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 DHL2004752002Compressor · stalledREJECTED TAKEOFF FOR INFORMATIONAL PURPOSES ONLY WT=152,000 LBS, TEMP=12.6, PRESS ALT=SEA LEVEL, AIRSPEED=60 KNOTS. SUSPECTED COMPRESSOR STALL WITH AN AUTO PACK TRIP. WIND WAS 89 AT CROSSWIND AT 10 KNOTS. ALSO FOR INFORMATIONAL PURPOSES ONLY. INSPECTED ENGSDR CHQA000477Compressor · damagedFLT 6490 DFW - OKC: JUST AFTER TAKEOFF THROUGH ACCELERATION ALTITUDE WITH ALL ENGINE INDICATIONS NORMAL, NR 2 ENGINE FLAMED-OUT. CREW ADVISED PRIOR TO V1, HEARD A POP. AN EMERGENCY WAS DECLARED AND NR 2 ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO DFW, MADSDR CA040414001Retaining Ring · collapsed(CAN) THE HOT SECTION WAS DISMANTLED FOR A SCHEDULED CT DISK REPLACEMENT. CT SHROUD SEGMENTS HAD SHIFTED AXIALLY. THE RETAINING RING HAD COME OUT OF THE GROOVE. THIS PROBLEM HAS BEEN DOCUMENTED ON OTHER ENGINES. MFG HAS ISSUED P/N 3110741-02 RETAINING RINGSDR QXEA200400253Fan Blade · damagedTUS FLIGHT 2505 RETURN TO FIELD: NR 1 ENGINE VIBRATION 2.4 MILS. MAINTENANCE REPLACED FAN BLADES IHI1387N, IHI1392N, IHI1399N, IHI1429N, IHI1495N, IHI1501N, IHI1683N, IHI1693N, INI1702N, IHI1735N, IHI1737N IHI1739N, IHI1741N, IHI1744N, IHI1745N, IHI1747N, IHSDR 2004UALA00291Compressor · seizedNR 1 ENGINE COMPRESSOR STALLED AND SUBSEQUENTLY SEIZED. OIL PRESSURE AND N2 WENT TO ZERO. NR 3 BEARING FAILED. OUTER RACE FRACTURED, BEARING CAGE DISINTEGRATED, ALL BALL BEARINGS WORN APPROXIMATELY 25 PERCENT ON OPPOSING SIDES. REPLACED ENGINE. CORRECTIVESDR 2004F00246Blade · crackedNR 2 RIGHT ENGINE FAILURE DURING TAKEOFF ROLL. TAKEOFF ABORTED. VISUAL INDICATES FAN BLADE CRACKED AT HUB AND SEPARATED. EVALUATION TO DETERMINE CAUSE BEING CONDUCTED BY HONEYWELL. (M)SDR CA040402004Retaining Ring · collapsed(CAN) THE HOT SECTION WAS GIVEN AN UNSCHEDULED HOT SECTION INSPECTION DUE TO PERFORMANCE SHIFT. A FEW CT SHROUD SEGMENTS HAD SHIFTED SLIGHTLY AND WERE RUBBED. THE RETAINING RING HAD COME OUT OF HTE GROOVE. THIS PROBLEM HAS BEEN DOCUMENTED ON OTHER ENGINES. SDR DL75K040274Compressor · damagedHIGH SPEED ABORT LEFT ENGINE APPARENT COMPRESSOR STALL, MAX AIRSPEED 99 KIAS. AFTER STOPPED LT ENG OIL PRESSURE IND WENT RED AND EGT WENT ABOVE RED LIMIT INDICATOR. LEFT ENG SHUTDOWN, MAX BRAKE TEMP -4- ON NR 6. FOUND METAL IN TAILPIPE. BORESCOPED HPC EXTESDR 033104Bolt · backed outPILOT REPORTS (GRINDING) SOUND WHEN PROPELLER IS SPUN BY HAND. THE ENGINE WAS SPLIT AT THE (C) FLANGE WHERE DEBRIS WAS NOTED AT THE 6 O'CLOCK AREA