JASC 7230
Service difficulty reports · 5,064
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 FDEA202309131592Compressor · loose#1 ENG FAN CASE AREA PROTECTIVE PLASTIC COVER FOR KEVLAR SEPERATING FROM COMPRESSOR CASING AT FWD EDGE SEVERAL PLACES REPAIRED #1 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WITH PATCH IAW B757 AMM: 72-34- 10-8-4SDR FDEA202309131590Compressor · loose#2 ENG LP COMPRESSOR CASE KEVLAR WRAPPING PROTECTIVE PLASTIC COVER, SEVERAL REPAIRS PATCHTAPE PEELING OFF. REPAIRED #2 ENGINE LP COMPRESSOR CASE TEFLON SLEEVE WIHT PATCH IAW B757 AMM 72-34- 10-8-4SDR DALA2023090607261Unknown · unknownSHIP 0175 - ATB/IFSD - AIRCRAFT RETURNED TO PRG DUE TO RIGHT ENGINE FAILURE AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN THE TAIL PIPE. ENGINE CHANGE COMPLETED.(5156318)SDR NACA202308284001Unknown · unknownDURING POST FLIGHT WALK AROUND #1 ENGINE #15 BLADE HAD A NICK ON LEADING EDGE. BLENDED #1 ENG FAN BLADE #15 WHICH IS 18" FROM BLADE TIP .015" WITHIN SERVICEABLE LIMITS AS PER PW AMM 72-31-02. NDT INSPECTION COMLETED.SDR NACA2023081900004Unknown · unknown#2 ENG #17 BLADE HAS NICK. REMOVED NICK AT #2 ENG BLADE #17. DISTANCE 2 3/8, LENGTH 0.591 DEPTH IS .073 IS WITHIN LIMITS IAW B767-300 AMM 72-31-02SDR NACA2023081900003Unknown · unknown#2 ENG #8 BLADE HAS NICK. REMOVED NICK AT #2 ENG BLADE #8. DISTANCE 11 1/8, DEPTH 0.65, LEGTH 0.458 IS WITHIN LIMITS. IAW B767-300 AMM 72-31-02SDR NACA2023081900002Unknown · unknown#2 ENG BLADE #7 HAS NICK. REMOVED NICK @ #2 ENG BLADE #7 DISTANCE 2.25 LENGTH -80 DEPTH .084, IS WITHIN LIMITS IAW B767-300 AMM 72-31-02SDR NACA2023081900001Unknown · unknown#2 ENGINE BLADE #2 HAS NICK. REMOVED NICK AT #2 ENG #2 BLADE DISTANCE 3/4 LENGTH =-204 DEPTH .054, IS WITHIN LIMITS IAW B767-300 AMM 72-31-02SDR ASAA2023081144556Bushing · missing#2 ENGINE VSV 3RD STAGE BRIDGE ON L/H SIDE ( "B" CHANNEL ) HAS 4 MISSING BUSHING. GROUNDED - YES. REMOVED #2 ENGINE VSV 3RD STAGE BRIDGE CONNECTING LINK REF. AMM 72-32-00-900-804-F00. REPLACED 4 EA. BUSHING ON BRIDGE CONNECTING LINK ASSY. REF. EIPC # 72-00-02-SDR ASAA2023080744488Unknown · unknownWHILE ACCOMPLISHING T/C SBCFM56-7B-72-0986-1 ON #2 ENG SN 658693 FOUND STAGE 2 ANTI ROTATION PINS AT 9:00 AND 3:00 ALF ROTATED BETWEEN 0 AND 45 DEGREES. