JASC 7240
Service difficulty reports · 509
Reports filed under 7240 · Turbine Engine Combustion Section, 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 jasc_code = '7240' 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 jasc_code = '7240' 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 CA060117002Duct · failedL14TH DUCT MSG ON DESCENT. ACTIONED CHECKLIST AND SHUTDOWN ENGINE. CHANGED DETECTOR ELEMENT A59WK. OP TEST CARRIED OUT IAW AMM SERV.SDR CA060112001Combustion Case · crackedCREW REPORTED ABNORMALLY HIGH TOT ON NR 1 ENGINE. INVESTIGATION REVEALED A CRACK IN THE RT ARMPIT AREA OF THE OUTER COMBUSTION CASE. THE OUTER COMBUSTION CASE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR SWAA053741Combust Chamber · crackedDURING SCHEDULED HC1 CHECK, FOUND NR 1 ENGINE, NR 8 FUEL NOZZLE BELOW IGNITER HOLE SECONDARY SWIRL NOZZLE VENTURI AREA OF MATERIAL CRACKED AND MISSING. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR CA051025005Combustion Case · cracked(CAN) AIRCRAFT TOT WAS RUNNING HIGH, N1 WAS ABOUT 91 PERCENT. BARFIELDED GAUGE, FOUND TO BE CORRECT. CHECKED THERMOCOUPLE RESISTANCE, ALSO FOUND TO BE WITH IN LIMITS. CHECKED ARM PIT'S WITH FINGER, FELT OKAY. CHECKED WITH MIRROR, FOUND CRACK THROUGH MESH ON SDR C2XA05IA118Turbine Blades · failedIAH - FLIGHT 2010, THE CREW REPORTED AN UNCOMMANDED ENGINE SHUT DOWN IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WASSDR 2006FA0000115Combust Chamber · crackedDURING AN INSPECTION FOR HIGH TOT THE OUTER COMBUSTION CAN WAS FOUND TO BE CRACKED IN THE LEFT (ARM PIT). (K)SDR 2005FA0001432Liner · burnedTHE CORE MAJOR MODULE 02X31733 FOR COMBUSTOR DISTRESS. THIS WAS CONFIRMED ON EXPOSURE, WHERE SIDNIFICANT BURNING AND BURN-THROUGH ON THE OUTER LINER WAS SEEN IN LINE WITH FUEL NOZZLE NR 15. THE COMBUSTION CHAMBER WAS PREVIOUSLY REPAIRED AND IS WITH MFG FOR ISDR 2005FA0001345Liner · destroyedTHE CORE MAJOR MODULE 02 X 31733 WAS REMOVED FROM ESN 731433 FOR COMBUSTOR DISTRESS. THIS WAS CONFIRMED ON EXPOSURE AT REPAIR STATION, WHERE SIGNIFICANT BURNING AND BURN THROUGH ON THE OUTER LINER WAS SEEN IN LINE WITH FUEL NOZZLE N-DEGREE 15. THE COMBUSTIONSDR CA050810003Combustion Liner · cracked(CAN) THE PILOT WAS EXPERIENCING HIGH TOT (WITHIN FLIGHT MANUAL LIMITATION) AND REPORTED THAT THE AIRCRAFT WAS FAILING THE POWER CHECK. THE ENGINEER VISUALLY INSPECTED THE ENGINE FOR DISCREPENCIES AND FOUND A 2 INCH CRACK IN THE ARM PIT OF THE OUTER COMBUSTIONSDR CA050726004Case · crackedDURING A SCHEDULED HOT SECTION INSPECTION, A CRACK WAS FOUND IN THE CASE WHERE THE FUEL NOZZLE SUPPORT IS LOCATED AT THE FIVE O`CLOCK POSITION. THE CRACK WAS RUNNING FROM THE EDGE OF THE NOZZLE DOUBLER PLATE TOWARDS THE RT IGNITER WELD.SDR