N242US, cancelled Apr 13, 2007
Service difficulty reports · 30
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N242US' AND deregistration_id = 'N242US-2007-04-13' 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 n_number = 'N242US' AND deregistration_id = 'N242US-2007-04-13' 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 RYNA200500028Pump · overheatedNR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEATED, RETURNED TO ACY DUE TO DECREASING A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP, AND SERVICED A-SYSTEM. BOTH SYSTEMS LEAKED AND OPERATIONALLY CHECKED GOOD. REF B737 SDR RYNA200500026Skin · crackedDURING WALKAROUND AFTER FLIGHT A SKIN CRACK AT BS 727B+18" AND JUST ABOVE STRINGER 16L WAS NOTICED. AIRCRAFT FERRIED TO FLIGHTSTAR FOR REPAIR. COMPLIED WITH FUSELAGE SKIN REPAIR AT BS 727B+18" AT STRINGER 16L PER SRM 53-30-3 FIG DETAIL VII.SDR USAASB01266Power Supply · dischargedBWI - THE EMERGENCY LIGHTS FOR THE LAST FIVE SEAT ROWS IN THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)SDR USAA010569Bulkhead · crackedCLT - FOUND PRESSURE WEB WITH CRACKS RANGING IN SIZE FROM .375 INCH TO 1.5 INCH, BS 178, WL 199 TO WL 234 LBL 10.5 TO RBL 10.5. DAMAGE REMOVED, REPAIR FILLERS AND DOUBLER INSTALLED PER EO 5300V153, EA 69712, SRM 53-10-11 FIG 1. (M)SDR USAA010570Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCHES AND 1.25 INCHES, BS 178, LEFT AND RIGHT SIDE CHORD, WL 195. DAMAGED SECTIONS CUTOUT, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157 AND SRM 51-10-02. (M)SDR USAA010571Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1.5 INCHES, BS 178, WL 195, LBL 25 AND RBL 25. REMOVED AND REPLACED INTERCOSTAL. (M)SDR USAA010572Bulkhead · crackedCLT - FOUND WEB CRACKED .250 INCH, BS 178 WL 195.7, LBL 23. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER PER EA 69714 AND SRM 53-10-11 FIG 2. (M)SDR USAA200101173Seal · leakingON CLIMB OUT FROM TPA, A VERY LOUD SQUEAL WAS COMING FROM THE FORWARD ENTRY DOOR. AC WAS PRESSURIZING, NOISE BECAME LOUDER AS AC CLIMBED HIGHER. FLIGHT RETRUNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.MAINTENANCE REMOVED AND REPSDR USAASB00298Duct · crackedLGA-MCO - FLT 2667 - DURING CRUISE, THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE ENGINE POWER WAS REDUCED. THE AIRCRAFT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUTDOWN OCCURRED. MAINSDR USAASB00073Controller · failedIAD - FLT 2808 - ON CLIMB OUT FROM IAD, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED CABIN PRESSURE CONTROLLER FUNCTIONAL TESTSDR USAA000046Skin · crackedSKIN CRACKED AT BS 727 STRINGER 16L AND 15L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)SDR USAA000038Stringer · corrodedSTRINGER 28R CORRODED AT BS 360. REPAIRED PER EA 66136 AND SRM 53-10-3 FIG 1. (M)SDR USAA000037Skin · crackedSKIN CRACKED AT BS 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 34. (M)SDR USAA000036Stringer · corrodedSTRINGER 27L CORRODED AT BS 986.5. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAA000035Skin · crackedSKIN CRACKED AT BS 727 PLUS 13, AND 2 INCHES ABOVE STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 66135. (M)SDR USAASB99116Fan · failedRIC - FLT 517 - EN ROUTE FOR CLT-DCA AT FL250, FLIGHT ATTENDANT REPORTED THAT A PASSENGER SMELLED SMOKE IN THE FIRST THREE ROWS OF CABIN. CAPTAIN TURNED GALLEY POWER OFF AND THE FLIGHT ATTENDANT WENT BACK AND CONFIRMED SMOKE COMING OUT OF THE AIR CONDITIONINGSDR USAA990182Skin · crackedTPA - DURING CX-3 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN SKIN STATION 943 STRINGER 24L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 63860. (M)SDR USAA980137Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 4 INCH BY 4 INCH STATION 908, STRINGER 21L. CUT OUT DAMAGE AND INSTALLED STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA980136Stringer · corrosionINT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES, STA 967 TO STA 987, STR 25R. INSTALLED REPAIR ANGLES AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)SDR USAA980135Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AROUND NUT PLATES STATION 235 BL '0' TO RBL 15 NOSE W/W CEILING TRANSVERSER BEAM. REMOVED AND INSTALLED NEW PREFAB TRANSVERSER BEAM, FABRICATED AND INSTALLED ZEE STRAPS. REPAIRED PER SDR USAA980134Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREAS CORROSION ON STRINGER 24L FROM BS 294.5 TO BS 325.3 STRINGER. INSTALLED DOUBLER REPAIR ANGLE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA980133Stringer · corrodedINT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORROSION STA 1006 STR 26L. INSTALLED REPAIR ANGLES, REPAIRED PER SRM 53-10-3. CORROSION TAKE NR: C53-202-01. CORROSION LEVEL: 2. (X)SDR USAA980132Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 30 INCH STATION 294 TO 325 STRINGER 24L. SPLICED IN NEW STRINGER SECTION, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M)SDR USAASB98015Light · failedCLT - FLT 209 - ON APPROACH INTO CLT, CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE RT MLG. CREW TESTED LIGHT AND CONFIRMED THE LIGHT WAS OPERATIONAL. CREW RECYCLED THE GEAR AND AGAIN RECEIVED NO DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEARSDR USAA980010Stringer · corrodedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BSL 967. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAA980009Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 767 STRINGER 19R FUSELAGE SKIN. REMOVED CRACKED SKIN AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)SDR USAASB97125Wire · brokenCMH - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 11 INOP. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT SOCKET. OPS CHECK GOOD. (M)SDR USAA960404Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CORROSION ON STRINGER, FORWARD OF AFT PRESSURE BULKHEAD STRINGER 26R BS 1016. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR USAASB96012Pressurization · lostFLT NR 818 - PIT - FLIGHT DIVERTED DUE TO LOSS OF PRESSURIZATION. (M)SDR USAA950194Switch · failedJAX - FLT 1606 - ON CLIMB NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDED THROTTLE AND LIGHT WENT OUT. FLIGHT DIVERTED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. REPLACED RIGHT MAIN OIL FILTER BYPASS SWITCH AND RIGHT MAIN OIL SCREEN. (W)
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