BETWEEN THE COMPRESSOR TURBINE BLADES AND SHROUD SEGMENTS. AFTER REMOVAL OF THE CT DISK, IT WAS NOTED THAT FOUR BSDR QXEA200400239Fan Blade · lack of lubeDEN FLIGHT 4182 RETURN TO FIELD, NR 1 ENGINE VIBRATION. MAINTENANCE REPLACED FAN BLADES SERIAL NUMBERS IHI7274N, IHI7276N, IHI7280N, IHI7281N, IHI7289N, IHI7291N, IHI7297N, IHI7298N, IHI7302N, IHI7303N. OPERAITONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA040326002Blade · bent(CAN) ON TAKE OFF, CREW HEARD A STRANGE WHINING SOUND. SOUND IDENTIFIED AS FROM NR 1 ENGINE. TAKE OFF REJECTED AT 30 KTS. MAINTENANCE FOUND BENT BLADE ON LOW PRESSURE COMPRESSOR IMPELLER. ENGINE REPLACED. CREW ON PREVIOUS FLIGHT HAD REPORTED A BIRD STRIKE.SDR 2004UALA00269Blade · crackedNR 2 ENGINE COMPRESSOR STALLED IN CRUISE. POWER REDUCED TO IDLE. THE 6TH STAGE HPC INNER SHROUD ASSEMBLIES (PW IPC 72-35-00-17-001/-010) WERE FOUND TO HAVE BEEN INSTALLED BACKWARDS. THIS ALLOWED THE SEAL LAND TO MAKE INTERMITTENT CONTACT WITH THE TRAILING ESDR KBM2004F00025Guide Vane · crackedREMOVAL OF ENGINE FOR DISC REPLACEMENT. FOUND CRACK ON 1ST STG NOZZLE GUIDE VANES. DURING 2ND STAGE TURBINE WHEEL AND BLADE REPLACEMENT 263 SB. REMOVED AND REPLACED ENGINE WITH RENTAL.SDR QXEA200400222Valve · malfunctionedPDX - FLIGHT 2166 BURNING OIL SMELL REPORTED IN CABIN BY TWO CREW MEMBERS DURING DESCENT. NO VISIBLE SMOKE REPORTED. ALL INDICATIONS IN COCKPIT NORMAL. REPLACED NR 1 AND NR 2 ENGINE P2.5/P3 SWITCHING VALVE PER P&W MM 72-30-00. GROUND RAN AIRCRAFT AT VARIOUSDR AWXA200400277Blade · crackedAFTER TAKEOFF, EN ROUTE. NR 2 ENG STALLED WITH EGT OVERTEMP OF 843 DEGREE, FOLLOWED ECAM & DECLARED EMERGENCY. MX R / R NR 2 ENG IAW T/C. BORESCOPE OF HPC REVEALED 1, 7TH STAGE BLADE FRACTURED ROOT, & A SECTION OF 7TH STAGE REAR DAMPER WIRE MISSING OVER A SPASDR CA040311008Disk · cracked(CAN) ENGINE WAS STRIPPED AS PART OF ROUTINE SCHEDULED OVERHAUL. VISUAL EXAMINATION OF HPC DISK 3 SHOWS CRACK IN RIM OF DISK. FURTHER INVESTIGATION IS UNDERWAY.SDR P5CA0401054Fan Blade · brokenNR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED.SDR CA040511005Engine · fod(CAN) AFTER TAKEOFF THE CREW REPORTED SMOKE IN THE CABIN. AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. BOROSCOPE INSPECTION REVEALED FOD (FOD TYPE WAS NOT IDENTIFIED) FROM 1ST TO 7TH STAGE COMPRESSOR OF LT ENGINSDR CA040303001Blade · damaged(CAN) A MECHANIC WAS CARRYING OUT A SERVICE CHECK AND HE NOTICED FOD IN THE RT ENGINE INTAKE. UPON INSPECTION OF THE INTAKE, FOUND A PIECE OF BLADE