Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 SWAA982569Light · looseDURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHT COVER LOOSE FROM ROW 18 THROUGH AFT. RESECURED TRACK LIGHT PER BOEING MM.SDR USAASB98267Wire · looseLGA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT SEAT ROW 11, LEFT HAND SIDE, INOPERABLE. MAINTENANCE ACCOMPLISHED AN INTERIM REPAIR PER ENGINEERING AUTHORIZATION NR 62698 WHICH INSTALLS A JUMPER WIRE FROM THE LIGHT ASSEMBLY ON SEAT ROW 9. A SPLICE WAS ISDR USAA980484Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A .125 INCH CRACK IN EXTERIOR SKIN STATION 380 BL 0. INSTALLED DOUBLER PER EA 62686 SB 737-53-1117 REV 2. (M)SDR USAA980528Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK FS 380 BL 0 BETWEEN STRINGER 27L AND 27R EXTERIOR SKIN. INSTALLED DOUBLER PER EA 62680 AND SB 737-53-1117 REV 1. (M)SDR USAA980527Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK L-1 DOOR UPPER HINGE CUTOUT STATION 312 BETWEEN STRINGER 9L AND 10L EXTERIOR SKIN. INSTALLED DOUBLER PER EX 62655. (M)SDR USAASB98259Battery Pack · dischargedIAH - MAINTENANCE FOUND THE AFT CENTER EMERGENCY EXIT AISLE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CABIN. (M)SDR USAASB98248Battery Pack · dischargedROC - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS HAD FAILED AFTER 30 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED DISCHARGED BATTERY PACKS IN POWER SUPPLIES M1133 AND M1137. OPERATIONAL CHECK. (M)SDR USAASB98244Battery · dischargedRDU - PILOT REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT FOR THE FORWARD MAIN ENTRY DOOR IS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND THE REFLECTOR ASSY FOR THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT ASSY. (M)SDR 98ZZZM779Reflector · inoperativeRDU - PILOT REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT FOR THE FORWARD MAIN ENTRY DOOR IS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND THE REFLECTOR ASSY FOR THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT ASSY. (M)SDR USAASB98233Transmitter · inoperativeCLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT OT 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. FLIGHT LANDED WITHOUTSDR 98ZZZM804Indicator · inoperativeCLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT TO 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. FLIGHT LANDED WITHOUTSDR USAASB98232Csd · failedMCI - FLT 128 - AIRCRAFT DEPARTED DEN WITH THE APU ON MEL. EN ROUTE TO PHL, THE NR 1 ENGINE GENERATOR FAILED IN FLIGHT. WITH ONLY ONE ELECTRICAL POWER SOURCE REMAINING, FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MSDR USAASB98224Sensor · failedCHS - FLT 888 - AT FL370 WITH AUTOPILOT/AUTOTHROTTLES ON, THE NR 2 ENGINE POWER STARTED TO DECREASE WITH THROTTLES SPLIT TWO INCHES. TURNED AUTOTHROTTLE OFF AND POWER BECAME STABLE. TURNED AUTOTHROTTLES BACK ON AND POWER STARTED TO DECREASE AGAIN. TURNED PMSDR F3LA98164Light · inoperativeDEN - UPON ARRIVAL, FLIGHT CREW REPORTED FLOOR PROXIMITY LIGHTING AT ROW 7 INOPERATIVE. REPAIRED WIRING AND SYSTEM CHECKED OK. (M)SDR USAASB98222Fire Loop · chafedPHL - FLT 1888 - EN ROUTE FROM MBJ TO PHL, THE NR 1 ENGINE FIRE WARNING DETECTION FAULT LIGHT ON THE ENGINE/APU FIRE PANEL ILLUMINATED. THE NR 1 ENGINE FIRE HANDLE FLASHED ON AND OFF DURING FIRE/OVERHEAT TEST WITH FAULT LIGHT ON. UPON LANDING IN PHL, LIGHT ESDR USAA980381Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN SKIN E/E DUCT COOLING OUTLET STATION 379 LBL 30. INSTALLED DOUBLER OF .100 INCH 