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 CA140820016Compressor · damaged(CAN) REJECTED TAKE-OFF, NR 1 ENGINE COMPRESSOR STALLED AT TAKEOFF POWER. OPERATOR CONFIRMED THAT THE EVENT COULD BE REPRODUCED DURING MAINTENANCE TROUBLESHOOTING. A BOROSCOPE INSPECTION WAS CONDUCTED AND DAMAGE WAS FOUND TO THE COMPRESSOR SECTION.SDR 9EKA20140806008Compressor · stalledWHILE FLYING A DISTANCE OF 100NM, FOR THE COMPLETION OF THE CONTRACT FLIGHT I HAD TWO COMPRESSOR STALLS. THE FIRST HAPPENED AT A CONSTANT POWER SETTING OF 80% TORQUE, 1000' PA, CAVU WITH WINDS 150/10 KTS, A HEADWIND. HEARD A LOUD BANG FOLLOWED BY YAWING OF THSDR CA140812005Compressor · malfunctioned(CAN) PILOT HEARD LOUD BANGS, TWO OF THEM. LOSS OF HORSEPOWER WITH RISE IN TIT, PILOT E-HANDLED ENGINE WITH NO FURTHER ISSUES. PILOT REPORTED TIT OVER 1000C WITH RED WARNING LIGHT ON. SUSPECT COMPRESSOR BEARING FALURE - METAL FOUND EJECTING FROM FORWARD TURBINSDR CALA2014080691745Compressor · stalledRT ENG SN 726726 HAD AUDIBLE COMPRESSOR STALL DURING ENG START AT STARTER CUT OUT AT APPROXIMATELY 47 -48%. VISUALLY INSPECTED NR 2 ENG CHIP DETECTORS & PERFORMED BORE INSPECTION OF ENG VIA PLUGS AP 2 & AP 8. NO ABNORMALITIES FOUND BY INSPECTION.SDR AALA20140826002Compressor · stalledRIGHT ENG COMPRESSOR STALLED. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG ON 8/03/2014. SYS GND CHECKED NORMAL OPERATION OPEN.SDR AALA20140802005Compressor · stalledRIGHT ENG COMPRESSOR STALLS. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG ON 08/03/2014. SYS GND CHECKED NORMAL OPERATION OPEN.SDR WI5R201407300001Blade · departedDURING BORESCOPE INSPECTION, ENGINE SN 141396, ONE OF THE IP COMPRESSOR BLADES WAS FOUND LIBERATED AT THE ROOT.SDR WI5R2014071000001Rotor · damagedDURING BORESCOPE INSPECTION FOR TAP ENROLLMENT, DAMAGE WAS NOTED ON THE LEAD EDGE OF THE HPC ROTOR. DISASSEMBLED REVEALED THIS WAS SECONDARY DAMAGE. 1 OF THE 3RD STAGE IP ROTOR BLADE FROM IPC ROTOR ASSY 61968, AU01065 LIBERATED AT THE ROOT.SDR CALA2014070800890Blades · bird ingestionBIRD STRIKE TO NR 2 ENG ON LANDING. PERFORMED VISUAL INSPECTION OF NR 2 ENG INLET & EXHAUST FOR DAMAGE. FOUND SEVERAL FAN BLADES BEYOND SERVICEABLE LIMITS. REPLACED COMPLETE SET OF FAN BLADES IAW AMM 72-21-02-400-801- F00 & PREFORMED VIBRATION SURVEY IAW AMSDR WX0A2014080572066Blade · damagedINGESTED BIRD AT V1 ENG GROWLED & 4.0 ENG VIBRATION DUE TO DAMAGE TO BLADES 30 & 31. REPLACED BLADES 30, 31, 12 & 13 IAW AMM 72-21-300-028-A & AMM 72-21-00-400-005-A. NO FURTHER DAMAGE NOTED.SDR VNAA2014070300003Blades · damagedCREW REPORTED BIRD STRIKE AFTER TAKEOFF AND DAMAGED FAN BLADES ON RT ENGINE. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED DEBRIS FROM RT ENGINE INLET, R & R 4 FAN BLADES AND PERFORMED CHECKS IASDR CA140701009Compressor · stalled(CAN) PASSING 44500 FT CLIMBING TO 45000 FT, THE CREW REPORTED THE LT ENGINE COMPRESSOR STALLED. THEY HEARD A LOUD NOISE FROM THE ENGINE. ACCORDING TO THE CREW REPORT, THE ENGINE ROLLED BACK TO FLIGHT IDLE AND PILOT THEN IMMEDIATELY PULLED THE THROTTLE LEVERSDR AALA20140623004Compressor · stalledREPEAT ITEM, DURING FUNCTIONAL CHECK FLIGHT, RT ENG COMPRESSOR STALLED DURING CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. REPLACED RT ENG. SYS GND CHECKED NORMAL OPERATION OPEN.SDR AALA20140620003Compressor · stalledDURING FUNCTIONAL CHECK FLIGHT RT ENG COMPRESSOR STALLED. ENG STABILIZED WHEN THROTTLE REDUCED TO MID-POINT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE WITH NO FAULTS FOUND. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR UTUR2014FA0000400Retaining Ring · missingKEY WASHERS THAT RETAIN COMPRESSOR BALANCE WEIGHTS WERE NOT BENT TO SECURE WEIGHTS. RETAINING RING THAT SECURE NR 1 BEARING OUTER HOUSING TO NR 1 BEARING INNER HOUSING WAS MISSING, UNINSTALLED.SDR UTUR2014FA0000399Washer · misinstalledKEY WASHERS, THAT RETAINED COMPRESSOR BALANCE WEIGHTS WERE NOT BENT TO SECURE WEIGHTS. RETAINING RING THAT SECURE NR 1 BEARING OUTER HOUSINGTO NR 1 BEARING INNER HOUSING WAS MISSING, UNINSTALLED.SDR CA140630020Compressor Wheel · seized(CAN) PILOTS EXPERIENCED STRONG VIBRATIONS ON ENGINE NR 1 FOLLOWED BY AN INCREASE IN INTER TURBINE TEMPERATURE (ITT). THEY ATTEMPTED TO REDUCE THE ITT TO NORMAL OPERATING LIMITS BY REDUCING POWER. HOWEVER, AFTER 2 MINUTES, ITT STARTED INCREASING WITHOUT ANY SDR CA140630012Compressor · making metal(CAN) DURING APPROACH, PILOT FELT A STRONG VIBRATION AND AN EXCESSIVE TEMPERATURE RISE IN NR 1 ENGINE, REDUCED POWER. AFTER 2 MINUTES, THE TEMPERATURE INCREASED AGAIN AND THE PILOT PROCEEDED TO TURN OFF THE ENGINE. LANDED ACFT SAFELY. DURING ON GROUND TROUSDR PCSA2014060501Compressor · stalledAT 3500’ NR 3 ENG COMPRESSOR STALL. RETARDED THRUST, SLOWLY INCREASED THRUST, COMPRESSOR STALLED AGAIN. THRUST AT IDLE, RETURNED TO MIAMI.SDR AALA20140603014Compressor · stalledCREW REPORTED LT ENG COMPRESSOR STALLED DURING CLIMB OUT. EMER DECLARED FLIGHT RETURNED CDG LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG AT CDG ON 06/07/2014. SYS GND CHECKED NORMAL OPERATION OPEN.SDR CA140602028Compressor · damaged(CAN) DURING A HOT SECTION INSPECTION OF THE NR 1 ENGINE, DAMAGE WAS FOUND AT THE 1ST STAGE COMPRESSOR IN THE FORM OF AN AIRFOIL TIP BENT BEYOND LIMITS.SDR ASMF2014061806019Blade · lack of lubeCAPTAIN REPORTED THAT DURING CLIMB, THE LT ENG VIBRATION REACHED 3.1 UNITS & DURING CRUISE THE VIBRATION WAS STABILIZED IN 4.1 UNITS. ACFT WAS SENT TO THE HANGAR & A BORESCOPE INSPECTION IAW AMM 72-00-00-200-808-F00, TRIM BALANCE IAW AMM 71-00-00 TASK 71-00-0SDR CA140527004Compressor Wheel · damaged(CAN) DURING MAINTENANCE THE FLUORESCENT PENETRANT INSPECTION OF THE HPC SPOOL STAGE 4-9 REVEALED SEVERAL RADIAL CRACK INDICATIONS AT THE INTERSTAGE SEAL TEETH. ACCORDING TO THE ENGINE SHOP MANUAL THE HPC SPOOL IS NOT REPAIRABLE AND WILL BE SCRAPPED.SDR SWAA2014052828420Compressor · damagedDIVERSION COMPRESSOR STALLED ON CLIMB OUT. FOUND STAGE 4 HPC DAMAGE OUT OF LIMITS NR 1 ENG. R & R THE NR 1 ENG ASSEMBLY.SDR YYFA20140519001Compressor