Boeing 737-524
Service difficulty reports · 1,586
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 = '737524' 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 = '737524' 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 CALA0300352Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT NUTPLATE HOLES BETWEEN STA 344 AND 360, LBL 10. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-40.SDR CALA0300348Fuse · blownINSPECTION FOUND THE LAST FOUR ROWS OF EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. THE RT AFT BATTERY PACK 5 AMP FUSE WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE LIGHTS WAS RESTORED.SDR CALA0300344Angle · corrodedINSPECTION FOUND ZEE ANGLE I/B OF L-2 DOOR CORRODED. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300359Skin · dentedMAINTENANCE REMOVED AN INTERIM REPAIR ON THE RT HORIZONTAL STABILIZER AT THE LEADING EDGE. THE DENT WAS NEAR A RIB AT LEADING EDGE STATION 184.66. THE FINAL TRIM OUT WAS 3.5 INCHES BY 4.5 INCHES. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING A FLUSH REPAIRSDR CALA0300341Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED WITH A SHARP CREASE IN THE CENTER OF THE DENT AT LEADING EDGE STA 184. REPAIRED IAW SRM 55-10-01 AND ECRA 5510-01647.SDR CALA0300340Intercostal · crackedINSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY, STA 312-328, LBL 50.5. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300339Intercostal · crackedINSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-10-51 AND 51-70-11.SDR CALA0300338Intercostal · crackedINSPECTION FOUND A .125 INCH CRACK IN INTERCOSTAL AT FORWARD ENTRY STA 328-344, LBL 50.5. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300337Gate · crackedINSPECTION FOUND A 0.33 INCH CRACK IN LOWER GATE OF L-2 DOOR. THE CRACK WAS LOCATED AT AFT CORNER FROM AFT MOST RIVET TOWARDS HINGE. INSTALLED HINGE AND SEALED RETAINERS ON NEW GATE IAW SRM 51-40-02.SDR CALA0300332Circuit Breaker · failedA HEAVY ELECTRICAL ODOR WAS NOTICED IN THE CABIN WHILE EN ROUTE TO DCA. THE ODOR WAS ACCOMPANIED BY FAILURE OF CABIN LIGHTS, OVEN, AND AUTOPILOT AND THE NR 1 ENGINE GENERATOR BUS OFF LIGHT, AND RIGHT EQUIP COOLING SUPPLY OFF LIGHT ILLUMINATED. THE AIRCRAFT LSDR CALA0300328Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN OUTBOARD OF EE ACCESS DOOR AT STA 338 BETWEEN STRINGER 24R AND 25R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5330-03260.SDR CALA0300334Wire Harness · burnedTHE AFT FUEL BOOST PUMP LOW PRESSURE LIGHT LEFT SIDE ILLUMINATED AFTER LANDING AT DFW. WHILE TROUBLESHOOTING THE PUMP THE WIRE BUNDLE AT STA 254 IN COCKPIT WAS FOUND BURNED. OVERHEATING OF THE PUMP WAS SUSPECTED TO BE THE CAUSE OF THE BURNT WIRING. THE FUELSDR CALA0300291Mount · corrodedINSPECTION FOUND RT AFT GALLEY FLOOR MOUNT CORRODED. THE FLOOR MOUNT WAS REPLACED IAW ECRA 2540-01305.SDR CALA0300289Mount · corrodedINSPECTION FOUND FORWARD LAV MOUNT CORRODED AT DOOR THRESHOLD AFT CORNER. THE AFT CORNER MOUNT WAS REPLACED IAW ECRA 2540-01436.SDR CALA0300288Support · gougedINSPECTION FOUND NR 1 FLAP TRACK FAIRING SUPPORT GOUGED AT I/B HINGE LUG. A NEW TRACK FAIRING SUPPORT WAS INSTALLED IAW MM 27-51-71.SDR CALA0300287Arm · gougedINSPECTION FOUND FAIRING SUPPORT ARM GOUGED AT RIGHT O/B MID FLAP CARRIAGE.REPLACED ARM IAW MM 27-51-34.SDR CALA0300286Isolator · crackedINSPECTION FOUND A 1 INCH CRACK IN RIGHT ENGINE AFT ISOLATOR ELASTOMER. THE NR 2 