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.

SDR WX0A2015033072495Blade · damagedENGINE NR 2 N1 VIBES READS 3.4 ON CLIMB OUT. ENG VIBES REACH 1.0 PASSING 200FL ON DESCENT 8000. ENG NR 2 VIBES SPIKED TO 8.8 THEN STABILIZED AT 4.0 FOR REMAINDER OF LANDING, COULD EASILY FEEL THE VIBE THROUGHOUT THE ACFT. INSPECTION OF ENG NR 2 INLET EVIDENMar 26, 2015 · N219NV · Airbus A320214SDR HEER2015FA0000103Bearing · spalledENGINE REMOVED 2-24-15 DUE TO METAL IN OIL. NR 2 BEARING EXHIBITED HEAVY SPALLING ON BALLS. INSTALLED NEW PART.Mar 22, 2015 · N15MX · Bell 407SDR WI5R2015032500001Blade · missingDURING OPERATION A "HOOTING" SOUND WAS PRESENT FROM IDLE THOUGH MCT POWER SETTING. A FIELD BORESCOPE INSPECTION REVEALED 1 OF THE IP COMPRESSOR BLADES HAD LIBERATED. THE REPAIR STATION INVESTIGATION HAS CONFIRMED THE FIELD FINDINGS. THERE WAS NO EVIDENCE OF Mar 20, 2015 · N53NW · Cessna 525ASDR CA150316004Blade · cracked(CAN) DURING INSPECTION OF ACFT BLOWER FAN, IT WAS NOTED THAT 4 OF THE FAN BLADES WERE CRACKED AT THE BASE.Mar 15, 2015 · Bell 205A1SDR UIEA2015031500180Liner · damagedENGINE 1 LINER SEGMENT AT 730 POSITION HAS A DENT & PUNCTURE IN HONEYCOMB OF LINER SEGMENT FWD OF FAN BLADES. R & R ENG 1 LINER 730 POSITION IAW AMM 72-33-05.Mar 15, 2015 · N640GT · Boeing 7673S1SDR YENA20150312042Compressor · stalledON CLIMBOUT, ENGINE 1 COMPRESSOR VANE ON ECAM. FOLLOWED QRH. IN CLIMB EPR FLEX EGT NR 1 100 DEGREES HIGHER THAN ENGINE 2. NR 1 ENGINE N2 PERCENT 86.6 AND ON NR 2, 84.4. R & R ENGINE NR 1. ALL OPS CHECK FOUND OK. NOTE: ON APPROACH INTO PBI PILOT DECLARED AN EMar 12, 2015 · N665JB · Airbus A320232SDR CA150313013Blade · separated(CAN) IAW "AVIATION OCCURRENCE REPORT" DATED MARCH, 11, 2015: AFTER LANDING ON RUNWAY 23, WHILE ON TAXIWAY P, SMOKE ODOR WAS DETECTED BY CAPTAIN AND WAS VERIFIED TO BE PRESENT WITH THE FIRST OFFICER. THE SMOKE ODOR APPEARED TO INCREASE AS WAS ACCOMPANIED WITHMar 10, 2015 · Piagio P180SDR R61A201503080158Blade · damagedSHORTLY AFTER TAKEOFF, CREW HEARD A LOUD NOISE, FELT VIBRATIONS AND NOTICED LP VIBRATION GAUGE INDICATING 4.6. CREW REQUESTED A RETURN TO FIELD AND DECLARED AN EMERGENCY. CREW REQUESTED A FLY BY TO CHECK ON STATUS OF GEAR. THEY LOOKED GOOD SO CREW LANDED WITMar 8, 2015 · N113HQ · Emb ERJ170200LRSDR AALA20150302002Sensor · failedLT ENG COMPRESSOR STALLED AT 10,000 FT. AIR INTERRUPTION, EMERGENCY DECLARED. LANDING UNEVENTFUL. NO ENG SHUTDOWN REPORTED. REPLACED ELECTRIC FAN INLET TEMP SENSOR IAW 73-21-02.Mar 1, 2015 · N387AM · Boeing 767323SDR HALA2015030100026Compressor · stalledOPEN-ATO-ENGINE RT COMPRESSOR STALL. REPAIR IN WORK.Mar 1, 2015 · N489HA · Boeing 717200SDR AALA20150226030Compressor · stalledAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RT ENG COMPRESSOR STALL & SHUT DOWN AT 3000 FEET & ACFT RETURNED. R & R RT ENG. FOUND