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 engine_model_key = 'GE90110B1' 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 engine_model_key = 'GE90110B1' 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 QEMY20261022001Seal · crackedSEAL-INTERSTAGE HPT ROTOR HAS CRACKS IN 4 LOCATIONS ON THE BAYONET TABS. THE CONDITION IS NOT SERVICEABLE OR REPAIRABLE. TO BE REPORTED IAW AMC-20-8A (J) ANY DEFECT IN A LIFE-CONTROLLED CRITICAL PART THAT CAUSES ITS RETIREMENT BEFORE THE COMPLETION OF ITS FULLSDR QEMY2026102100882Seal · crackedTHE SEAL-INTERSTAGE HPT ROTOR HAS CRACKS IN 4 LOCATIONS ON THE BAYONET TABS. THE CONDITION IS NOT SERVICEABLE OR REPAIRABLE. TO BE REPORTED I AW AMC-20 8A (J) ANY DEFECT IN A LIFE-CONTROLLED CRITICAL PART
THAT CAUSES ITS RETIREMENT BEFORE THE COMPLETION OF ITSDR UIEA2026101600990Engine · bird ingestionDURING TAXI, ATC REPORTED TO US THAT OUR RIGHT ENGINE INGESTED A FOREIGN OBJECT. PERFORMED BIRD STRIKE INSPECTION AND ENGINE FOREIGN OBJECT INSPECTION. NO DAMAGE NOTED ON RIGHT ENGINE AND A/C EXTERIOR PER AMM 05-51-03 AND AMM 71-00-00. A/C OKAY FOR SERVICE.SDR 2025FA0000732Case · damagedDURING ROOT CAUSE ANALYSIS WHILE PROCESSING OF A CUSTOMER COMPLAINT MTU MAINTENANCE HANNOVER GMBH CHECKED PREVIOUSLY REPAIRED GE90 FAN STATOR MODULES. WITHIN THE FRAMEWORK OF INTERNAL INVESTIGATION MTU-H RAISED AN INQUIRY AT THE OEM. DURING THE OEM EVALUATIONSDR UIEA2025082101132Shutoff Valve · faultedBLEED OFF ENG R EICAS WITH APU ALREADY ON DEFERRAL. REPLACED RH ENG HPSOV PER AMM 36-11-07 & IPC 36-11-02-0113. OPS CHECK NORMAL. PERFORMED ENG RUNS & ACCOMPLISHED ENG AIR SUPPLY OPS TEST PER AMM 36-10-00. OPS CHK GOOD. NO FAULTS NOTED. ALSO, R & R PRSOV CONSDR FDEA202507171232Oil System · leakingOIL QTY ON RIGHT ENGINE WENT TO 4 QTS ABOUT 3.5 HOURS INTO FLIGHT. EVENTUALLY DECREASED TO ZERO OIL QTY ABOUT 1.5 HOURS LATER. OIL PRESSURE DECREASED TO 35 IN DESCENT, NEVER ANY LOWER. NEVER GOT ANY EICAS MESSAGES OR SECONDARY INDICATIONS. REMOVED AND RESDR KCSA2025032410Circuit Card · unserviceable100240750 - DETECT FIRE ENGINE LEFT (BOTH FIRE LOOP #1 AND #2). PERFORMED GENERAL VISUAL INSPECTION OF LEFT-HAND ENGINE, FIRE LOOP 1 AND LOOP 2 IAW B777-200 WDM 26-11-11. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED LEFT-HAND ENGINE FIRE DETECTION CARDSDR FDEA202501150071Controller · failedANTI ICE ENG L EICAS DISPLAYED IN FLIGHT. EMERGENCY DECLARED, T/S ACTIVE MX MSG 30-10291, FOUND SOLENOID ON LH ENG ANTI ICE CONTROLLER BAD, REMOVED AND REPLACED ANTI-ICE VALVE CONTROLLER IN REF. ABOVE, ALL CHECKS GOOD, NO ACTIVE MSG OR EICAS, ALSO REF. TSDR