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 2006UALA00574Compressor · stalledENGINE NR 2 COMPRESSOR STALL - RTFL. ALL TROUBLE SHOOTING CHECKS RETURN NO DEFECTS.SDR AWXA200600465Actuator · malfunctionedCREW REPORTED THAT DURING TAKEOFF RECEIVED A NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE PRIOR TO 80 KNOTS, ABORTED TAKEOFF. RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED HIGH POWER PERFORMANCE TESTS IAW AIRBUS 319 TSM 75-30-00-810-843. FAUSDR AWXA200600468Warning Light · false activationFLT 841 - CREW REPORTED THAT DURING TAKEOFF RECEIVED NR 1 ENGINE COMPRESSOR VANE FAULT ON ECAM. ABORTED TAKEOFF UNDER 70 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED HIGH POWER ASSURANCE TESTS IAW AWA TASK CARD F5M71302. OPERASDR AWXA200600466Actuator · lack of lubeCREW REPORTED, RECEIVED A NR 1 ENGINE VANE FAULT AND ABORTED TAKEOFF AT 60 KNOTS. CREW REPORTED NO OTHER ABNORMAL ENGINE READINGS AND OBSERVED NO COMPRESSOR FAULTS. CREW RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT IAW AIRBUS TSM 73-0SDR 06FDEA0973Compressor · stalledDEPARTING 23R IND USING STD PWER, EXPERIENCED COMPRESSOR STALLS ON NR 2 ENGINE. REJECTED TAKEOFF AT 50KTS AND EXITED RWY. ENGINE GAUGES WERE NORMAL EXCEPT NR 2 EPR, WHICH BARELY CLIMBED WHEN POWER WAS APPLIED. LEARN FROM THE MISTAKES OF OTHERS. REMOVED ANDSDR CA060307008Vane · chafed(CAN) NR 1 ENG STALL, ENG 1 SHUTDOWN AND LANDED. BORESCOPE CARRIED OUT IAW AMM 72-00-00-200-003 AND 72-31-00-290-001 FOUND 3 RD STAGE VSV VANES RUBBING ON IB END MAKEING A GROOVE WITH DISPLACED METAL AT BOTH ENDS OF VANE TRAVEL. (TC NR 20060307008)SDR XN0A1308Compressor · stalledCOMPRESSOR STALL (OFF IDLE) NR 2 ENGINE. INSPECTED NR 2 ENGINE INTAKE AND EXHAUST, NO DEFECTS NOTED. PERFORMED ENGINE POWER RUN, NR 2 ENGINE IAW B727 MM 71-00-00, NO DEFECTS NOTED. SUSPECT HIGH CROSS WIND COMPONENT, NR 2 ENGINE NO DEFECT NOTED.SDR 2006UALA00343Blade · damagedCREW REPORTS MOMENTARY ENGINE 2 COMPRESSOR STALL UPON LEVEL OFF AT FL310. HPC BORESCOPE INSPECTION REVEALED 6TH STAGE BLADE DAMAGE BEYOND LIMITS. REPLACED HPC STG 6 BLADES.SDR MASA200600516Fan Blade · failedASH 6531 COS - THE CREW DIVERTED INTO FMN DUE TO A LOSS OF POWER ON THE NR 2 ENGINE AND A LOUD BANG FOLLOWED BY THE CREW SHUTTING DOWN THE ENGINE. UPON LANDING IT WAS DETERMINED THAT ICE HAD FORMED AT POTABLE WATER SERVICE PANEL AND WAS INGESTED BY THE NR 2 ESDR 2006UALA00350Compressor · stalledCOMPRESSOR STALL DESCENDING OUT OF FL370. RECOVERED INSTANTLY. NO FLUXUATIONS IN ANY ENG PARAMETERS,ONLY AN AUDIBLE REPORT. :ACP STEPS 1 