METHODS. REPAIRED IAW SRM, AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0251096Bulkhead · crackedFOUND CRACK ON UPPER BULKHEAD IN THE NOSE WHEEL WELL. TRIMMED OUT CRACK ENSURING A .50 INCH MINIMUM RADIUS. VERIFIED CRACK REMOVED USING HFEC METHOD AND MADE A .040 INCH INSURANCE CUT. FABRICATED A FILLER FROM .050 INCH, A DOUBLER FROM .063 INCH AND TWO TAPSDR P2EA2002M018LightDuring operational check at scheduled inspection the R/H AFT Emergency Light was found defective. Removed and replaced Light assembly IAW MM 33-51-81. This is closing action for P2EA2002M018. Reference VAM 037, dated 03/24/02SDR TSAA0221093Controller · failedFLT 66 - HNL-OGG - PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED AT 14,000 FT AND STANDBY LIGHT CAME ON. SWITCHED TO STANDBY MODE. CABIN RATE STARTED CLIMBING AND DESCENDING AT 4,000 FPM. SWITCHED TO MANUAL DC THEN AC MODE AND STILL UNABLE TO CONTROL PRESSURIZSDR P2EA2002M013Controller · failedAIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. AIRCRAFT LANDED AND RETURNED TO BLOCKS WITH NO INCIDENT. REMOVED AND REPLACED PRESSURE CONTROLLER IAW MM 21-31-21. OPERATIONAL CHECK NORMAL.SDR P2EA2002M016Hinge Fitting · vibratesINTERMITTENT VIBRATION OBSERVED AROUND THE AFT GALLEY FLOOR AREA. REMOVED AND REPLACED THE NR 4 HINGE FITTING ON THE LT HORIZONTAL STAB IAW MM 27-31-13. NO VIBRATION NOTED TO THIS DATE.SDR P2EA2002M011Structure · vibrationDURING FLIGHT A FLIGHT ATTENDANT REPORTED VIBRATION AT THE AFT GALLEY FLOOR. VIBRATION STOPPED AND THEN STARTED AGAIN DURING FLIGHT. ALL SYSTEMS INDICATED NORMAL AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION AND LANDED WITH NO INCIDENT. AIRCRAFT WAS INSPECSDR P2EA2002M028Bleed Valve · lack of lubeNR 2 ENGINE COMPRESSOR STALLED AS THE THROTTLES WERE ADVANCED FOR TAKEOFF. LUBED THE NR 2 ENGINE BLEED VALVES IAW AMM 75-31-0. RAN ENGINE, OPS CHECKED GOOD.SDR P2EA2002M005Fitting · looseAIRCRAFT VIBRATES AT 280 KIAS OR .73 MACH AND GREATER VIBRATION FELT ON COCKPIT FLOOR, CABIN FLOOR TO AFT GALLEY. INSPECTED ELEVATOR AND ELEVATOR TAB AND FOUND THE LEFT HAND ELEVATOR TAB CONTROL ROD FITTING LOOSE. RETORQUED THE LEFT HAND ELEVATOR TAB CONTROLSDR TSAA0233028Battery Pack · dischargedREPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2002F00111Valve · malfunctionedFLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. REF TSSDR TSAA0221021Sensor · malfunctionedFLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2002F00110Valve · malfunctionedFLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)
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