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 UALA2011020200575Compressor · vibratesENG 2 COMPRESSOR VANE ON UPPER ECAM. ENGINE WAS SHUTDOWN AND RESTARTED. FAULT CLEARED BUT RETURNED WHEN THROTTLE ADVANCED TO BREAKAWAY THRUST. LAST LEG FAULT CHANNEL A & B VSV ACT-HC-EEC2 WITH FLT DATA FAULT SVA TK IN FLT PH 02. CHECKED IAW TSM. ACCOMPLISSDR UALA2011020200564Blade · vibrationNR2 ENGINE HAS HISTORY OF HIGH VIBS FELT IN AIRFRAME AND FOLLOWS THROTTLE. ACCOMPLISH A FAN BLADE ROOT LUBE IAW SVC TIP MM. REQUIRES VIBE SURVEY IAW MM TEST NR8 AT 1.4 EPR. ACP FAN BLADE ROOT LUBE IAW MM.SDR UALA2011020100549Blade · out of tolerancePROMINENT VIBRATION ON TAKEOFF UNTIL FIRST POWER REDUCTION. CREW TOLD LOCAL MECH VIBS ON ENG 2 WERE 2.8 AND ENG 1 WAS 2.4 AND THOUGHT VIB FELT WAS FROM RT ENG. CHECK INLET AND EXH AND MAIN CHIP DETECTORS OF BOTH ENG'S. CHECK FOR ANY LOOSE VIB SENSORS OR CONNECSDR FDEA201101310431Compressor · stalledCOMPRESSOR STALL DURING TAKEOFF ROLL, UNSURE OF ENGINE, INDICATION WERE MOMENTARY ILLUMINATION OF ENG FAIL LIGHT ACCOMPANIED BY AN ENG COUGH. ENGINE RECOVERED IMMEDIATELY. TAKEOFF WAS REJECTED. PERFORMED NR 1 ENGINE BORESCOPE INSP IN REF TO MM 72-00-00. NSDR MHI2011F00000Cover · crackedDURING SCHEDULED INTERNAL COMPONENT REPLACEMENT OF THE GAS GENERATOR THE MECHANIC FOUND THAT THE COMPRESSOR COVER OF THE COMPONENT WAS CRACKED. THE CRACK WAS LOCATED ON THE TABS OF THE COMPRESSOR COVER. THE GAS GENERATOR HAS BEEN SENT TO MFG FOR FURTHER EVALSDR UALA2011012800481Blades · damagedRT ENGINE SURGE DURING CRUISE WITH LIGHT TURBULENCE AT FL380. EPR DROPPED .20 & N1 10 PERCENT. NO YAW FELT OR AUDIBLE STALL. PARAMETERS RECOVERED AND ARE NORMAL NOW IN SMOOTH AIR. NO EICAS MSGS. REFER TO FAULT CODE 71-05-21-02. CHECK IAW FIM. COMPLETED INSP SDR VNAA2011013100011Compressor · damagedON CLIMBOUT FROM GNV, CREW REPORTED THE LEFT ENGINE FAILED AT ABOUT 3,000 FEET WITH SEVERE VIBRATION AND LOSS OF THRUST DOWN TO BELOW IDLE. ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUTS. CREW SHUT DOWN THE LEFT ENGINE PER QRH, RETURNED TO GNV AND LANDED WISDR UALA2011012500405Guide Vane · crackedLT ENG VANE BENT WITH CRACK VISIBLE BEHIND FAN BLADES. FBO REPORTED ALUMINUM EXIT GUIDE VANE AT 05:30 IS BOWED AND CRACKED. NO CRACKS ALLOWED IAW MM. R & R THE VANE IAW MM. REMOVED FAN CASE EXIT GUIDE VANE AT THE 7 O'CLOCK POSITION AS VIEWED FROM THE REAR SDR MASA2011012601795Fan Blade · lack of lubeCW NR 2 ENGINE FAN BLADE LUBE PER ECTM1707. MX C/W LUBE OF THE ENGINE FAN BLADES.SDR UALA2011012400395Fan