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 HALA0800443Blade · damagedOPEN - BIRD STRIKE INSPECTION OF RT ENG REVEALED A CORNER PIECE MISSING FROM ENG STATOR VANE PLATFORM BASE AT 3 O'CLOCK POSITION. OK TO OPERATE IAW AMM 72-33-02-206--00-N00 TABLE 603. TRANSCRIBED TO MIC SHEET, NO OTHER DAMAGE NOTED AS PER FIM 71 FAULT INDES,SDR 865FLP2936Compressor · stalledNR 1 ENGINE COMPRESSOR STALLED AT 1000 FT AND WAS SECURED. ENGINE WAS RELIT PRIOR TO LANDING. ENGINE POWER ASSURANCE RUN ON GROUND DETECTED NO DISCREPANCIES.SDR NWAA081239989Compressor · stalledDURING TAKEOFF ROLL AT 110 KNOTS, ENGINE NR 2 EXPERIENCED 2 COMPRESSOR STALLS. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO GATE. FLIGHT CREW REPORTED SNOW CONTAMINATED RUNWAYS. MAINTENANCE PERFORMED POST STALL INSPECTIONS AND GROUND RUN ON ENGINE NR 2.SDR AALA200800723Compressor · damagedDFW INFLIGHT T1649/26MAR - NUMBER TWO ENGINE COMPRESSOR STALLED AT 200 FEET DURING TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LARGE AREA OF DAMAGE TO ACOUSTIC LINER AND HONEYCOMB IN FAN BYPASS DUCT. REPLACED NUMBER TWO ENGINE ON 27 MAR AT DSDR 2008FA0000265Compressor · separatedON CLIMB THROUGH FL140 CREW HEARD BANG FROM RT ENGINE WITH VIBRATION. RT ITT INCREASED 150C BUT NO OVER TEMP. REDUCED POWER, THEN BROUGHT POWER BACK UP, WITH SAME RESULT. CREW LANDED WITHOUT INCIDENT AND ENGINE REMOVED AND SENT FOR REPAIR AND OVERHAUL. (K)SDR DL76L080400Case · crackedNR 1 ENG CHANGE DUE TO FAN CASE CRACK.SDR SWIA200819388Fan · out of balanceFLT 6434 - LEFT ENGINE VIBE GAUGE BEGAN TO INCREASE. COMPLIED WITH ENGINE FAN TRIM BALANCE IAW 71-00-00. OPS CHECK GOOD.SDR F3LA200800129Bearing · failedDURING CRUISE, FLIGHT CREW REPORTED VIBRATION FOLLOWED BY ECAM WARNING OF NUMBER 1 ENGINE OIL FILTER CLOG, LOSS OF OIL PRESSURE, INCREASE IN OIL TEMPERATURE AND LOSS OF OIL LEVEL. THE ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFSDR UALA2008111301456Fan · vibrationLEFT ENGINE HAS PRONOUNCED VIBRATION AT 76 PERCENT N2 ABOVE 2.0. *S/D* LUBED FAN BLADES AND TRIM BALANCED. VIBRATION IS NOW WITHIN LIMITS.SDR CA080401002Blade · damaged(CAN) WHILE PERFORMING AC DAILY INSP, NR (3) ENGINE C-1 FAN ASSY WAS FOUND TO HAVE SUBSTANTIAL DAMAGE TO (3) BLADES. THE (3) BLADES HAD SIGNIFICANT L/E DEFORMATION WITH ONE EXHIBITING VISUAL CRACKING. THE C-1 FAN WAS REMOVED FROM SERVICE AND REPLACED. THE AC SDR HALA0800399Blade · nickedETOPS SIGNIFICANT SYSTEM, SMALL NICK FOUND ON NR 1 ENG ON NR 7 FAN BLADE APPROX 5 INCHES FROM BLADE ROOT AREA C. REPAIRED FAN BLADE BY BLENDING AND PERFORMING FPI PER MM 72-31-02-308-003-N00.
