JASC 7230
Service difficulty reports · 5,064
Reports filed under 7230 · Turbine Engine Compressor 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 = '7230' 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 = '7230' 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 ASAA2019052729490Pin · migrated#1 ENGINE 3RD STAGE ANTI ROTATION SLAB HEADED PIN AT 9 OCLOCK ALF HAS ROTATED 90 DEGREES AND HAS STARTED TO MIGRATE. REF T/C SBCFM56-7B-72-0986-1. PHOTOS IN INSPECTION SERVER REF L/P 11759592, 3RD STAGE AT 3 OCLOCK , ANTI ROTATION REMAINS ROTATED LESS THAN 45 SDR CA190607003Bearing · failed(CAN) CUSTOMER REPORTED THAT THE LEFT HAND ENGINE WAS SHUT DOWN IN FLIGHT AFTER THE CREW HEARD A LOUD NOISE WITHOUT ENGINE ALARM. SMOKE WAS OBSERVED AT THE STATION AND IN THE CABIN. (TC# 20190607003)SDR ASAA2019052529491Seal · missingWHILE ACCOMPLISHING TC 78472010 ON ENGINE #1 FOUND TWO PLATFORMS #14 AND #21 MISSING PLATFORM SEAL ON ONE SIDE. GROUNDED - YES. REMOVED AND REPLACED #14 AND #21 PLATFORMS ON #1 ENG PER T/C 78472010. REF T/C FOR WORK ACCOMPLISHED.SDR ASAA2019052529489Spacer · debondedWHILE ACCOMPLISHING TC 78472010 FAN BLADE LUBE, FOUND OVER NINE SPACERS DISBONDED ON ENGINE #1. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SPACERS ON #1 ENG. PER T/C 78472010. REF T/C FOR WORK ACCOMPLISHED.SDR WI5R2019052200001Rotor · fracturedAPPROXIMATELY 30 MINUTES INTO A 2.5 HOUR FLIGHT, A LOUD BANG WAS REPORTED. FIELD BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. REPAIR STATION DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD SDR ASAA2019051929390Compressor Blade · wornREF T/C 78472010 FAN BLADE LUBRICATION #2 ENG SUBTASK 839-032 BLADES #5 & #11 CU-NI-IN COATING MISSING BEYOND AREA X. GROUNDED - YES. ADDITIONAL PARTS RECORDED ON MIG2A-11960055. REMOVED & REPLACED 3 PAIRS OF FAN BLADES ON #2 ENG. REF AMM 72-21-02 AND TASKCARDSDR ASAA2019051829388Spacer · debonded#2 ENG FAN BLADE #1 SPACER DISBONDED. GROUNDED - YES. REPLACED #2 ENG FAN BLADE SPACER #1 PER T/C 78472010.SDR AALA201905199024Manifold · failedAIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF #2 ENGINE OIL QUANTITY AND OIL PRESSURE LOSS. RT ENGINE WAS SHUT DOWN. FLIGHT DIVERTED TO OPO. AFTER 3 HOURS OF FLIGHT, OIL QTY INDICATED 11, AN HOUR LATER INDICATED 8 AND THEN CONTINUED DOWN OVER TSDR AALA201905159017Compressor Blade · damagedAIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF AT 40-60 KNOTS DUE TO ENGINE ONE COMPRESSOR STALL. NO INJURIES REPORTED. FLIGHT RETURNED TO GATE FOR MAINTENANCE INSPECTION. MAINTENANCE ACCOMPLISHED BORESCOPE OF