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 DXTA2009010203451Fan Blade · damagedDISCOVERED DAMAGE TO TWO OF THE LT ENGINE FAN BLADES. THERE IS ALSO DAMAGE TO THE ENGINE SHROUD AT THE 7 O-CLOCK POSITION.SDR UALA2008122607011Compressor · damagedSILENT SURGE DETECTED - NR 1 ENGINE. MM BORESCOPED ENGINE AND FOUND NUMEROUS STAGE-8 AND STAGE-9 HP COMPRESSOR BLADES DAMAGED, WITH PIECES MISSING AND BENT AIRFOILS. THE ENGINE WAS REPLACED PRIOR TO FURTHER FLIGHT.SDR HALA2008122000897Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, NR 2 ENG HAS A NICK ON ONE OF THE N1 FAN BLADES. BLENDED BLADE PER AMM 72-31-02. EDDY CURRENT INSP. NO CRACKS NOTED. DIMENSIONS .093 BY 5/8 INCH IN AREA "D" OF BLADE.SDR ZZDA2008188Plug · looseON DEPARTURE, FIRE DETECTOR LEFT ENGINE FAIL ILLUMINATED AT 12,000 FEET, WENT OUT AT ABOUT 13,000 FEET FOLLOWED BY A LEFT ENGINE FIRE INDICATION. INDICATION WENT OUT WHEN THROTTLE WAS MOVED TO IDLE. OVERWEIGHT LANDING APPROX 106,500 LBS. FOUND BORESCOPE PLUSDR CA081223001Bearing · failed(CAN) NR 3 BEARING FAILURE FOUND AT DISASSEMBLY.SDR CA081217001Compressor · fod(CAN) AIRCRAFT WAS ON TAKEOFF ROLL WHEN THE PILOTS HEARD A LOUD BANG FROM ENGINE NR 2 & EXPERIENCED A YAW TO THE RIGHT AS THEY APPROACHED 110 KNOTS. THE PILOTS THROTTLED BACK, ABORTED THE TAKEOFF, TAXIED BACK TO THE RAMP AND SHUTDOWN THE ENGINES. PASSENGERSSDR USAA2008121592222Compressor · stalledFLT 2131 - BOS-LGA - EMERGENCY LANDING - THREE LOUD BANGS WERE HEARD WITHIN TWO MINUTES BELOW LEFT WING AND VIBRATION WAS FELT AT FLIGHT LEVEL 16000. CAPTAIN DECLARED EMERGENCY AND RETURNED TO BOSTON. AIRCRAFT LANDED NORMALLY AND TAXIED TO THE GATE. REPLACESDR AALA200803087Compressor · contaminatedJFK INFLIGHT - CREW REPORTED SMOKE IN COCKPIT AND SMOKE ALARMS COULD BE HEARD IN CABIN. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUND OIL IN HIGH PRESSURE COMPRESSOR STAGES 1, 2 AND 3 ON NR 2 ENGINE. REPLACED NR 2 ENGINE ON 12 DEC AT JFK. SYSTEM GROUNSDR UALA2008120806770Fan Blade · damagedBIRD INJESTION NR 2 ENGINE. RTFL. CREW REPORTS 4EA FAN BLADES FOUND DAMAGED UPON ARRIVAL. INSPECTION COMPLETED, BLADES REPLACED.SDR AALA200803046Fan Blade · damagedLIM INFLIGHT, DURING TAKEOFF BIRDS INGESTED INTO NUMBER ONE ENGINE. CREW REPORTED ENGINE INDICATIONS OF FLUCTUATION. RETURNED TO LIM AND LANDED WITHOUT INCIDENT. FOUND FAN BLADE DAMAGE AND INLET COWLING DAMAGE. REPLACED ALL FAN BLADES AND ACCOMPLISHED A TSDR PCSA2008120301Blade · brokenAMERIJET FLIGHT SXM - SJU NUMBER ONE ENGINE VIBRATION FOLLOWED BY HIGH FUEL FLOW. PERFORMED A PRECAUTIONARY SHUTDOWN. MAINTENANCE DISCOVERED A BROKEN C2 BLADE AND COMPRESSOR DAMAGE.SDR 2009FA0000237Impeller · damagedDURING TAKEOFF (ASCENT), ACFT SUFFERED A BIRD STRIKE IN THE RT ENGINE. THE PILOT VERIFIED HIS PARAMETERS AND THEY DID NOT HAVE ANY VIBRATION. HOWEVER, HE SMELLED BURNED BIRD AND DECIDED TO RETURN TO DEPARTURE AIRPORT. DURING THE WALK AROUND INSP, THE PILOT SDR USAA2008120592185Bearing · failedFLT 1419 PHL-LAX - EMERGENCY LANDING - CREW REPORTED A COMPRESSOR STALL AT FL310 ON