2024-T3 PER EA 62079 AND BOEING SB 737-53-1117. (M)SDR SWAA981803Skin · dentedDURING SCHEDULED TRAN CHECK, FOUND AFT CARGO DOOR SKIN DENTED. REPAIRED PER BOEING MM.SDR USAASB98211Light · inoperativePIT - MAINTENANCE FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT ROW 5C INOP. MAINTENANCE REMOVED AND REPLACED THE BUTTON LIGHT COVER AT SEAT ROW 5C. OPERATIONAL CHECK GOOD. (M)SDR USAA980344Skin · crackedCLT - DURING DAILY CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK BL 0 BETWEEN STATION 727D AND 727E ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAA980359Skin · crackedCLT - DURING CX-1 CHECK EDDY CURRENT INSPECTION, FOUND A 1.2 INCH CRACK BELLY SKIN RADIO RACK EXHAUST CUTOUT STATION 380 BETWEEN STRINGER 28L AND STRINGER 27R. INSTALLED DOUBLER .0012024T-3 PER SB AND EA 62242. (M)SDR USAA980342Skin · crackedTPA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN EXTERNAL SKIN AFT ENTRY DOOR, FWD FLANGE 1 INCH ABOVE LOWER HINGE CUTOUT. INSTALLED DOUBLER OF .050 2024 T-3 PER SRM 52-00-01 FIG 202. (M)SDR USAA980341Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN OUTER SKIN AFT ENTRY DOOR, AFT LWR CORNER OF UPPER HINGE CUTOUT AT EXTERNAL DOOR SKIN. INSTALLED DOUBLER OF .071 2024-73 PER EA 62252. (M)SDR USAA980340Skin · crackedTPA - DURING A CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN OUTER SKIN FWD SERVICE DOOR AFT UPPER CORNER AT LOWR HINGE CUTOUT AT DOOR EXTERNAL SKIN. INSTALLED DOUBLER OF .063 2024-T3 PER EA 62251. (M)SDR USAASB98216Battery Pack · dischargedPHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 21 AND 22 INOP. MIANTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK GOOD. (M)SDR USAASB98208Control Valve · failedDEN - FLT 136 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM DEN. FLIGHT RETURNED TO FIELD AT DEN AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK FLOW CONTROL VALVE. OPERATIONAL CSDR USAASB98207Air Distr · odorCLT - FLT 1267 - ON TAKEOFF FROM LGA, CREW NOTICED A STRONG SMELL OF RUBBER BURNING IN THE COCKPIT AND THE CABIN. THERE WERE NO SIGNS OF SMOKE SMELL AND THE APU WAS OFF AT THE TIME. SMELL DISSIPATED ON CLIMB-OUT. FLIGHT CONTINUED ONTO CLT AND LANDED WITHOUTSDR USAA980335Web · damagedCLT - DURING DROP IN CHECK VISUAL AND EDDY CURRENT, FOUND A 40 INCH SQUARE HEAT DAMAGED AREA APU TORQUE BOX UPPER WEB BS 1088 - BS 1121 LBL 40 RBL 40 WEB CENTER. INSTALLED NEW FLOOR WEB SECTION PER SRM 53-80-13. (X)SDR USAA980325Stringer · corrodedCLT - DURING A PILOTS REPORT READING VISUAL INSPECTION, FOUND A 1 INCH BY .5 INCH CORROSION AREA STATION 1113 AND STATION 1123 RIGHT SIDE TORQUE BOX STRINGER. REPLACED WITH IDENTICAL PART PER SRM 51-40-02 AND BAC DRAWING 6546579. (M)SDR USAA980324Stringer · damagedCLT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH WARPED AREA HEAT DAMAGE STATION 1100 APU TORQUE BOX STRINGER. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)SDR USAA980323Stringer · damagedCLT - DURING A PILOTS REPORT READING INSPECTION, FOUND A 1 INCH BY 1 INCH WARP AREA STRINGER STATION 1100. REPLACED WITH IDENTICAL PART PER BAC DRAWING 65-46579. (M)SDR USAA980322Stringer · corrodedCLT - DURING A PILOT'S REPORT READING INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION. REPLACED WITH IDENTICAL PART PER BAC DRAWING 65-46579. (X)SDR USAA980321Angle · damagedCLT - DURING A PILOT'S REPORT READING VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH WARP. SPLICED IN NEW SECTION OF CHORD ANGLE PER SRM 53-80-13 AND BAC DRAWING 65-46579. (X)SDR USAASB98196Battery Pack · dischargedIAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR SWAA981504Skin · gougedDURING SCHEDULED TRAN CHECK, FOUND L/E GAUGED AT NR 4 SLAT TAI CUTOUT. REPAIRED INTERNAL AND EXTERNAL SURFACES PER BOEING SRM.SDR SWAA981486Clip · damagedDURING SCHEDULED TRAN CHECK, FOUND FRAME WITH 2 CLIPS ELONGATED HOLES LBL 20 AND 26. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981485Skin · delaminatedDURING SCHEDULED TRAN CHECK, FOUND DELAMINATED RT HORIZ STAB UPPER SURFACE O/B T/E PANEL. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981484Frame · damagedDURING SCHEDULED TRAN CHECK, FOUND DAMAGE AT FASTENER HOLES ON BS 1006 FRAME BL 0 BETWEEN STR 27L TO 27R. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981483Skin · crackedDURING SCHEDULED TRAN CHECK, FOUND EXTERNAL FUSELAGE SKIN GOUGED AT BS 1032 STR 9L. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981482Shear Tie · crackedDURING SCHEDULED TRAN CHECK, FOUND CRACKED SHEAR TIE AT BS 1006 LBL 6 TO LBL 8 AFT BAY BETWEEN STR 27 RT AND 27 LT. REMOVED AND REPLACED PER BOEING SRM.SDR USAASB98195Battery Pack · dischargedROC - MAINTENANCE FOUND ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1132 FAIL AFTER 10-15 SECONDS OF OPERATION. ALSO FOUND THE AISLE BULLNOSE EMERGENCY LIGHT AT STATION 590L INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY M11SDR SWAA981407Web · misdrilledDURING SCHEDULED TRANSITION CHECK, FOUND PREVIOUSLY PLUGED HOLE IN WEB AT BS 279 WL 192 LBL 16. REPAIRED PER BOEING MM.SDR SWAA981406Angle · damagedDURING SCHEDULED TRANSITION CHECK, FOUND ANGLE BS 1000, RBL 45, WL 208 HAS ELONGATED FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.SDR F3LA98140Beam · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON LT MAIN LANDING GEAR BEAM LOWER SURFACE AND DAMAGED PANEL MOUNT HOLE OUTBOARD OF STABILIZER LINK MOUNT POINT. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM 51-20-10 AND ESDR F3LA98139Strap · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON STRAP UNDER UPPER ANGLE OF FRAME AT BS 847, RBL 14-30. MAINTENANCE REMOVED AND REPLACED STRAP PER SRM 51-40-2 AND 53-00-07. (M)SDR F3LA98138Frame · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR FRAME, BS 794.5, RBL 24. MAINTENANCE REMOVED CORROSION (4.5 INCH BY 39 INCH) AND REMOVED AND REPLACED FRAME FROM STRINGER 16R TO 27R PER SRM 53-60-15, SRM 51-40-2, SB 737-53-1096, AND DRAWISDR F3LA98137Fitting · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON RT MAIN LANDING GEAR STABILIZER BEAM AFT FITTING. MAINTENANCE BLENDED CORROSION. REMOVED AND REPLACED BEAM AND AFT FITTING PER OHM 57-41-01 AND MM 32-13-21. (M)SDR F3LA98136Web · crackedPAE - DURING C-CHECK INSPECTION, REPORTED CRACK AND CORROSION ON WEB AROUND FASTENER AT BS 294.5, WL 208, LBL 56. MAINTENANCE REMOVED DAMAGED WEB, FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-01 AND 51-40. (M)SDR F3LA98135Cylinder · corrodedPAE - DURING C-CHECK INSPECTION, REPORTED NOSE LANDING GEAR OUTER CYLINDER THREADS ARE CORRODED AND HAVE SHARP EDGES. MAINTENANCE REPAIRED PER SRM 32-21-58, OHM 20-50-3 AND OHM 20-42-10. (M)SDR USAASB98177Valve · failedCLT - FLT 1065 - AFTER TAKEOFF FROM CLT, THE AUTO PRESSURIZATION SYSTEM FAILED. CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL OPERATION. DECISION WAS MADE TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCSDR SWAA981336Channel · damagedDURING SCHEDULED TRAN CHECK, FOUND HAT CHANNEL AT BS 986.5, WL 208 WITH ELONGATED HOLES LBL 22 TO 36. REPAIRED PER BOEING SRM.
Back to Boeing 737-301