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 2006FA0001152Damper · brokenAIRCRAFT ARRIVED 10/31/2006 TO TROUBLESHOOT A RUMBLE FROM THE NR 1 ENGINE. UPON INVESTIGATION, FOUND 1 FAN BLADE TO HAVE A BROKEN MIDSPAN DAMPER. (K)SDR DL777060929Compressor · damagedNR 1 ENG SHOWED TREND SHIFT. C/W BORO OF HPC COMPRESSOR. FOUND 6TH STAGE PC COMPLETELY FO OUT. OUT OF LIMITS IAW MM. NR 1 ENG S/N 51177 ENG CHANGE REQUIRED. C/W ENG CHANGE IAW TRANS 11T003.SDR C2XA06SH125Case · corrodedSHV - DURING C-CHECK THE NR 1 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSITION.SDR CA061106018Line · broken(CAN) WHILE IN CRUISE THE NR 3 ENGINE ROLLED BACK TO 60% NG.. A PRECAUTIONARY SHUT DOWN OF THE ENGINE WAS COMPLETED AND THE AIRCRAFT RETURNED TO BASE. ON INSPECTION OF THE ENGINE IT WAS FOUND THAT THE P3 SENSE LINE, FROM THE GAS GENERATOR CASE TO THE P3 FILTERSDR 2006FA0001087Shaft · spalledFOUND SPALLING ON BEARING RACE AT 2.5 BEARING CONTACT POINT. FOUND VISIBLE LINE ON 2.5 BEARING ROLLERS MATCCHING SPALL LINE ON SAG SHAFT. COMPRESSOR ASSY INSTALLED ON AC 6/SEPT/2006, TIME IN SERVICE SINCE INSTALLATION OF COMPRESSOR ASSY 105.1 HOURS, 220 CYCLSDR GTIA200600084Stator Vane · lack of lubeNR 2 ENG COMPRESSOR VANE ECAM RT AFTER POWER ADVANCE TO FLEX TAKEOFF. LOW SPEED ABORT, NR 2 ENG SHUTDOWN IAW ECAM. MAINTENANCE LUBED VSV SYSTEM.SDR VNAA0610043Fan Blade · damagedCREW REPORTED THAT THE NR 2 ENGINE FAN BLADES NEED INSPECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED FOUR DAMAGED BLADES. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR CA061220003Turbine Blades · damaged(CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A DECAY ON ENGINE PARAMETERS. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED DAMAGE TO COMPRESSOR AND POWER TURBINE BLADES. MFG WILL MONITOR INVESTIGATION OF THE EVENT ANDSDR CA061106015Diffuser · loose(CAN) SHORTLY AFTER LEVELLING OFF AT 17000 FEET, THE NR 2 ENGINE BEGAN TO SURGE AFFECTING ALL ENGINE PARAMETERS. THE POWER WAS REDUCED TO ALLEVIATE THE RESULTING OVER TEMPERATURE CONDITION. AT POWER SETTING ABOVE 70% NG THE ITT WOULD FLUCTUATE WILDLY TO OVER SDR AALA20060892Compressor · stalledDCA INFLIGHT - AFTER TAKE OFF HEARD LOUD BANG AND LIGHT LEFT YAW. ENGINE PRESSURE RATIO DROPPED TO .27 THEN RECOVERED. ALL ENGINE INDICATIONS NORMAL. LANDED DCA WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 20 OCTOBER AT DCA DUE TO STALLS. SYSTEM GROUND CHECKSDR SWAA064109Compressor · stalledCREW REPORTED LOUD BANGING SOUND ON LT SIDE OF FUSELAGE DURING DESCENT AND AFTER ADDING POWER TO ENGINES. SUSPECT NR 1 ENGINE COMPRESSOR STALL. R&R NR 1 ENGINE MEC AND FUEL PUMP PER MM. R&R CIT SENSOR PER MM.SDR 2006UALA01980Compressor · stalledRETURNED TO FIELD DUE TO NR 2 ENGINE COMPRESSOR STALL. NR 2 ENGINE COMPRESSOR STALLED DURING CLIMB FROM LAX. LOST 50% THRUST FOR ABOUT 5 SECONDS. ALL INDICATIONS WERE NORMAL AND AIRCRAFT RETURNED TO FIELD. NO EMERGENCY DECLARED. NO OVER WEIGHT