THE ENGINE AND FOUND DAMAGE TO THE 6TH AND 7TH STAGSDR ASAA2019051429337Spacer · debondedNR 1 ENGINE, SPACERS 19, 21, 24 ELASTOMER DISBONDED AT 2 LOCATIONS REF T/C 78472010. GROUNDED - YES. REPLACED NR 1 ENG SPACERS 19, 21 AND 24 PER T/C 78472010.SDR CA190524003Housing · damaged(CAN) DURING TAKE-OFF ROLL CREW NOTICED ENGINE HIGH ITT AT RED BAND. AIRCRAFT RETURNED TO ITS ORIGINAL DEPARTURE AND LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING. (TC# 20190524003)SDR ASAA2019051329322Shim · wornNR 1 ENGINE ESN 894137 TC 78472010 FOUND ALL FAN BLADE SHIMS WORN OUT OF LIMITS AMM TASK 72-21-02-200-801-F00. GROUNDED - YES. REPLACED ALL FAN BLADE SHIMS. REF T/C 78472010.SDR ASAA2019051329320Blade · wornNR 1 ENGINE ESN 894137 TC 78472010 FOUND SIX FAN BLADES FAILED INSPECTION FOR CUNI MISSING. POSITIONS 2, 3, 8, 14, 15 AND 20. GROUNDED - YES. REPLACED 6 EA. BLADES. REF T/C #78472010.SDR AALA201905139001Compressor Blade · damagedAIRRAFT WAS GROUNDED: PILOT ABORTED TAKEOFF DUE TO RIGHT ENGINE POPING AND FLAMES. SUSPECT RIGHT ENGINE COMPRESSOR STALL. ABORT AT 50 KTS. MAINTENANCE ACCOMPLISHED A BORESCOPE OF THE ENGINE AND FOUND SOME DAMAGED COMPRESSOR BLADES. AN ENGINE CHANGE HAS BEEN DSDR CA190718005Engine · failed(CAN) SHORTLY AFTER TAKEOFF THE RH ENGINE EXPERIENCED A SUDDEN LOSS OF POWER ALONG WITH A VIBRATION. THE ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER ISSUES. A QUICK INSPECTION THROUGH THE EXHAUST DETERMINED THSDR CA190524002Carbon Seal · leaking(CAN) CUSTOMER REPORTED THAT DURING CLIMB WET-SOCKS SMELL IN COCKPIT. THE PILOT ELECTED TO RETURN BACK TO THE AIRPORT AND LANDED. ALTHOUGH OXYGEN MASKS WERE USED, THERE IS NO REPORT OF CREW OR ANY PERSONNEL REQUIRING MEDICAL ATTENTION. AFTER TROUBLESHOOTING, ISDR ASAA2019050829271Blade · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 2 ENG. T/C 78472010, FOUND BLADE NR 12 WITH MISSING CU-NI-IN COATING BEYOND LIMITS. GROUNDED - YES. NR 2 ENG S/N 658831, FAN BLADES NR 12 AND NR 24 REPLACED DURING ACCOMPLISHMENT OF T/C 78472010 ON W/O # 443954.SDR ASAA2019050629256Spacer · debondedPER T/C 78472010 NR 2 ENGINE FAN LUBE SPACERS NR 3,5,8,910,11,13,14,16,17,18,19,20,21,22,23, AND 24 ELASTOMER STRIPS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE FAN LUBE SPACERS NR3,5,8,9,10,11,13,14,16,17,18,19,20,21,22,23, AND 24 ELASTOMER STSDR SWIA2019050645828Pin · defectiveENGINE 1 N1 VIBRATION. AT CRUISE, MOVED THROTTLES FROM CLIMB TO CRUISE RANGE. N1 VIBRATION INCREASED TO 2.1 WITH NOTICEABLE VIBRATION CHANGE AND SOUND. CONTINUED TO DECREASE POWER UNTIL VIBRATION IN