QEMY20241004001Hp Turbine · damagedDURING THE INSPECTION PROCESS AT GE WALES, A DEFECT ON THE DISK HPT STG 2 HAS BEEN NOTED. SURFACE DT HAS INDENTATIONS (360°) CAUSED BY THE MATING OF THE STAGE 1 DISK. THIS IS A KNOWN FIELD CONDITION. DR #01996080 REJECTED BY THE OEM. 1ST TIME EXPOSURE OF THIS SDR FDEA202410011412Engine · damagedSTARTING CLIMB FROM FL380 TO FL400. WHEN THRUST STARTED TO INCREASE, FELT A MAJOR JOLT FOLLOWED BY MAJOR VIBRATIONS, SMOKE & FUMES IN COCKPIT. LT GEN DRIVE & L ENG OIL PRESSURE LIGHTS ILLUMINATED. DONNED MASKS, DECLARED EMERGENCY & RAN CHECKLISTS. SHUTDOWSDR UIEA2024082700847Oil Filter · warning messageENG OIL FILTER L STATUS.(<P>PERFORMED FIM TASK 79-21 TASK 819. PERFORMED PROCEDURE E (1A), (1B), (1C) & (1D).</P> / <P>PERFORMED ENGINE FLUSH PER AMM 12-22-01. REPLACED LH ENG OIL FILTER PER AMM 79-21-07 & IPC 79-21-03-03. PERFORMED ENGINE RUN PER AMM TASK 71-SDR P5CA2024060400011Engine · failed(IFSD) ON TAKEOFF, HEARD A LOUD BANG ON THE RIGHT SIDE. RH ENG N1 ROLLED BACK. CONDUCTED RIGHT ENGINE VISUAL INSPECTION AND SEVERE DAMAGE FOUND. SHUTDOWN RIGHT ENGINE AT 0120Z(<P>MX IN WORK WHILE IN AOGM FOR #2 ENG FAILURE. REMOVED AND REPLACED RH ENG IAW EA SDR KCSA2024042715Fire Loop · false indicationOVERHEAT CIRCUIT 2R. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT MESSAGE. CLEARS, NO DEFECTS NOTED AT THIS TIME. FIRE LOOP 2 ENGINE RIGHT. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT. MESDR KCSA2024042714Fire Warning · illuminatedSTATUS MESSAGES: OVERHEAT CIRCUIT R2. TRANSFERRED TO DMI #100122850 IAW B777 MEL REFERENCE 26-11-2. CATEGORY C. DUE 5-7-24. PLACARDS INSTALLED. STATUS MESSAGE: FIRE LOOP 2 ENGINE RIGHT. TRANSFERRED TO DMI #100122851 IAW B777 MEL REFERENCE 26-11-1-1. CATEGORY CSDR KCSA2024042513Detection Sys · false activationOVERHEAT CIRCUIT R2 STATUS MESSAGE. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST IAW B777 AMM 26-11-00. ALL CHECKS GOOD. FIRE LOOP 2 ENGINE RIGHT. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPESDR QEMY20240524001Seal · nickedON INCOMING INSPECTION, A NICK/SCRATCH HAS BEEN FOUND ON 1 OFF AIR HOLE AFT CHAMFER, MEASURING: CIRCUMFERENTIAL 0.018 RADIAL 0.005 AXIAL (DEPTH) 0.0009. IT WAS NOTED THAT A SHOT PEEN LAYER WAS PRESENT, INDICATING THE CONDITION HAD POTENTIALLY BEEN PREVIOUSLY RSDR FDEA202402050138Gearbox · damagedPERFORMED PRECAUTIONARY ENGINE SHUTDOWN WON RT ENGINE IN CRUISE FL280. IN TITAN INDICATION WAS SECONDARY ENG DISPLAY APPEARING ON MFD & OIL QUANTITY 3. OIL TEMP & PRESSURE INDICATED NORMAL. AFTER APPROX 5 MINS, OIL PRESSURE SLOWLY BEGAN DECREASING OVER 30-40 SDR