THE NR 2 ENGINE. AIRCRAFT DESCENDED TO 280 AND VIBRATIONS CONTINUED. ENGINE WAS SHUT DOWN DUE TO BLUE ELECTRICAL SYSTEM FAILURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO CSDR RYNA200800044Fan Blade · out of balanceDURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALANSDR USAASB08116Compressor · leakingON TAKEOFF FROM ORD, EN ROUTE TO CLT, CREW REPORTED A STRONG ODOR WITH SMOKE DETECTORS SOUNDING OFF. NO VISUAL INDICATION OF SMOKE WAS NOTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE FOUND OIL RESIDUE IN APU DISTRIBUTION DUCT. CLEANEDSDR ASMF 20081102Fan Blade · nickedDURING OVERNIGHT CHECK, FOUND A NICK OF 0.005 INCHES DEPTH ON THE LEADING EDGE OF ONE FAN BLADE AT .4375 INCHES FROM THE ROOT, AND A NICK OF 0.0035 INCHES OUT OF LIMITS ON THE LEADING EDGE OF THE OTHER FAN BLADE AT .7500 INCHES FROM THE ROOT. RT ENG WAS REPLACSDR COMA2008111970002Fan Blade · defectiveEN ROUTE ATL-MKE THE LEFT ENGINE VIBRATION INDICATION REACHED 1.8 AMBER, REDUCED THRUST TO INDICATE GREEN. CREW DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED ALL FAN BLADES ON THE LEFT ENGINE.SDR AALA200802527AFan Blade · bird ingestionINFLIGHT - AT ROTATION CREW REPORTED LOUD BANG AND VIBRATION FROM NUMBER TWO ENGINE DUE TO BIRDSTRIKE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 21NOV AT JFK DUE TO BLADE AND FAN CASE DAMAGE. SYSTEM GROUND CHECKED NORMAL OPESDR DL76G081580Blades · damagedRIGHT ENGINE BIRD INGESTION, ENGINE VIBS, DIVERTED TO DKR 3 FAN BLADES ARE DAMAGED BORO WAS GOOD. REPLACED FANBLADE SETS.SDR HALA2008111100844Fan Blade · damagedUPON ARRIVAL FOUND NR 1 ENGINE HAD 2 1ST STAGE FAN BLADES WITH DAMAGE OUT OF LIMITS. ALSO 8-9 BLADES NEED TO BE BLENDED. REMOVED & REPLACED NR 1 ENGINE 1ST STAGE FAN BLADES PER AMM 72-31-02, OK FOR SERVICE.SDR CA081125017Blades · fractured(CAN) DURING CRUISE AT FL170, THE LT ENG LOST POWER AND THE TEMP INCREASED TO 850 DEGREES C. (1) PASSENGER SAW FLAMES OUT THE EXHAUST. THE ENG WAS SHUTDOWN AND A SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSP FOUND FRACTURED COMPRESSOR TURBINE BLADES. THE ESDR CA081114005Impeller · cracked(CAN) HOT SECTION INSPECTION WAS BEING CARRIED OUT BY ENGINE SHOP ON ENGINE SN P44659C AND IT WAS NOTED THAT THE IMPELLER WAS CRACKED. THIS IMPELLER IS NOT TRACKED. THE TIMES ON THE IMPELLER SINCE INSTALL ARE 2407.0 AND 3434 CYCLES. THIS IS NOT THE 1ST INSTANCSDR CA090129001Cap · disconnectedRIGHT ENGINE N1 VIB ICON AND THE PILOTS REPORTED THE FAN VIBES REACHING 2.9 MILS. UPON LANDING AT AN OUTSTATION, A MECHANIC WAS SENT TO INVESTIGATE THE ISSUE. AFTER REMOVING THE FORWARD SPINNER IT WAS FOUND THAT THE FORWARD "BLIND" CAP OF THE FAN SHAFT HAD CSDR CA081104002Compressor · seized(CAN) DURING CRUISE, THE RT GENERATOR KICKED OFF-LINE. SHORTLY AFTER THAT TEMP INDICATIONS IN THE RT ENG CLIMBED CAUSING THE FLIGHT CREW TO SHUT DOWN THE ENGINE AND CONTINUE ON TO LAND AT THE SCHEDULED POINT OF LANDING. THE STARTER GEN WAS REMOVED AND THE COMPSDR SWAA085963Bushing · missingAIR TURNBACK/DECLARED EMERGENCY. DURING CLIMB NR 1 ENG