JASC 7230
Service difficulty reports · 5,066
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 20001115SH005Stator · failedKIN/JFK - FLT JM 017 - EN ROUTE, FLIGHT DIVERTED DUE BAD WEATHER. AFTER TAKEOFF AND DURING CLIMB PHASE AT 17,000 FEET, A LOUD BANG WAS HEARD FOLLOWED BY THE NR 1 ENGINE EGT GOING OVER ITS LIMIT. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED. INSPECTION PERSDR 20000509SH042Seal · crackedPART RECEIVED FROM WESTFIELD GAGE FOR FPI IAW V2500 MANUAL REVISION 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO A CRACK (ONE PLACE ON TOP SURFACE, 0.200 INCH LONG). NOTE: SUBMITTER STATED SECOND TIME THIS SSDR AU000376Bearing · failed(AUS) ENGINE NR 1 BEARING FAILED.SDR 20000509SH007Bearing · scoredENGINE WAS REMOVED FOR ''NR 4 BEARING INSPECTION/REPAIR''. THE NR 4 BEARING EXHIBITED AXIAL SCORING OF THE ROLLERS AND OUTER RACE. . (X)SDR 20000509SH017Disk · scratchedNEW PART RECEIVED FROM HONEYWELL WITH NUMEROUS SCRATCHES AROUND DISK IN THE POST FIR TREE AREA. LOT NR: 00P048. (X)SDR C2XA00BT019Compressor · contaminatedBTV - REPORTED SMOKE IN CABIN AFTER TAKEOFF AIRCRAFT RETURNED TO BTV UNEVENTFULLY. MAINTENANCE RAN BOTH ENGINES AND OPS CHECKED SYSTEM GOOD. FOUND THE SMELL TO BE COMPRESSOR WASH FLUID THAT HAD GOTTEN INTO THE BLEED AIR SYSTEM. AIRCRAFT RETURNED TO SERVICE.SDR AU000368Seal · worn(AUS) NO3 ENGINE NO1 CARBON SEAL EXCESSIVELY WORN AND CHIPPED ALLOWINGOIL TO PASS INTO THE AIR SYSTEM.SDR 20000512SH023Seal · crackedPART RECEIVED FROM WESTFIELD GAGE CO., FOR FLUORESCENT PENETRANT INSPECTION IAW IAE V2500 PROPULSION SYS ENG MANUAL, REV 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT F.P.I. DUE TO A CRACK ONE PLACE ON TOP SURFACE, 0.200 ISDR AU000123Seal · leaking(AUS) RT ENGINE COMPRESSOR BEARING OIL SEAL SUSPECT LEAKING. OIL CONTAMINATION OF COMPRESSOR.SDR 20000509SH006Seal · crackedFLUORESCENT PENETRANT INSPECTION IAW I.A.E. V2500 PSEM, REV 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501). PART REJECTED AT F.P.I. DUE TO A CRACK ON THE TOP SURFACE, 0.180 INCH LONG (AS MARKED). (X)SDR 20000505SH014Disk · damagedNEW PART RECEIVED FROM HONEYWELL WITH DAMAGE IN POST FIR TREE AREA. LOT NR 99P189. (X)SDR DL73K000682Bullet · dentedEN ROUTE FROM BDL TO FLL, NR 1 ENGINE HAD COMPRESSOR STALLS. CREW PULLED THROTTLE TO IDLE. DIVERTED TO BOS. BOS MTC FOUND NR 1 ENGINE NOSE BULLET DETACHED AND FAN DAMAGE.SDR 20000816SH022Diffuser · mismanufacturedOUTER DIAMETER OF VANE SUPPORT RING IS TOO LARGE (10.221 INCHES). IMPROPER MANUFACTURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AALA20000595Compressor · stalledSFO - FLT 0129 - DURING INITIAL CLIMB, COMPRESSOR STALLED. CREW REPORTED THROTTLE BACK, THEN PUSH POWER UP. SHUT DOWN ENGINE, DIVERTED TO SFO AND LANDED WITHOUT INCIDENT. CURENTLY UNDER INVESTIGATION. (X)SDR SWAA000614Blade · bird strikeAIR TURNBACK, BIRD STRIKE IN NR 1 ENGINE INTAKE. COMPLIED WITH BIRD STRIKE BORESCOPE INSP. R&R NR 1 ENGINE FAN BLADE SET AND NR 1 ENGINE PRECOOLER VALVE PER MM.SDR AU000349Seal · worn(AUS) NO1 ENGINE NO1 CARBON SEAL SEVERELY WORN. CONTAMINATED BLEED AIRENTERED COCKPIT CAUSING PROBLEMS WITH FLIGHT CREW.SDR GAIA00110Compressor · stalledFLT 2009 - OAK-MHR - NR 2 ENGINE COMPRESSOR STALL WITH DROP OF .30 EPR. ENGINE STABILIZED, MAX EGT 850 DEGREES. PRECAUTIONARY ENGINE SHUT DOWN WAS PERFORMED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MHR. REMOVED AND REPLACED NR 2 ENGINE IAW WORK CARD BH-7194SDR CA000320017Carbon Seal · leaking(CAN) AN OIL SMELL COULD BE DETECTED FROM THE AIR DISTRIBUTION SYSTEM. THE NR 1 ENGINE, 1 AND 3 CARBON SEALS WERE REPLACED.SDR AC2A0000038Gear Shaft · wornGEARSHAFT RECEIVED NEW FROM AVIALL IN ORIG UNOPENED PACKAGE. PN 23056634. ATTEMPT MADE TO INSTALL PART IN COMPRESSOR SPLINE ADAPTER OF ENGINE. RETAINING RING THAT SECURES GEARSHAFT IN SPLINE ADAPTER WOULD NOT FIT IN GROOVE. INSUFFICIENT CLEARANCE BETWEEN RSDR CA000511020Compressor · cracked(CAN) 1.5 INCH CRACK FOUND ON COMPRESSOR SCROLL STARTING ALONG AFT RADIUS OF SCROLL PROGRESSING TOWARD DISCHARGE ELBOW AND TURNING TO MIDDLE OF OUTSIDE FACE.SDR C2XA00TY006Carbon Seal · wornEWR - FLT 4209 - CREW REPORTED THAT AFTER TAKEOFF SMOKE WAS NOTICED IN THE CABIN AND RECEIVED A LAVATORY SMOKE INDICATION ON THE EICAS. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE RIGHT ESDR 20000427SH032Shaft · damagedAFTER SHOP MAINTENANCE AND RETURN TO SERVICE, ENGINE SUSTAINED TRANSPORT DAMAGE TO FAN SECTION. THE ENGINE WAS RETURNED TO THE SHOP FOR REPAIR AND TEST RUN. DURING TEST RUN, OIL LEAKAGE OCCURRED FORCING A DISASSEMBLY OF THE ENGINE. AFTER DISASSEMBLY, NOTED SDR K4HA99107Blade · brokenYQX - FLT 13283 - LOST NR 2 ENGINE AT ALT AFTER VIBRATION WAS FELT. SECURED ENGINE ACCORDING TO CHECKLIST. WHEN INSPECTED FOUND C1 BLADES BROKEN. REMOVED AND REPLACED NR 2 ENGINE IAW 71-00-02. B747 MM TESTED AND OPS CHECK GOOD. (M)SDR AALA006047Engine · stalledSJC - NR 2 ENGINE COMPRESSOR STALLED IN FLIGHT LEVEL 35,000 FT, RA-24 DEG CELSIUS, .78 MACH, CLEAR SKIES, EPR DROPPED FROM 1.8 TO 1.5, EGT ROSE TO 430 DEG COMPARED TO NR 1 ENGINE AT 370 DEG. REMOVED AND REPLACED NR 2 ENGINE PER RNOM T/C 0099. ENGINE TEST ANDSDR UPS00531973Engine · malfunctionedBURNT OIL