ASMF200507006Combust Chamber · damagedDURING LT ENGINE BOROSCOPIC INSPECTION, DETECTED COMBUSTION CHAMBER DAMAGED WITH 2 AXIAL CRACKS INTERSECTED WITH CIRCUMFERENTIAL CRACK OUT LIMITS. LT ENGINE REPLACED AND TESTED IAW MM 71-00-02 AND MM 71-00-00, RESPECTIVELY. ALL CORRECT.SDR ALGA101180Shroud · defectiveFUEL NOZZLE REMOVED FOR STARTING PROBLEM. HOUSING UNSCREWED FROM SHROUD. SHROUD STAYED IN LINER FERRULE. DIMENSIONALLY CHECKED LINER FOUND TOO SMALL AND TAPERED CAUSING INTERFERENCE FIT. REPLACED WITH SERVICEABLE LINER.SDR KBM2005F00084Combust Chamber · crackedCOMBUSTION CAN, CRACKED ON LEFT SIDE. REMOVED AND REPLACED. (K)SDR CA050328002Combustion Liner · cracked(CAN) COMBUSTION LINER FOUND CRACKED WHEN REMOVED DURING UNRELATED SCHEDULED MAINTENANCE. NO CRACKS ALLOWED IN SUBJECT AREA. THIS IS AN ON GOING PROBLEM WITH THIS PART.SDR CA050321009Combustion Liner · cracked(CAN) 3 INCH BURN THROUGH INNER LINER IN COMBUSTION AREA. ONE SMALL PINHOLE THROUGH PRIMARY SHROUD OR CAP. THE CAP ON THE AFT FACE OF THE UNIT HAD CRACKED ABOUT 120 DEGREES AROUND THE CIRCUMFERENCE. THE BURN THROUGH WAS VISIBLE WITH THE BOROSCOPE INSPECTION SDR CA050321006Plenum · cracked(CAN) WHILE CONDUCTING AN ENGINE INSPECTION, A 2 INCH CRACK WAS DISCOVERED ON THE PLENUM NEAR THE BLEED AIR OUTLET. THE ENGINE WAS REMOVED AND THE CRACKED PART REPLACED. A FLEET WIDE ENGINE INSPECTION OF THE SAME DEFECT WAS CARRIED OUT. NO OTHER DEFECTS FOUSDR CA050222003Combustion Liner · cracked(CAN) PART CRACKED IN DOUBLE LIP AREA. NO CRACKS ALLOWED IN THIS LOCATION. MAJORITY OF COMBUSTION LINERS REMOVED ARE FOUND CRACKED IN THIS AREA.SDR CA041221002Combust Chamber · cracked(CAN) DURING CLIMB THE ENG EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY AUTO-FEATHER. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A FRACTURED COMBUSTOR SMALL EXIT DUCT AND ASSOCIATED CT BLADE AND VANE DAMAGE.SDR CA041129017Combustion Liner · cracked(CAN) THE PILOTS WERE DOING TRAINING, THEY NOTICED AN INCREASE IN TOT. DID A POWER CHECK AND FOUND THAT THE ENGINE WAS BELOW SPEC. AIRCRAFT RETURNED TO BASE AND IT WAS DISCOVERED THAT THE THERE WAS A 1 INCH CRACK THAT FOLLOWED A WELD IN THE E ARM PIT AREA. NSDR DL76L040861Combust Chamber · crackedENGINE FAILED BORO OP 5067 COMBUSTION CHAMBER LINER CRACKED. REPLACED ENGINE.SDR CA040816004Combustion Liner · cracked(CAN) CRACK FOUND DURING REMOVAL FOR UNRELATED SCHEDULED MAINTENANCE.SDR JJWA0055791Combust Chamber · crackedNOTICE HIT TOT ON A NORMALLY COOL RUNNING TURBINE, OVER A PERIOD OF A FEW FLIGHTS TOT CLIMBED MORE. PERFORMED NORMAL BARFIELD TOT TESTING AND BLEED VALVE CLOSURE TESTS, THEN DID THE HAND FEEL TEST DURING START AND IDLE AND FOUND AIR LEAKAGE AT LEFT AFT AIR TUSDR