LANDING. TSDR CA061016006Case · cracked(CAN) SHORTLY AFTER TAKE-OFF AT 500FT AGL THE CREW REDUCED POWER TO CLIMB POWER AND REALIZED THAT THE LT ENGINE ITT ROSE RAPIDLY TO APPROXIMATELY 850-900 DEGREES CELSIUS. THE OVER-TEMPERATURE LIGHT ILLUMINATED AND THE ENGINE OIL TEMPERATURE WAS ALSO RISING. THSDR SCS4200600001Blade · out of toleranceENGINE WAS REMOVED FROM SERVICE DUE TO A DAMAGE IN C9 BLADE (AREA "E") OUTSIDE BLENDABLE LIMITS ACCORDING TO P&W ENGINE MANUAL. THE DENT WAS DISCOVERED BY BOROSCOPE INSPECTION. DEPTH OF DAMAGE= APPROX .037 , BLEND LIMIT =.031. DURING SHOPVISIT THE BLADE WAS MISDR ARWA20061001Compressor · stalledLOG PAGE NR 124562. ABORTED TAKEOFF AT 105 KTS FOLLOWING NR 4 ENGINE COMPRESSOR STALL. INSPECTED NR 4 ENGINE COMPRESSOR SURGE BLEED VALVE AND TIGHTEN ALL SENCE LINES IAW MM 75-30-01/201; OPERATIONAL CHECK NORMAL ON ENGINE RUN IAW M/M 71-00/501.SDR HALA0600801Fan Blade · damagedDURING ETOPS 2 CHK MINOR L/E FOD, DAMAGE NOTED TO NR 2 ENG FAN BLADE WHERE MARKED. NICK DAMAGE DIMENSIONS ARE 5/16" BY 1/8" DEEP 4" FROM BLADE TIP. MOC CONTACTED. NOT WITHIN DISPATCH LIMITS FAN BLADE BLENDED IAW AMM 72-31-02 IAW AMM 72-31-02 PARA 2 ITEM 4D SDR 2006FA0001025Compressor Wheel · cracked(REF NR: 6841.5.30) DURING A SCHEDULED INSPECTION, EDDY CURRENT NDT REVEALED A CRACK IN THE LT ENGINE HP COMPRESSOR STAGE 1 ROTOR. (K)SDR VNAA0610007Fan Blade · damagedCREW REPORTED DAMAGE TO NR 2 ENGINE FAN BLADES. MAINTENANCE INSPECTED AND FOUND DAMAGE TO TWELVE BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR HALA0600745Fan Blade · damagedETOPS SIGNIFICANT SYSTEM - ON OVERNIGHT CK, FOUND 2 NICKS ON NR 1 ENG, FAN BLADE NR 1. 1ST NICK IS LOCATED IN AREA -A- 2.5 INCHES FROM TIP MEASURING .015 INCH DEEP. 2ND NICK IS LOCATED IN AREA -F- 9.6 INCHES FROM TIP MEASURING .040 INCH DEEP. INSP & FOUND NSDR 2006UALA01867Compressor · stalledNR 2 ENG COMPRESSOR STALL IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL, ENG POWER WAS DECELERATING. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE, REPLACED ELECTRONIC ENGINE CONTROL, REPLACED IPCV VALVE, HPSOV,SDR HALA0600733Blade · damagedETOPS SIGNIFICANT SYSTEM, DAMAGE IS IN 'AREA C' PER AMM 72-31-02. REPAIRED BLADE PER AMM 72-31-02-308-003-N00. DAMAGE IS IN 'AREA C' PER AMM 72-31-02. REPAIRED BLADE PER AMM 72-31-02-308-003-N00.SDR CA060927001Scroll · cracked(CAN) DURING SCHEDULED 100/300 HR INSPECTION COMPRESSOR SCROLL FOUND CRACKED ON VISUAL INSPECTION. A/C GROUNDED AND COMPRESSOR REPLACED. RECOMMEND BETTER DAILY INSPECTIONS BEFORE FIRST FLIGHT. (TC NR 20060927001)SDR 2006FA0000957Impeller · damagedDURING REPLACEMENT OF THE S16 SHAFT, IT WAS DISCOVERED THAT THE OUTER LAND OF THE SNAP RING GROOVE WAS VERY THIN AND THE INNER EDGE WAS LIFTING AND (2) .3750 INCH LONG PIECES CAME OFF OF THE LAND. WHEN THE SNAP RING WAS REMOVED THE GROVE FOR THE SNAP RING SESDR ANCF200600033Compressor · stalledPILOT REPORT: ONE MINUTE AFTER TAKEOFF, LT ENGINE COMPRESSOR