FDEA202301200148Actuator · failedL/H ENGINE I/B FAN COWL OPEN ACTUATOR UPPER ROD END BROKEN. REMOVED L/H ENGINE INBOARD FAN COWL ACTUATOR REF AMM 71-12-01-4 R/I. INSTALLED NEW FAN COWL OPENING ACTUATOR ON #1 ENGINE, RH (INBOARD) SIDE REFERENCE BOEING 777 AMM 71-12-01-4. OPERATIONAL CHSDR P5CA2022111700204Exciter · faultedSINGLE IGNITOR FAIL, NO LIGHT. R/ #2 ENGINE(<P>CONTINUE OPS PER MEL 74-00-01A TRANSFER TO MDDR 175362. CAT A DUE 18NOV22.</P> / <P>LOG PAGE 1584511 M6: R/R RH ENGINE #2 EXCITER IAW AMM 74-11-01. PERFORMED AUDIBLE OPS CHECK IAW AMM 74-00-00. OPS CHECK NORMAL ONSDR NM1Y2021080300001Shaft · abnormalDURING THE HPC CONE SHAFT FPI INSPECTION DURING AN HPC MODULE SHOP VISIT, SAFRAN AIRCRAFT ENGINES DISCOVERED AN UNUSUAL 8 MM LONG CRACK IN THE SLOT AREA. THE TC HOLDER HAS BEEN INFORMED AND INVESTIGATIONS ARE ON-GOING.SDR FDEA202012303220Heat Shield · crackedON CHECK FOUND NR 1 ENGINE AFT FAIRING HEATSHIELD WITH 2 SEPARATE CRACKS. ATTACHED PICTURES WITH DIMENSIONS. COMPLIED WITH E.A. #: G-5450-T0358849 PT 2. NR 1 ENGINE AFT FAIRING HEATSHIED CRACKED INTERIM REPAIR.SDR Q2SA20201129442Smoke Warning · false activationAIRCRAFT GROUNDED. DURING APPROACH, LAV SMOKE ALARM SOUNDED. NEGATIVE FIRE FOUND, RESET ALARM. ICN MX RESET THE SELF TEST SWITCH AND THEN OPERATIONS CHECKED NORMAL, AS PER AMM 26-13-00/501.SDR Q2SA20200914435Outflow Valve · inoperativeAIRCRAFT GROUNDED, UNABLE TO CONTROL CABIN ALTITUDE PRESSURIZATION. CABIN PRESSURE OUTFLOW VALVE ASSEMBLY REPLACED, IAW AMM 21-31-03-000-812-002/21-31-03-400-811-002. TEST PASSED AND STATUS CLEARED.SDR Q2SA202001132424Light · inoperativeAIRCRAFT GROUNDED. EXTERNAL EMER LIGHTS NOT WORKING AT DOORS 1R AND 1L. EXTERNAL EMERGENCY LIGHT BULBS REPLACED AND TEST OK IAW AMM 33-51-04-960-801.SDR CA190730008Axle · sheared(CAN) DURING REPLACEMENT OF #6 M/W FOUND MLG AXLE SLEEVE RETAINER PIN SHEARED AND SLEEVE MIGRATION OF APPROX 0.400` AFT AND 0.300` INBD. RESOLUTION L/H MAIN LANDING GEAR CENTER AXLE REPLACED AS PER AMM 32-11-26. (TC# 20190730008)SDR DALA2020012973598Tube · damagedDUE TO OIL QUANTITY FELL TO L01 ON LEFT ENGINE. PRESSURE AND TEMP NORMAL. PRECAUTIONARY DIVERSION. FOUND THE NR 4 AND 5 BEARING SUPPLY OIL TUBE DAMAGE. REMOVED AND REPLACED THE OIL TUBE IAW AMM 70-00-01-400-804-H01. LEAK CHECKED GOOD.SDR Q2SA20180528392Hmu · unknownRT ENGINE INLFIGHT SHUTDOWN, STARTED NORMALLY. IAW FIM 73-22 THE HMU WAS REPLACED. THE AIRCRAFT GROUNDED. FDE RECEIVED MAINT MSG 73-34802. FOLLOWED FIM 73-22 TASK 849 ITEM C (1) TO (7) ACCOMPLISHED AND FOUND GOOD. NO FAULT NOTED IAW FIM 73-22 TASK 849. RSDR CALA2018040901137Warning Message · false