CA040816007Combustion Liner · cracked(CAN) CRACK FOUND IN COMBUSTION LINER WHEN REMOVED FOR TURBINE INSPECTION. NO CRACKS ALLOWED IN THIS AREA.SDR CA040816005Combustion Liner · cracked(CAN) COMBUSTION LINER FOUND CRACKED DURING TURBINE REMOVAL. NO CRACKS ALLOWED IN THIS AREA.SDR CA040217013Combustion Liner · cracked(CAN) THE LT ENGINE WOULD NOT PRODUCE RATED POWER, IN FACT IT ONLY WENT TO 80 PERCENT. THE CREW ABORTED THE TAKEOFF ROLL AND RETURNED TO THE HANGAR. ON INVESTIGATION, A CRACK WAS FOUND ON THE LOWER CENTER OF THE COMBUSTION CASE. THE CRACK GOES AROUND AN UNUSESDR CA040816008Combustion Liner · cracked(CAN) CRACKS FOUND IN OUTER COMBUSTION CASE ARMPIT AREA ON NORMAL DAILY INSPECTION. NO CRACKS ALLOWED IN THIS AREA.SDR CA030612006Case · cracked(CAN) AFTER INPSECTION WITH THE ENGINE RUNNING A LEAK CHECK WAS CARRIED OUT BY PLACING A HAND IN AREA OF THE FUEL NOZZLE AND AIR WAS FELT. THE ENGINE WAS SHUT DOWN AND A CLOSE INSPECTION WAS CARRIED OUT IN THE AREA OF WHERE THE NOZZLE ADAPTER PLATE IS WELDED TSDR CA030612005Case · cracked(CAN) ROUTINE INSPECTON AND CHANGING FUEL NOZZLE IT WAS SUSPECTED THAT THERE WAS A CRACK ALONG THE WELD WHERE THE FUEL NOZZLE ADAPTER IS ATTATCHED TO THE END OF OUTER COMBUSTION CASE. ON CLOSER INSPECTION IT WAS NOTED THAT THE CRACK COVERED OVER HALF OF THE WSDR HEEA087520Case · crackedOUTER COMBUSTION CASE CRACKED. REPLACED CASE.SDR ALGA086239Combustion Liner · cracked.020 INCH GAP BETWEEN AREA (A) AND AREA (B). CRACKS IN DEFLECTOR PLATE.SDR 2003FA0000414Combust Chamber · crackedOUTER COMBUSTION CAN CRACKED 180 DEGREES AROUND FUEL NOZZLE WELD. PRIOR TO CRACK THE ENGINE WAS RATED AS A +22 MGT. THE ENGINE WAS -6 MGT WHEN CRACK WAS DISCOVERED. THE CRACK IS NOT VISIBLE TO THE PILOT DURING PREFLIGHT. AN INSPECTION MIRROR IS REQUIRED TO SESDR CA030404001Combust Chamber · cracked(CAN) WHILE IN CRUISE FLIGHT THE PILOT NOTICED NR 2 ENGINE TOT WAS HIGHER THAN THAT OF NR 1 ENGINE. PILOT ATTEMPTED TO CARRY OUT A POWER CHECK ON NR 2 ENGINE BUT WAS UNABLE TO COMPLETE THE CHECK DUE TO TOT REACHING RED LINE.AIRCRAFT RETURNED TO BASE AND THE AMSDR C2XA03CL079Combustion Liner · wrong part3/25/03 EXPRESS JET AIRLINES WAS NOTIFIED BY ROLLS ROYCE THAT AIRCRAFT 11109, NR 2 ENGINE HAD THE WRONG P/N COMBUSTION LINER INSTALLED AT THE FACTORY. THE AIRCRAFT WAS FERRIED TO CLEVELAND FOR A ENGINE CHANGE. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONALSDR AUS20030266Liner · cracked(AUS) ENGINE COMBUSTION LINER FAULTY. THE LINER WAS NOT CLEAN SO IT WOULD HAVE BEEN DIFFICULT TO ASCERTAIN SERVICEABILITY A POSSIBLE CRACKED WELD APPROXIMATELY 75MM (2.95IN) LONG RUNNING FROM THE 6 O'CLOCK TO THE 8 O'CLOCK POSITION. ONE CRACK APPROXIMATELY SDR HEEA085046Combustion Liner · damagedCOMBUSTION CASE HAS STRIPPED THREADS IN IGNITER BOSS. REPAIRED.SDR ALGA084097Combust Chamber · crackedCRACKED. EXCESSIVE CORROSION ON ARMPIT AT PATCH AREA, POSSIBLY CAUSED BY BRAZE FILLER MATERIAL. CRACK FOLLOWS WELD SEAM AND EXTENDS INTO PATCH. SCRAPPED PART. HOLDING FOR FINAL DISPOSITION.SDR HEEA083759Case · crackedFUEL NOZZLE BOSS CRACKED. REPLACED WITH SERVICEABLE CASE.SDR HEEA083757Case · damagedIGNITER BOSS HAS STRIPPED THREADS. REPAIRED.SDR HEEA083644Valve · stickingBURNER DRAIN VALVE STICKING. REPAIRED.SDR C2XA02CL227Combustion Liner · crackedCLE FLIGHT#3280 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT AFTER TAKEOFF FROM CLEVELAND.THE ODOR WAS NOTED WHEN THE PACKS WERE OPERATED FROM THE ENGINE BLEED.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED SDR 2002FA0001286Seal · crackedSEAL REJECTED FOR CRACK AT 1 PLACE ON BACK WALL OF THE PILOT GROOVE SEAL AS MARKED ON THE PART.SDR 2002FA0001287Seal · crackedSEAL REJECTED AT FPI FOR VOID WITH LINEAR INDICATION ON SEAL LAND EXCEEDING 3X1 LIMIT.SDR GTIA021071Combust Chamber · wornBOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE IGNITER PORT NR 4. BURNER CANS HAVE BEEN REPACED DURING SHOP VISIT.SDR XNOA01066Case · damagedNR 2 ENGINE FIRE WARNING AFTER TAKEOFF. AFTER PULLING THROTTLE TO IDLE, INDICATION WENT OUT. ELECTED TO RETURN FOR OVERWEIGHT LANDING. T/S AND FOUND NR 12 LP FUEL NOZZLE FLANGE BURN HOLE IN ENG CASE. REPLACE NR 2 ENG ASSY PER ENA AMM A300-71-00-00 PERFORMESDR EOO2002F0000ACombust Chamber · crackedAIRCRAFT SUDDENLY STARTED TO RUN HOT, SUBSEQUENT POWER CHECK SHOWED ENGINE RUNNING 75 DEGREE C, HOTTER THAN PREVIOUS POWER CHECK TWO DAYS BEFORE. AIRCRAFT LANDED AND ON INSPECTION IT WAS FOUND THAT THE OUTER COMBUSTION CAN WAS CRACKED IN THE ARMPIT AREA.SDR CA020829009Case · cracked(CAN) ENGINE ASSEMBLY HAD HIGH TOT. UPON INSPECTION ENGINEER DISCOVERED CRACK IN ARMPIT AREA.SDR CA020903002Fuel Nozzle · failed(CAN) AT TERMINATING A ROUTINE 7 DAYS INSPECTION ON THE AIRCRAFT, THE MECHANIC SPOTTED A ROUND DISCOLOURED 'DOT' ON THE ENGINE CASING, TWO FUEL NOZZLES WERE REMOVED TO INVESTIGATE WITH A BORESCOPE TO CONFIR M APPARENT DAMAGE IN THE FUEL COMBUSTION LINER. ENGINSDR HEEA080638Drain Valve · corrodedENGINE BURNER DRAIN VALVE WILL NOT CLOSE - CORROSION. REPAIRED.SDR SWAA021567Engine · overtempAIR TURN BACK, NR 2 ENG EGT IND OVERTEMP, (965 DEGREES FOR 1 SECOND). COMPLIED WITH ENG BOROSCOPE INSPECTION AND PWR ASSURANCE RUN. NO DAMAGE NOTED. OPS CK GOOD PER MM. MAINTENANCE FERRY TO PHX AND REMOVED AND REPLACED NR 2 ENG PER MM.SDR R7MR35576Liner · crackedCOMBUSTION CHAMBER LINER, CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
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