SDR CA080314009Bearing · failedENGINE REMOVED FOR ITT EXCEEDANCE, AUTO IFSD, SMOKE IN COCKPIT/CABIN, OIL DEBRIS ON ALL CHIP DETECTORS. TEARDOWN OF ENGINE REVEAL NR 4 BEARING FAILURE AND ALSO NR 3 BEARING FAILURE. EXCESSIVE DAMAGE IN COMPRESSOR AREA DUE TO BOTH SUPPORTING BEARING FAILURE. SDR HALA0800384Blade · nickedETOPS SIGNIFICANT SYSTEM, SMALL NICK FOUND ON LEADING EDGE OF NR 2 ENG, BLADE NR 23 APPROX 6 INCHES FROM ROOT. REPAIRED BY BLENDING PER AMM 72-31-02-308-003-N00. PERFORMED DYE PEN INSP ON REPAIRED AREA, NO TROUBLE FOUND.
SDR HALA0800370Blade · nickedFOUND TWO NICKS ON NR 1 ENGINE FAN BLADES, ONE ON EACH BLADE, BLADES NR 7 AND NR 8. REMOVED AND REPLACED NR 7, NR 8 BLADE PER AMM72-38-15. VIBRATION CK PEND. VIBRATION CK GOOD PER AMM71-00-03.SDR HALA0800386Blade · damagedETOPS SIGNIFICANT SYSTEM, ON WALKAROUND ON NR 2 ENGINE FOUND 1 DING ON BLADE 1, 9 APPROX 5 INCHES FROM BLADE ROOT AREA C PER MM 72-31-02-3-08-003. BLENDED BLADE PER MM TASK 72-31-02 AREA C LEADING EDGE. NEEDS DYE PENETRANT INSPECTION PER AMM 70-11-06/201. RSDR DL764080317Blades · shearedCREW REPORTS RT ENG COMPRESSOR STALL DURING INITIAL PWR FOR T/O. ABORTED T/O AT 10 KTS, CREW OBSERVED RT EGT DROP TO NEAR ZERO FOR A BRIEF SECOND AFTER BANG. NO EICAS MESSAGES, MTC IN PROGRESS. ALITALIA BORO INSP IN WORK. BOROSCOPE INSPECTION REVEALED 3 BLSDR 2008FA0000184Compressor · damagedDURING PERFORMANCE OF A SCHEDULED 1800 HOUR HOT SECTION INSPECTION OF THE RT ENGINE, AT 1771 HOURS AND 7 YEARS TIS SINCE OVERHAUL, INITIAL VISUAL INSPECTION OF THE CT BLADES TIP CLEARANCE REVEALED CLEARANCES IN EXCESS OF ALLOWABLE FOR RETURN TO SERVICE. IT WASDR QXEA200800234Servo · inoperativePDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND NR 1 ENGINE IBV SERVO INOPERATIVE, REMOVED AND REPLACE IBV SERVO COMPLETED GROUND RUNS, ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SESDR HALA0800364Blade · nickedNR 2 ENG FOUND NR 18 BLADE NICKED ON LEADING EDGE 6" FROM TIP. BLENDED DAMAGE 3/16" DEEP PER AMM 72-31-02-308-003, FIG 804 TO WITHIN REPAIRABLE LIMIT FOR AREA C.SDR CA080229010Scroll · cracked(CAN) COMPRESSOR 