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023080644487Unknown · unknownWHILE ACCOMPLISHING TC: SBCFM56-7B-72-0986-1, FOUND STAGE 2 ANTI ROTATION PIN @ 9:00 POSITION HAS ROTATED BETWEEN ZERO BUT LESS THAN FOURTY FIVE DEGREES. ENG #1 S/N: 658688. GROUNDED - YES. ON DEFERRAL.SDR 2023FA0000401Stator Vane · warning messageDURIG CRUISE AT 18000 FT ENG 1 COMPRESSOR VANE APPEARS ON ECAMSDR QR9R2023072800001Compressor · out of limitsAXIAL COMPRESSOR MOD 02 ASSEMBLY FAILED DURING RUNOUT CHECK (BEYOND ALLOWABLE LIMIT).SDR CALA2023063002110Compressor · stalledLEFT ENG COMPRESSOR STALL AT 1500 FT TWICE PERFORMED MAG CHIP DETECTOR INSPECTION ON LT ENGINE IAW AMM 79-21-03-404-074-R00. NO DEFECTS FOUND. NR 1 ENGINE REPLACEMENT ACCOMPLISHED. REF WORKCARD 19-7200-9-0001. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1812852SDR 2023FA0000324Vane · separatedOPERATOR NOTICE LOSS IN ENGINE POWER. KEYSTONE TESTED THE ENGINE TO VERIFY POWER NUMBERS. TECHNICIAN INSPECTED THE COMPRESSOR TO DISCOVER DIFFUSER VANE ASSEMBLY HAD VANES SEPARATING FROM AFT PLATE. PART PREVIOUSLY OVERHAULED FROM APPROVED VENDOR.SDR DALA2023061204752Unknown · unknownSHIP 0171- ATB- RIGHT ENGINE BIRD STRIKE ON TAKEOFF W/ SURGE MESSAGE. CORRECTIVE ACTION: C/W RIGHT ENGINE BIRD STRIKE INSPECTION, ALL INSPECTIONS CHECK GOOD.(4801878)SDR CALA2023060201743Compressor · fumesUPON TAKEOFF STRONGFUMES THROUGHOUTCABIN. NO SMOKE OR HAZEFUMES CAME AND WENT REF TSM TASK 71-00-00-810-801-A PARAGRAPH 4 FAULT ISOLATION, COMPLETED UP TO 4.J. ( BLIND CAP SEAL REPLACED ON LOG 4675692) . CONTINUE WITH BORESCOPE OF LP COMPRESSOR. REF TSM TASK 7SDR ASAA2023052143317Hook · wornWHILE ACCOMPLISHING ASA T/C SBCFM56-7B-72-1074-1 FOUND J HOOK WORN THROUGH AND MISSING MATERIAL AT 2 LOCATION ON #1 ENGINE 4TH STAGE VSV. PER STEP 8 A1 REQUIRES ENGINE CHANGE. CAN BE DEFERRED FOR A MAX OF 10 CYCLES , ENGINE SERIAL NUMBER 804627. GROUNDED - YESSDR 2023FA0000260Drum · crackedCRACK IDENTIFIED IN THE 9-12 DRUM (LLP). ENGINE SN V18736 WAS INDUCTED FOR INVESTIGATION OF HIGH N2 VIBRATION AND PERFORMANCE LOSS. THIS IS A FIRST RUN ENGINE WITH NO PRIOR SHOP VISITS FROM NEW. DURING THE DISASSEMBLY AND INVESTIGATION OF THE HPC THE CHCEC HASSDR AALA202305129630Sense Line · damagedAIRCRAFT WAS GROUNDED: ENGINE #2 ROLLED BACK TO APPROXIMATELY 50 % N1 FOR 3-5 SECONDS, THEN RETURNED TO NORMAL ON CLIMBOUT. EMERGENCY DECLARED; FLIGHT RETURNED TO PHX LANDING SAFELY. MAINTENANCE REPLACED ENGINE #2 PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) SDR AALA202305121845Fitting · faultyAIRCRAFT WAS GROUNDED: ENGINE #2 ROLLED BACK TO APPROXIMATELY 50 % N1 FOR 3-5 SECONDS, THEN RETURNED TO NORMAL ON CLIMBOUT. EMERGENCY DECLARED; FLIGHT RETURNED TO PHX LANDING SAFELY. MAINTENANCE REPLACED ENGINE #2 PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) SDR DALA2023032802384Unknown · unknownSHIP 669 -ATB/IFSD- PERFORMED AIR TURN BACK FOR LEFT ENGINE STALL ON CLIMB OUT. N1 ROLLED BACK AND ENGINE WAS SHUT DOWN BY CREW. METAL FOUND IN TAIL PIPE. CORRECTIVE ACTION: R/R NUMBER 1 ENGINESDR 2024FA0000897Compressor Blade · fracturedCT BLADE SEPARATED FROM ENGINE WITH ENGINE ONLY 3049 HRS AND 3090 CYCLES SINCE OEM REPAIR ON COMPRESSOR. AIRCRAFT WAS ON A CROSS COUNTRY FLIGHT OVER MOUNTAINS WHEN CT BLADES SEPARATED.SDR DALA2023032102115Unknown · unknown'SUPPLEMENTAL INFOMATION' SHIP 180 -DIV/IFSD- DIVERTED TO LHR DUE TO LEFT ENGINE COMPRESSOR STALL. FLIGHT CREW SHUTDOWN ENGINE ON APPROACH DUE TO RISING EGT. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN TAIL PIPE, REPLACED LEFT ENGINE. (4638134)SDR CALA2023031000685Compressor · stalledCOMPRESSOR STALL NUMBER2 RETRN TO FIELDENGINE WAS NOT SHUT DOW ACCOMPLISH COMPLETE TROUBLESHOOTING OF SURGE OR STALL ON ENGINE 2 PER TSM 71-00-00-810-809-A. MAINTENANCE CONTROL FOR EVALUATION. PERFORMED BOROSCOPE INSPECTION ON NUMBER 2 ENGINE COMPRESSOR SECTIOSDR ASAA2023030242144Engine · worn#1 ENG SN 804679 HPC STAGE 3 STATOR INNER HONEYCOMB SEAL AFT J-HOOK AT 12 O'CLOCK WORN OUT OF LIMITS. 008" REMAINING MATERIAL AND MOVE THAN HALF ONE SHROUD LENGTH LONG. REF ASA TC SBCFM56-7B-72-1074-1. GROUNDED - YES. REMOVED ESN 804679. REF ASA SHOP W/O # 194SDR ASAA2023030242143Engine · worn#2 ENG SN 804685 HPC STAGE 3 STATOR INNER HONEYCOMB SEAL AFT J-HOOK AT 12 O'CLOCK IS COMPLETELY WORN THROUGH THE MATERIAL REF TC SBCFM56-7B-72-1094-1. GROUNDED - YES. REMOVED ESN 804685. REF ASA SHOP W/O # 1944793.SDR ASAA2023022742086Engine · vibration#1 ENGINE TREND DATA SHOWS A RAPID RISE IN LOW PRESSURE ROTOR VIBRATION LEVELS AFTER ENGINE INSTALLATION. GROUNDED - YES. REMOVED #1 ENGINE ESN 874470. REF ASA SHOP W/O 1944222.SDR DALA2023022401412None · noneSHIP 6712 -ATB/DE- FLIGHT RETURNED TO ATL DUE TO REPORTED RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: T/S AND REMOVED AND REPLACED ENGINE.SDR ASAA2023022042089Engine · vibrationDURING CLIMB JUST PRIOR TO LEVEL OFF, # 1 ENG VIBE. VIBE 4.1 CONSULTED QRH, DURING THIS TIME A/C LEVELED AT FL 340 & THRUST REDUCED. VIBE REDUCED TO 3.0 10 MINUTES LATER VIBE AT 2.5. GROUNDED - YES. REMOVED #1 ENGINE ESN 874470. REF ASA SHOP W/O 1944222.SDR ASAA2023021641998Engine · damagedWHILE PERFORMING T/C SBCFM 56-7B-72-1074-1 , FOUND STAGE 3 AFT L-HOOK TO BE WORN THROUGH COMPLETELY AT 12 O'CLOCK POSITION ENGINE REMOVED REQUIRED WITH IN 10 CYCLE S/N 896963. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE. TRANSFERRED DEFECT TO SHOP W/O # 194SDR CALA2023021600464Engine · stalledCREW REPORTS #1 ENGINE STALL ECAM FOLLOWED BY EGT IN RED, ENGINE WAS SHUTDOWN. PER CREW ENGINE WINDMILLED APPROX 80 MINUTES AND THEY DID NOT RECALL IF POSITIVE OIL PRESSURE WAS MAINTAINED. LANDING WAS UNDER WEIGHT AND NORMAL. TOMC-MEREDITH ADDED ESN V11464 81SDR DALA2023020700965Not Reported · not reportedSHIP 3166 -ATO- CREW REPORTED AT 80 KNOTS HAD LOUD BANG AND LOSS OF LEFT ENGINE THRUST. INSPECTION REVEALED METAL IN LEFT ENGINE TAILPIPE. CORRECTIVE ACTION: REPLACED NBR 1 ENGINE. LP 2611412SDR DALA2023020700922Not Reported · not reportedSHIP 3125 -ATB- RETURNED TO TPA DUE TO #1 ENGINE STALL AND EGT RISE. THROTTLE PULLED BACK AND ATTEMPTED TO PUSH THROTTLE UP, EGT FOLLOWS. REPORTS OF AN AUDIBLE BANG. FOUND EXTENSIVE DAMAGE TO 4TH STAGE LPT BLADES. CORRECTIVE ACTION: C/W #1 ENGINE CHANGE REF AMSDR ASAA2023012341596Guide Vane · degradedWHILE PERFORMING T/C 78472022 SDI BORO HPT BLADES ON ENGINE #2 S/N 896824 FOUND OF STAGE 1 LPT NOZZLE GUIDE VANES. GROUNDED - YES. REMOVED ENGINE, INSTALLED ENGINESDR DALA2023011300280Compressor · stalledSHIP 6808 -ATO/FIRE- DECLARED EMERGENCY DUE TO RIGHT ENGINE COMPRESSOR STALL ON TAKEOFF ROLL WITH A CONTAINED TAIL PIPE FIRE. CORRECTIVE ACTION: R/R #2 ENGINE PER AMDS WORK CARD ALL CHECKOUTS COMPLETE.SDR ASAA2023010741493Nozzle · damagedWHILE PERFORMING ASA T/C 78472020 ON THE #1 ENG NOTED A THROUGH HOLE IN THE HPT NOZZLE OUTER PLATFORM AT THE LEADING EDGE @ 7 O'CLOCK ALF TOTAL AREA OF THE HOLE IS 0.002. GROUNDED - YES. REMOVED ENGINE SN 896273. REF ASA SHOP W/O #1938400, ESN 896273.SDR ASAA2023010741492Guide Vane · crackedWHILE PERFORMING ASA T/C 78472022 ON #1 ENG NOTED 2 LPT NGV'S WITH INTERSECTING CRACKS . ONE HAS MULTIPLE HOLES THIS IS AN UNSERVICEABLE CONDITION. ALSO THERE ARE 2 LPT NGV'S WITH FULL CRACKS. GROUNDED - YES. REMOVED ENGINE SN 896273. REF ASA SHOP W/O #1938400SDR 2023FA0000022Shaft · damagedHPC REAR SHAFT,GALLING LOC.2 IAW SUBTASK 72-41-13-220-189 NOT PERMITTED. LLP TO BE RETIRED WITH 12843 CYCLES SINCE NEW (LIFE LIMIT WAS 20000 CYCLES)SDR OZCA340274230105Compressor · stalledDURING TAKEOFF REACHING 1000FT ENGINE2 FAILED . CONSULTED WITH CREW AND THEY STATED THAT IT WAS A COMPRESSOR STALL – MAINTENANCE INSPECTED THE INLET AND FOUND NO DISCREPANCIES. INSPECTED COMPRESSOR VG ACTUATING SYSTEM WITH NO DEFECTS NOTED. RAN ENGINE AT LOW ASDR ASAA2023010441416Hook · wornWHILE ACCOMPLISHING ASA T/C SBCFM56-7B-72-1074-1, FOUND AFT WSIWDE OF THE STAGE 3 J-HOOK COMPLETELY WORN THROUGH THE MATERIAL AT THE E12 O'CLOCK POSITION, 2 