JASC 7230
Service difficulty reports · 5,064
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 UIEA2019031403539Acoustic Liner · delaminatedDURING INSPECTION ON NR 1 ENGINE ACCUSTICAL LINER SEGMENT FROM 4 O CLOCK TO 6 O CLOCK POSITION WAS FOUND WITH DELAMINATION.(<P>REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT IAW AMM 72-33-01-004-001-H00 AND 72-33-01-404-011-H00.</P>)SDR ASAA2019031028561Spacer · debondedPER TC 78472010 FAN BLADE LUBRICATION NR 1 ENGINE SPACER NR 21 AND NR 24 ARE DISBONDED. GROUNDED - YES. REMOVED & REPLACED NR 21 & NR 24 SPACERS ON NR 1 ENGINE REF TC 78472010.SDR ASAA2019030828562Spacer · debondedWHILE ACCOMPLISHING T/C #78472010, FAN LUBE NR 1 ENGINE. FOUND 3 SPACERS DISBONDED NR 14, NR 16, AND NR 20. GROUNDED - YES. REPLACED THE NR 14, 16, AND 20 FAN BLADE SPACERS (NR 1 ENG S/N 445486) REF T/C 78472010.SDR QMLA2019030619025Impeller · damagedON AIRWORTHINESS CHECK DAMAGE WAS OBSERVED ON THE NR 2 ENGINE IMPELLER BLADES.SDR HALA2019030600090Blade · damagedETOPS SIGNIFICANT SYSTEM - FOUND DAMAGE ON NR 15 COMPRESSOR BLADE ON NR 2 ENG. 5 INCHES FROM BLADE TIP DENT DIMENSION X AT .162 INCH DIMENSION Y .094 DIMENSION Z 1.04 INCH. FOUND DIM X=.162 DIM Y=.094 DIM Z= 1.04. FOUND TO BE OUT OF LIMITS PER AMM 72-31-41-000SDR UIEA2019030503474Blade · nickedNR 2 ENGINE HAS FAN BLADE WITH NICK BLADE MARKED.(<P>LOCATED AND BLENDED OUT NR 2 ENGINE FAN BLADE MARKED PER AMM 72-31-02-308-055-1-00.</P>)SDR UIEA2019030503478Blade · nickedENGINE NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES HAVE NICKS ON THE LEADING EDGES.(<P>BLENDED OUT ENG NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES LEADING EDGES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION ON THE BLENDED AREAS.SDR ASAA2019030428461Spacer · debondedNR 1 ENG FAN BLADE SPACERS NR 1,4,6,13,16,19 HAS RUBBER DISBOND. GROUNDED - YES. REPLACED NR 1 ENG FAN BLADE SPACERS REF T/C # 78472010.SDR ASAA2019030128438Platform · wornNR 1 ENG HAS 24 WORN PLATFORMS. GROUNDED - YES. REMOVED AND REPLACED ALL 24 PLATFORMS ON NR 1 ENG. REF T/C 78472010.SDR ASAA2019030128437Spacer · wornNR 1 ENG HAS 5 WORN SPACERS. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG 5 WORN SPACERS REF T/C 78472010.SDR UIEA2019030403453Fan · out of balanceRIGHT ENGINE FAN VIBRATIONS HIT 4.5 IN CLIMB & MAINTAINED 4.5 LEVEL CRUISE FLIGHT(<P>PERFORMED FAN TRIM BALANCE ON RT ENG IAW AMM 72-31-00. FAN VIB CORRECTED TO 0.8. REF LOG PAGE 1026507-6: ECM C/W. </P>)SDR ASAA2019022728382Blade · damagedDURING ACCOMP T/C 78472010 FOUND NR 12 BLADE CU-NI COATING MISSING OUT OF LIMITS NR 1 ENG. GROUNDED - YES. REMOVED AND REPLACED NR 12 BLADE AND NR 24 BLADE , REQUIRES ENGINE VIBRATION SURVEY REF