LIBERATED NOSE BULLET & EXTENSIVE DAMAGE TO IGV CASE.Feb 26, 2015 · N575AM · Doug DC982SDR ZN3R2015FA0000086Bearing · separatedREPAIR AND O/H FOR A METAL CONTAMINATION INSPECTION. DISASSEMBLY FINDINGS REVEALED THE SOURCE OF THE METAL CONTAMINATION WAS THE NR 4 ROLLER BEARING. THE BEARING EXHIBITED HEAVY SPALLING WITH DISCOLORATION IN THE FORM OF HEAT DAMAGE WITH ROLLER BEARING CAGE Feb 25, 2015SDR CA150303008Compressor · stalled(CAN) NR 1 ENGINE COMPRESSOR STALL.Feb 18, 2015 · Cndair CL6002C10SDR TAMF2015FA0000068Blades · damagedDURING THE 360 OF THE ACFT, DETECTED A FOD AT LT ENGINE, WITH FAN BLADES NR 8, 9, 22 DAMAGE, NICKED, AND INLET COWL WITH DAMAGE IN THE ACUSTIC PANELS. A VISUAL INSPECTION OF THE LOW PRESSURE COMPRESSOR WAS PERFORMED AND IS NOT REQUIRED A BOROSCOPE INSPECTION TFeb 17, 2015 · N331QT · Airbus A330243FSDR 9EKA02162015003Turbine · crackedDURING 25 HR SCHEDULED INSPECTION, CRACK WAS FOUND IN EXHAUST AREA OF NR 1 POWER TURBINE. MM WAS REFERENCED & NO CRACKS ARE ALLOWED, AWAITING PT CHANGE.Feb 13, 2015 · N512EV · Bell 214STSDR USAA2015021100008Compressor · stalledENGINE NR 1 COMPRESSOR STALL DURING THRUST REDUCTION AT ALTITUDE. NO ENG PARAMETERS EXCEEDED. NORMAL OPERATIONS RESUMED. ENG NR 1 CHANGED DUE TO FAILED BORESCOPE INSPECTION.Feb 10, 2015 · N746UW · Airbus A319112SDR WI5R201502050001Blade · missingDURING INSPECTION, ENGINE 3RD IP COMPRESSOR BLADES WAS FOUND LIBERATED AT THE MIDSPAN. ADDITIONAL DAMAGE WAS NOTED ON THE LE OF THE HPC ROTOR.Feb 3, 2015 · Cessna 525ASDR VMIA201506101671Bearing · failedENGINE FAILURE INFLIGHT DUE TO COMPRESSOR BEARING NR 2 FAILURE.Jan 26, 2015 · N709AC · Aerosp AS355F1SDR ASMF201503007Blade · vibrationDURING CLIMB, THE LT ENG VIBRATION REACHED 3.8 UNITS. PERFORMED A BORESCOPE INSPECTIONS IAW AMM 72-00-00-200-808-F00, AMM 72-00-28-00-200-808-F00, AMM 72-00-00-200-804-F00, AMM 72-00-00-200-807-F00, TRIM BALANCE IAW AMM 71-00-00, TASK 71-00-00-750-803-F00, PLJan 24, 2015 · N904AM · Boeing 737752SDR Y3AR2015FA0000019Bearing · damagedFOUND NR 2 COMPRESSOR BALL BEARING TO BE MAKING METAL. REMOVED FROM SERVICE AND FOUND DAMAGED BALL.Jan 8, 2015SDR CALA2015010900028Compressor · stalledRIGHT ENG COMP STALL & DISPLAYED ENG FAIL AT 80 KTS ON FULL POWER TO DUE STRONG LT CROSSWINDS & WIND SHEAR. COMPLIED WITH ENG STALL INSPECTION IAW MM 71-00-00-200-809. ALL CHECKED OK. COMPLIED WITH NR 2 ENG BORESCOPE IAW 71-00-00-200. ALL DAMAGE FOUND, ALLJan 8, 2015 · N78009 · Boeing 777224SDR FDEA201501080096Blade · damagedDURING BIRD STRIKE INSPECTION, FOUND FOUR FAN BLADES DAMAGED NR 3 ENG. REFERENCE WRI 05-50/1662 FOR PARTS IAW BIRD STRIKE CHECK IAW AMM 05-62-00-6 & AMM 72-00-00-6-1 K. INSPECTED NR 3 ENG CORE INLET FOR EVIDENCE OF FOD INGESTION. NO DEBRIS OR FOD NOTED AT CJan 8, 2015 · N307FE · Doug MD1030FSDR ASMF201503001Blade · damagedDURING