NORMAL RANGE. ENGINE VIBRATION WOULD THEN INCREASE AGAIN INTOSDR WI5R2019050300000Rotor · fracturedDURING TROUBLE SHOOTING FOR ELEVATED ITT TRENDS, A BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE DETERMINED THERE WERE TWO MISSING 3RD STAGE IP BLADES.SDR ASAA2019043029205Blade · damagedNR 2 ENG NR 10 FAN BLADE ROOT AT CONCAVE SIDE HAS CUNI COATING DAMAGE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED BOTH NR 10 AND NR 22 FAN BLADES IN CONJUNCTION WITH FAN BLADE LUBRICATION. REF T/C FOR WORK ACCOMPLISHED AND VIB SURVEY.SDR MASA2019043011835Compressor · odorSMOKE IN LAVATORY MESSAGE IN FLIGHT. PERFORMED RH ENG COMPRESSOR RINSESDR CA190503003Packing · leaking(CAN) CUSTOMER REPORTED THAT DURING FLIGHT PILOT HAD A HEADACHE DUE TO OIL SMELL IN THE CABIN. ON TROUBLESHOOTING NOTICED OIL WETNESS WAS FOUND AROUND THE #5 BEARING HOUSING AREA ON #1 ENGINE. FURTHER TROUBLESHOOTING IS GOING ON. (TC# 20190503003)SDR QEMY202001230001Spool · crackedWHILE AT THE GE AVIATION WALES ENGINE SHOP AT THE INSPECTION PROCESS A JAL GE90-94B, ESN 900455, HPC 8-10 SPOOL HAS FAILED ECI. THE SPOOL WAS FITTED NEW AT LAST SHOP VISIT. THE SPOOL HAS BEEN RETURNED TO THE OEM FOR FURTHER INVESTIGATION ON CASE #01142583.SDR FDEA201904161067Panel · corrodedENG NR 2 OGV ANNULUS FORMER PANELS MISSING AT THE 6,9 AND 12 O CLOCK POSITION HAVE EVIDENCE OF CORROSION WHERE MISSING. ITEMS CURRENTLY ON OIL AS FOLLOWS: 12 O`CLOCK - 72-30 4464. 6 O'CLOCK 72-30-4323 9 O'CLOCK 73-30-4324 ANNULUS FORMER STRIPS REMOVED AND PITSDR FDEA201904161066Panel · delaminatedENG NR 2 ICE RING PANELS HAVE DE-LAM FROM THE CASING AND HAVE CORROSION UNDERNEATH. REMOVED CORROSION IAW AMM 72-34-10-8-4 AND REPLACED ICE IMPACT PANELS IAW AMM 72-34-10-358-031-R04.SDR UIEA2019041763894Vane · damaged(SEVERAL) # 2 ENGINE FAN EXIT CASE VANES HAVE MISSING SEALANT AT INSTALLATION BOLTS .(<P>APPLIED SEALANT AT # 2 ENGINE FAN EXIT CASE VANES BOLTS IAW B767 AMM 72-34-06-404-001-N00.</P>)SDR FDEA201904151065Acoustic Liner · damagedATRITION LINER DAMAGE ON ENG NR 2 AT 6 O' CLOCK POSITION DAMAGE. REPLACED ENG NR 2 ATTRITION LINERS DUE TO CORROSION DISBOND/CORROSION BELOW IAW AMM 72-34-10-028-122.SDR CA190428001Seal · leaking(CAN) OIL ODOR NOTED IN CABIN DURING CLIMB, VISIBLE SMOKE/HAZE NOTED IN CABIN AT TOP OF CLIMB, ENGINE POWER REDUCED AND SMOKE/HAZE CLEARED AND OIL ODOR REDUCED. AIRCRAFT RETURNED TO BASE WITH NO FURTHER INCIDENT. POST FLIGHT INVESTIGATION REVEALED OIL CONTAMISDR CA190415019Blade · broken(CAN) KING AIR 200 AIRCRAFT WAS ON CLIMB THROUGH APPROXIMATELY FL200, THE RIGHT HAND