RUB STRIP MISSING, REAR ACOUSTIC LINER DAMAGE AND TWO DAMAGED FAN BY PASS STATOR BLADES. ONE FAN BLADE DAMPENERSDR S04472017Blade · missing747F B18708 A/C GTB DUE TO HEAVY SNOW AT LUX. ENG-2 SURGED AND FLAMEOUT DURING T/O ROLL (GROUND SPEED<45 KNOTS), GTB AGAIN. GROUND INSP FOUND METAL DEBRIS IN ENG-2 TAIL PIPE. BORESCOPE ALL 4 ENGINES, FOUND ENG-3 4 EA HPC 1ST STAGE BLADES L/E AND T/E TIP MATESDR QXEA200400179Fan Blade · wornMFR - FLIGHT 2557 ON FLIGHT FROM PDX TO ONT AIRCRAFT DIVERTED TO MFR DUE TO NR 1 ENGINE VIBRATION. REPLACED FAN BLADES SERIAL NUMBERS, IHI3069N, IHI3130N, IHI3140N, IHI3144N, IHI3149N, IHI3150N, IHI3156N, IHI3158N, IHI3160N, IHI3178N, IHI3180N, IHI3182N, IHI3SDR GTIA040152Blade · damagedDTW - FOUND SEVERAL C1 BLADES HAVE FOD DAMAGE NR 1 ENGINE. REMOVED AND REPLACED 12 EACH C1 BLADES. (M)SDR AALA20040299Compressor · stalledJFK - INFLIGHT T0167/22 AT 175K LEFT HAND ENGINE COMPRESSOR STALLED WITH LOUD BANG AND AIRCRAFT YAW. FIVE SECONDS LATER SECOND COMPRESSOR STALL AND ENGINE STARTED TO ROLL BACK. ENGINE THRUST LEFT APPEARED MOMENTARILY. THROTTLE REDUCED AND STALL CLEARED. THSDR AWXA200400204Fan Blade · damagedAUS - ENGINE FOD - DURING RON INSPECTION MAINTENANCE FOUND 33 FAN BLADES DAMAGED ON THE NR 2 ENGINE. SUSPECT DAMAGE WAS CAUSED BY MISSING ACOUSTIC LINER SCREWS. MAINTENANCE PERFORMED FOD INSPECTION IAW T/C I8M05030, BORESCOPED ENGINE IAW T/C I5M72025, REMOVESDR 15HA0458004Compressor · damagedDURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINATED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED THE PRESENCE OF A PIECSDR CA040302002Blade · separated(CAN) ON 2ND FLIGHT OF THE DAY, A SUDDEN PARTIAL POWER LOSS OCCURRED ON NR 1 ENGINE, A STRONG SMELL ACCOMPANIED THE POWER LOSS. ENGINE NR 1 WAS SUBSEQUENTLY SHUT DOWN. THE AIRCRAFT COMPLETED AN UNEVENTFUL UNSCHEDULED LANDING. UPON SUBSEQUENT INSPECTION IT WASDR P5CA0401042Compressor · stalledNR 3 ENG COMPRESSOR STALL. ENG SHUTDOWN. REPLACED ENG PER WIC M7100-002 / M7100-011. ENG RUN & OPS CHECK NORMAL.SDR MALA040209Fan · seizedNR 4 ENG 1ST START HOT, 2ND START HOT, GROUND PERSONNEL SAW NO ROTATION. QRH WAS FOLLOWED TEMP MAX 680 TRANSIENT. MX INSPECTED NR 4 ENG FOUND FAN SECTION SEIZED AND CHIP DETECTOR CONTAMINATED. INSTALLED 3 ENG FERRY KIT AS PER TASK CARD 3 ENG FERRY ON NR 4 ESDR AUS20040101Impeller · damaged(AUS) LT ENGINE LP IMPELLER BADLY DAMAGED. FURTHER INSPECTION ALSO FOUND SEVERE DAMAGE TO THE HP IMPELLER AS WELL AS THE GAS GENERATOR CASE AND THE LP DIFFUSER CASE. A