STALL WAS PRESENTED AND A STRONG SHAKE ON THE AIRPLANE WAS FELT. LT THROTTLE LEVER WAS REDUCED UNTIL COMPRESSOR STALL STOPPED. ENGINE COMPRESSOR STALL CHECK LIST WAS PERFORMED A NORMAL LANDING WAS PESDR MASA200602259Fan Blade · lack of lubeASH 7137 IAD. AC DIVERTED TO RDU FOR NR 2 ENGINE VIBE. MX LUBED THE FAN BLADES.SDR 2006UALA01770Compressor · stalledAFTER FCU CHANGE NR 1 ENG HAD COMPRESSOR STALL ON DECEL AT APPROX 1.12 EPR, THEN 3 MORE STALLS AT IDLE THEN AUTO SHUTDOWN. NR 1 ENG RESTART FAILED, ENG HUNG STARTED AT 40% N2 WITH N1 ROTATION, EGT AT 225 DEG, FUEL FLOW NORMAL AT .6, DUCT PRESS WAS 30 PSI. FOSDR 06FDEA03190Case · chafedENG NR 1 FAN CASE AT AFT 1:00 POS FOUND WITH CHAFE MARK AT 8 PLACES (P/N 51G478). CHAFE MARK MEASURED AND FOUND 3 AREAS OUT OF LIMIT PER AMM 72-33-06-6. REFER TO E.A.1-7233-103553. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR CA061006004Engine · fire(CAN) DURING FLIGHT THE FIRE WARNING ACTIVATED. THE FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A PUNCTURED GAS GENERATOR CASE AND FIRE DAMAGE TO THE ENGINE. MFG WILL INVESTIGATE THE EVENT AND SDR CA060906012Compressor · fod(CAN) DURING ROUTINE INSPECTION IT WAS NOTED THAT THE AXIAL COMPRESSOR WHEEL HAD SUFFERED FOD, WHICH WAS BEYOND LIMITS. THERE WAS NO EVIDENCE THAT THE INTAKE COWL HAD LOST ANY HARDWARE WHICH MAY HAVE CAUSED THIS. NOR WAS THERE ANY RESIDUAL PARTICLES/OBJECTS FOSDR NOCA12906Blades · bird strikeBIRD STIRKE ON TAKE OFF FROM BJL RT ENGINE, FAN VIB 4.1 RECORDED. LANDED SAFELY AT BJL AFTER FUEL DUMPED. REPLACED 4 FAN BALDES, OPS NORMAL.SDR COMA0670185Fan Blade · vibratesFLIGHT 5617 - EN ROUTE JAN-BOS DURING CLIMB ENCOUNTERED VIBRATION FROM THE LEFT ENGINE, FLIGHT DIVERTED TO CVG. REPLACED THE LEFT ENGINE FAN BLADES.SDR UPS06147833Compressor · stalledINSPECTION TYPE: N/A AIR DIVERT, INITIAL DESCENT COMPRESSOR STALL WITH NO SECONDARIES. ON SUBSEQUENT DESCENTS NUMEROUS COMPRESSOR STALLS ON NR 1 ENGINE. NO FLUCTUATIONS ON ANY OF THE ENGINE INSTRUMENTS. PERFORMED ENGINE STALL PROCEDURES. DECLARED EMERGENCY BECSDR 2006UALA01664Engine · malfunctionedSMOKE/ODOR IN CABIN, LANDED UNDER AMBER, MASKS & ALL SLIDES DEPLOYED. REPLACED NUMBER 1 ENGINE DUE TO OIL WETTING, BURNING AND DEBRIS FOUND AT STAGES 3 & 4 OF HPC.SDR CA060906020Fan Blade · damaged(CAN) DURING CLIMB THE ENGINE WAS REPORTED TO EMIT A LOUD NOISE ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER. THE ENGINE WAS SHUT DOWN, AN EMERGENCY DECLARED AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN SDR ASMF200608016Blade · brokenDURING THE BOROSCOPIC INSPECTION RELATED TO THE EO 987211 R4 PERFORMED DURING OVERNIGHT CHECK, WERE DETECTED SEVERAL BLADES WITH DENTS OUT OF LIMITS AND ONE BLADE BROKEN IN T2 SECTION. LT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-01, ALL CORRECSDR UIEA200600216Compressor · stalledRTO: NR 2 ENGINE COMPRESSOR STALL ON T/O ROLL. EGT 1111 DEGREES FOR 4 SECONDS. FOUND METAL IN TAIL PIPE. LOCKED OUT