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 UALA2011082204487Guide Vane · damagedNR 2 ENGINE EXIT GUIDE VANES HAVE METAL TAPE COMING LOOSE. RETAPED NR 2 ENGINE EXIT GUIDE VANES FROM 9 O'CLOCK TO 3 O'CLOCK POSITIONS.SDR UALA2011082204440Structure · damagedNR 1 ENGINE COMPRESSOR SECTION HAS A 1X1 HOLE AT 6 O'CLOCK POS IN HONEYCOMB UNDER BLADES. MX DETERMINED THE DEPTH OF OF THE HOLE TO BE ONE-QUATRER OF AN INCH DEEP, IT IS NOT THRU THE GLASS REINFORCED COMPOSITE LAYER. REF AMM 72-32-85. OK. TO CONTINUE IN SERVICSDR CA110929008Compressor Blade · broken(CAN) ENGINE BEING INDUCTED AT MFG. ENGINE REMOVED FOR HIGH TIME AND DURING BOROSCOPE OF ENGINE, HEAVY DAMAGE FOUND ON COMPRESSOR BLADES, STG 3, 4, 5, 6 AND 10. DAMAGE ON STG 4 AND 6 IS OUTSIDE ENGINE MANUAL LIMIT, 1 OFF, STAGE 4 BLADE BROKEN AT MID SPAN. OTSDR VNAA2011081800011Blade · bentCREW REPORTED POSSIBLE BIRD STRIKE ON TAKEOFF. NO VIBRATION INDICATION NOTED. AT CLT, MAINTENANCE INSPECTED, FOUND THREE (3) BENT BLADES IN RIGHT ENGINE FAN, REMOVED AND REPLACED THREE (3) SETS OF BLADES AND PERFORMED CHECKS USING MAINTENANCE MANUALS. AIRCRSDR Y2PA2011081400021Fan Blade · damagedACFT IN CRUISE FLIGHT AT FL360, CREW HEARD WHAT SOUNDED LIKE A COMPRESSOR STALL ON LT SIDE. ON CLOSING THE LT THROTTLE, NR 1 ENGINE WAS OBSERVED TO BE WINDING DOWN. DECLARED AN EMERGENCY. FOLLOWED COM PROCEDURE FOR ENGINE FAILURE ON DESCENT & DIVERTED. NRSDR UALA2011081504312Rub Strip · missingNR 2 ENGINE RUB STRIP MISSING AREA APPEARS LARGER THAN 2 X 1 INCHES. MEASURES 2.5 X 5 INCHES DAMAGE IN INNER LAYER. DAMAGE LESS THEN 3" IN DIA NEEDS TO BE REPAIRED WITHIN 500T OR 200C PER MM. THE DAMAGED AREA WAS INSPECTED PER CAPTAIN'S REQUEST THE DAMAGE ISDR CA110916001Seal · damaged(CAN) COMPONENT WAS FOUND WITH CYCLE EXCEEDED BY 714 IAW MM AIRWORTHINESS LIMITATIONS. COMPONENT REPLACED.SDR UALA2011081004184Tape · tornCREW REPORT: LT ENGINE SPEED TAPE ON FAN EXIT VANE IS TORN AND MISSING PIECES. ACP'D 'RE-TAPE' OF FAN-EXIT GUIDE VANES. OK TO CONTINUE IN SERVICE. REVIEWED WITH SAMC-EMC.SDR SWAA115652Engine · failedAIR TURNBACK, NR 1 ENGINE COMPRESSOR STALLED DURING CLIMBOUT FROM INITIAL TAKEOFF 1000FT. REMOVED AND REPLACED NR 1 ENGINE IAW MM.SDR DALA1147039881Fan Blade · brokenDURING TAKEOFF ROLL JUST ABOVE 80 KNOTS A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT SHIMMY. FLIGHT CREW ABORTED TAKEOFF AND NOTICED ENGINE NR 2 VIBRATION. ENGINE NR 2 WAS SHUTDOWN. MAINTENANCE