DENT WAS ALSO FOUND IN THE COMBUSTION CHAMBER OUTER LINER. SUSPECT CAUSED BY FOD.SDR RYN2004F00028Compressor · damagedDURING CLIMB OUT, NR 2 ENGINE STALLED. APPROPRIATE PROCEDURES WERE FOLLOWED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPACED NR 2 ENGINE.SDR GTIA040187Nose Cowl · damagedFTW - NR 2 NOSE COWL LIP RING HAS OVERHEAT INDICATIONS. MEASUREMENTS OBTAINED EXCEEDED UPPER LIMIT FOR 2024-T42 MATERIAL. NR 2 ENGINE NOSE COWL S/N 099-362. REMOVED AND REPLACED SAS WO B00127-11N-00001. (M)SDR MEX2004054Blade · damagedDURING TRANSIT CHECK IT WAS DETECTED LT ENGINE FAN BLADE WITH DAMAGE. DAMAGE WAS 4 INCHES DOWN OF THE BLADE ROOT ON THE ATTACH BORDER WITH /75 INCH LARGE AND .240 WIDE AN IT WAS BROKEN. BOROSCOPIC INSPECTION WAS PERFORMED ON 6 AND 7 STAGES BEING ALL CORRECT.SDR DL757040137Blade · damagedFAILURE OF LEFT ENGINE ON CLIMBOUT AT FL230. EGT, N2 & FF WERE NORMAL. EPR AND N1 ROLLED BACK TO IDLE. A/C YAW INDICATED COMPLETE LOSS OF THRUST. WINDMILLED FOR 15 MIN, POSITIVE OIL PRESSURE. DURING BOROSCOPE FOUND DAMAGE TO 6TH AND 7TH STAGE COMPRESSOR BSDR MEX2004044Disc · damagedDURING TRANSIT CHECK, MAINTENANCE FOUND DAMAGE OUT OF LIMITS, CAUSED BY FOD IN THE RT ENGINE FAN BLADES. TECHNICAL PERSONNEL WAS SENT TO HMO TO ATTEND THE DAMAGES. THE C1 DISK WS REPLACED AND ENGINE TESTED IAW MM 72-00-3, ALL CORRECT. (M)SDR 187532Compressor · stalledFLIGHT 4593 PIT-TOL. AFTER THE A/C RETURNED TO PIT DUE TO MULTIPLE COMPRESSOR STALLS, THE A/C WAS PARKED WHEN A BAGGAGE CART CAME LOOSE FROM THE TUG THAT WAS PULLING IT AND SLAMMED INTO THE AFT PART OF THE A/C FUSELAGE BEHIND THE CARGO DOOR.SDR UO22004F00000Stator · damaged4TH LPC STATOR LOST 1 EACH VANE, RELATED DAMAGE INCLUDES HIGH AND LOW PRESSURE COMPRESSORS, AND HIGH AND LOW PRESSURE TURBINES.SDR SWAA040258Fan Blade · damagedDECLARED EMERGENCY/AIR TURN BACK, INFLIGHT ENGINE SHUTDOWN. PASSING APPROX 8000 FEET, HEARD A POP AND FELT SLIGHT VIBRATION. ALL INSTRUMENTS SHOWED NORMAL. CLIMB SEEMED A LITTLE LOW FOR POWER SETTING. ISOLATED VIBRATION TO NR 2 ENGINE. REMOVED AND REPLACESDR MASA200400044Fan Blade · vibrationCREW REPORTED NR 1 ENGINE HIGH VIBE DURING TAKE-OFF. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX BORESCOPED THE ENGINE AND WAS GOOD. MX NOTICED SEVERAL FAN BLADES WITH CHIPS. MX REPLACED THE FAN BLADES. OP CHECKS GOOD.SDR F3LA200400003Fan Blade · bentON WALKAROUND, FLIGHT CREW REPORTED NR 1 ENGINE BLADES BENT. REPLACED DAMAGED FAN BLADES AT POSITIONS 2, 3, 4, 6, 7, 8, 9, 10, 11, 12, 15, 16, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 34, AND 35. POSITIONS 14, 18, 32 AND 36 WERE NOT MOVED. POSITISDR F3LA200400001Fan Blade · bentDURING CLIMBOUT, FLIGHT CREW REPORTED ABNORMAL NR 2 ENGINE NOISE (NO ABNORMAL ENGINE VIBRATION). FOUND FAN BLADES BENT DUE TO ICE INGESTION. REPLACED NR 2 ENGINE FAN BLADES PER MM 72-21-00-300-028, PERFORMED NR 2 ENGINE TRIM BALANCE PER MM 77-32-34-750-001 ASDR WRLA200408Fan Blade · shingledENGINE 1 VIBRATION HIGH ALERT DISPLAYED ON TAKEOFF, ABORTED TAKEOFF AT 15 KNOTS. INSPECTED NR 1 ENGINE IAW FIM 77-32-01 FOUND FAN BLADES SHINGLED, FREED BLADES, NO DAMAGE NOTED, LUBED FAN SHROUDS AND ROOTS. OPS CHECKED GOOD ON GROUND RUN.SDR MDR04043Compressor Wheel · crackedA CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR SN 677782, WAS REMOVED FOR HSI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY CURRENT. THE CRACK WASDR JYD2004F00003Compressor Wheel · crackedA CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR, SN 677782, WAS REMOVED FOR HSI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY CURRENT. THE CRACK WSDR QXEA200400044Compressor · damagedDEN FLIGHT 4275, RETURNED TO FIELD, NR 2 ENGINE FAN VIBRATION. BLENDED DAMAGED BLADES. COMPLIED WITH NDT. REMOVED AND REPLACED ENGINE. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERICE.SDR 54148Plenum · crackedFOUND CRACKED AT DRAIN BOSS.SDR CA040115002Plenum · cracked(CAN) FLIGHT CREW RECEIVED SPLIT SECOND FIRE WARNING INDICATION ON LT ENG. DUE TO BRIEF NATURE OF IND FLIGHT CREW MONITORED GAUGES, DETERMINED FALSE INDICATION. SHORTLY AFTER ENG STARTED LOSING PWR UNTIL IT REACHED ABOUT 55 PERCENT TORQUE. UPON INSP, LT ENG PSDR CA040116004Compressor Wheel · fractured(CAN) FOLLOWING UNEVENTFUL LANDING AND ROLL-OUT, CREW NOTED VIBRATION AND RISING ITT. ENGINE WAS SECURED. POST FLIGHT EXAMINATION SHOWED THAT ROTOR 1 OF THE HPC HAD .3333 OF ONE AIRFOIL MISSING.SDR ERAA092666Case Half · damagedCOMPRESSOR CASE REC'D ON EXCHANGE WITH DAMAGED 6TH STAGE VANES. AS PER MR. GEORGE HICKS OF ALCOR, RETURNING REQUESTING WARRANTY EXCHANGE. RETURNING ON REPAIR ORDER RW-897299SDR QXEA200400011Engine · vibrationPDR FLIGHT 2553 RETURN TO FIELD - NR 1 ENGINE N1 VIBRATION 1.7 TO 1.9. COMPLIED WITH PIN LUBES AND ENGINE RUNS. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR TRB2004F00008Check Valve · failedDURING TAKEOFF THE LT ENGINE ITT EXCEEDED THE LIMITS. REMOVED AND REPLACED THE LT ENGINE P2.5 CT CHECK VALVE.
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