390.6 SINCE 2000 HOUR INSP. CRACK LOCATED BY ENGINEER DURING GROUND RUN UP FOLLOWING SCHEDULED INSP. LOCATED BY AIR LEAK FOUND BY BARE HAND CHECK. CRACK LOCATED SLIGHTLY BELOW SCROLL ARMPIT REINFORCEMENT PATCH AREA, NOT IN NORMAL CRACK LOCATISDR CA080227007Bearing Race · spalledDURING FLIGHT THE PILOT HAD A CHIP LIGHT INDICATION. UPON INSPECTION, THE CHIP PLUG HAD LITTLE DEBRIS AND SMUDGE. THE CHIP WAS CLEANED, REINSTALLED AND FURTHER GROUND RUNS WHERE CARRIED OUT PRIOR TO FLIGHT. NO FURTHER ISSUES WERE NOTED AND THE FLIGHT CONTINSDR CA080215005Case Half · damaged(CAN) ON SPLITTING THE COMPRESSOR CASE HALVES FOR AN INSPECTION, IT WAS NOTED THERE WERE AREAS OF THE PLASTIC COATING THAT WERE MISSING. CASES REPLACED. (TC NR 20080215005)SDR AALA200800325Blade · failedMIA INFLIGHT T15FEB - NUMBER ONE ENGINE SURGING AFTER TAKEOFF AT 800 TO 900 FEET. CREW DECREASED THROTTLE AND SURGING STOPPED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND COMPRESSOR BLADE FAILURE. REPLACED NUMBER ONE ENGINE ON 16 FEB AT MIA. SYSTEMSDR VNAA0802009Blades · damagedCREW REPORTED A BIRD STRIKE TO THE RIGHT HAND ENGINE ON APPROACH. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGINE AND FOUND REMAINS AND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES IN ACCORDANCE WITH THE AIRCRAFT MAINTENASDR DL76G080193Fan Blade · damagedON T/O BIRD STRIKE LEFT ENG VIBS HIGH RETURNED FOR LNDG. NO SMELL IN CABIN ASSOC W/BIRD STRIKE NOTED. REPLACED DAMAGED FAN SETS NR 1 ENG. BOROSCOPED HPC FOUND NO BIRD STRIKE DAMAGE AFTER REMOVING BLADES VISUALLY INSPECTED CORE INTAKE FOUND NO DEBRIS. CORE SDR DL76G080190Fan Blade · damagedLEFT ENGINE INGESTED BIRDS AFTER TAKEOFF. CREW REPORTED LEFT ENG HIGH VIBRATION ENGINE NOT SHUTDOWN. RETURNED TO ACC. 6 FAN BLADES BEYOND LIMITS. HAVE NOT BORO CORE AT THIS TIME SENDING AMTS, BORO EQUIP AND FAN BLADES. REPLACED DAMAGED FAN SETS NR 1 ENG SDR SWIA200819219Compressor · smokeFLT NR 5833. SHORTLY AFTER TAKEOFF, RECEIVED SMOKE TOILET CAUTION MESSAGE, PERFORMED COMPRESSOR WASH ON BOTH ENGINES TO REMOVE DEICE FLUID FROM ENGINES IAW AMM 72-00-00.