LOCATIONS WITH FIRST LOCATION SHOWING J-HOOK LIBERATION AND SECOND LOCATION SHOWING REMAINING J-HOOK MASDR 2023FA0000252Platform · missingDURING CLIMB, HEARD A BANG SOUND ASSOCIATED WITH A LATERAL MOVEMENT OF THE AIRCRAFT AND OIL SMELL IN THE CABIN. NO. 2 ENGINE RPM DECREASED WITH HIGH VIBRATIONS. THROTTLE WAS REDUCED ON THE AFFECTED ENGINE AND NOTICED A RISE IN EGT. AN IMMEDIATE DECISION WASSDR I5EA2023010600001Engine · stalledNR 1 ENGINE COMPRESSOR STALLED AND LOST POWER, ACFT UNABLE TO HOLD ALT LT ENG OUT ALT FL 220 PULL TO IDLE ACFT VIBRATION AND STALL STOPPED. PROBLEM CONTINUED AT FL280 FLOWING QRH. NR 1 ENGINE POWER RESTORED DIVERTED TO TPA. REMOVED AND REPLACED LT ENGINE ISDR CALA2022122303478Blades · damagedNR 2 ENG HAD SEVERAL COMPRESSOR STALLS DURING CLIMB. EGT EXCEEDANCE OBSERVED. HAD THE THROTTLE BACK AT IDLE AND ENGINE STABILIZED. RETURNED TO HKG. IAW FIM 71-05 FAULT TREE 803, FOR T/SHOOTING. CHECKED INLET, EXHAUST. CHECKED MCDS, EPCS PERFORMANCE & EGT EXSDR ASAA2022122721251Hook · wornREF T/C #SBCFM56-7B-72-1074-1 ON WING BORESCOPE INSPECTION OF METALLIC, HYBRID VSV SYSTEM FOR ROTOR TO STATOR CONTACT. FOUND STAGE 3 J-HOOK AT 6 OCLOCK WORN COMPLETELY THROUGH. GROUNDED - YES. ACCOMPLISHED ENGINE REMOVAL OF ESN # 897-310 REF T/C # 7847000. DEFSDR ASAA2022121041100Spacer · wornWHILE DOING T/C # 78472010 FAN BLADE LUBE. FOUND #1 ENG SPACERS AT #12,17,18,20,21,23, AND 24 POSITION WORN. GROUNDED - YES. REMOVED AND REPLACED #1 ENG SPACERS AT #12,17,18,20,21,23 AND 24 POSITION PER TASKCARD 78472010.SDR ASAA2022120941099Hook · wornWHILE ACCOMPLISHING ASA T/C SBCFM 56-7B-72-1074-1 NOTED THAT THE AFT SIDE OF THE 3RD STAGE J-HOOK IS COMPLETELY WORN THROUGH AT BOTH THE 6 O'CLOCK AND 12 O'CLOCK POSITIONS, SEE INSP SERVER FOR PICTURES AND REPORT. PER T/C STEP 8 ENG MUST BE REMOVED WITHIN 10 CSDR UIEA2022120701206Engine · stalledNR 2 ENGINE N2 VIBRATION 5.0 AND NR 2 COMPRESSOR STALLED ON CLIMB OUT. R & R NR 2 ENGINE IAW WORD CARD 71-099-02-01. OPS CHECK GOOD</P>)SDR CALA2022120703331Actuator · failedCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS NORMAL. - ENG 1 ENG 1 COMPRESSOR VANE PARAMETERS NORMAL ACCOMPLISHED POWER ASSURANCE RUN .ACOMPLISHED AMM TASK 75-32-41-00-010-A UP TO STEP E . TEST FAILED MESSAGE CAME BACK ENG1 COMPRESSOR VANESDR DALA2022120607804Blades · damagedDIVERSION TO LAS DUE TO NR 1 ENGINE HIGH N1 VIBRATIONS, HIGH EGT, AND SUSPECTED STALL ON LEFT SIDE. MAINTENANCE FOUND EXTENSIVE LPT BLADE DAMAGE. ENGINE CHANGE CURRENTLY IN PROGRESS.
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