ENGINE MADE A SINGLE LOUD BANG, A FLAME WAS OBSERVED TO BE EMITTED OUT OF THE EXHAUST, FOLLOWED BY SPARKS. THE FLIGHT CREW CONDUCTED A PRECAUTIONARY ENGINE SHUTDOWN, DECLARED SDR UIEA2019041503879Blade · nickedNR 2 ENG HAS 1 EACH FAN BLADE WITH A SMALL NICK ON L/E 3/4 OF AN INCH FROM BLADE TIP. BLENDED #2 ENG #37 FAN BLADE IAW B767 AMM 72-31-02. FOUND TO BE WITHIN LIMITS IAW B767 AMM 72-31-02.SDR AALA2019041509021Blade · damagedAIRCRAFT WAS GROUNDED, PILOT REPORTS THE #1 ENG SN# V11099 OBSERVED SYMPTOMS INDICATING A LOSS IN HPC PERFORMANCE, INCREASE IN EGT, WF, LPR, CET, N2, ICT2, DECREASE IN TER3. DECREASE IN TAKEOFF EGT MARGIN. MAINTENANCE ACCOMPLISHED BORESCOPE INSPECTION ON STASDR CA190326009Compressor · fod(CAN) THE RENTAL ENGINE RAN HOT FROM THE FIRST DAY I FLEW IT. THE STARTS WHERE VERY SLOW BUT STILL IN PARAMETERS. THE TOT WAS APPROX. 580 DEGREES AT GROUND IDLE AND 580-600 AT FLIGHT IDLE WITH 18-20 PSI TQ. THE SECOND STARTS WERE OK, THEY WOULD BE ON THE HOTTESDR CA190326008Impeller · damaged(CAN) DURING MAINTENANCE THE #2 ENGINE WAS DISCOVERED TO HAVE IMPELLER DAMAGE. AFTER A BOROSCOPE WAS CARRIED OUT FURTHER DAMAGE WAS FOUND ON THE DIFFUSER CHANNELS AND ENGINE CASING. AFTER CONSULTING WITH THE ENGINE MANUFACTURER, IT WAS DETERMINED THAT THE DAMASDR ASAA2019032428759Blade · damagedPER T/C 78472010 NR 2 ENGINE FAN BLADE LUBE NR 8 BLADE CU-NI MISSING MORE THAN LIMITS. GROUNDED - YES. REMOVED AND REPLACED NR 8 AND NR 20 FAN BLADE PAIR ON NR 2 ENGINE REF T/C 78472010.SDR ASAA2019032428756Spacer · debondedPER T/C 78472010 NR 2 ENGINE FAN LUBE NR 3, 4, 7, 8, 19, 20, 21, 22 AND 24 SPACERS ELASTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SPACERS ON NR 2 ENGINE REF T/C 78472010.SDR UIEA2019032203647Seal · out of positionNR 1 ENG AFT EDGE OF FAN CASE I/B T/R SEAL OUT OF RETAINER (<P>REINSTALLED SEAL IN RETAINING ON NR 1 ENG AFT EDGE OF FAN CASE I/B T/R IAW SOPM 20-50-02</P>)SDR ASAA2019031928682Blade · wornREF LOG PAGE 11986685 PER T/C 78472010 NR 1 ENGINE FAN LUBE NR 4 AND NR 16 BLADES CU-NI COATINGS BEYOND LIMITS ARE MISSING. GROUNDED - YES. REMOVED AND REPLACED FAN BLADES NR 4 AND NR 16 ON NR 1 ENG REF T/C 78472010.SDR ASAA2019031928681Blade · wornPER T/C 78472010 NR 1 ENGINE FAN LUBE NR 1 AND NR 16 BLADES CU-NI COATINGS BEYOND LIMITS. ARE MISSING. GROUNDED - YES. REMOVED AND REPLACED FAN BLADES NR 1 AND NR 13 PAIR REF T/C 78472010 FAN BLADE LUBRICATION.SDR ASAA2019031928680Spacer · debondedPER T/C 78472010 NR 1 ENGINE FAN LUBE SPACERS NR 4,5,11,12,15,16,17,19 AND 23 ARE DISBONDED AT THE ELASTOMERS. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SPACERS ON NR 1 ENGINE. REF T/C 78472010 FAN BLADE LUBRICATION.SDR CA190507012Stator · broken(CAN) UPON ROUTINE INSPECTION OF COMPRESSOR CASE HALFS (WHILE ENGINE WAS REMOVED FROM AIRFRAME) IT WAS FOUND THAT ONE OF THE 6TH STAGE STATOR BLADES HAD BROKEN OFF ONE OF THE CASE HALFS AND BEEN INJESTED INTO THE COMPRESSOR CENTRIFUGAL COMPRESSOR SECTION, AND SDR CA190319013Actuator · malfunctioned(CAN) RH FADEC FAULT 1, R ENG LPC SVA ACTUATOR NOT IN COMMAND POSITION. LPC SVA ACTUATOR REPLACED. LOW-PRESSURE COMPRESSOR (LPC) STATOR VANE ACTUATOR (SVA)SDR ASAA2019031828668Blade · wornWHILE ACCOMPLISHING TASKCARD 78472010, FOUND NR 1 ENG FAN BLADE NR 17 WITH MISSING CU-NI-IN COATING ON CONCAVE SIDE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED NR 17 AND NR 5 FAN BLADE PAIR ON NR 1 ENG. FAN BLADE LUBRICATION.SDR ASAA2019031828667Blade · wornWHILE ACCOMPLISHING TASKCARD 78472010, FOUND NR 1 ENG FAN BLADE NR 13 WITH MISSING CU-NI-IN COATING ON CONCAVE SIDE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED NR 13 AND NR 1 FAN BLADE PAIR REF. T/C 78472010 FAN BLADE LUBRICATION.SDR ASAA2019031828666Spacer · debondedWHILE ACCOMPLISHING TASKCARD 78472010, FOUND NR 1 ENG FAN BLADE SPACERS 1, 3, 6, 18, 19 WITH DISBONDED ELASTOMERS. GROUNDED - YES. REMOVED AND REPLACED SPACERS 1, 3, 6, 18 AND 19 ON NR 1 ENG REF. T/C 78472010 FAN BLADE LUBRICATION.SDR CA190315011Pressure Sensor · inoperative(CAN) L ENG NACELLE OVHT CAUTION IN FLIGHT. HPC VALVE AND PRESSURE SENSE LINE INSPECTED - SATIS LHE HPC BLEED PRESSURE SENSOR REPLACED, TEST SATIS (TC# 20190315011)SDR ASAA2019031428615Frame · corrodedCORROSION UNDER NR 2 ENGINE FAN FRAME NUTPLATES EXCEED ALLOWABLE BLEND LIMIT PER AMM 72-23-05-700-801-F00. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG REF T/C 78471000 AND 78471001.SDR ASAA2019031328599Actuator · leakingNR 1 ENG DRIPPING FUEL FROM THE RIGHT VSV DRAIN @ 15DPM. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG RT VSV ACTUATOR REF AMM 75-31-01. OPS AND LEAK CHECK GOOD REF AMM 75-31-01.SDR WI5R2019031500001Rotor · damagedDURING TROUBLE SHOOTING FOR ELEVATED ITT TRENDS, A BORESCOPE INSPECTION FOUND DAMAGE TO THE HPC ROTOR AND A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD STAGE IP BLADE.SDR UIEA2019031403540Blade · nickedENG #2 DURING ACCOMPLISHMENT OF LP COMPRESSOR ROTOR BLADES INSPECTION WERE FOUND SEVERAL BLADES WITH NICKS AND DENTS WITHIN LIMITS THAT WILL NEED BLEND. REPAIRED BLADES ON #2 ENGINE IAW AMM 72-31-02-308-055-H00.
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