THRU 7 OF COMPRESSOR STALL TROUBLESHOOTING MANUAL REF 71-00-92 INCLUDING BOROSCOPE STEP 3 REF MM 72-00-41. NO LIMITING DESDR KBM2006F00067Bleed Valve · intermittentDURING GROUND RUN-UP BLEEDVALVE CLOSING AND OPENING INTERMITTENTLY, REMOVED AND REPLACED. (K)SDR AALA20060110Compressor · stalledSERIES OF COMPRESSOR STALLS ON NR 2 ENGINE AT ROTATION THROUGH CLIMB. WOULD NOT CLEAR IN POWER REDUCTIONS. REPORTS OF ENGINE FIRE FROM AIR TRAFFIC CONTROL AND FLIGHT ATTENDANTS. ENGINE FIRE SEVERE DAMAGE CHECKLIST COMPLETED. RETURNED TO SJO AND LANDED WITHSDR SWAA060524Compressor Wheel · wornDURING SCHEDULED HC2 CHECK, FOUND NR 1 ENGINE FAN DISK WORN ON TOP SURFACE OF FWD FLANGE ALL THE WAY AROUND HUB. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR CA060208006Scroll · cracked(CAN) ON INSPECTION THE ENGINEER WAS TAKING APART THE ANTI-ICE BODY 6856984 FOR INSPECTION AND FOUND A CRACK AROUND THE BOSS. (TC NR 20060208006)SDR MWEA060012Blades · bentLEFT ENGINE COMPRESSOR STALL/SURGE. REMOVED BENT TIPS AS NECESSARY ON VARIOUS ENGINE BLADES AND BLENDED AS REQUIRED PER IAW BOEING MM 72-33-22.SDR DL757060104Engine · malfunctionedAT FLT LVL 360 LOUD BANG FROM LEFT ENGINE. ENGINE SHUT ITSELF DOWN. PASSENGERS ON LEFT SIDE OF A/C SAW FLAMES FROM TAILPIPE OF LEFT ENGINE. REPLACED ENGINE.SDR CA060227010Compressor · seizedTHE ENGINE ACCESSORY GEARBOX CHIP DETECTOR WARNING ANNUNCIATED IN FLIGHT AND AN UNSCHEDULED LANDING WAS CARRIED OUT. SUBSEQUENT INSPECTION REVEALED SEIZURE OF THE COMPRESSOR SECTION. P&WC WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABSDR C2XA06CL021Blades · damagedCLE FLT 2503 THE CREW REPORTED THE NR 2 ENGINE HAD HIGH VIBRATION (LP) WHEN THE THRUST LEVER WAS ADVANCED FROM FLIGHT IDLE. ALSO REPORTED A BURNING SMELL IN THE COCKPIT. EMERGENCY WAS DECLARED ON DESCENT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCESDR AWXA200600201Compressor · stalledDFW - ENGINE ANOMALY - FLIGHT CREW REPORTED THAT AT FL 350 AND MODERATE TURBULENCE THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALLS. THE ENGINE DID NOT FLAME OUT AND THERE WEREN'T ANY PARAMETERS EXCEEDED. AIRCRAFT LANDED IN DFW WITHOUT FURTHER INCIDENT. MAINSDR ASMF200602001Fan Blade · damagedDURING TRANSIT CHECK, DETECTED 09 LEFT ENGINE FAN BLADES WITH DAMAGES. ONE OF THEM WAS OUT OF LIMITS. 