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 NACA20020044Cylinder · crackedDISCREPANCIES: #3 ENGINE BACKFIRE, LOW BMEP @ 0010Z.CORRECTIVE ACTION: REPLACED #3 ENGINE, #5 CYLINDER.SDR 2002UALA01447Compressor · stalledCOMPRESSOR STALL INCURRED DURING REVERSE THRUST. SURGE INSPECTION/CHECK WAS PERFORMED, WITH NO DISCREPANCY FOUND. THE 14TH STAGE CONVERTER VALVE WAS REPLACED AS A PRECAUTION.SDR UPS02439437Plug · looseINSPECTION TYPE:N/A AIR TURNBACK ENG FIRE NR 3 ENGINE. FOUND BORESCOPE PLUG AT 2 O'CLOCK POSITION ON DIFFUSER CASE LOOSE. REINSTALLED PLUG AND SAFETIED IAW 72-00-00. RAN NR 3 ENGINE WITH NO RISE IN TEMP. A/C RETURNED TO SERVICE.SDR P5CA0200699Compressor · stalledCLIMBING THROUGH 15,000 FT NR 3 ENGINE COMPRESSOR STALLED. EGT WAS 100 DEGREES CELCIUS. LOWER THAN OTHER MOTOR & N2 WAS LOWER WITH NACELLE ANTI-ICE ON. TROUBLESHOT ENGINE PER MM 71-00-43, PERFORMED INSPECTION PER MM 72-00-00 & BORESCOPE OF ENGINE IAW MM 72-SDR AUS20021076Rotor · damaged(AUS) NO2 ENGINE COMPRESSOR AXIAL ROTOR DAMAGED BEYOND LIMITS. SUSPECTCAUSED BY FOD.SDR CA020930002Compressor · failed(CAN) ON CLIMB A LOUD BANG WAS HEARD FOLLOWED BY A/C YAW. TGT PEAKED AT 1150-DEG C AND ENGINE SPOOL DOWN. A/C RETURNED SAFELY TO FIELD ON ONE ENGINE. ENGINE INSPECTION REVEALED METAL IN TAIL PIPE AND SEIZED LP SYSTEM. FAN AND BOOSTER FOUND OK. INTERROGATION OSDR CA020906004Compressor · damaged(CAN) AFTER LANDING, SPARKS NOTICED COMING OUT BY LT ENGINE TAIL PIPE. ALL PARAMETERS NORMAL, METAL DEBRIS IN TAIL CONE. BOROSCOPE FOUND EXCESSIVE COMPRESSOR DAMAGE. ENGINE REPLACED.SDR 2002F00978Gas Generator · malfunctionedLEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. OIL PRESSURE WAS BELOW 60 PSI, LEFT ENGINE SHUTDOWN. LEFT GAS GENERATOR AND POWER SECTION WERE REPLACED. (M)SDR AWXA200200774Bearing · failedSTL - DIVERSION - FLT 0695 - EN ROUTE FROM CMH TO LAX THE NR 2 ENGINE COMPRESSOR STALLED TWO TIMES AT FL 370, EGT RED LINED AND OIL PRESSURE PEAKED AT 330 PSI THEN SLOWLY DROPPED TO -0- PSI, SHUTDOWN ENGINE PER ECAM INSTRUCTIONS AND DIVERTED TO STL. ENGINE ISSDR AUS20020938Impeller · fod(AUS) RH ENGINE LOW PRESSURE IMPELLER DAMAGED BEYOND LIMITS BY FOD.SDR 2002UALA01313Compressor · stalledCOMPRESSOR STALL ON LEFT ENGINE AT TAKEOFF. ENGINE EXPERIENCED A GROUP 3 (TAKEOFF) SURGE. REMOVED ENGINE FOR HIGH COMPRESSOR OVERHAUL.SDR 2002F01043Blade · erodedAT C-CHECK, FOUND NR 3 ENGINE C-1 DISK BLADES DAMAGED AT LEADING EDGES. (M)SDR 2002UALA01287Blade · failedRIGHT ENGINE COMPRESSOR STALL - HIGH EGT ON CLIMB OUT. SEVENTH STAGE COMPRESSOR BLADE FAILURE. ON TEARDOWN, FIVE EACH BLADES WERE COMPLETELY MISSING FROM THE DISK.SDR AUS20020814Compressor Wheel · damaged(AUS) NR 2 ENGINE N2 VIBRATION LEVELS HIGH. BORESCOPE INSPECTION FOUND DAMAGE TO THE FIFTH