FOUND FAN BLADES DAMAGED AND 1 BLADE BROKEN OFF AT THE BLADE ROOTSDR UALA2011080504077Blade · damagedBIRD STRIKE TO NR 1 ENGINE. ACCOMPLISH AIRFRAME BIRD STRIKE CONDITION INSPECTION PER AMM. ACCOMPLISHED BIRD STRIKE INSPECTION PER MM. FOUND 1 BLADE DAMAGED. NEED TO REPLACE 1 PAIR OF BLADES PCN 230-2728.SDR 2011FA0000528Compressor Wheel · damagedALUMINUM, STANDARD, 470 RIVETS ATTATCHING THE GASKET ON THE INTAKE SHROUD HAVE CORRODED HEADS THAT SEPERATED AND WERE SUCKED INTO THE COMPRESSOR THROUGH THE SCREEN AND CAUSING DAMAGE TO FIRST STAGE COMPRESSOR WHEEL. COMPRESSOR WHEEL WAS REPAIRED.SDR UALA2011072703849Fan Blade · damagedNR 1 ENG FAN BLADE AT 6 O`CLOCK POS HAS A NICK IN IT. DETERMINED DIMENSIONS OF NICK TO BE 1-32 INCH DEEP BY 1-16 INCH LONG IN AREA AT, 5 INCHES FROM BLADE TIP. DRESSED. REPAIRED NICK PER AMM TASK.SDR CA110803011Compressor · leaking(CAN) ON DEPARTURE, THE PILOT NOTED SMOKE IN CABIN DURING INITIAL CLIMB. THE FLIGHT WAS ABORTED AND THE ACFT RETURNED TO POINT OF ORIGIN WHERE AN UNEVENTFUL LANDING WAS MADE. POST FLIGHT INSPECTION FOUND OIL COMING OUT OF THE COMPRESSOR AREA, INLET, DRAIN. TSDR R61A20110191Fan Blade · bentCREW REPORTED BIRD STRIKE TO E-2 DURING CLIMBOUT OF CLT. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. A/C LANDED WITHOUT INCIDENT. MAINTENANCE COMPLETED BIRD STRIKE INPECTION AND REPLACED E-2 B, 1, 13, 14, 15, AND 27 FAN BLADES PER EMB AMM.SDR CA110725002Compressor · failed(CAN) CREW REPORT A FOUL ODOR EMANATING THROUGH CABIN ON CLIMB, ODOR DISSIPATED IN CRUISE. ON DESCENT/APPROACH, A TOXIC SMELL PERMEATED THROUGHOUT CABIN. SOME CREW MEMBERS WERE REPORTING SORE THROAT ASSOCIATED WITH THE TOXIC ODOR AND WANTED TO USE OXYGEN MASSDR HALA2011072400331Blade · damagedETOPS SIGNIFICANT SYS - RT ENG BLADE NR 36 HAS NICK ABOUT 4.5" FROM BLADE TIP. BLENDED RT ENG NR 36 BLADE IAW AMM 72-31-02. WITHIN LIMITS IAW AMM (AREA A). NO CRACKS NOTED DURING EDDY CURRENT INSP. OK FOR SVC.SDR CA110727002Compressor · failedENGINE FAILURE OCCURED. PRELIMINARY INSPECTION REVEAL COMPRESSOR FAILURE.SDR UALA2011071703631Fan Blade · damagedDURING WALK AROUND CREW FOUND DAMAGE TO ONE OF THE FAN BLADES ON NR 2 ENGINE. DETERMINE DIMENSIONS AND REPORT TO SAMC. BLADE NR 18. DAMAGE DETERMINED TO BE IN AREA 2 ON THE LEADING EDGE. LENGTH OF NICK IS 0.215" (ALONG L/E), AND 0.080"DEEP. DAMAGE HAS BEESDR ANCF2011052900081Blade · damagedBIRD STRIKE, DURING TAKEOFF (V1) ON ENG NR2, HIGH