TASK CARD 78472010 FOR SURVEY.SDR ASAA2019022728381Platform · wornENGINE PLATFORMS AT POSITIONS 4,15, 19 WORN BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED AIRCRAFT ENGINE NR 1 PLATFORMS AT POSTION 4,15, 19 REF TASK CARD 78472010.SDR WI5R2019022800001Rotor · fracturedDURING FLIGHT, THE CUSTOMER REPORTED A 'BANG'. FIELD TROUBLESHOOTING INDICATED THE N1 SPOOL WAS DIFFICULT TO ROTATE AND THERE WAS DAMAGE NOTED ON THE 3RD STAGE IP ROTOR BLADES. DISASSEMBLY OF THE ENGINE CONFIRMED FIELD FINDINGS AND ONE MISSING 3RD STAGE IP BLSDR CA190227014Engine · stalled(CAN) JUST AFTER TAKE-OFF, PASSING 500 FEET`, AT GEAR UP RETRACTION, A LOUD SOUND REPETITIVELY FOR 3 CONSECUTIVE TIMES, #1 ENGINE STALL, NO LIMIT OR TEMP EXCEEEDANCE OBSERVED REDUCED, THRUST TO 75 % N1 AND STALL COND CEASED. CREW DECLARED A PAN PAN PAN & THEYSDR ASAA2019022428331Blade · wornPLATFORMS 1-24 ON NR 1 ENG WORN. GROUNDED - YES. REMOVED AND REPLACED PLATFORMS 1-24 ON NR 1 ENG.SDR UIEA2019022503377Blade · nickedNR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 1 HAS A NICK AT L/E CONTOUR. INSPECTED AND FOUND TO BE .0003" IN DEPTH, MAX ALLOWABLE .060". NR 1 FAN BLADE FOUND TO BE IN LIMITS AND SERVICEABLE IAW AMM 72-31-02-226-019.SDR UIEA2019022503378Blade · nickedNR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 20 HAS A NICK AT L/E CONTOUR. BLENDED THE NICK AND RAISED MATERIAL ON THE NR 2 FAN BLADE 20, MATERIAL LOSS AFTER REPAIR .028,MAX ALLOW .060, VERFIED CONDITION OF BLADE VIA NDT, BLADE FOUND TO BE SERVICEABLE, NO FURSDR 9WGA20190225301Compressor · stalledON TAKE-OFF ROLL, ENGINE #2 COMPRESSOR STALL AT 80 KTS. ENGINE REQUIRES REPLACEMENT. ENGINE REPLACEMENT DUE TO CHRONIC ISSUE, SPECIFIC REASON UNKNOWN. WILL EVALUATE AT TEST CELL.SDR HALA2019022500062Compressor · leakingSOCKS SMELL ON DESCENT OUT OF 8000' ODOR STRONGEST OVER WING INTENSIFYING AT LANDING.// CONFIRMED ODOR COMING FROM #2 ENG WITH BOTH PACKS RUNNING REF. TSM 71-00-00-810-847 ACP'D TO STEP 5. NO CONTAMINATION FOUND. NEXT STEP BORESCOPE. ACCOMPLISHED TSM 71-00-00-SDR UIEA2019022503382Blade · nickedFOUND COMPRESSOR BLADE ON THE NR 1 ENGINE WAS FOUND DAMAGED. FOUND THE NR 1 BLADE NICKED, MEASURED .064 DEEP. BLENDED NICK DOWN TO .094 IAW AMM 72-31-02-308-045-1400. PERFORMED FLOURESCENT PENETRATION INSPECTION IAW AMM 72-31-02 & NDT 70-11-06, NO DEFECSDR ASAA2019021628213Elastomer · debondedWHILE ACCOMPLISHING TASK CARD NO. 1 ENGINE ALL SPACERS WERE DIFFICULT TO REMOVE PER TSR AND WHILE INSPECTING SPACERS FOUND NR 3 & NR 14 SPACERS ELASTOMERS DISBONDED. GROUNDED - YES. PER INSPECTION, SPACERS REPLACED.SDR CA190220017Stator Vane · worn(CAN) ENGINE ASSY P/N 6078T7G01, WAS INSTALLED. AT 12054 :22 ENGINE HOURS, 11860 CYCLES, AS A PREVENTIVE ACTION, A SPECIAL DETAILED INSPECTION OF COMPRESSOR VARIABLE VANE SPINDLE AXIAL MOVEMENT HAS BEEN PERFORMED USING GUIDELINES AND LIMITS FROM GE HEAVY MAINTSDR AALA201902189010Compressor · stalledAT FL360, NR 2 ENGINE COMPRESSOR STALL AND EGT OVERTEMP. NR 2 ENGINE AUTO SHUTDOWN, FOLLOWED ECAM PROCEEDURES, NR 2 ENGINE MASTER SWITCH OFF AND LANDED. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED NR 2 ENGINE IAW 26L40071004 AND 26L00071015.SDR W6JA20190214030Blade · damagedDURING TAKEOFF ROLL OUT, JUST PAST V1, CREW HEARD A SERIES OF POPPING NOISES FROM THE NR 2 ENGINE. DUE TO CURRENT AIRSPEED, CREW OPTED TO CONTINUE ROTATION & LIFTOFF. NR 2 ENGINE INDICATIONS BEGAN TO FLUCTUATE & PIC REDUCED POWER TO IDLE, WHILE SIC DECLARED ANSDR UIEA2019021303209Blade · damagedFOUND MULTIPLE BLADES (FAN) WITH DAMAGE ON #1 ENG.(<P>BLADES REQ REWORK DUE TO DAMAGE BLADE 34 REMOVED 1.2 IN BEND LEADING EDGE TO TRAILING. BLADE 30 REMOVED .7 IN BEND LEADING TO TRAILING. BLADE #4 CONTOURED .4 - 3" FROM LEADING EDGE BLADE 1 CONTOURED .2 IN BSDR DALA2019021200940Compressor · stalledIFSD & ATB - DUE TO THE LOSS OF THE NR 1 ENGINE. AT APPROX 600FT AGL, FLT CREW REPORTED LEFT ENGINE COMPRESSOR STALL AND ENGINE ROLL BACK. CREW FOLLOWED QRH AND SHUT DOWN ENGINE. MAINTENANCE FOUND TURBINE DAMAGE. THE ENGINE WAS REPLACED.SDR NM1Y2019021100001Seal · damagedDURING ROUTINE ENGINE SHOP VISIT, THE 2-5 SPOOL FROM ENGINE WAS FOUND WITH A STG 1 SEAL TEETH MISSING FRAGMENT.
NO ABNORMAL ENGINE RUNNING CONDITION WERE REPORTED BY THE CUSTOMER BEFORE ENGINE INDUCTION IN OUR SHOP. THE ENGINE WAS REMOVED FOR SCHEDULED HIGH-SDR ASAA2019021028140Spacer · debondedWHILE ACCOMPLISHING TASK CARD FOUND FAN BLADE SPACERS 6, 8, 13, 19, AND 24 DISBONDED ON NR 1 ENGINE. GROUNDED - YES. REMOVED AND REPLACED SPACERS 6, 8, 13, 19, AND 24 ON NR 1 ENGINE REF TASK CARD. VIBE SURVEY WILL BE ACCOMPLISHED.SDR UIEA2019021103184Blade · damaged#2 ENGINE LP BLADE #14 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103185Blade · damaged#2 ENGINE LP BLADE #19 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103186Blade · damaged#2 ENGINE LP BLADE #25 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103187Blade · damaged#2 ENGINE LP BLADE #27 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103188Blade · damaged#2 ENGINE LP BLADE #28 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02 FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103189Blade · damaged#2 ENGINE LP BLADE #11 DAMAGED.(<P>INSPECTED BLADE #11 IAW B767 AMM 72-31-02,DAMAGED FOUND TO BE WITHIN ALLOWABLE LIMITS WITH NO FURTHER ACTION REQUIRED.</P>)SDR UIEA2019021103190Blade · damaged#2 ENGINE LP BLADE #32 DAMAGED.