Boeing 737-201
Service difficulty reports · 2,471
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 = '737201' 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 = '737201' 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 USAASB98220Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE FORWARD PASSENGER ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98217Indicator · malfunctionedTYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINESDR 98ZZZM819Transmitter · malfunctionedTYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINESDR USAASB98212Oil Cooler · failedBWI - FLT 2662 - UPON CLIMB-OUT FROM BWI, THE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND AT FL 160. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. TEMPERATURE REMAINED IN YELLOW BAND FOR 12 MINUTES THEN WENT TO THE EDGE OF GRSDR USAASB98215Battery Pack · dischargedPHL - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR F3LA98161Pressure Blkhd · crackedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 7 INCH/8 INCH CRACK IN NOSE WHEEL WELL PRESSURE WEB. OUTBOARD RT SIDE AFT OF DOWNLOCK VIEWER. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER SRM 51-40-2, FIG 1. CYCLES: 1,199. (X)SDR USAASB98203Fire Loop · failedPIT - FLT 278 - AIRCRAFT WAS RELEASED WITH THE NR 1 ENGINE GENERATOR ON MEL. WHILE EN ROUTE FROM PHL TO DTW, THE APU FIRE WARNING DETECTOR LIGHT ILLUMINATED NECESSITATING AN APU SHUTDOWN. WITH ONLY ONE ELECTRICAL POWER SOURCE REMAINING, FLIGHT DIVERTED TO NESDR F3LA98144Battery Pack · dischargedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY. (X)SDR USAA980314Skin · crackedCLT - DURING VISUAL CHECK INSPECTION, FOUND A 2.25 INCH CRACK AT BS 767 AND STR 19R ON SKIN. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (X)SDR USAASB98182Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT SERVICE DOOR INOP DURING THE TRANSIT CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98180Light · inoperativeALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT IN THE COCKPIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB98179Switch · failedBOS - FLT 921 - ON CLIMB-OUT FROM BOS, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS BROUGHT BACK TO IDLE AND AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS SHUT DOWN AFTER LANDISDR USAA980262Skin · crackedPHL - DURING RON, FOUND SMALL 1 INCH CRACK VERIFIED BY DYE CHECK ON SKIN ABOVE STR 18R AND STA 757 JUST AFT OF WING-TO-BODY FAIRING. INSTALLED EXTERNAL REPAIR PER SRM 53-30-3. (X)SDR USAASB98175Battery Pack · dischargedALB - MAINTENANCE FOUND THE AFT ENTRY AND AFT SERVICE DOOR EXTERIOR EVACUATION LIGHTS AND THE INTERIOR SIDEWALL EMERGENCY EXIT SIGNS BY EACH DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE RIGHT SIDE OF THE AFT CARGO COMPARTMENT BEHIND THESDR USAA980299Skin · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSELAGE SKIN 1 INCH FORWARD OF BS 727B .5 INCH ABOVE STRINGE R16R. INSTALLED EXTERNAL REPAIR DOUBLER PER EA 62067. (M)SDR USAASB98172Battery Pack · dischargedALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY EVACUATION LIGHTS INOP, LEFT OVERWING EXIT HATCH SIDEWALL EXIT LIGHT, THE LEFT OUTSIDE EXIT HATCH WING LIGHT AND THE LEFT GRUOND ILLUMINATION LIGHTS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT SDR USAASB98167Seal · out of positionPIT - FLT 856 - AFTER TAKEOFF FROM PIT, AIRCRAFT FAILED TO PRESSURIZE. A LOUD AIR NOISE WAS HEARD COMING FROM DOOR R1. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE-INSTALLED THE R1 DOOR SEAL AND SECURED THE SERVICE DOOR. PRESSSDR USAASB98166Oven · overheatedPGV - FLT 1077 - AT FL 350 EN ROUTE TO JAX FROM LGA, THE FORWARD GALLEY OVEN CAUGHT FIRE. THE FLIGHT ATTENDANT USED A FIRE EXTINGUISHER AND PUT OUT THE FIRE. THIRTY MINUTES LATER THE FIRE RESTARTED AND SMOKE ENTERED THE COCKPIT. CAPTAIN DECLARED AN EMERGENCSDR USAASB98163Shut Off Valve · failedPIT - FLT 296 - CREW ADVISED VIA ACARS WERE ENCOUNTERING PROBLEMS WITH THE DUCT PRESSURES. AT CLIMB POWER, THE LEFT DUCT PRESSURE READS 80 PSI WHILE THE RIGHT READS 38 PSI. THE DECISIION WAS MADE TO DIVERT TO PIT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LASDR USAASB98161Harness · failedSAV - FLT 2238 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE GENERATOR DROPPED OFF LINE. AFTER LEVELING OFF, THE CREW TRIED TO PUT THE GENERATOR BACK ON LINE BUT WAS NOT SUCCESSFUL. THE NR 1 ENGINE CSD WAS ALREADY ON MEL AND WITH THE APU BEING THE ONLY SOURCE OF SDR USAASB98160Adc · failedCLT - FLT 8036 - DURING CRUISE, CREW REPORTED A TOTAL NR 1 AIR DATA COMPUTER FAILURE. CREW PULLED AND RESET RN 1 CADC CIRCUIT BREAKERS. SYSTEM RESETS, THEN FAILS AGAIN. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SDR USAASB98159Hydraulic Line · leakingBOS - FLT 354 - AFTER TAKEOFF FROM BOS, CREW RECEIVED A NOSE LANDING GEAR RED LIGHT ALONG WITH A VIBRATION. CREW DECIDED TO RETURN TO FIELD TO BOS. RECEIVED THREE GEAR GREEN LIGHTS WHEN GEAR WAS LOWERED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYSDR USAASB98156Switch · failedPHL - FLT 452 - ON CLIMB-OUT FROM PHL, AT APPROX 5,000 FT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. LIGHT REMAINED ON WHEN POWER WAS REDUCED TO IDLE THRUST ON THE NR 1 ENGINE. CREW SHUTDOWN THE NR 1 ENGINE IN FLIGHT AND RETURNED TO FIELD AT PHL WSDR USAASB98154Battery Pack · dischargedCMH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA980281Angle · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727 RBL 6.5 ATTACH ANGLE. REPAIRED PER SRM 51-10-1. (M)SDR USAA980280Beam · frettedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCH FRETTED AREA BETWEEN BS 663-727 BEAM. INSTALLED REPAIR STRAP AND REPAIRED PER EA 44092. (M)SDR USAA980297Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1.3750 INCH AREA OF CORROSION ON FLOORBEAM STA 106 LBL 18. INSTALLED T-CAP PER TR 53-10-05C. (X)SDR USAASB98153Engine · overtempPIT - FLT 1894 - AFTER TAKEOFF FROM PIT, THE NR 1 ENGINE ENCOUNTERED HIGH OIL TEMPERATURE. FLT RETURNED TO FIELD AT PIT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ENGINE WAS NOT SHUT DOWN IN FLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ESDR USAA980259Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .0625 INCH LONG FORWARD ENTRY DOOR SKIN SCUFF PLATE. INSTALLED REPAIR DOUBLERS AND TRIPLER, REPAIRED PER EA 44026 AND BOEING DRWING 65C27257. (M)SDR USAA980258Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 344 STRINGER 27R FRAME. INSTALLED REPAIR DOUBLER AND FILLER, REPAIRED PER SRM 51-40-3 FIG 1. (M)SDR USAA980257Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION,K FOUND 3 INCH CRACK IN FUSELAGE FRAME BS 747 BETWEEN STRINGER 13/14L. INSTALLED FRAME REPAIR AND REPAIR PER SRM 53-40-4. (M)SDR USAA980256Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION FOUND CRACK .25 INCH LONG STATION 722 TO 725 BL '0' LONGITUDINAL FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 AND BOEING DRAWING 65C34537. (M)SDR USAA980255Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK STATION 707 TO 714 LBL 25 INCHES LONGITUDIAL FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA980254Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BL '0' AT BS 661 