OVERNIGHT CHECK, IT WAS DETECTED IN THE RT ENG A MISSING MATERIAL AT FAN BLADE ABRADABLE SHROUD & DISTORTION AT FAN BLADE LE. PERFORMED REVISION DETECTING A MISSING MATERIAL AT RT ENG FAN BLADE OF 1.0 INCH LENGTH, 0.200 INCH DEPTH, 0.500 INCH WIDE, SO Jan 7, 2015 · N788XA · Boeing 737752SDR UIEA2015010400001Blade · bentRIGHT ENG FAN BLADE BENT ON POST FLIGHT. INSPECTED NR 2 ENG, FOUND LE DISTORTION BLADES 21, 22 & 23 FIRST STAGE FAN. ALL DISTORTIONS WITHIN LIMITS IAW AMM 72-31-02-226-019 STEP 1 M.Jan 3, 2015 · N640GT · Boeing 7673S1SDR REXA2014123101242Compressor · stalledDURING DECENT, EXPERIENCED LT ENGINE COMPRESSOR STALL, CREW DECLARED EMERGENCY. MAINT IS TROUBLESHOOTING. ADDITIONAL INFORMATION TO BE PROVIDED. AT 23000 FT THE LEFT ENGINE STARTED POPPING AND LOSING POWER BUT WOULD INSTANTLY COME BACK. THE ITT WOULD STDec 31, 2014 · N903XJ · Cndair CL6002D24SDR FDEA201412174136Blade · damagedRIGHT ENG VIBRATION DURING CLIMB PASSING 1000` AGL. ENG SECONDARY VIBRATION MONITOR DISPLAYED 5.0 N1 ON RT ENG. VIBRATION FELT IN YOKE, RUDDER PEDALS & FLOOR. NO OTHER ABNORMAL INDICATIONS. DUMPED FUEL & RETURNED. FOUND NR 2 FAN BLADE TE TIP CAP & TE GUARDec 17, 2014 · N853FD · Boeing 777FS2SDR HALA2014121300209Compressor · stalledCOMPRESSOR STALL ON LT ENGINE 1000 FT, MAX POWER. ACCOMPLISHED AMM 72-00-00-200-801 FROM PAR D THRU E(3) 15856. REMOVED NR 1 ENGINE IAW M144-717. ENGINE RUN, LEAK-CHECK OF INHIBIT PORT ON TUBE BETWEEN FMU AND BVV AT BOTTOM OF ENGINE GOOD IAW AMM 71-00-11Dec 13, 2014 · N487HA · Boeing 717200SDR ASMF201501019Blade · damagedDURING TRANSIT CHECK, IT WAS DETECTED NICKS IN TWO INLET CASE FAN BLADES OF THE RT ENG. PERFORMED REVISION DETECTING TWO NICKS OUT OF LIMIT IAW AMM 72-24-02. INSPECTION PERSONNEL EVALUATED THE DAMAGE, CONFIRMING THE NICKS OUT OF LIMITS IAW AMM 72-24-02. THEDec 12, 2014 · N859AM · Boeing 7378Q8SDR CA141126002Housing · damaged(CAN) ENGINE P-44016 WAS BROUGHT INTO THE TURBINE SHOP FOR ROUTINE OVERHAUL AND WHEN THE ENGINE WAS TAKEN APART THE COMPRESSOR HOUSING WAS DAMAGED IN THE AREA WERE THE NR 2 IMPELLER SITS AND RIDES IN. THIS AREA HAS A SPRAY METAL REPAIR THAT IS DONE TO BUILD UPNov 26, 2014 · Swrngn SA227ACSDR SWIA201440169Pin · unserviceableRT ENGINE VIBRATION REACHED 5.2 AT FL 360. REPLACED FAN BLADE PINS WITH SERVICEABLE UNITS. LUBED FAN BLADE TANGS AND REINSTALLED ORIGINAL SET OF FAN BLADES IAW ENGINE MANUAL.Nov 26, 2014 · N802SK · Cndair CL6002D24SDR CA141202003Compressor · damaged(CAN) THE CUSTOMER REPORTED THAT DURING TAXI THE THEY HEARD POPPING SOUNDS FROM THE ENGINE. THEY RETURNED TO THE RAMP AND THE PILOT SHUT DOWN THE ENGINE. THE ENGINE WOULD NOT RE-START AND THERE WERE STILL POPPING SOUNDS HEARD. THE ENGINE WAS REMOVED AND SENT TNov 16, 2014 · Lear 60LEARSDR CA141114008Compressor · failed(CAN) CREW STATED THEY HEARD POPPING ON TAKEOFF