POPPED AND BANGED AT 10,000 FT. FOUND RT VSV ACTUATOR BELLCRANK TO 3RD STG ARM NUT BUSHING MISSING. INSTALLED BUSHING & HARDWARE PER MM.SDR 08FDEA04576Blade · damagedNR 3 ENGINE S/N 451539 10TH STAGE COMPRESSOR BLADE T/E TIP AREA HAS A DING 0.036 INCH WITH 0.020 TEAR ON THE CONVEX SIDE. BLENDED BLADE TIP AND REMOVED THE DAMAGED AREAS AND PERFORMED AN INSPECTION TO ENSURE DEFECTS HAVE BEEN REMOVED IAW MD-10-10 AMM 72-36-00SDR UALA2008111306270Fan Blade · dentedNUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES. ALL DAMAGED FAN BLADES BLENDED ON BOTH NR 1 & NR 2 ENGINES.SDR AALA200802396ACompressor · stalledORD INFLIGHT - CREW REPORTED SUSPECTED NUMBER ONE ENGINE COMPRESSOR STALL DURING CLIMB THROUGH 25000 FEET. FELT AND HEARD BANG N1 ENGINE PRESSURE RATIO RAPID FLUCTUATION. CREW BROUGHT ENGINE TO IDLE. FLIGHT ATTENDANTS REPORTED EXTREME VIBRATION ON LEFT SIDESDR SWAA085793Compressor · stalledAIR TURNBACK / DECLARED EMERGENCY. COMPRESSOR STALL IN THE NR 2 ENGINE AT 1,100 FT. WHILE REDUCING POWER TO CLIMB THRUST. REMOVED AND REPLACED NR 2 ENGINE PER MT.SDR CA081017004Blade · damaged(CAN) IT WAS NOTICED ON A GROUND RUN AFTER THE ENGINE WAS INSTALLED THAT THERE WAS A SQUEALING NOISE COMING FROM THE ENGINE. THE ENGINE WAS REMOVED AND FORWARDED TO THE ENGINE SHOP FOR EVALUATION. UPON DISASSEMBLY THE NR 1 IMPELLER WAS FOUND TO HAVE A PIECE OFSDR Q2SA789001Compressor · stalledEN ROUTE FROM SPIM TO KMIA DURING CLIMB AND CRUISE, NR 2 ENGINE EXPERIENCED HIGHER EGT READING (70 DEG) THAN OTHER ENGINES. REDUCED THRUST SETTINGS ON NR 2 ENGINE LOWERED HIGHER EGT READING TO 30 DEG ABOVE OTHER ENGINES, WITH NO ROUGHNESS OR APPARENT ENGINE ISDR CA081016012Compressor · seized(CAN) ACFT WAS EN ROUTE WHEN THE LT ENGINE LOST POWER. THE CREW COMPLETED EMERGENCY PROCEDURES, SECURED THE ENGINE AND FEATHERED THE PROPELLER. THEY DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION, WHERE THE ACFT PERFORMED A SINGLE ENGINE LANDING. POST FSDR CNM2008F00002Compressor · stalledDURING CRUISE AT FL 300 NR 3 ENG COMPRESSOR STALLED N1 DROPPED TO APPROXIMATELY 70 PERCENT VIBRATION FELT IN NR 3 THROTTLE/ FUEL LEVEL/ FIRE HANDLE AS WELL AS AIRFRAME. (K)SDR USAA920081714Pin · vibrationFLT NR 2134 - EMERGENCY LANDING, AT CRUISE POWER, A BANG WAS HEARD AND SEVERE VIBRATION FELT. THE FLT CREW PULLED POWER BACK TO IDLE AND VIBRATION STOPPED. ON ATTEMPT TO RESTORE POWER TO CLIMB, WHILE TRANSITIONING THRU 40-45% N1, VIBRATION AND BANG RESUMED. SDR 08FDEA03784Compressor · stalledNR 1 ENG COMPRESSOR STALLED ON CLIMB AT ABOUT 8000 FT TWO EVENTS OCCURRED ABOUT 3 MINUTES APART. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED. PLACED IN WORK. NR 1 ENGINE CHANGE APPROVED. PLANT ENGINEERING. REMOVED AND REPLACED NR 1 ENGINE IAW WORKCARD 71TSDR ZES2008F00001Diffuser · corrodedDURING ENGINE START OIL PRESSURE REMAINED AT ZERO PSI WITH A LOW OIL PRESSURE LIGHT WHEN ENGINE REACHED IDLE. SHUT DOWN ENGINE. INVESTIGATION REVEALED THE ENGINE DRIVEN HYDRAULIC PUMP LOCKED UP DUE TO A PIECE OF METAL THAT HAD DETACHED FROM THE DIFFUSER