VIBRATION FELT AND STRONG NOISE WITH HIGH THRUST SETTING FG VIB N1 ENG NR2 REACHED 7 UNITS. R & R FAN ROTOR BLADES POS 9, 10, 11, 27, 28 AND 29 IAW AMM TASK 72-21-00-000-007, AMM 72-21-00-300- 028. REPLACEMENSDR CA110712004Impeller · mismanufacturedNEW FROM MFG, IMPELLER, PN 2660-1624-01, TOP EDGE OF IMPELLER RUBS ON BOTTOM OF STATOR HOUSING. IMPELLER SUSPECTED OF BEING DIMENSIONALLY INCORRECT. SENT BACK TO MFG FOR WARRANTY. THIS IS OUR SECOND OCCURANCE.SDR ASAA11510052Shim · wornREF T/C 78472002 FAN BLADE LUBE NR 1 ENG FOUND 24 WORN FAN BLADE SHIMS DURING LUBE. REPLACED 24 EA FAN BLADE SHIMS P/N 340 252 307 0 AND VERIFIED OK REF T/C 78472002 NR 1 ENG.SDR IPXA11667902Blade · damagedINSPECTION TYPE:E TOP, ATB - BIRD STRIKE ON TAKEOFF, LT FAN VIBRATION 5.0. ALL OTHER ENG INDICATIONS NORMAL. REPLACED 5 EA DAMAGED BLADES IAW EO80C2-7230-43438-A & AMM 72-31-02-4 VIB SURVEY W/I LIMITS IAW AMM 71-00-00-5.SDR AALA20110708SJU01Compressor · stalledSJU INFLIGHT STT-JFK. CREW REPORTED ON CLIMBOUT RIGHT ENGINE COMPRESSOR STALLS. RETARDING RIGHT THROTTLE AND COMPRESSOR STALL CEASED. EMERGENCY DECLARED FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT SSDR IPXA1B67755Actuator · inoperativeIFSD - NR 3 ENGINE COMPRESSOR STALL. EMERGENCY DECLARED FOUND VSV ACTUATOR INOPERATIVE. REPLACED VSV ACTUATOR IAW AMM 75-31-02-4. OPS AND LEAK CHECK GOOD.SDR CA110706002Impeller · mismanufacturedNEW IMPELLER FROM MFG HAD DAMAGE (DEEP NICK) ON IMPELLER VANE. SENT BACK TO MFG. DAMAGE OCCURED AT MFG, AS DAMAGE WAS PRIMERED OVER.SDR CA110707001Compressor Blade · damagedON POWER UP FOR TAKEOFF, CREW RECEIVED ECAM MESSAGE "ENGINE SURGE" FOLLOWED BY "ENG FAIL" MESSAGE. ACFT RETURNED TO GATE FOR INVESTIGATION. BOROSCOPE INSPECTION REVEALED MODERATE HP COMPRESSOR STAGE 5 BLADE DAMAGE AND SUBSTANTIAL HP COMPRESSOR STAGE 6 BLADE SDR CA110704004Compressor Blade · damagedSHORTLY AFTER TAKEOFF, THE CREW HEARD A LOUD BANG AND FELT A SEVERE VIBRATION, THE ENGINE INDICATION AND CREW ALERTING SYS (EICAS) DISPLAYED THE NR 2 ENGINE INTER TURBINE TEMP (ITT) AT 960C AND THE N2 CORE VIBRATION AMBER MESSAGE. THE CREW SHUTDOWN THE NR 2 ESDR CA110627011Engine · damaged(CAN) UNCONTAINED EVENT DURING FLIGHT, THE PILOT HEARD LOUD NOISES AND SAW SPARKS FROM THE ENGINE. IT WAS SHUTDOWN AND A SAFE LANDING FOLLOWED. POST FLIGHT INSP FOUND A SEVERELY DAMAGED COMPRESSOR AND SMALL PIECES CAME OUT THE INTAKE AND PUNCHED HOLES IN THESDR UALA2011062203055Blades · nickedNR 2 ENGINE HAS A NICK ON BLADE NR 12 AND A NICK ON BLADE NR 15. REPAIRED BLADES.SDR ASAA1159907Screw · out of positionNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS AFTER LAST FAN LUBE. DATA SCATTER INDICATES HARDWARE INSPECTION AND FAN RELUBE REQUIRED. C/W TASK CARD PERFORMED ON BOARD TRIM BALANCE AND VIBRATION SURVEY. POSITION NR 2 SDR UALA2011061402939Fan Blade · damagedENG 2 BIRD STRIKE. LCL MAINT REPORTS 2 EA FAN BLADES (21 & 22) WITH LEADING BEND IN AREA "AT" BEYOND LIMITS OF AMM. NO CRACKS NOTED AND NO EVIDENCE OF CORE INGESTION NOTED. VISUAL INSPECTION OF INLET AND SURROUNDING AREA ACCOMPLISHED, NO CRACK AT BEND BLADESDR SWAA114338Engine · malfunctionedINFLIGHT SHUTDOWN / DECLARED EMERGENCY. LOUD BANG AND REPORTED FLAMES FROM NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR USAA20110615BB053Fan Blade · damagedATH FLT 759 EN ROUTE ATH TO PHL. DURING TAKEOFF, AT ABOUT 50 FT AGL, A LOUD NOISE FOLLOWED BY A LEFT ENGINE VIBRATION OCCURRED. THE LEFT ENGINE POWER WAS PULLED BACK. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO THE FIELD IN ATH. THE FLIGHT LANDED WSDR 2011FA0000704Blades · fracturedAFTER ABOUT 1.5 HRS OF FLIGHT, THE PILOTS RETURNED TO LANDING AND SAID THAT THE NR1 ENGINE HAD A HIGH FREQUENCY RUMBLE AND JUST BEFORE LANDING, THE TQ AND EPR GAUGES DECRESED RAPIDLY, WHILE THE ENGINE TEMP AND OIL IND WERE STILL GREEN. AFTER SHUTDOWN, THE INLESDR A6WA201140500Engine · failedIN CLIMB, BETWEEN 8000-8500 FT A/P LT ENG MADE LOUD BANG FOLLOWED BY SHUDDERING AND VIBRATION ITT WELL ABOVE 900 DEGREES. BROUGHT LT ENGINE THRUST TO IDLE VIBRATION DAMPENED. ADVANCED ENGINE THRUST, BROUGHT NO ADDITIONAL THRUST RAN IMMEDIATE ACTION CHECKLISTSDR FDEA201106092172Blades · damagedON CLIMBOUT, HEARD VERY LOUD BANG, ACFT YAWED RT AND NR 2 ENGINE SPOOLED DOWN, NO RED ECAM. NR2 ENG FLUCUATED AT IDLE WITH HIGH EGT FOR ABOUT 30 SECS. ECAM SHOWED NR2 OVERLIMIT BUT GAUGES DID NOT SHOW ANY. ENGINE STABILIZED AT IDLE, LT IT RUNNING THERE, ALOSDR E3MA20110610Stator · failedSIGNIFICANT TORQUE SPLIT INDICATED ON VEMD FOLLOWED BY AN UNCOMMANDED ENGINE SHUTDOWN DURING CRUISE FLIGHT. A SUBSEQUENT BORESCOPE INSP OF NR 2 ENGINE, REVEALED A CRITICAL FAILURE OF THE COMPRESSOR TURBINE STATOR.SDR REXA201100348Blades · dirtyAIR RETURN RT ENG VIBE 2.0 IN FLT. MTX WILL PERFORM ENG TANG BLADE LUBE BLADES HAVE BEEN REMOVED CLEANED AND LUBED WILL START THE INSTALL PROCESS NOW IAW AMM 72-20-00.