Blade · damagedBIRD STRIKE, 300 FEET ON FINAL APPROACH. SUSPECT SOMEWHERE ON LOWER RT SIDE. ACCOMPLISHED BIRD STRIKE INSPECTION AND REPLACED NR 2 ENGINE.SDR SAJFCALS100004Arm · failedB18207, IN ROUTE, DURING CLIMB PHASE (ALT 12,000 FEET), ENG 2 SURGED AND EGT OVER LIMIT(MAX. EGT 722?). ENG 2 IFSD AND AIRCRAFT TURNED BACK. VISUAL INSPECTION FOUND AN METAL PARTICLE ON EXHAUST NOZZLE, THE ENGINE WAS REMOVED FROM SERVICE. FOUND THE SIXTH STAGESDR MASA2011012201770Fan Blade · lack of lubeNR 2 ENG N1 VIBE 1.8. MX PERFORMED FAN BLADE LUBE, POWER RUNS OPS GOOD.SDR MASA2011011901710Fan Blade · lack of lubeNR 2 ENGINE FAN VIBE ABOVE 1.7 IN CLIMB, ACFT RTF. MX CW TEMP RO CRJ9-72-0093 FOR FAN BLADE LUBE.SDR TRBA2011007Servo Valve · malfunctionedAFTER T/O ENGINE NR1 HAD A COMPRESSOR STALL. TORQUE SPIKED 10 PERCENT. PERFORMED GROUND RUN PERFORMANCE CHECK NR1 ENG IAW ATR72 JIC 72-00-00-ERU 10040. NO DEFECTS NOTED. CANNOT DUPLICATE. ACFT TAKEN OUT OF SERVICE FOR SUSPECTED COMPRESSOR STALLS ON NR1 ENGSDR CA110110001Impeller · erodedHP IMPELLER WITH HEAVY EROSION, THINNING AND CRACKING AT THE BACKPLATE. THE TOTAL TIME ON THE ENGINE IS QUITE LOW. WE RECOMMEND ADDITIONAL INSPECTIONS ARE WARRANTED FOR THIS OPERATOR/ENVIRONMENT.SDR CA110124014Compressor · stalledPOWER ROLL BACK DURING CRUISE AT FL410, LOUD NOISES SOUNDING LIKE COMPRESSOR STALLS WERE HEAR FOR APPROX 10 SEC. AFTER WHICH THE ENG POWER ROLLED BACK TO IDLE. THE FLIGHT WAS DIVERTED AND LANDED SAFELY. TROUBLESHOOTING IS ON-GOING. (SDR 2011020500132/DXTA2011SDR UALA2010123004765Spinner · damagedNR 1 LOP, FLIGHT DIVERTED. NR 1 ENGINE SPINNER IS NOT SERVICEABLE. R & R SPINNER. FOUND OIL IN STARTER DRIVE DRAIN LINE ALSO PMA DRIVE AND DEOILER LEAKING. STARTER DRIVE SEAL, DEOILER OIL SEAL AND PMA DRIVE SEAL HAVE BEEN REPLACED. ALSO ENG DRIVE PAD COVESDR IPXA11564071Support Bracket · crackedINSPECTION TYPE:C3, NR1 ENG OTBD COMPRESSOR ROD SUPPORT BRACKET IS CRACKED. REMOVED NR1 ENG OTBD COMPRESSION ROD SUPPORT BRACKET AND INSTALLED NEW BRACKET IAW SPM 70-51-00-400-000, AMM 70-51-00-2.SDR ZZDA2010656Compressor · stalledLEFT ENGINE COMPRESSOR STALL ALERT IN CLIMB THROUGH FL230. TRANSFERRED TO NRWC N082031 ITEM 1, ENGINE FAILED BORESCOPE, REF ITEM 3 LOG PAGE 1696965.SDR UALA2010122104672Blade · bentFOUND ON ARRIVAL RT ENGINE FAN BLADE BENT AT TIP. DAMAGE IS APPROX 1' BY 1.250. BLENDED BLADE IAW MM. EDDY CURRENT MUST BE ACP WITHIN 120 HRS. ACP'D EDDY CURRENT INSP ON BLENDED BLADE.SDR SROM2010017Compressor Blade · nickedNR 2 ENG BIRD STRIKE AND