activationENGINE OIL FILTER RT STATUS MESSAGE DURING DESCENT. FLT CREW FOLLOWED CHECKLIST AND SHUTDOWN THE ENGINE. INSPECTED OF DEBRIS MONITORING SYSTEM SENSOR AND REPLACED THE RT ENGINE OIL FILTER, NO DEBRIS FOUND AND LEAK CHECKED OK. ACCOMPLISHED AN IN-FLIGHT WINDMILSDR DALA2018040902303Packing · leakingDIVERTED, DUE TO THE RIGHT ENGINE OIL QUANTITY INDICATED 7 QUARTS AND WAS DECREASING. MAINTENANCE FOUND THE RIGHT ENGINE STARTER LEAKING AT GEARBOX SPLIT LINE. REPLACED THE STARTER PACKINGS AND COMPLIED WITH HIGH POWER RUN, NO LEAKS NOTED. AIRCRAFT RETURNEDSDR DALA2017091800002Oil System · leakingRETURNED TO DEPARTURE DUE TO THE LEFT ENGINE OIL QUANTITY WAS DECREASING. REPLACED THE ENGINE.SDR DALA2017091806954Seal · leakingRETURNED TO DEPARTURE DUE TO THE LEFT ENGINE OIL QUANTITY DECREASING. REPLACED THE IDG GEARBOX SEAL.SDR FDEA201708222331Line · chafedAT 6 30 INTO FLIGHT, RIGHT ENGINE OIL QTY DROPPED TO 4 AND STATUS ALERT. OIL CONTINUED TO DROP TO ZERO AND THEN OIL PRESSURE STARTED TO FLUCTUATE AND DROP. ALERTED GOC AND COORDINATED DIVERT TO PACD. SHUT DOWN RIGHT ENGINE WHEN "ENG OIL PRESS R" CAME ON ATSDR DALA2017041202957Blade · tornDURING BORESCOPE INSPECTION, FOUND A TEAR IN THE 5TH STAGE HPC BLADE.SDR DALA2017041703128Blade · damagedNR 2 ENGINE HAS DAMAGE TO STAGES 3, & 5 HPC BLADES THAT EXCEED AMM 72-00-00-290-803-H01 LIMITS. COMPLIED WITH ERA 557259-14 REV ORIG, SECTION I .SDR FDEA201609043116Sensor · false indicationENGINE OIL FILTER SENSOR RT ON STATUS PAGE FOLLOWED BY ENGINE OIL FILTER BYPASS RT, ALERT ON EICAS. PERFORMED CHIP CHECK ANALYSIS AND NO M50 MATERIAL FOUND IN THE DEBRIS. REPLACED OIL FILTERSDR Q2SA20150921227Line · leakingHYD PRESSURE SYS C, HYD QTY LOW SYS C: FOUND NR 12 BRAKE LINE LEAKING. INSTALLED TEMPORARY FLEX LINE ON NR 12 BRAKE IAW AMM 20-10-10. OPS AND LEAK CHECK GOOD IAW AMM 29-11-00.SDR CA150807002Radar · failed(CAN) 12NM OUT ON LOCALIZER 08L, ACFT STARTED WEAVING. FOUND LT RADAR GAIN AT MAX. RIGHT GAIN AT CAL. RETURNED LEFT TO CAL. RT RADAR SYS TESTED IAW AMM 34-43-00-730-803-002.SDR CA150623009Idg · failed(CAN) RIGHT GEN DRIVE FAIL, APU REQUIRED FOR REMAINDER OF FLIGHT. RESOLUTION RT ENG DRIVEN GEN REPLACED IAW 24-11-01-401. LEAK CHECK CARRIED OUT NO LEAKS, POWER PLANT TEST CARRIED OUT IAW TASK 71-00-00-800-833-H00. OPERATIONAL TEST FOR RT IDG CARRIED OUT IASDR CA150515005Warning System · activated(CAN) FLIGHT REPORTED FLAP RUDDER FAIL MSG ON ECAM, NO PAN PAN. DID ORDER ERS TO MONITOR & MEET ACFT ON LANDING. NO FURTHER INFO WAS PROVIDED. TROUBLESHOOTING CARRIED OUT IAW FIM 27-82-00-810-811. CHECKED SERVICEABLE.SDR