SMELL COMING FROM RT PACK. TURNED LEFT PACK OFF SMELL CONTINUED. TURNED RIGHT PACK OFF SELL WENT AWAY. OPENED ISOLATION VLV AND TURNED OFF L ENG BLEED AND OIL SMELL RETURNED IMMEDIATELY, RT ENG BLEED AND OIL SMELL DISSIPATED. REMOVED AND REPLACED SDR 20000412SH012Disk · damagedNEW PART RECEIVED FROM HONEYWELL WITH DAMAGE ON FORWARD SIDE IN POST FIR TREE AREA. REF: LOT NUMBER 99P243. (X)SDR 20000403SH005Shroud · damagedDISASSEMBLY INSPECTION REVEALED DETAIL VANE OF 10TH/11TH SHROUD BROKEN OUT CAUSING SECONDARY HPC BLADE/VANE DAMAGE. SHROUD WILL BE FORWARDED TO PRATT & WHITNEY ENGINEERING FOR FAILURE INVESTIGATION. (XSDR 20000626SH023Lock · unsecureIMPROPER ASSEMBLY. WING BORESCOPE INSPECTION DISCLOSED ONE 7TH STAGE BLADE LOCK NOT CRIMPED. DIS-ASSEMBLY INSPECTION VERIFIED ON WING FINDINGS. REVIEW OF PAST BUILD AND PROCEDURES BEING PERFORMED TO DETERMINE ROOT CAUSE. LAST BUILD PERFORMED AT CRS WA2D259SDR 0000806601Engine · bird strikeWHILE CLIMBING AT 2000 FT AGL, THE NR 1 ENGINE SUSTAINED A BIRSTRIKE. THE ENGINE COMPRESSOR STALLED AND WAS SHUT DOWN. THE FLIGHT DIVERTED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND EVIDENCE OF BIRD INGESTION. A BOROSCOPE ISDR 20000619AP010Compressor · stalledVCV - DURING TAKEOFF, THE NR 3 ENGINE COMPRESSOR STALLED AND HIGH VIBRATION WAS NOTED. ABORTED TAKEOFF, RETURNED TO BLOCK. MAINTENANCE FERRIED TO IND. ENGINE NR 3 WAS REPLACED. (M)SDR 20000919SH008Diffuser · crackedDIFFUSER ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR AALA20000354Compressor · stalledHNL - FLT 8 - AFTER TAKEOFF, NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. RETURNED AND LANDED HNL WITHOUT INCIDENT. (M)SDR 00FDEA00123Compressor · stalledUPON GEAR RETRACTION EXPERIENCED COMPRESSOR STALL ACCOMPANIED LOUD BANG/SHUDDER, DECREASE AND RECOVERY OF NR 2 EPR, LEFT PACK TRIPPED OFF ON AUTO PACK TRIP. COMPLIED WITH CTR ENG COMPRESSOR STALL CK FOR HIGH PWR STALL. INSPECTED ENG INLET AND EXHAUST AREAS, SDR AC2A0000021Scroll · crackedCRACKED SCROLL. INSTALLED NEW SCROLL. (X)SDR AC2A0000016Scroll · crackedSCROLL CRACKED AT NORMAL LOCATION. REPLACED SCROLL. (X)SDR 2000UALA00083Blade · separatedDIVERSION TO STL DUE TO N2 COMPRESSOR STALL AT FL350. AFTER PATCH WITH SAMC ALL AGREED TO NR 2 ENGINE SHUT DOWN AND STL DIVERT. AN AMBER ALERT WAS DECLARED AND EMERGENCY EQUIPMENT WAS REQESTED BY DISPATCH THROUGH STL TRACON. *S/D* A HPC 4TH STAGE BLADE FAISDR SWAA000300Blade · bird strikeNR 1 ENG ENCOUNTERED A BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION AND REMOVED AND REPLACED NR 1 ENG FAN BLADES PER MM.SDR CA000218023Bearing · making