SDR 2008FA0000099Scroll · brokenCOMPRESSOR (PN 23065593 SN CAC45245) WAS RECEIVED INTO THE SHOP FOR REMOVAL AND REPLACEMENT OF THE SCROLL (PN 23074076(B) SN 40353) FOR A VISIBLE OPEN HOLE OR BROKEN OFF HEX EXTERNAL BOSS LOCATING PIN AT THE TURNING VANE LOCATION ON THE SCROLL. THE OPERATOR CSDR UIEA200800023Compressor · stalledCOMPRESSOR STALL ON ENGINE 1. N1 DECREASED FROM 105 PERCENT TO 100 PERCENT REDUCED THRUST TO 33 PERCENT N1 STABILIZED FL 390, TAT -21 DEGREES. ON LANDING ROLLOUT, NR 1 N1 DECREASED AND EGT INCREASED TO 900 DEGREES. REPLACED ENGINE.SDR UPS08451576Fan Blade · damagedAFTER LANDING IN MEM, MX REPORTED DAMAGE TO MULTIPLE FAN BLADES AND INSIDE OF COWLING ON NR 2 ENGINE. THERE WERE NO IN FLIGHT INDICATIONS. REMOVED AND REPLACED 6 PAIRS OF FAN BLADES IAW MM 72-31-02. REMOVED AND REPLACED NR 2 ENG NOSE COWL IAW T C 5027. REPSDR U30A200800002Compressor · deterioratedFLT 270 ON CLIMBOUT, LEVEL 8000FT, FLT CREW HEARD 4-5 BANGS, WITH VIBRATION. CREW REVIEWED ENG & SYS PAGES OF ECAM, ALL NORM. NO ECAM MESSAGES OR WARNINGS. SUSPECT COMPRESSOR STALL, RETURNED TO EWR. LANDING UNEVENTFUL. BORESCOPED ENGINES NO DEFECTS NOTED.SDR ASMF200801002Blades · damagedDURING OVERNIGHT CHECK, 10 FAN BLADES OF THE RT ENG WERE DETECTED WITH DENTS AND LOSS OF MATERIAL DUE TO AN FOD. MAINTENANCE PERFORMED A BOROSCOPIC INSP IAW MM 72-00-00 AND NO ADDITIONAL DAMAGES WERE FOUND; THE 10 DAMAGED BLADES WERE REPAIRED IAW MM 72-33-21,SDR VNAA0801006Engine · failedCREW REPORTED A SMOKE TOILET CAUTION MESSAGE 5 SECONDS AFTER TAKEOFF. CREW ELECTED TO RETURN TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE RIGHT HAND ENGINE. MAINTENANCE FOUND EXTERIOR OIL LEAKAGE AT STAGES 2-5 OF THE SDR DLM88080095Fan Blade · bentDURING CLIMB-OUT, NR 1 ENG HAD TWO COMPRESSOR STALLS AND FLAMES AS REPORTED BY F/A AND PASSANGERS. REPLACED 1ST STAGE FAN BLADES PER TRANS 9T133.SDR SIMA200802105Blades · damagedON FLIGHT 3714, CREW REPORTED IN CRUISE FLT ENGINE 1 N1 VIB IND STARTED TO CLIMB AND THEN WENT INTO AMBER AT 1.9 CREW REDUCED POWER AND AT FIRST VIB IND WENT DOWN. IT THEN STARTED TO CLIMB AGAIN AND COULD BE FELT IN MAIN CABIN. CREW THEN DECLARED AN EMERGENCSDR DL764080074Compressor · failedATB DUE NR 2 ENGINE SURGE ENGINE WAS NOT SHUTDOWN C/FOUND METAL IN TAILPIPE. REPLACED NR 2 ENG. REPLACED RIGHT ENGINE.SDR COMA0870001Fan Blade · lack of lubeFLIGHT 5448 - LEFT ENGINE VIBE AT 1.9 AT CLIMB, REDUCED POWER TO 68% TO GET TO GO GREEN. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE FAN BLADES PER EO 72-017.SDR 2008UALA00097Blade · bentONE BLADE ON LEFT ENGINE BENT OVER 90 DEGREES. REPLACED BLADE NR 37 DUE TO BENT AND OPPOSITE BLADE NR 18 PER MM 72-31-02. THREE OTHER BLADES NR 35, 36, 38 ARE CF'D. ACCOMPLISHED RII INSPECTION OF NR 35 36 AND 38 BLADES PER MM 72-31-02, OK FOR FINAL .020\ INSDR SWIA200819019Stator Vane · damagedFLT 3976 - LEFT ENGINE STATOR VANE REQUIRES REPLACEMENT. REPLACED STATOR VANE IAW GE MM SEI 756 SP-47.