AND ITT STARTED CLIMBING. THE RT ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WITH AN UNEVENTFUL LANDING. THE FDR SHOWS 965C MAX FOR 2 SECONDS. THE HPC HAS MAJOR IMPACT DANov 11, 2014 · Cndair CL6002B19SDR RJEF20141112001Compressor · bird ingestionDURING APPROACH, THE PILOT REPORTED A BIRD STRIKE ON ENG 2 & SMOKE FROM ENG 2 EXHAUST WAS NOTED. ENG 2 WAS SHUTDOWN INFLIGHT & THE ACFT WAS RETURNED. NO OVERWEIGHT LANDING WAS REPORTED. PERFORMED AIRCRAFT VISUAL INSPECTION FOR FOD PER AMM 05-50-02-200-801Nov 11, 2014 · N984TA · Emb ERJ190100IGWSDR YTRA2014111832201Compressor · stalledON DEPARTURE THE ENG EXPERIENCED A COMPRESSOR STALL WITH SIGNIFICANT YAW.Nov 11, 2014 · N373RL · Bell 407SDR SWIA201439904Blade · vibrationDURING FLIGHT, THE NR 1 ENGINE LOW PRESSURE VIBRATION REACHED 4.0 CAUTION AND FLUCTUATED BETWEEN 3.7 AND 4.0 ENTIRE FLIGHT. DIVERTED, REMOVED NR 1, 25, 26 FAN BLADES PINS OF LT ENGINE AND CLEANED AND INSPECTED AND LUBRICATED IAW AMM. PERFORMED VIBRATION CHECNov 10, 2014 · N117SY · Emb ERJ170200LRSDR CA141202017Compressor · damaged(CAN) ACFT CAME BACK FROM A FLIGHT FOR REFUEL. ENGINE START AFTER THE REFUEL WAS OK. AS THE PILOT STARTED PULLING THE COLLECTIVE, THE LT PS WAS SURGING/VIBRATION WAS FELT, ITT WENT HIGH, PILOT SHUTDOWN THE ENGINE. COMPRESSOR DAMAGE WAS OBSERVED. CUSTOMER ALRNov 8, 2014 · Bell 212SDR CA141202004Blade · failed(CAN) WHILE IN FLIGHT, CREW FELT A THUMP WITH NO IMMEDIATE ENGINE INDICATION CHANGES. THE CREW NOTICED A SLIGHT T5 RISE WHICH STABILIZED. WHILE REDUCING COLLECTIVE ON APPROACH, THE NR 2 ENGINE LOST POWER AND HAD FLUCTUATING ENGINE INDICATIONS. THE CREW SHUTDONov 5, 2014 · Skrsky S76BSDR 2016FA0000286Rotor · crackedTHIS CRACK EXTENDS OVER THE ENTIRE LENGTH OF THE MOUNTING FLANGE AND OVER THE 2 SEAL FINS TOWARDS STAGE 8. IN THE COURSE OF THE TEARDOWN OF THE HPC ROTOR, MORE CRACKS WERE NOTED IN THE AREA OF THE FLANGE ON THE IBR 7.Oct 31, 2014SDR USAA2014103100010Blade · out of balanceSTRONG VIBRATION FELT THROUGHOUT ACFT, BUT STRONGEST IN AFT SECTION. ENG 1 & 2 VIBRATION NO MORE THAN 1.2 TO 1.4 INCHES CRUISE & 2.8 INCHES DECENT. ACCOMPLISHED JOB CARD 26T00027006 ELEVATOR SERVO CONTROLS & HINGE BEARINGS FOR PLAY. SPICED SEAL IN PANEL 197Oct 30, 2014 · N122US · Airbus A320214SDR ASOA20141027113Blade · separatedENGINE NR 1 FAILED AT 2200 MSL. R & R NR 1 ENGINE, OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE. NO N2 ROTATION. 6TH STAGE COMPRESSOR BLADE HAD LIBERATED.Oct 24, 2014 · N16571 · Emb EMB145LRSDR USAA2014102000003Compressor · stalledENGINE NR 2 COMP STALL. 