FDEA201504171254Eec · inoperativeDURING CRUISE THE LT ENGINE FLAMED OUT, WOULD NOT RESTART. LEFT FUEL CONTROL VALVE ILUMINATED SHUTTING DOWN LEFT ENGINE. INFLIGHT START CHECKLIST ACCOMPLISHED LEFT ENGINE WOULD NOT RESTART. INTERROGATED MAT AND FOUND ENG EEC C1 L FAULT LATCHED (FAULT CODE )SDR CA150312005Fan · failed(CAN) AS REPORTED BY CABIN CREW, FREQUENT AND NUMEROUS ODORS DETECTED IN GALLEY, PASSENGER CABIN, AND LAVATORY AREAS DURING FLIGHT. POWER TO IFE SYSTEM, READING LIGHT CONTROL, PASSENGER CALL SYS, ETC WERE TURNED OFF FOR REMAINDER OF FLIGHT. RESOLUTION IFE COSDR 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 GUARSDR 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 DIMINISHEDSDR CA140523002Oven · overheated(CAN) WHILE EN-ROUTE, FIRE WITH BLACK SMOKE REPORTED BY F/A IN REAR GALLEY OVEN. 2 FIRE EXTINGUISHERS USED TO PUT OUT THE FIRE. F/A OBSERVED SPARKS ABOVE OVEN. ALL ELECTRICAL POWER TURNED OFF TO THE AFT GALLEY OVEN AND NO FURTHER SERVICE WAS CONDUCTED. NO SDR CA140404003Pump · failed(CAN) FLIGHT DEPARTED AND ACFT BEHIND WITNESSED VAPOUR COMING FROM RT ENGINE. ONCE IN THE AIR HYDRAULIC PRESSURE IN RT PRIMARY PUMP WENT TO ZERO. MAINTENANCE ADVISED AFTER LANDING, IT WAS A BLOWN SEAL. CREW DECLARED AN EMERGENCY WITH ATC AND AFTER QUICK CONSSDR FDEA201306171317Scavenge Pump · failedRT ENGINE APPEARED TO BE LOOSING OIL BEFORE START, LEFT 24 QTS, RIGHT 23 QTS. AFTER 3 HOURS OF FLIGHT RT ENG SLOWLY DECREASED TO 14 QTS WHILE LT ENG REMAINED AT 19 QTS. JUST PRIOR TO ENTERING ETOPS, RT ENG REDUCED TO 13 QTS LT AT 19 QTS. DIVERTED. OIL WENT SDR Q2SA20130528203Skin · damagedLEFT WING L/E OTBD OF ENGINE PANEL, OPEN. DURING INVESTIGATION FOUND APPROX 11 X 7 INCH SECTION OF SKIN DETACHED FROM RIVET ROW ON NR 5 SLAT STA 711.5 ACCOMPLISHED EAM 7727003R0 PART 1. R & R L/E SLAT IAW AMM 27-81-15/401.SDR CA130222006Compressor · damaged(CAN) STARTING RT ENGINE, FUEL FLOW .3 TO .4 ON START. ENGINE ACCELERATED TOWARDS IDLE, STARTER CUTOUT, FUEL FLOW DID NOT INCREASE AND ENGINE HUNG AND WOUND DOWN. ON RESTART ALL NORMAL. ACFT FLEW 1 LEG, AND THEN MAINTENANCE AT NEXT BS T/S. ENGINE REPLACED SDR 2013FA0000078Bushing · galledAFTER VISUAL INSPECTION, RT MLG FOUND HAS A GALLED BUSHING ON RETRACTION TRUNNION SLEEVE. FOUND THE AREA OF THE PITTING ON THE SLEEVE. AREA IS WIDTH APPROX 2 CM AROUND THE SLEEVE. PERFORMED IAW RECOMMEND TO REMOVE THE BRONZE TRANSFER WITH SCOTCHBRITE , THE SDR Q2SA20121023198Sign · inoperativeLEFT DOOR AFT INTERIOR EMERGENCY EXIT SIGN INOP. TRANSFER TO DI 2789 PER MEL 33-51-01. PLACARD INSTALLED.
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