metal(CAN) COMPRESSOR BEARING FOUND MAKING NOISE AND OIL CONTAMINATED WITH METAL FRAGMENTS. REPLACED.SDR CA000218010Bearing · spalled(CAN) PREMATURE SPALLING ON INNER RACE OF NR 2 BEARING LEAD TO THE REMOVAL OF THE COMPRESSOR ASSY.SDR MALA000136Sensor · obstructedGPZ - FLT 3271 - COMPRESSOR STALL AT 500 FT IN NO ICE, ETOT WAS BEING DIALED DOWN, AIRCRAFT WAS DE-ICED FOR FROST IN THE MORNING, TEMP AT GPZ -18C, IT STALLED AT LEAST 3 TIMES TREND SHOWS HOTTER ON THE LEFT. BORESCOPED RT ENGINE CND. REMOVED OBSTRUCTION FROMSDR CA000215011Scroll · cracked(CAN) COMPRESSOR SCROLL FOUND CRACKED. FAA MADE AWARE OF THE PROBLEM THROUGH ALLISON ROLLS ROYCE. .SDR SCNA00014Compressor · malfunctionedDURING LEVEL OFF AND ON DESCENT, THE NUMBER TWO ENGINE UPON ADVANCING THRUST LEVERS EXPERIENCED COMPRESSOR STALL. ENGINE RUN CARRIED OUT. HOT AND COLD INSPECTION CARRIED OUT AS PER MM 7200. SURGE BLEED OPERATION CHECK OKAY AS PER 7200.SDR CA000215010Impeller · failedCOMPRESSOR IMPELLER FAILED, FAA MADE AWARE OF THE PROBLEM THROUGH ALLISON ROLLS ROYCE.SDR EIA2000006Blade · damagedNFFN - DURING POST-FLIGHT WALK AROUND INSPECTION, FOUND NR 1 ENGINE WITH NUMEROUS DAMAGED FAN BLADES. FOUND BLADES 1, 25, 27, 31, 33, 11, 34, 13, 42, 22 DAMAGED OUT OF LIMITS. REPLACED A TOTAL OF 18 FAN BLADES PER WORKCARD F7208. RII ACCOMPLISHED. (M)SDR 20000330SH017Blade · bentDURING WALKAROUND INSPECTION, SEVEN N1 FAN BLADES WERE FOUND BENT BEYOND LIMITS ON NR 1 ENGINE. AIRCRAFT WAS GROUNDED NAN. FAN BLADES WERE REPLACED AND TEST RUN CARRIED OUT BY EVERGREEN. (X)SDR 2000ZZZX595Plenum · mismanufacturedREPAIRED PART FROM HONEYWELL. DIM. C OUT OF LIMITS. (X)SDR 2000UALA00041Blade · crackedRIGHT ENGINE SUFFERED A FLAME-OUT DURING INITIAL CLIMB FROM FL330 TO FL370. TWO RESTARTS ATTEMPTED WITH NO HELP. ENGINE SURGED AT FL330 NO VIBRATION. AFTER LANDING MECHANIC FOUND METAL IN TAILPIPE. *S/D* C5 BLADE FAILURE DUE TO IMPACT DAMAGE. BLADE WAS ISDR BJNA000102Blade · damagedNR 2 ENGINE FLAMED OUT ON TAKEOFF ROLL. INSPECTION OF ENGINE DETERMINE CAUSE TO BE INGESTION OF FOD, DAMAGING C-1, C-7, C-8 AND C-9 COMPRESSOR BLADES. (M)SDR TWAA0001701Blade · damagedJUST AFTER TAKEOFF THE LEFT ENGINE HAD TWO COMPRESSOR STALLS AND THEN LOST POWER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO DEN. FOUND EVIDENCE OF A BIRD STRIKE CAUSING DAMAGE TO SEVERAL FIRST STAGE COMPRESSOR BLADES. THE ENGINE WAS REPLACED.SDR AU000186Blade · failed(AUS) THIRD STAGE COMPRESSOR DISC AND BLADES DESTROYED. DOWNSTREAM COMPRESSOR DAMAGE. NO DAMAGE TO THE FIRST TWO STAGES.
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