1ST STALL AT 600FT AGL, ENG QUICKLY RECOVERED ENG STALLED 2ND TIME AT 2500FT WHILE CLIMBING, ALSO RECOVERED QUICKLY. ENG WAS AT TOGA THRUST FOR THE 1ST COMP STALL, WAS AT CLIMB THRUST WHEN 2ND COMP STALL OCCURRED. ENG FAILED BORESCOPEOct 17, 2014 · N672AW · Airbus A320232SDR CA141023002Compressor · damaged(CAN) IN CRUISE AT FLIGHT LEVEL 370, THE NR 1 HAD A STALL, FOLLOWED BY VIBRATION INDICATION OF 6.6 UNITS ON THE NR 1 ENGINE N3 COMPRESSOR. THRUST LEVER WAS REDUCED BELOW VIBRATION ADVISORY AND SLOWLY ADVANCE TO NORMAL THRUST AND ENGINE AGAIN EXPERIENCED A STALOct 16, 2014 · Airbus A330243SDR ANCF2014101001Compressor Blade · damagedPIREP DURING TAKEOFF ROLL AT V1, BIRD IMPACT SUSPECTED, AFTER THAT STRONG VIBRATION WAS FELT AT ENG 2, WITH AN ECAM ADVISORY 9.0 VIB N1 WHEN POWER WAS APPLIED. IAW AMM 72-00-20-200-006-A BORESCOPE INSPECTION OF BASTER, HPC STAGES 1, 3 & 8 & COMBUSTION CHAMBEROct 10, 2014 · N992TA · Airbus A319112SDR FDEA201409272823Balance Weight · out of positionAS THE THROTTLES DECREASED AT TOP OF CLIMB THE AIRCRAFT DEVELOPED A SIGNIFICANT VIBRATION THAT COULD BE FELT & HEARD. THE LT ENG N1 VIBRATION WAS 3.2, ALL OTHER PARAMETERS WERE NORMAL ON BOTH ENGS. RETARDING THE THROTTLE 10% N1 IN CRUISE AT FL310 DIMINISHEDSep 27, 2014 · N880FD · Boeing 777F28SDR QMLA2014091814112Compressor Blade · damagedDURING THE FIRST 600 HOUR ENG INSPECTION, PERFORMED AXIAL COMPRESSOR BLADE INSPECTION CHECK FOR DAMAGE & SERVICEABILITY, DISCOVERED ONE BLADE HAD FOD DAMAGE AT THE TIP THAT EXCEEDED THE REPAIR LIMITS FOR LEVEL 2 TECHNICIANS. FURTHER DAMAGE TO THE ENG IS UNKNOSep 18, 2014 · N328CH · Urocop EC130B4SDR ABXA20140910291Engine · bird ingestionON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. RESep 10, 2014 · N315AA · Boeing 767223SDR CA140918011Bellcrank · cracked(CAN) FLIGHT CREW RECORDED A RIGHT ENGINE N2 OVERSPEED (RED INDICATING ABOVE 99.3 N2) WHILE ON AN APPROACH TO LAND. MAINTENANCE TROUBLESHOT THE IDENTIFIED DEFECT AND FOUND THE VARIABLE GUIDE VANE BELLCRANK (GE IPC FIG 10 ITEM 390, P/N 5026T46G01) FRACTURED AT Sep 8, 2014 · Cndair CL6002B19SDR UHLA2014090800624Blade · damagedENCOUNTERED MULTIPLE BIRD STRIKES SHORTLY AFTER TAKEOFF. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R ENGINE 2 BLADES 2, 3, 16, AND 17. DID RII AND HIGH POWER RUNS. HIGHEST VIBE WAS 1.4 FOR LP AT MAX THROTTLE.Sep 8, 2014 · N215JQ · Emb ERJ170200LRSDR SIMA20140908003Compressor Blade · lack of lubeAT INITIAL CRUISE FLIGHT, NR 2 ENG FAN REACHED APPROX 3.5 VIBRATION. AOM VOL 1 PROCEDURE FOLLOWED. REDUCTION IN THRUST EVENTUALLY HELPED A BIT. FOLLOWED PROCEDURE IN AMM 22-21-02 & PERFORMED THE VIBRATION CHECK IAW 71-00-00. PERFORM BLADE LUBE WITHIN 50 F Sep 8, 2014 · N523AE · Cndair CL6002C10SDR CA140826022Rotor · seized(CAN) DURING REVENUE FLIGHT, AS A CARGO FLIGHT, DURING CLIMB CONDITION AT AROUND 16500 THE LEFT ENGINE PARAMETERS STARTED FLUCTUATING AND ENGINE SHUTDOWN BY ITSELF. NO AIR RESTART ATTEMPTED, SINCE PROP DID NOT FEATHER WHEN CLA FUEL CUT OFF POSITION SELECTED. AAug 16, 2014 · Dhav DHC8314
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