INGESTION AT THE 9 O’CLOCK POSITION. BLOOD AND FEATHERS FOUND ON BLADES IN BYPASS PATH AND BOOSTER INLET. CONDITIONAL INSP COMPLIED WITH IAW AMM 05-51-18 AND 71-00-00. NO DEFECTS NOTED. ENGINE BORESCOPE INSP OF HIGH PRESSURE COMPRESSSDR CA101217002Bearing · failed(CAN) ACFT WAS CLIMBING UP A SLOPE AND PREPARING TO SET UP AN APPROACH FOR LANDING ON TOP OF A RIDGE WHEN THE ENGINE APPEARED TO HAVE LOST POWER OR QUIT. THE PILOT LOWERED THE COLLECTIVE AND DESCENDED TO SET UP FOR LANDING, FLARED FOR LANDING AND LANDED HARD.SDR MASA2010121601471Blade · lack of lubeLEFT ENGINE VIBE IN YELLOW (3.8) DURING TAXI. MX C/W BLADE LUBE.SDR HALA2010121400587Rib · crackedOPEN - ETOPS SIGNIFICANT SYS - CRACK MEASURING 8.5 INCHES FOUND ON AFT FAN CASE RIB AT 4:00 ON NR1 ENG SN 580320. REPAIR IN WORKSDR MASA2010121301440Fan Blade · lack of lubeRIGHT ENGINE VIBE AT 1.2 IN CRUISE. MX CW RT ENGINE FAN BLADE LUBE.SDR COMA2010121090014Pin · sticksON CLIMBOUT FROM MSP RECEIVED RIGHT ENGINE FAN VIB. EMERGENCY DECLARED, A/C RETURNED TO MSP LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE FAN BLADE RETAINING PINS (28EA), VIB CHECK GOOD.SDR CA101208003Blades · damaged(CAN) FLIGHT CALLED FLIGHT DISPATCH VIA THE SAT PHONE FOR A PATCH TO MOC DUE TO AN ENGINE VIBRATION DURING THE CLIMB. CREW ADVISED MOC THAT THEY WERE UNABLE TO ATTAIN CLIMB POWER DUE TO A HIGH ENGINE VIBRATION. IT WAS DECIDED TO RETURN BACK TO POINT OF DEPARTUSDR HALA2010112900573Fan Blade · damagedETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE FAN BLADE 1ST STAGE NR 33 DAMAGED APPROX 1 INCH FROM BLADE TIP L/E. PERFORMED 1ST STAGE FAN ROTOR BLADE INSPECTION PER AMM 72-31-02-226-007-G00. REPAIRED BLADE NR 33 PER AMM 72-31-02/801 MARKED BLADE WITH AN X NEAR REPASDR HALA2010112900571Blade · damagedETOPS SIGNIFICANT SYSTEM, NR 2 ENGINE FAN BLADE 1ST STAGE NR 33 DAMAGED APPROX 1 INCH FROM BLADE TIP L/E. PERFORMED 1ST STAGE FAN ROTOR BLADE INSPECTION PER A MM 72-31-02-226-007-G00. REPAIRED BLADE NR 33 PER AMM 72-31-02/801, MARKED BLADE WITH AN X NEAR REPSDR ZZDA2010593Compressor · stalledCOMPRESSOR STALL LEFT ENGINE AFTER TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD 603. LEAK AND OPS CHECK GOOD.SDR CA101119002Bolt · mismanufactured(CAN) A BATCH OF 310 GAS GENERATOR CASE P3 CABIN BLEED RETAINING BOLTS (P/N MS9677-07) WERE DELIVERED TO MANUFACTURER THAT DO NOT MEET THE ASME DRAWING REQUIREMENTS. THE SCALLOPS ON THE HEAD OF THE BOLT ARE NOT OF SUFFICIENT LENGTH. THESE SCALLOPS ARE REQUIRSDR DALAFAR145SDR104Nut · missingUPON DISASSEMBLY