Blade · damagedDURING WALK AROUND INSPECTION FOUND ENG BLADE DAMAGE ON LT ENG INTAKE C1 BLADES.SDR SIMA20140517010Frame · corrodedLEFT ENG HAS CORROSION ALONG THE LOWER SURFACE BETWEEN THE CONTAINMENT RING & THE FWD FRAME, ABOVE THE GENERATORS. REMOVED LT ENG CORROSION FROM ALONG THE LOWER FRONT FRAME FWD FLANGE, ABOVE THE GENERATORS IAW RRMM 72-25-45-300-805 & 70-00-00-300-805, APPLIEDSDR AALA20140515003Compressor · stalledDFW CREW REPORTED RT ENG COMPRESSOR STALLED. CREW SHUTDOWN ENG, SINGLE ENG TIME 30 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG AT DFW ON 05/16/2014. SYS GND CHECKED NORMAL, OPERATION SDR UIEA2014051300178Blade · erodedENG 2 FAN BLADES LE TOWARD TIP HAVE EROSION. BLENDED SMALL NICKS AT VARIOUS FAN ROTOR BLADES ON ENG 2 IAW 72-31-02, NO FURTHER DEFECTS NOTED.SDR UIEA2014051300177Guide Vane · delaminatedENG 2 OUTLET GUIDE VANE, AFT OF FAN, AT 0900 POSITION, NEEDS LE TAPE. INSPECTION FINDS DELAMINATION WITHIN ALLOWED LIMITS IAW AMM 72-33-00. APPLIED REPAIR WITH APPROVED TAPE IAW AMM 72-33-00-228-046-H00.SDR USAA2014051200003Blade · damagedCREW REPORTED A BIRD STRIKE ON TO AT ABOUT 800 FEET AGL. ONLY ONE BIRD WENT INTO LT ENG. ENG CONTINUES TO RUN WITH NORMAL INDICATIONS. CREW DECLARED AN EMERGENCY & RETURNED TO FIELD AT LGA. AFTER LANDING, CREW SHUT ENG DOWN. ACCOMPLISHED BIRD STRIKE INSPECSDR DALA14027549011Blade · damagedCREW DIVERTED, DUE TO AN ENGINE STALL ON THE NR 1 ENGINE. MAINTENANCE FOUND 1 FAN BLADE DAMAGED BEYOND LIMITS AND SOME ACOUSTIC PANEL DAMAGE IN THE COLD STREAM. ENGINE WAS CHANGED.SDR EVCA2014042800058Compressor · crackedENG COMPRESSOR SCROLL CRACKED.SDR CA140423012Blade · loose(CAN) ENGINE WAS REMOVED FROM THE ACFT AFTER BORESCOPE INSPECTION REVEALED SUBSTANTIAL DAMAGE IN THE COMPRESSOR. ONCE INSPECTED IN THE SHOP, IT WAS NOTED THAT APPROXIMATELY 6 COMPRESSOR BLADES IN THE 12TH STAGE WERE MISSING, CAUSING DAMAGE FROM STAGES 12-14. SDR CALA2014042190877Compressor · stalledLT ENG COMPRESSOR STALL ON TAKEOFF CLIMBING THRU 1000 FT. STALL WAS AUDIBLE 4X. ENG RECOVERED & CONTINUED TO OPERATE NORMALLY DURING RETURN TO FIELD. REPLACED ENG IAW 71-00-02 CONFIG 1.SDR CALA2014041790864Compressor · stalledFLIGHT EXPERIENCED COMPRESSOR STALL ON CLIMB.SDR CA140424010Blade · fractured(CAN) DURING NEW ACFT FLIGHT TEST, ON THE 2ND TAKEOFF, THE ENGINE LOST POWER AND THE PILOT HEARD METALLIC NOISES. THE TAKEOFF WAS ABORTED. MFG LOCAL FIELD SERVICE REPRESENTATIVE WILL BE ON SITE ON 15 APRIL TO ASSESS ENGINE CONDITION. UPDATE NR 1: INSPECTION SDR ASMF2014061706003Blade · lack of lubeCAPTAIN REPORTED THAT DURING CRUISE, BOTH ENGS VIBRATION REACHED 3.2 & 3.6 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE FAN ROTOR BLADE OF THE RT ENG IAW AMM 72-21-00 & FAN TRIM BALANCE TEST 14B IAW AMM 71-00-00, BEING WITHIN LIMITS.SDR A6WA201441411Bracket · crackedLEFT ENG LOWER FAN CASE BRACKET CRACKED. R & R WITH NEW SERVICEABLE BRACKET IAW REO 601R-71-61-3941 REV A.SDR A6YA2014041431460Compressor Blade · brokenTHE FLIGHT CREW CALLED & STATED THE RT ENG WAS MAKING A WHINING SOUND & THERE WAS AN ODOR JUST AFTER LANDING. ALL IN FLIGHT ENG INDICATIONS WERE REPORTED AS NORMAL. THE FLIGHT CREW WAS ASKED TO START THE RT ENG. THE GND IDLE WAS OBSERVED FLUCTUATING FROM 54%SDR DALA14020599205Compressor · stalledPERFORMED AIR TURN BACK DUE TO NR 2 ENGINE COMPRESSOR STALLS ABOVE IDLE DURING CLIMBOUT. EMERGENCY WAS DECLARED. BOROSCOPED ENGINE. R & R SEVERAL PARTS. ENGINE STILL STALLING. R & R NR 2 ENGINE.SDR UIEA2014032800133Blade · nickedENGINE 3 HAS NR 2 FAN BLADE THAT IS NICKED BEYOND LIMITS, SPECIFIED IN AMM 72-31-02. NICK IS APPROXIMATELY .040 INCHES IN WIDTH & .040 INCHES IN DEPTH. REPAIRED NR 2 FAN BLADE AREA F TO MIN LIMITS IAW 72-31-02.SDR UIEA2014032800132Blade · nickedENGINE 3 HAS 31 FAN BLADE THAT ARE NICKED BEYOND LIMITS SPECIFIED IN AMM 72-31-02. NICK IS APPROXIMATELY .020 INCHES IN WIDTH & .020 INCHES IN DEPTH. ITEM REPAIRED IAW AMM 72-31-02.SDR QMLA2014032714032Compressor · crackedDURING ACFT AIRWORTHINESS CHECK, A 3/8 INCH CRACK WAS NOTED ON THE RT SIDE OF THE ENGINE COMPRESSOR ASSEMBLY IN THE COMPRESSOR HOUSING.SDR WI5R2014032800001Blade · missingDURING A BORESCOPE INSPECTION, A THIRD STAGE IP ROTOR BLADE WAS FOUND MISSING. SECONDARY DAMAGE WAS NOTED TO THE COMPRESSOR ROTOR. DISASSEMBLY CONFIRMED ONE BLADE ON THE THIRD STAGE IP ROTOR IS MISSING.SDR 2014FA0000182Blade · failedWHILE PERFORMING POST OVERHAUL TEST OF ENGINE, ENGINE HAD RUN NORMALLY FOR 15 TO 20 MINUTES AND HAD BEEN STARTED AND STOPPED NORMALLY FOUR OR FIVE TIMES, TEST PROCEEDING NORMALLY UNTIL THIRD POINT DOWNWARD JUST SETTING IN FOR DWELL TIME, A LOUD MECHANICAL BANGSDR SWAA2014030625799Compressor · stalledAIR TURN BACK, ON DEPARTURE LT ENG COMPRESSOR STALL 2 TIMES WITHIN 3 MINUTES BETWEEN COMPRESSOR STALLS. R & R NR 1 ENG IAW TASK CARD.SDR CA140226007Compressor · seized(CAN) ENGINE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED THAT DURING FLIGHT, THE OIL PRESSURE LIGHT TURNED ON AND THE ENGINE WAS IMMEDIATELY SHUTDOWN. POST CHECK OF THE ENGINE REVEALED THE COMPRESSOR WAS SEIZED, METAL IN THE OIL FILTER AND METAL ON SDR USAA2014022400002Blade · damagedHIGH VIBRATION ENG NR 1 DURING DESCENT N1 9.9 N2 NORMAL. ACCOMPLISHED BIRD STRIKE INSPECTION IAW JC 26L00005007. ACCOMPLISHED BORESCOPE INSPECTION IAW JC 26L40072006. FOUND BLADES 27, 28, 29 & 30 DAMAGED. R & R DAMAGED BLADES IAW TASK AMM 72-21-00-300-029A.SDR ASMF201403004Blade · lack of lubeAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG VIBRATION REACHED 0.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE RT ENG FAN ROTOR BLADES & FAN DISK IAW AMM 72-21-02 & VIBRATION TEST NR 7 WAS PERFORMED IAW MM 72-00-00, SDR ABXA2014021114Case · corrodedFAN EXIT CASE INNER SKIN CORRODED AT NR 7 FAN FRAME STRUT. BLENDED AREA IAW GECF6-80A ESM 70-42-00. REPAIRED AREA IAW ABX AIR REA-C072- 60864 RFTS NR E-46177 REVISION DATE 2-11-14. SDR INFO PN 9295M34G15, SN 3HY20080, AFT FAN CASE, CORRODED, RT, NAC 160.0.
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