04 FAN BLADES WERE REPLACED IAW M/M 72-33-21 AND 06 WERE REWORKED IAW M/M 72-33-22. ENGINE WAS OPERATIONAL CHECKED IAW MPCM 71-00-01 AND M/M 71-00-00, TESTSDR AALA20060073Blade · failedSEA INFLIGHT T875/01FEB, AFTER TAKEOFF AT 6000 MEAN SEA LEVEL HEARD A BAND AND INDICATIONS FOR LEFT ENGINE ROLLED BACK TO ZERO. ENGINE SHUTDOWN WAS COMPLETED AND RETURNED TO SEA AND LANDED WITHOUT INCIDENT. THERE WERE NO FIRE INDICATIONS AND NO BOTTLES USED.SDR CA060608005Impeller · cracked(CAN) PILOT REPORTED HIGH TURBINE TEMPERATURES IN FLIGHT, RETURNED TO MAINTENANCE FACILITY AND FOUND CRACK IN COMPRESSOR SCROLL AREA UPON VISUAL INSPECTION AFTER LANDING. ENGINE ASSY WAS REMOVED AND COMPRESSOR INLET WAS INSPECTED AND FOUND TO HAVE A DAMAGED ISDR DL76G060095Compressor · damagedDURING ETOPS PDC FOUND PIECE OF 5TH STAGE VSV LEVER ARM IN COWLING. VSV LEVER AT 8 O`CLOCK POS VERIFIED BROKEN VANE SPINS FREELY IN CASE. BOROSCOPED HPC AND FOUND NUMEROUS BLADES DAMAGE 6TH STAGE. REPLACED ENGINE.SDR AWXA200600133Blade · lack of lubeOAK - ABORTED TAKEOFF - FLT 855 - CREW REPORTED THAT IMMEDIATELY AFTER FLEX POWER WAS SET RECEIVED ENG 2 COMPRESSOR VANE FAULT. CREW ABORTED T/O AT LESS THAN 10 KNOTS. MAINTENANCE TROUBLESHOT AND PERFORMED VSV BLADE LUBE IAW AMM 75-32-42-640-010.SDR SWAA060255Compressor · stalledAIR TURNBACK, NR 2 ENGINE COMPRESSOR STALLED. PERFORMED ENGINE BOROSCOPE & FOUND DAMAGE TO 7TH, 8TH & 9TH STAGE HPC BLADES BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR 2006FA0000076Turbine Wheel · migratedDURING A ROUTINE 600 HR BORESCOPE INSP OF THE GAS GENERATOR TURBINE BLADES, 2 BLADES WERE FOUND TO HAVE MOVED AFT IN THEIR (FIR-TREE) TYPE MOUNTS IN THE TURBINE DISK. 1 BLADE WAS FOUND TO HAVE MOVED .1250-.2500 INCH, AND THE OTHER LESS THAN .1250 INCH. THE BSDR SWAA060198Compressor · stalledABORT T/O, NR 1 ENGINE COMPRESSOR STALLED. PERFORMED ENGINE BOROSCOPE & FOUND DAMAGE TO 7TH, 8TH & 9TH STAGE HPC BLADES BEYOND LIMITS. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR SWAA060197Compressor · stalledAIR TURNBACK, NR 1 ENGINE COMPRESSOR STALLED. PERFORMED ENGINE BOROSCOPE & FOUND DAMAGE TO 8TH STAGE HPC BLADES BEYOND LIMITS. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR 2006F00001Engine · flamed outFELT VIBRATION AT 27,000 ENROUTE. SPARKS, FLAMES EMITTING FROM ENGINE COMPARTMENT. SHUTDOWN ENGINE, EMERGENCY LANDING. PRELIMINARY CAUSE SUSPECTED TO BE FROM COMPRESSOR RUB. ENGINE UNDERGOING EVALUATION. TIME SINCE OVERHAUL 1648.SDR ARWA20060101Engine · stalledLOG PAGE NR 117483. NR 3 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE. (SEE LOG PAGE NR 117486) REMOVED NR 3 ENGINE DUE TO COMPRESSOR STALLED AND REPLACED NR 3 ENGINE IAW ARROW AIR MM CHECK CARD NR 143-R7101; RUN UP CHECK GOOD. ACCOMPLISHED RED BORDER NR 18948SDR SQJ2006F00001Tube · brokenBLEED AIR TUBE (PN