OF THE ROTOR STACK, SHOP NOTICED 48 NUTS OUT OF 60 MISSING FROM THE STACK WHICH HOLDS THE LLPS TOGETHER. THE LLPS AND HARDWARE INVOLVED ARE AS FOLLOWS: 1-2 SPOOL PN 1558M31G07, SN GWNOEW92, STAGE 3 HPC DISK PN 2116M23P01, SN XALG9478, 4-9 SPOSDR AALA20101118GRU01Compressor · stalledGRU - CAPTAIN REPORTED LOUD BANG AND RIGHT ENGINE COMPRESSOR STALL (SINGLE ENGINE TIME 20 MINUTES). THE CREW RECEIVED A FIRE LIGHT ON RIGHT ENGINE AND PULLED A BOTTLE FOR IT. EMERGENCY DECLARED FLIGHT RETURNED GRU LANDED WITHOUT INCIDENT. DURING INSPECTION SDR CA101222011Bearing · failed(CAN) ENGINEERING INVESTIGATION REPORT EIR PT6A 2010-087 ENGINE, SERIAL NUMBER , WAS SENT TO VECTOR ATLANTIC AFTER THE OPERATOR REPORTED OIL PRESSURE DROP DURING FLIGHT AND FOLLOWED BY FINDING METAL CHIPS (BRONZE) IN THE MAIN OIL PRESSURE FILTER DURING SUBSEQUSDR FDEA201011154375Fan Blade · bentDURING TAKEOFF GOT "ICE DETECTED" FOLLOWED BY EVM COMP NR 3 ENG 5.6 WITH AMBER BOX. CREW FELT THE EXCESSIVE VIBRATION. ON ARRIVAL INSPECT FAN AREA AND FOUND 2 FAN BLADE BENT. FOUND ALSO SLIGHT REMAIN OF BLOOD AROUND THE ICE DECTECTOR AND NEAR THE OUTER FAN ASDR USAA2010111592601Fan Blade · bird ingestionFLT 739 PHL-PIT - RTF/EL - THE NR 2 ENGINE WAS IMPACTED BY A FLOCK OF GEESE AT 1500FT. THE CAPTAIN PULLED BACK TO IDLE AFTER EXPERIENCING ENGINE VIBRATION, DECLARED AN EMERGENCY AND RETURNED TO PHL. MAINTENANCE REPLACED SEVERAL DAMAGED FAN BLADES AND OUTBOARSDR AALA20101107DFW16Compressor · stalledDFW - CREW REPORTED LEFT ENGINE COMPRESSOR STALLED (SINGLE ENGINE TIME 10 MINUTES). EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. LEFT ENGINE CHANGED ON 11/09/2010 AT DFW. SYSTEM GROUND CHECK NORMAL OPERATION.SDR HALA2010110500521Stator · damagedETOPS SIGNIFICANT SYS - NR20 AIRFOIL ON RT ENGINE HAS NICK IN AREA F. BLENDED NR7 AIRFOIL IAW AMM 72-31-02-308. PERFORMED FPI IAW AMM 70-11-06/201 NO CRACK INDICATION.SDR HALA2010110500520Stator · damagedETOPS SIGNIFICANT SYS - _RT ENGINE NR7 AIRFOIL HAS NICK IN AREA A, TIP. BLENDED NR7 AIRFOIL IAW AMM 72-31-02-308 PERFORMED FPI IAW AMM 70-11-06/201, NO CRACK INDICATION.SDR HALA2010110500519Fan Blade · damagedETOPS SIGNIFICANT SYS - NR1 ENGINE 1ST STAGE FAN BLADES NR5, NR10, NR24, NR27,AND NR30 HAVE NICKS, ALL 5 FAN BLADES NICK IN AREA A. BLENDED BLADES IAW AMM 72-31-02 PERFORMED FPI IAW AMM 70-11-06/201 NO CRACKS INDICATED. BLADES THAT WERE BLENDED NR 5,10,24,27 SDR FDEA201011044255Blades · damagedON TAKEOFF LT ENG COMPRESSOR STALL. ABORTED TAKEOFF AT 20 KNOTS, PERFORMED VISUAL INSPECTING OF INTAKE & EXHAUST. NO DEFECTS NOTED. THERE WAS A "L ENG SURGE BITE" ON THE MX PAGE. BITE CHECK OF BVCU SHOWED F0 04 F1 & F2 TPU SHOWED. PERFORMED BORESCOPE INSDR AALA20101103MIA01Compressor · stalledMIA - CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED ON CLIMB. RIGHT ENGINE SHUTDOWN FOR APPROXIMATELY 10 SECONDS THEN RE-STARTED AND SET AT IDLE FOR LANDING. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHSDR SWAA106549Engine · stalledAIR TURNBACK/ DECLARED EMERGENCY. COMPRESSOR STALL ON NR 1 ENGINE AFTER TAKEOFF AT 4000FT. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR IPXA10563251Compressor · stalledFLIGHT CREW REPORTED THAT ON TAKEOFF AT 400 FT THE LT ENGINE COMPRESSOR STALLED 6 OR 7 TIMES WITH SIGNIFICANT YAW. SUPPLEMENTAL ETOPS REPORT ACCOMPLISHED NR1 ENGINE. R & R IAW UPS TASK CARDS 5001(RR0, 5001-1 (RR) AND 5002RR.SDR UALA2010101903863Liner · crackedNR 2 ENGINE INLET ATTRITION LINER HAS A 3 INCH CRACK AT 6:00 POSITION. MEASURED AND FOUND DAMAGE ATTRITION LINER LOWER OB PANEL TOTAL DAMAGE IS 26.81%. STARTED ATTRITION LINER REPAIR PER MT 72-017. DAMAGE REMOVED AND INSTALLED FILLER MATERIAL AT 14:00. NEEDS SDR REXA201000215Fan Blade · lack of lubeON CLIMBOUT OF KATL EN ROUTE TO KCLE, THE LT ENGINE N1 VIBES WENT 2.0 MILS WHICH IS IN THE AMBER RANGE. THE FLIGHT CREW COMPLETED THE QRH AND CONFERRED WITH MAINTENANCE CONTROL BY ACARS. DUE TO A LACK OF MAINTENANCE FACILITIES IN KCLE THE CREW WAS ADVISED TOSDR HALA2010101600471Blade · damagedETOPS SIGNIFICANT SYS - DURING RT ENG INSP FOUND NICK IN L/E OF FAN BLADE 16" FROM ROOT BLADE NR15 MARKED. FOUND NICK TO BE IN AREA C AND BLENDED AREA 16" FROM ROOT TO .30"X1". IAW AMM 72-31-02-308-003-N00. REF LOG 368278 ITEM 62FOR EDDY CURRENT DMI VISUAL INSDR IPXA10663155Compressor · stalledINSPECTION TYPE:ETOP, RT ENGINE HAD 4 COMPRESSOR STALLS AT 200 FT, NO HIGH EGT OR ENGINE EXCEEDENCE. CHECKLIST WAS ACCOMPLISHED, TRIED ONE MORE RECOVERY, HOWEVER ENGINE STALLED AGAIN. ENGINE WAS SHUTDOWN, LANDING WEIGHT WAS 320.00. R & R ENGINE.SDR UALA2010101103786Blade · damagedON ARRIVAL FOUND NR 2 ENGINE FAN BLADE NR24 DAMAGED BY BIRDSTRIKE. REPLACED FAN BLADES NR 5 AND NR 24 IAW MM.SDR A6WA201040752Compressor · damagedAFTER T/O WITH CLIMB POWER SET, LT ENGINE LOUD NOISE & SHOOK, ITT WENT RED FOR APPROX 3 SECONDS, ACCOMPANIED BY BURNED ODOR IN COCKPIT. C/W QRH, PULLED LT THROTTLE BACK AND AT THAT POINT AMBER VIBE ICON ON LT ENG NR 2, RETURNED TO DEPARTURE, DID NOT LAND OVER
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