STAGE HIGH PRESSURE COMPRESSOR.SDR CA020906002Impeller · cracked(CAN) FIRST STAGE IMPELLER DAMAGE. THE ENGINE WAS REMOVED DUE TO A CRACK IN THE FIRST STAGE IMPELLER WHICH WAS NOTICED THROUGH THE INLET COWL. THE IMPELLER WAS REMOVED AND A COMPLETE DOD INSPECTION ACCOMPLISHED.SDR AUS20021167Blade · separated(AUS) LT ENGINE SECOND STAGE COMPRESSOR BLADE SEPARATED FROM WHEEL. INSPECTION FOUND A SMALL STAIN AT THE BLADE STUMP INDICATING THAT A SMALL CRACK HAD BEEN PRESENT FOR SOME TIME. THE CRACKING HAD BEEN INITIATED BY CORROSION PITTING. THE ADJACENT BLADE HAD SDR AUS20020746Spacer · damaged(AUS) ENGINE FIRST STAGE COMPRESSOR SPACER DAMAGED DUE TO RUBBING ONTHE FIRST STAGE COMPRESSOR STATORS.SDR AWXA200200667Blade · failedPHX - EMERGENCY LANDING - EN ROUTE FROM AUS TO PHX FLIGHT CREW NOTICED A NR 1 ENGINE VIBRATION WITH A SPIKE IN EGT, ALL ENGINE GAUGES LOOKED NORMAL, LANDED AT PHX. DAMAGE NOTED TO TURBINE SECTION, MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PER T/C'S R5M7SDR CA020806007Seal · failed(CAN) THIS ENGINE WAS REMOVED DUE TO HIGH OIL CONSUMPTION, REFURBISHED AND WITH BELOW 2000 HRS ON WING . BEARING SEALS FAILED. SEALS HAD JAMMED IN THEIR HOUSINGS IN REARWARD POSITION RENDERING THEM USELESS.SDR 2002UALA01205Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. ENGINE RECOVERED. NR 2 ENGINE HAD A GROUP 3 (TAKEOFF) SURGE. THE ENGINE SELF RECOVERED. ENGINE WAS REPLACED AT TERMINATION OF THE FLIGHT FOR COMPRESSOR REFURBISHMENT.SDR MEX2002230Compressor Wheel · damagedDURING PREFLIGHT CHECK, FOUND SEVERAL DAMAGED BLADES OF RIGHT ENGINE DUE TO ADVERSE METOROLOGICAL CONDITION ON ROUTE. DISK C1 WAS REPLACED IAW MM, NOSE COWLING IAW MM AND BULLET ASSY. TESTED OK.SDR ERAA080480Diffuser · damagedALUMINUM DAMAGED BY IMPELLER. REMOVED AND RE-APPLIED PLASMA SPRAY ON CONTOUR. (OVERHAULED).SDR PNSA020702Compressor · crackedEngine removed for low power. During disassembly found 2nd stage compressor missing one piece from trailing edge of vane appeared to be fatigue crack.SDR 2002FA0000877Disk · out of toleranceNEW COMPRESSOR WHEEL RECEIVED FROM HONEYWELL WITH DAMAGE GREATER THAN .001 INCHES BY FIR TREE AREA.SDR UHL2002F00003Disk · failedCREW HEARD (CLUNKING NOISE) FROM NR 1 ENGINE FOLLOWED BY FAILURE OF NR 1 ENGINE. TORQUE NOSE GEAR AND FF DROPPED TO ZERO. (AUTO SHUTDOWN) EVENT OCCURRED AT APPROX 7000 FT MSL. 15 MINUTES PRIOR TO FAILRE, CREW ACCOMPLISHED NORMAL TREND MONITORING. EMERGENCYSDR GTIA020846Blade · nickedNR 1 ENGINE C1 FAN BLADES ARE ROUGH AND HAVE NICKS. NR 1, SN 718528, FAILED BORESCOPE INSPECTION , C-7 DISK 10 BLADES WITH NICKS AND MISSING MATERIAL. 