SDR CA080116019Impeller · saturated(CAN) AFTER UNEVENTFUL AND NORMAL SHUTDOWN, PILOT NOTICED A POOL OF OIL UNDER THE AC AND OIL ALL OVER THE ENGINE COWLS AS WELL AS SOAKING THE IB .2500 OF THE MAIN ROTOR BLADES. THERE WERE NO OIL TEMP OR PRESSURE CAUTION WARNINGS OR ENGINE CHIP LIGHT INDICATIONSDR CA071227002Sensing Element · chafed(CAN) RT 14TH STAGE DUCT MESSAGE DURING CLIMBOUT. FLIGHT RETURNED TO AIRFIELD. MAINTENANCE INSPECTION DISCOVERED 14TH STAGE COWL DUCT INSULATION BROKEN AND CHAFING ON SENSING LOOP. BOTH SENSING LOOP AND DUCT WERE REPLACED AND ENGINE RUN’S WERE C/O AND THE AC SDR HALA0700537Blade · damagedETOPS SIGNIFICANT SYSTEM, NR 1 ENG NR 1 BLADE HAS TEAR ON LEADING EDGE APPROX 3/4 INCH FROM TIP, APPROX 1/8 INCH DEEP AND 1/8 INCH WIDE, AREA A. BLENDED BLADE ON NR 1 ENG PER AMM 72-31-02. OK FOR SERVICE.SDR CA071219002Blade · failed(CAN) ENGINE SURGE ON LANDING. ENGINE RETURNED TO SHOP FOR SUSPECTED HPC STG 1 BLADES DAMAGE. DURING ENGINE DISSASEMBLY HPC ROTOR WAS FOUND WITH HEAVY DAMAGE, SUSPECT DAMAGE CAUSED BY A BLADE FAILURE AT PLATFORM. ALL FAILED PARTS WILL BE RETURNED TO THE OEM FOSDR 2007UALA05074Compressor · stalledRTFL DUE TO NR 1 ENGINE SURGE (COMPRESSOR STALL) AS A RESULT OF A BIRDSTRIKE.
SDR 2007UALA05072Compressor · stalledNR 2 ENGINE COMPRESSOR STALL REPORTED. IFSD.SDR CA071217001Fan Blade · damaged(CAN) CREW REPORTED N2 VIB ICON (RT ENG) POSTED DURING CRUISE AT FL320. CREW FOLLOWED QRH AND COULD NOT CONTROL VIB IFSD AND DIVERTED. MAINTENANCE OBSERVED FOD DAMAGE TO FAN BLADES. ENGINE REMOVED AND REPLACED (TC NR 20071217001)SDR MASA200700836Fan · damagedFOUND INDICATION OF ARC OUT AT THE 12 O'CLOCK POSITION IN AREA 8. REMOVED AND REPLACED FAN DISK, ALL OPS CHECK GOOD.SDR SIMA200733702Compressor · stalledCREW HAD SEVERAL E1 COMPRESSOR STALLS IMMEDIATELY AFTER TAKEOFF, FLEX THRUST WAS USED FOR TAKEOFF. SHUT DOWN LEFT ENGINE IN FLT PER CHECKLIST. REMOVED AND REPLACED LT ENGINE ASSEMBLY IAW EC 71-002. AIRCRAFT RETURNED TO SERVICE.SDR USAA920071227Engine · stalledENG NR 2 COMPRESSOR VANE FAULT, COMPRESSOR STALLED AND ENG NR 2 SHUTDOWN. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF HPT STAGES THROUGH 8 HPC AND 1ST STAGE BLADES AND VANES. SUBSTANTIAL WEAR OBSERVED THROUGHOUT ALL AREAS INSPECTED AS WELL AS MODERATE HEATSDR AALA20072265Fan · fodORD INFLIGHT - NUMBER ONE ENGINE LOST POWER DURING CLIMB. CREW HEARD LOUD POPS. PULLED THROTTLE TO IDLE AND LEFT NUMBER ONE ENGINE AT IDLE FOR LANDING. NUMBER ONE ENGINE PARAMETERS WERE NORMAL. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE AND I
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