ENGINE PER GMM 3.23.8. ENGINE TO BE REPLACED.SDR 200608221Fan Blade · bentFLIGHT 6484 GPT ON TAKEOFF ROLL, APPROXIMATELY 50 KNOTS, CREW EXPERIENCED UNKNOWN AND CONSTANT HUMMING NOISE, NO SIGNIFICANT VIBRATION ASSOCIATED WITH IT. ACCOMPLISHED RTO. OCM DISCOVERED A BENT FAN BLADE IN THE NR 2 ENGINE. FURTHER INVESTIGATION REVEALED NSDR 2006UALA01629Blades · failedENG 2 STALL. TRANSIENT STALL SHORT ECAM THEN ALL PARAMETERS NORMAL AT TOP OF DESCENT. NR 2 ENGINE S/N V10784 HAS ONE HPC 6TH STAGE BLADE MISSING 1/2 AMOUNT OF BLADE. ALL OTHER 6TH STAGE HPC BLADES HAVE NUMEROUS AMOUNTS OF DAMAGE AND MATERIAL LOSS. ENGINE FSDR AWXA200601519Compressor · stalledLAS - SMOKE - FLT - 198 - AIRCRAFT REJECTED TAKEOFF AT 30 KTS, DUE TO NR 2 ENGINE COMPRESSOR STALL. SMOKE IN THE CABIN. THE PILOT DECLARED AN EMERGENCY AND EMERGENCY EQUIPMENT WAS DISPATCHED. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT.SDR CA060818005Case · eroded(CAN) AIRCRAFT WAS IN FOR AN INSPECTION. THE COMPRESSOR CASE HALVES HAD 23 HOURS LT TO A 1750 INSPECTION. MFG REQUESTED THAT WE CARRY OUT THE INSPECTION. IT WAS FOUND THAT THE 2ND AND 3RD STAGE STATOR BLADES WERE SO UNDER CUT FROM EROSION (NEAR THE ROOT OF THESDR COMA0670170Fan Blade · out of balanceFLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 22.SDR COMA0670169Fan Blade · out of balanceFLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 20.SDR COMA0670168Fan Blade · out of balanceFLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 6.SDR COMA0670167Fan Blade · out of balanceFLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 7.SDR COMA0670166Fan Blade · out of balanceFLIGHT 5232 EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 21.SDR COMA0670165Fan Blade · out of balanceFLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 8.SDR CA061006013Compressor · seized(CAN) THE ENGINE WAS REPORTED TO EMIT A LOUD NOISE AND SUBSEQUENTLY FLAMED OUT IN FLIGHT. POST-FLIGHT INSPECTION REVEALED METAL DEBRIS IN THE OIL, RUBBING NOISES FROM THE POWER SECTION AND A SEIZED COMPRESSOR. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOSDR HALA0600577Blade · damagedON WALK-AROUND ROUND NICK ON LT ENGINE 4 O'CLOCK POSITION. INSPECTED AND BLENDED BLADE IAW MM 72-31-02.CONDITION CK GOOD. EDDY CURRENT CK NO CRACK INDICATION. BLEND DEM .218 INCHES DEPTH, 1.875 INCHES LENGTH BLADE NR 11.SDR 06FDEA2924Compressor · stalledAS WE APPLIED T/O POWER (STD POWERS) HEARD A LOUD BANG (COMPRESSOR STALL) AND REJECTED T/O BEFORE T/O POWER WAS SET. MAX SPEED 20KTS WIND 12KT X-WIND. SAT CONFIRMED NR 2 ENGINE COMPRESSOR STALL. C/W AMM 71-00-000-6 3.B. CENTER ENG COMPRESSOR STALL INSPESDR CA060905008Blades · damaged(CAN) PROBLEMS WERE REPORTED WITH THE ENGINE SHORTLY AFTER TAKE-OFF. THE AIRCRAFT SUBSEQUENTLY CRASHED. PRELIMINARY INVESTIGATION EVIDENSED COMPRESSOR BLADE DISTRESS. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 2006090500
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