2 BLADES DAMAGED NEAR TIP (1) MEASURES .140 INCH LONG (2) MEASURES .165 INCH LONG WITH A CRACK PROPAGATINGSDR HEEA080433Shaft · wornSHAFT HAS SPALLING AND STEP WEAR ON GEAR TEETH BEYOND NORMAL WEAR.SDR CA020710003Blade · fractured(CAN) RIGHT ENGINE OF A/C B3967, EXPERIENCED IFSD IN WESTERN CHINA (CHONGQING) ABOUT 10 MINUTES AFTER TAKING OFF. A LARGE "BANG" WAS HEARD AT THE ALTITUDE OF 6000 METERS ( REPORTED BY THE PILOT). A/C RETURNED TO GATE SAFETY WITH SINGLE ENGINE. BOROSCOPE INSSDR HEEA080400Stud · brokenREMOVED DUE TO COMPRESSOR SCROLL STUD BROKEN. UPON INSPECTION OF COMPRESSOR PARTS NOTED WORN TANGS AND SLOTS, CHIPS AND PITS ON CARBON FACE.SDR 2002UALA01150Compressor · stalledCOMPRESSOR STALL ON NR 4 ENGINE. SUPPLEMENTAL DATA UPDATE THIS IS A GROUP 3 (TAKEOFF ) SURGE DUE TO EXCESSIVE HPC REAR STAGE BLADE TIP CLEARANCE. ENGINE WAS REPLACED AT TERMINATION OF THE FERRY FLIGHT FOR COMPRESSOR REFURBISHMENT. PW4000 ENGINE TAKE-OFF SURGSDR 2002UALA01121Compressor · stalledAIRCRAFT SUSTAINED COMPRESSOR STALL ON TAKEOFF NR 2 ENGINE. NO SHUTDOWN.SDR 2002FA0000809Spline Adapter · frettedNEW COMPRESSOR SPLINE ADAPTER WAS PURCHASED FROM MANUFACTURER. SERVICE BULLETIN T-069 WAS PACKAGED WITH THE SPLINE ADAPTER, PROVIDING INSTRUCTIONS TO MODIFY THE IMPELLER THAT THE ADAPTER WAS GOING TO BE INSTALLED IN. BULLETIN WAS LATER RECALLED BY MANUFACTURESDR 02FDEA00449Compressor · stalledIMMEDIATELY AFTER LEVEL OFF AT FL350, NR 2 ENG EXPERIENCED SEVERE COMPRESSOR STALLS. PWR WAS REDUCED, WHEN PWR WAS INCREASED STALL RETURNED. F/F & EGT FLUX WAS EVIDENT AND N1 & 2 MOVED ACCORD. QRH PROC WAS ACCOMPL DURING DESCENT AND RETURNED TO ABQ. WHEN HSDR C2XA02CL139Compressor · stalledORF FLIGHT 3037 THE CREW REPORTED THE NR 1 ENGINE DID A COMPRESSOR STALL WHEN TAKEOFF POWER WAS APPLIED. THE ITT ALSO INCREASES TO 920 DEGREES. MAINTENANCE REPLACED THE NR 1 ENGINE. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR 2002F00971Blade · missingAIRCRAFT EN ROUTE TO GEG FROM SLC, HEARD LOUD NOISE IN RIGHT ENGINE. ENGINE WAS SHUT DOWN. PRELIMINARY INVESTIGATION SHOWS PT DISC WITH SEVERAL BLADES MISSING. (M)SDR 2002UALA01072Compressor · stalledCOMPRESSOR STALL OF NR 1 ENGINE. ENGINE RECOVERED AND RESUMED NORMAL OPERATION.SDR 2002UALA01067Rub Strip · debondedDIVERTED UNDER AMBER ALERT DUE TO VIBRATION IN NR 1 ENGINE. ENGINE REPLACED. HPC RUB STRIP DISBONDED CAUSING COMPRESSOR VIBRATION. ENGINE UPGRADED WITH RUB STRIP MODIFICATION.SDR CA020618006Compressor · seized(CAN) IN CRUISE PILOT SAW AND HEARD RT ENGINE FLUCTUATION, POWER BACK THE ENGINE TO FLIGHT IDLE & STILL FLUCTUATING, TORQUE GOING DOWN, ITT GOING UP, SHUT DOWN ENGINE AND LANDED AT DESTINATION WITHOUT ANY PROBLEM. SENT MECHANIC ON SITE, FOUND THAT COMPRESSOR SSDR CA020702004Engine · failed(CAN) THE ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED COMPRESSOR FOD. THE ENGINE WAS DISASSEMBLED & THE COMPRESSOR ROTOR ASSY WAS DETACHED FROM