SDR 2011FA0000332Compressor · separatedRETURNED FOR A REPORTED IN FLIGHT SHUTDOWN. REPAIR AND O/H DISASSEMBLED THE ENGINE IAW THE CURRENT MM FOR ENGINEERING INVESTIGATION. DISASSEMBLY FINDINGS REVEALED SEPARATION OF THE SECOND STAGE COMPRESSOR ROTOR ROTATING SHROUD. THE SHROUD WAS SUBMITTED TO PSDR AALA20110601MIA02Compressor · stalledMIA - CREW REPORTED AFTER TAKEOFF RIGHT ENGINE COMPRESSOR STALLED. EXHAUST GAS TEMPERATURE IN RED, AIRCRAFT VIBRATIONS AND FLAMES NOTED OUT OF RIGHT ENGINE. RETARDED RIGHT THROTTLE TO KEEP EGT IN LIMITS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUTSDR CA110531011Scroll · cracked2 INCH CRACK FOUND DURING SCHEDULED MX INSPECTION. SOME CASE MATERIAL FOUND MISSING. RECORDS INDICATE SCROLL PREVIOUSLY REPAIRED FOR A CRACK IN 2004. SCROLL TO BE FWD FOR REPAIR.SDR CA110606005Compressor · stalled(CAN) ABORTED TAKEOFF, DURING T/O, 2 COMPRESSOR STALLS WERE HEARD COMING FROM THE RT ENGINE. THE T/O WAS ABORTED AND THE ACFT RETURNED TO GATE. TROUBLESHOOTING IS ON-GOING.SDR CA110525009Stator · damagedDAMAGE WAS FOUND ON FAN STATOR VANES OF BOTH ENGINES. 12 VANES WERE FOUND DAMAGED ON THE LT ENGINE AND 11 VANES ON THE RT ENGINE. ALL DAMAGES ARE ON THE L/E OF THE VANE.SDR MASA2011052302826Blade · lack of lubeLEFT N2 VIBE CTN IN FLT. MX R2 ENG BLOCKER DOOR, LUBE SCAVENGE FILTER, PERFORM BLADE LUBE.SDR MASA2011052002790Fan Blade · vibrationNR 2 ENG FAN VIBE IN FLT AT 2.0. PERFORMED BLADE SHAKE AND RAN ENGINES WITH CREW. VIBE WITHIN LIMITS. APPLIED 50 CYCLE RO FOR BLADE LUBE.SDR UALA2011051602413Fan Blade · damagedENG NR 1: FAN BLADES NR 34, HAS DAMAGE ON LEADING EDGE ONE NICK. ACCOMPLISHED BLADE REPAIR REF MM.SDR QMLA2011050911056Impeller · damagedPART OF THE GASKET OF THE INLET SCREEN CAME LOOSE AND WAS INGESTED INTO THE ENGINE. ONE BLADE ON THE COMPRESSOR HAD DAMAGE THAT CAUSED A LOUD WHINING NOISE WHEN THE ENGINE WAS OPERATED. THE ONLY DAMAGE THAT CAN BE OBSERVED IS THE COMPRESSOR BLADES. IT IS BESDR ASAA1159622Seal · tornWHILE ACCOMPLISHING T/C 78472002 FOUND NR 2 ENGINE FAN BLADE PLATFORMS WITH TORN SEALS (24 EA) P/N 340 001 816 0. REMOVED & REPLACED NR 2 ENGINE FAN BLADE PLATFORMS (24 EA) P/N 340 001 816 0 REF T/C 78472002.SDR ZZDA2011452Compressor · stalledLEFT ENG COMPRESSOR STALL IN FLIGHT. SHUT DOWN LEFT ENGINE IAW CHECKLIST. WOULD NOT RUN SMOOTHLY ABOVE IDLE. REMOVED AND REPLACED NR 1 ENG REF W/O 235947. T/C 603. ALL OPS CHECKS GOOD.
Back to JASC 7230