(<P>BLENDED DAMAGED AREA IAW B767 AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR UIEA2019021103191Blade · damaged#2 ENGINE LP BLADE #36 DAMAGED.(<P>INSPECTED #36 BLADE IAW B767 AMM 72-31-02,DAMAGED FOUND TO BE WITHIN ALLOWABLE LIMITS WITH NO FURTHER ACTION REQUIRED.</P>)SDR UIEA2019021103192Blade · damaged#2 ENGINE LP BLADE #18 DAMAGED.(<P>REMOVED AND REPLACED #18 BLADE IAW B767 AMM 72-31-02.</P>)SDR UIEA2019021103193Blade · damaged#2 ENGINE LP BLADE #3 DAMAGED.(<P>REMOVED AND REPLACED #3 BLADE IAW B767 AMM 72-31-02.</P>)SDR UIEA2019021103194Blade · damaged#2 ENGINE LP BLADE #26 DAMAGED.(<P>REMOVED AND REPLACED #26 BLADE IAW B767 AMM 72-31-02.</P>)SDR UIEA2019021103195Blade · damaged#2 ENGINE LP BLADE #31 DAMAGED.(<P>REMOVED AND REPLACED #31 BLADE IAW B767 AMM 72-31-02.</P>)SDR UIEA2019021103196Blade · damaged#2 ENGINE LP BLADE #13 DAMAGED.(<P>BLENDED DAMAGED AREA IAW AMM 72-31-02,FOUND TO BE WITHIN ALLOWABLE LIMITS.</P>)SDR CA190219008Blade · distorted(CAN) DURING CLIMB OUT THE LEFT-HAND ENGINE EMITTED A LOUD NOISE, PROMPTING THE CREW TO SHUT DOWN THE ENGINE. THIS IS FOLLOWED BY SMOKE ENTERING THE CABIN. THE CREW THEN DECIDED TO DIVERT FOR A SAFE LANDING. THE AIRCRAFT LANDED UNEVENTFULLY 15 MINUTES LATER ANSDR ASAA2019020728115Blade · wornWHILE ACCOMPLISHING TASK CARD, S/N 894424 FOUND MISSING AND CHIPPED CU-NI-IN COATING BEYOND LIMITS OF AREA X. BLADES NR 1 DD459254-L NR 6 S/N DD458565-G NR 11 S/N DD458388-Y NR 21 S/N DD456868-U. GROUNDED - YES. REPLACED NR 1 ENGINE FAN BLADES NR 1, 6, 11 & 21SDR UIEA2019020603130Blade · nicked#1 ENGINE 1ST STAGE FAN ROTOR HAS 1EA BLADE WITH A NICK IN THE LE APROX 5" FROM THE ROOT SECTION.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-02-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</SDR UIEA2019020603132Blade · nicked#2 ENGINE #13 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM,72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603133Blade · nicked#2 ENGINE #4 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603134Blade · nicked#1 ENGINE 1ST STAGE FAN ROTOR HAS !EA BLADE WITH A NICK IN THE LE APPROX. 7" FROM TIP.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603136Blade · damaged#1 ENGINE 1ST STAGE FAN ROTOR LAS 1EA BLADE WITH A NICJ=K IN THE LE APPROX 12" FROM TIP.(<P>BLENDED AND PERFORMED DPI IAW B767 AMM 72-31-02 AND B767 SOPM 20-2-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR ASAA2019020128022Case · damagedDURING REPAIR OF NR 1 ENGINE FLANGE B SCALLOPED FAN CASE FOUND CASE NOT REPAIRABLE. GROUNDED - YES. REMOVED & REPLACED NR 1 ENGINE. ACCOMPLISHED NR 1 ENGINE DUCT PURGE PER PWRPL-71EA-11276. COMPLETED MIG-2C 316258.
Back to JASC 7230