THE GG CASE.AFTER DE-MATING THE ENGINE COMPRESSOR ITWAS APPARENT THA THE ROTOR BSDR HEEA080085Liner · damagedCOMPRESSOR LINER DAMAGED PRODUCING TORQUE FLUCTUATIONS. REPLACED WITH SERVICEABLE PART.SDR C1HA200296015Compressor · stalledON TAKEOFF IN LAS HAD COMPRESSOR STALL, PULLED OFF RUNWAY CALLED MX CONTROL. RAN UP ENGINE, ALL ENGINE PARAMETERS NORMAL. INSPECTED ALL ENGINES AND NO DEFECTS FOUND. RAN ENGINES AT TAKEOFF POWER. ALL PARAMETERS NORMAL. OK FOR SERVICE PER M/M 71-00.SDR DL76L020645Compressor · stalledCOMPRESSOR STALL AT TOP OF DESCENT WHILE PULLING BACK POWER. REPLACING ENGINE.SDR CA020813006Compressor · failed(CAN) CREW REPORTED 3. MILS VIBRATION AT DECENT AT 70 PERCENT. LATER A LOUD BUZZ AT CRUISE, AND VIBRATION WAS 1.8 MILS. BOROSCOPED ENGINE, A GROUND RUN VIBRATION WAS WITHIN LIMITS. A ONE HOUR FLT AND A BUZZING COULD BE HEARD FROM A/C. AC/DC GENERATORS & HYDRASDR USA2002F00045Annular Filler · separatedAT ROTATION, FLAMES WERE SEEN COMING FROM THE RIGHT ENGINE. AT APPROXIMATELY 300 FEET, THE CREW HEARD A NOISE, FELT THE AIRCRAFT YAW, AND RECEIVED WARNING INDICATIONS. EGT ON THE RIGHT ENGINE READ 1000. CREW ACTIVATED ONE FIRE BOTTLE. FLIGHT RETURNED AND LSDR 2002UALA00945Blade · fracturedRETURNED TO FIELD DUE TO NR 1 ENGINE COMPRESSOR STALL. CAUSE OF STALL WAS FOUND TO BE LIBERATED SECTION OF HIGH PRESSURE COMPRESSOR (HPC) 5TH STAGE BLADE. LIBERATION CAUSED DOWNSTREAM DAMAGE, INCREASED TIP CLEARANCE, AND REDUCED SURGE MARGIN OF HPC TO STALL SDR CA020612006Spur Adapter · spalled(CAN) ENGINE CHIP LIGHT FOUND METAL PARTICLES ON BOTH CHIP PLUGS. 2 1/2 BEARING AND INNER RACE ON THE SPUR ADAPTER FOUND SPALLED.SDR 2002UALA00923Blade · failedRIGHT ENGINE FAILED. BORESCOPE INSPECTION REVEALED FAILED HIGH PRESSURE COMPRESSOR STAGE 4 BLADES, CAUSING MAJOR INTERNAL ENGINE DAMAGE AND AUTO-SHUTDOWN. ENGINE WAS REPLACED.SDR DL72S020607Compressor · damagedNR 3 ENG WOULD NOT ACCELERATE ON ADDING T/O POWER. ABORTED T/O AT ABOUT 30 KTS. BORESCOPE INSPECTED 3 ENG 6 AND 7 STG COMP. FOUND 7 STG COMP BLD DAMAGE BEYOND M/M LIMITS. FULL LENGTH OF BLD. ALL BBLDS DAMAGED (361774). REPLACED 3 ENG PER CARD DECK 4T203SDR W6N2002F00000Bolt · looseWHILE IN FLIGHT/ FLIGHT CREW NOTICED SMOKE IN THE CABIN. LANDED AIRCRAFT SAFELY. MECHANICS FOUND OIL IN THE ENVIRONMENTAL BLEED AIR ON THE RT ENGINE. INSPECTED ENGINE AND FOUND LOOSE THRU BOLTS ON THE COMPRESSOR BEARING STUDS. REMOVED ENGINE SENT. DISASSESDR IXXA0200027OStator Vane · malfunctionedAFTER TAKEOFF FROM TOL, THE FLIGHT CREW EXPERIENCED A WINDSHEAR WARNING ALERT. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE NUMBER THREE ENGINE EXCEEDED NORMAL OPERATING TEMPERATURES. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE
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