CASE SDR 2008FA0000609Blade · failedTHIRD STAGE COMPRESSOR BLADE, ONE OF THE BLADES WAS "THROWN" FROM THE PART. NOTE: THIS COMPRESSOR WHEEL IS A ONE-PIECE BLADE DISK. (K)SDR 2008FA0000621Compressor Wheel · separatedTHE CREW REPORTED VIBRATION AND ITT RISE. POWER WAS PULLED BACK TO IDLE AND THE AC LANDED WITHOUT INCIDENCE. DISASSEMBLY FINDINGS REVEALED THE LPC2 ROTOR ASSY (PN 307241613). DISC PN 30603731, SN 990316003093, EXHIBITED MATERIAL LOSS IN THE FORM OF A DISC POSSDR PCS2008F00000Compressor · failedDURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESSOR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POSTSDR DXTA200808163231Compressor · stalledLT ENGINE EXPERIENCED COMPRESSOR STALL AS THROTTLES WERE ADVANCED FOR TAKEOFF. N1 WAS APPROX 70 PERCENT WHEN STALL OCCURRED. ACCOMPLISHED TROUBLESHOOT FOR COMPRESSOR STALLS IN AUTO MODE, DCU DOWNLOAD. REMOVED AND VISUALLY INSPECTED BOV ASSY. NO DEFECTS NOTEDSDR DXTA200803231Compressor · stalledLEFT ENG EXPERIENCED COMPRESSOR STALL AS THROTTLES WERE ADVANCED FOR TAKEOFF. ABORTED TAKEOFF. (S)SDR SWAA084419Engine · stalledNR 1 ENG COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENG PER MT.SDR SWAA084418Engine · stalledDECLARED EMERGENCY, NR 1 ENG COMPRESSOR STALLED, VIBRATION INDICATION AND N1 ROLLED BACK TO 15 PERCENT. REMOVED AND REPLACED NR 1 ENG PER MT.SDR ASM2008F00001Blade · bentDURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLASDR CA080805011Scroll · cracked(CAN) WHILE CARRYING OUT A DAILY CHECK, A CRACK WAS FOUND ON THE COMPRESSOR SCROLL ON TOP, PARALLEL TO SHROUD HSG AND NEAR THE RT ELBOW. ACFT WAS GROUNDED. COMPRESSOR ASSY IS AN ON-CONDITION ITEM BUT THERE IS AN INSP EVERY 2000 HOURS. AS YOU CAN SEE THIS SCROLSDR YENA2008073Compressor · stalledFLT 1262, LGB-SMF, AIR RETURN TO LGB, ENG NR 1 COMPRESSOR STALL (ECAM) THRUST LEVERS AT CL DETENT LEVEL AT FL230 "BANG" AND YAW AND VIBRATION SAW ZERO EPR, THEN WENT BACK TO NORMAL. DID NOT SHUT DOWN IAW QRH 6-26. PERFORMED TSM 71-00-00-710-013-A, GVI, BLEEDSDR 2008UALA04067Bearing · failedNR 1 ENGINE COMPRESSOR STALL. RTFL. FOUND FAILURE OF NR 4 BEARING. CHANGED ENGINES.SDR 2008UALA03992Guide Vane · damagedBIRD STRIKE TO LT ENG. ABORTED TAKEOFF AT 120 KNOTS. *S/D* ACCOMPLISHED ENGINE CORE BORESCOPE INSPECTION, NO DAMAGE. FOUND 3 FAN EXIT GUIDE VANE BASES DAMAGED AT 4 O'CLOCK. REPAIRED PER AMM 72-33-02-801. SUBSEQUENT ENGINE GROUND RUNS OK. AIRCRAFT RETURNSDR USAA920081437Pin · stalledFLT 792, ACFT EXPERIENCED NR 1 ENG FAILURE AFTER TAKEOFF. CAPTAIN REPORTED A LOUD BANG PRIOR TO FINAL FLAP RETRACTION PROBABLY FROM A COMPRESSOR STALL. THEN EXPERIENCED ENG SURGING, VIBRATION AND A MAX ENG TEMP READING. THE CREW SHUTDOWN ENG AND RETURNED TO SDR 7KF2008F00000Compressor · fodDURING FLIGHT WITH 2 MEDICAL PERSONNEL AND PILOT ABOARD HEADING BACK TO AIRPORT NR 1. ENGINE MADE A LOUD NOISE AND FLAMED OUT, PILOT NOTED ENGINE INDICATIONS AND SECURED THAT ENGINE, DECLARED AN EMERGENCY WITH TOWER AND LANDED AC WITHOUT INCIDENT. AFTER INVE
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