FLOORBEAM. INSTALLED REPAIR ANGLES, REPAIRED PER BOEING REPAIR DRAWING 65C34537. (M)SDR USAA980253Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 707-714 25 INCH RBL WL 203.5 LONGITUDIAL FLOORBEAM WEB. CUTOUT CRACKED AREA AND INSTALLED WEB REPAIR, REPAIRED SRM 51-40-2. (M)SDR USAA980252Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER 8R STATION 365, 1 INCH BY 3 INCH. SPLICES IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-2 FIG 3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA980251Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 358-360 UPPER SIDE OF STRINGER 27L. INSTALLED NEW SPLICE ANGLE AND REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-202-02, CORROSION LEVEL 2. (M)SDR USAA980250Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 A PLUS 7 INCH STRINGER 17R SKIN. INSTALLED DOUBLERS, REPAIRED PER SRM 53-30-3. (M)SDR USAA980249Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 378 BL '0' SKIN. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 53-30-04. (M)SDR USAA980248Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 7R AND STRINGER 5R BS 460-480, .75 INCH BY 2 INCH. INSTALLED STRINGER REPAIRS AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA980247Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS .25 INCH BY .25 INCH EACH STRINGER 3R BS 440 TO BS 460. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA980246Stringer · corrodedINT - DURING Q-5 CEHCK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER STATION 425 TO 470 STRINGER 4R, 2 INCH BY 1.5 INCH. REMOVED AND REPLACED STRINGER 4R FROM 425-470, REPAIRED PER SRM 53-10-3 FIG 3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. SDR USAA980245Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER STATION 420-440 STRINGER 7R, 1 FT BY 3 INCH. REMOVED AND REPLACED STRINGER 7R FROM STRINGER 420-440. (M)SDR USAA980244Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORRSION ON STRINGER STATION 410-463 STRINGER 3R, .5 INCH BY 1.0625. REMOVED AND REPLACED STRINGER 3R FROM STATION 410-463, REPAIRED PER SRM 53-10-3 FIG 3. CORROSION TASK NR C-53-107-01, CORROSION LEVELSDR USAA980243Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK RIGHT FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTALLED EXTERNAL DOUBLER, REPAIRED DRAWING 65C27287 AND TYPICAL REPAIR 53-10-19 REV A. (M)SDR USAA980242Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA TWO PLACES BS 304, STRINGER 25L, BS 286.5, STRINGER 25L STRINGER. INSTALLED STRINGER SPLICE BS 304 AND 286.5 STRINGER 25L, REPAIRED PER SRM 53-10-3 FIG 1 SHEET 8. CORROSION TASK NSDR USAA980241Stringer · crackedINT - DURING Q-5 CHECK VISUAL (HFEC) INSPECTION, FOUND 3 CRACKS 3 FASTENERS HOLES CRACKED APPROX .125 INCH EACH, BS 320-BS 336, STRINGER 20 STRINGER. SPLICED IN NEW SECTION OF STRINGER, SRM 53-10-3 FIG 1. (M)SDR F3LA98080Gcu · failedPHX - FLT 429 - DURING DESCENT INTO PHX, FLIGHT CREW REPORTED NR 1 GENERATOR OFF BUS LIGHT ILLUMINATED FOLLOWED BY THE SMELL OF ELECTRICAL SMOKE WITH A SMALL AMOUNT OF VISIBLE SMOKE NOTICED. COMPLIED WITH SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. AIRCRAFSDR USAA980265Skin · crackedPHL - DURING RON FOUND 2 INCH CRACK IN FUSELAGE SKIN RIGHT SIDE BETWEEN STATION 400 AND STATION 420 BETWEEN STRINGER 23RT AND 24RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)SDR USAA980264Skin · crackedPHL - DURING RON, FOUND 2 CRACKS, IN EACH LONG RIGHT SIDE FUSELAGE SKIN BETWEEN STATION 797 AND 767 BETWEEN STRINGER 18RT AND 19RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)
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