C46P181211) WAS REMOVED TO GAIN ACCESS TO PYLON. WHEN TUBE WAS REMOVED 2 PIECES OF CURLED METAL FOUND LODGED IN NACELLE ANTI-ICE SHUTOFF VALVE (PN 27441482). PIECES OF METAL WERE REMOVED W/O EFFORT. INSP WAS PERFORMED ON TUBE, FOUND WHENSDR CA060110005Shroud · distortedDURING A RECTIFICATION INSPECTION OF RENTAL ENGINE, CT SHROUD SEGMENT RETAINING RING OF POST SB 1627 CONFIG FOUND LOOSE AND MINOR SHIFTING OF CT SHROUD SEGMENT WAS NOTED. CT SHROUD SEGMENT-RETAINING RING WAS OF POST SB 1627 CONFIG AND CT SHROUD SEGMENTS (P/N SDR ALG2006F00004Compressor · fodA LOUD ENGINE WHINE OCCURRED DURING TAKEOFF. THIS FLIGHT WAS A MAINTENANCE OPERATIONAL CHECK FLIGHT. A VISUAL INSPECTION REVEALED FOD DAMAGE TO THE ENGINE COMPRESSOR. THE ENGINE WAS REMOVED AND A SERVICEABLE ENGINE WAS INSTALLED. (K)SDR ZN3R556712Stator · separatedENGINE 4TH LPC STATOR HAD INNER RING FRACTURE, LEADING TO A SINGLE VANE SEPARATING FROM THE STATOR ASSEMBLY. THE VANE CAUSED DAMAGE TO THE HPC AREA OF THE ENGINE. AIRCRAFT DID NOT EXPERIENCE ANY PROBLEMS WITH ENGINE DURING FLIGHT, AND PERFORMED SCHEDULED LANSDR CA060129013Compressor · damaged(CAN) DURING DESCENT, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION, ACCOMPANIED BY NOISE AND FLAMES EMANATING FROM THE EXHAUST. THE ENGINE WAS SHUT DOWN IN FLIGHT, AN EMERGENCY DECLARED AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSSDR CA060103001Engine · failedAT APPROXIMATELY 09:30 THIS MORNING, THE RT ENGINE OF KING AIR 200 HAD AN IN-FLIGHT TORQUE ROLL BACK TO APPROX 200 FT LBS, WITH A RISE IN ITT TO APPROX 680 DEG C, WITH A POPPING NOISE AND CORRESPONDING FLAMES FROM THE RT ENGINE EXHAUST. THE CREW INITIATED THESDR CA060503006Plenum · cracked(CAN) AIRCRAFT TOOK OFF FROM AIRPORT RUNWAY 15 OR A COURIER FLIGHT. THE AIRCRAFT CRASHED ABOUT 500 METERS EAST OF, AND APPROXIMATELY ABEAM, THE SOUTH END OF RUNWAY 15, ABOUT 300 METERS BEYOND THE AIRPORT PERIMETER. A POST-CRASH FIRE OCCURRED. THE AIRCRAFT WAS SDR CA060503005Plenum · cracked(CAN) AC TOOK OFF, AC CRASHED, POST-CRASH FIRE OCCURRED. AC WAS DESTROYED. BOTH PILOTS FATALLY INJURED. DURING TEAR-DOWN OF RT ENG (WHICH WAS FOUND TO BE OPERATING AT HIGH POWER ON IMPACT) P3, BLEED AIR BOSS WELDS WERE EXAMINED BY FPI USING A 2X POWER MAGNIFYISDR 2005FA0001612Diffuser · separatedCOMPRESSOR REPORTED STALLING. VERIFIED ON TEST CELL. UPON DISASSEMBLY DIFFUSER VANE RING WAS FOUND TO HAVE THE AFT STUD BAND (RING) SEPARATED FROM THE DIFFUSER ASSEMBLY BODY. DIFFUSER INSTALLED NEW AT LAST OVERHAUL 449.3 HOURS PRIOR.SDR CA051222003Blades · damagedRT ENG IFSD WHEN AT