ENGINE AFT MOUNT WAS REMOVED AND REPLACED IAW MM 54-42-11.SDR CALA0300276Angle · corrodedINSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300275Angle · gougedINSPECTION FOUND L-ANGLE AT LT VERTICAL STABILIZER BOTTOM INSIDE PANEL 9507 GOUGED. THE GOUGED SECTION OF L-ANGLE WAS REMOVED AND REPLACED IAW ECRA 5380-01013.SDR CALA0300269Skin · dentedINSPECTION FOUND A DENT WITH GOUGE IN LT HORIZONTAL STABILIZER UPPER SPAR SKIN. THE DENT WAS LOCATED 51 INCHES O/B FROM I/B EDGE AND 3.5 INCHES AFT OF FORWARD SPAR. THE DENTED AREA WAS CUTOUT AND A DOUBLER WAS INSTALLED IAW SRM 55-10-01, FIGURE 207.SDR CALA0300268Attach Angle · corrodedINSPECTION FOUND Z-ATTACH ANGLE CORRODED AT L-2 DOOR ENTRYWAY. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300282Structure · wornWEAR DAMAGE WAS FOUND AT THE UPPER SURFACE OF THE OUTBOARD FLANGE OF RT KEEL BEAM LOWER STRUCTURE JUST FORWARD OF STA 727 WHILE AIRCRAFT WAS IN MAINTENANCE CHECK AT HOU. THE WEAR WAS CAUSED BY THE FLOATING NUT PLATES ATTACHED TO THE OUTBOARD FLANGE OF THE LOWSDR CALA0300249Strip · crackedINSPECTION FOUND A .25 INCH CRACK AT O/B CORNER OF RT WHEEL WELL FORWARD FAIRING AFT ATTACH STRIP. AN ANGLE WAS INSTALLED IAW SRM 51-40-02.SDR CALA0300238Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-30-51.SDR CALA0300237Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 380-400, BL 0. THE INTERCOSTAL WAS REMOVED NAD REPLACED IAW SRM 53-30-51.SDR CALA0300213Skin · crackedTHE AIRCARFT FUSELAGE SKIN SUSTAINED LIGHTNING STRIKE DAMAGE AT STA 747 S1R AND STA 727 S1R. THE DAMAGE WAS IN THE FORM OF A .5 INCH CRACK AND A .1562 INCH HOLE. THE SKIN WAS REPAIRED IAW SRM 53-00-01.SDR CALA0300205Fuse · blownINSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE AT ROW 1AB TO 3AB. THE BATTERY PACK FUSE WAS FOUND AT FAULT. THE FUSE WAS REPLACED AND OPERATION OF THE EMERGENCY AISLE PATH LIGHTS CHECKED GOOD.SDR CALA0300194Skin · puncturedTHE UPPER SURFACE SKIN PANEL OF THE RT ELEVATOR SUFFERED SMALL PUNCTURE DAMAGE AT APPROXIMATELY ELEVATOR STATION 105.1 WHILE AIRCRAFT WAS IN 1/4D CHECK AT HOU. THE DAMAGE WAS THROUGH ALL PLIES, BUT THERE WAS NO CORE DAMAGE. THE PUNCTURE WAS APPROXIMATELY 4.2SDR CALA0300211Skin · puncturedAIRCRAFT SUFFERED HAIL DAMAGE TO THE RT ELEVATOR UPPER SKIN PANEL. THE HAIL IMPACT CAUSED A SMALL PUNCTURE AT APPROXIMATELY ELEVATOR STATION 129.4 AND 9.25 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE WAS THROUGH ALL PLIES AND TO THE CORE. THE SSDR CALA0300210Skin · dentedAIRCRAFT SUFFERED HAIL DAMAGE TO THE RT ELEVATOR UPPER SKIN PANEL. THE HAIL IMPACT CAUSED A SMALL DENT AT APPROXIMATELY ELEVATOR STATION 88.9 AND 10.25 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES AND THE COSDR CALA0300209Skin · puncturedTHE AIRCRAFT SUFFERED HAIL DAMAGE IN THE FORM OF A SMALL PUNCTURE TO THE LT ELEVATOR UPPER SKIN PANEL AT APPROXIMATELY ELEVATOR STATION 128.79. THE HOLE WAS APPROXIMATELY 17.5 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVALSDR CALA0300208Skin · dentedTHE AIRCRAFT SUFFERED HAIL DAMAGE TO THE LT ELEVATOR UPPER SKIN PANEL AT APPROXIMATELY ELEVATOR STATION 110.49. THE HAIL IMPACT CAUSED A SMALL DENT APPROXIMATELY 4.5 INCHES FORWARD OF THE ELEVATOR TRAILING EDGE. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLSDR CALA0300207Skin · dentedTHE AIRCRAFT SUFFERED HAIL DAMAGE TO THE UPPER SKIN PANEL OF THE LT ELEVATOR. THE HAIL IMPACT CAUSED A SMALL DENT AT APPROXIMATELY ELEVATOR STATION 86.8. THE DAMAGE CLEAN UP REQUIRED REMOVAL OF ALL PLIES. THE DENT WAS APPROXIMATELY 15.5 INCHES FORWARD OF THSDR CALA0300198Skin · puncturedTHE LT ELEVATOR UPPER SKIN WAS DAMAGED BY HAIL. THE DAMAGE CONSISTED OF ONE PUNCTURE AND THREE DENTS. THE SKIN WAS REPAIRED IAW ECRA 5520-01325.SDR CALA0300197Skin · puncturedTHE RT ELEVATOR UPPER SKIN WAS DAMAGED DURING A HAIL STORM. THE DAMAGE CONSISTED OF ONE PUNCTURE AND 10 SMALL DENTS. THE SKIN WAS REPAIRED IAW ECRA 5520-01326.SDR CALA0300196Skin · dentedTHE RT AILERON SKIN WAS DENTED IN THREE PLACES BY HAIL. THE DENTS MEASURED 0.023 INCH DEEP X 0.75 INCH DIAMETER, 0.031 INCH DEEP X 0.75 INCH DIAMETER, AND 0.028 INCH DEEP X 1 INCH DIAMETER. THE SKIN WAS REPAIRED IAW ECRA 5760-01008.SDR CALA0300195Skin · dentedTHE LT AILERON UPPER SKIN WAS DENTED BY HAIL. ONE DENT MEASURED 0.027 INCH DEEP AND 1.25 INCH DIAMETER. THE OTHER MEASURED 0.031 INCH DEEP AND 0.75 INCH DIAMETER. THE DAMAGED SKIN WAS REPAIRED IAW ECRA 5760-01007.SDR CALA0300148Cable · out of rigTHE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM EWR. APPROPRIATE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN GEAR AIR/GROUND SENSE TELEFLEX CABLE OUT OF ADJUSTMENTSDR CALA0300147Floor Support · crackedINSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT AT STA 344, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-3.SDR CALA0300144Skin · dentedINSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01.SDR CALA0300131Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 380, STRINGER 17L. INSTALLED REPAIR IAW SRM 53-00-01.SDR CALA0300130Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 400 BELOW STRINGER 17L. A REPAIR WAS INSTALLED IAW SRM 53-00-01.SDR CALA0300127Fitting · wornINSPECTION FOUND THE R/H ELEVATOR O/B HINGE FITTING WORN. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-51-02 AND 51-40-02.SDR CALA0300110Charger · inoperativeINSPECTION FOUND FIRST CLASS CABIN SEATS WITH EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE DURING "A" CHECK. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-02.SDR CALA0300059Skin · crackedINSPECTION FOUND A 1.5" CRACK IN FUSELAGE SKIN BELOW AFT CARGO PIT THRESHOLD AT STA 807, S26R-S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-03214.SDR CALA0300028Skin · gougedINSPECTION FOUND GOUGE AND DENT IN AFT CARGO DOOR SKIN AT AFT SIDE. REPAIRED DOOR IAW SRM 53-00-01 AND 52-30-01.SDR CALA0300074Crease Beam · dentedTHE FUSELAGE SKIN WAS FOUND DENTED COMMON TO THE CREASE BEAM BETWEEN STA 360 TO STA 380. FURTHER INSPECTION FOUND THE CREASE BEAM OUTBOARD CHORD AND SHEAR WEB DAMAGED. THE SKIN DENT WAS WITHIN SRM LIMITS. THE DAMAGE WAS REPAIRED IAW ECRA 5310-04100. A DIP WAS SDR CALA0300117Skin · corrodedINSPECTION FOUND FORWARD CARGO DOOR CUTOUT SKIN CORRODED ON INNER SIDE JUST BELOW LOWER AFT DOOR STOP, STA 450, STRINGER 22R.. THE CORRODED SECTION WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01121.SDR CALA0300042Skin Panel · gougedINSPECTION FOUND THE LOWER L/H SIDE OF RUDDER LEADING EDGE SKIN PANEL GOUGED. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5540-01162.SDR CALA0300041Bear Strap · corrodedINSPECTION FOUND CORROSION AT THE INSIDE SURFACE OF THE BEAR STRAP AT THE LOWER AFT CORNER OF THE FORWARD CARGO DOOR CUTOUT. THE CORROSION WAS REMOVED AND REPAIR WAS PERFORMED IAW ECRA 5331-01121.
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