FLT LVL 30,000 FT, CREW REPORTED EXCESSIVE VIBRATION ON RT ENG WAS FELT AND THEN SHUT DOWN ON ITS OWN. CREW THEN FOLLOWED QRH, DECLARED EMERGENCY AND DID A SINGLE ENGINE LANDING WITH NO FURTHER INCIDENT. A LOT OF BLADES DAMAGED INSIDE INLSDR DL75K050798Manifold · crackedLEFT ENGINE SURGE AFTER START. REPLACED P4.9 MANIFOLD AND 14TH STAGE BLEED CONVERTER VALVESDR CA060129016Case · fractured(CAN) DURING APPROACH, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY NOISE AND VIBRATION. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT ISPECTION REVEALED A FRACTURED INLET CASE STRUT. (TC NR 20060129016)SDR AU510002194Fan Blade · bird strikeNR 2 ENGINE FAN BLADES (4OFF) DAMAGED BY BIRDSTRIKE.SDR AU510001954Compressor · misrepairedNR 3 ENGINE FIRST STAGE COMPRESSOR BLADE BLENDED BEYOND LIMITS IN MAINTENANCE MANUAL. RECORDS GAVE NO INDICATION OF BLEND REPAIR BEING CARRIED OUT.SDR AU510001637Spacer · incorrect(AUS) NR 2 ENGINE FAN BLADE SPACERS WERE INCORRECT PART. FAN BLADES NR 9, NR 10, NR 17, NR 18, NR 19 AND NR 20 WERE AFFECTED. INCORRECT PN 340-001-261-0 SPACERS FITTED. CORRECT PNO 340-001-215-0. INCORRECT PART. PERSONNEL/MAINTENANCE ERROR. (CASA NR 510001637SDR AU510001475Pin · loose(AUS) DURING FAN LUBE INSPECTION OF THE FAN HUB FOUR (4) FORWARD BOOSTER SPOOL PINS WERE FOUND TO BE VISIBLY LOOSE. AFTER A TORQUE CHECK OF THE REMAINDER, A FURTHER FIVE (5) PINS WERE FOUND TO BE LOOSE. TOTAL NUMBER OF UNDERTORQUED PINS NINE (9). (OTHER CAUSE:SDR AALA20050813Compressor · stalledSTL - AT FL280 RIGHT ENGINE COMPRESSOR STALLED. OPERATED ENGINE AT IDLE AND LANDED STL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR PCSA12070501Compressor · stalledFLIGHT 723 DEPARTED MIA AND CLIMBED TO 34,000 FT CRUISE ALTITUDE, CREW REPORTED NUMBER 2 ENG COMPRESSOR STALLED, POWER WAS REDUCED AND NR 2 ENG CONTINUED TO COMPRESSOR STALL. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, ALL FLIGHT CONDITIONS WERE NORMASDR DHL2005753004Compressor · stalledCREW REMARKS NOTED COMPRESSOR STALL ON T/O, ENGINE UNKNOWN. OAT +2 C, P.A. 19FT, TOGW 152,900, IAS 0 (GS EST 10 KNTS) B.E. N/A. INSPECTED INLET AND EXHAUST SECTIONS ON ENGINES 1, 2, AND 3 IAW AOPM CH 1.8 PG. 5, NO DEFECTS NOTED AT THIS TIME.SDR 2005FA0001561Blades · debondedDURING ROUTINE ENGINE A-CHECK INSPECTION, FOUND 15 OUT OF 24 (CHOCKING PADS) ON BASE OF ENGINE FAN BLADE TO HAVE MIGRATED AFT OF NORMAL POSITION DUE TO DEBONDING OF (CHOCKING PAD). THIS CONDITION WAS CAUSING ABNORMAL ENGINE VIBRATION DURING ENGINE GROUND OPER
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