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 = 'CF680C2B2' 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 = 'CF680C2B2' 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 USAA2012022400015Engine · malfunctionedPHL FLT 751 EN ROUTE BRU TO PHL. DIRTY SOCKS SMELL NOTED IN COCKPIT AND CABIN 5 MINUTES BEFORE TOUCHDOWN, WHICH LASTED APPROXIMATELY 2 MINUTES, THEN DISSIPATED. MAINTENANCE REPLACED THE RIGHT ENGINE ASSEMBLY. HPC STAGE 5 BORESCOPE - ORGANIC DEPOSIT FOUND, SDR USAA2012012300034Servo Valve · failedPHL FLT 723 EN ROUTE DUB TO PHL. R ENG LOW OIL PRESS ON LANDING ROLL OUT; PRECEDED BY R GEN OFF INTERMITTENT INDICATIONS ON FINAL APPROACH. RIGHT ENGINE SHUTDOWN AT 1937Z. RIGHT OIL PRESSURE LESS THAN 10. REMOVED AND REPLACED ENGINE MEC ASSY. GRD RUN UP SDR USAA2011102600007Pressure Switch · faultyPHL - FLT 702 EN ROUTE PHL TO FRA. ENG FUEL FILTER R ENG DISPLAYED. REMOVED AND REPLACED RT ENG FUEL PRESSURE SWITCH, & RT MAIN FUEL FILTER.SDR TAMF2011FA0000167Engine · leakingLT ENGINE OIL PRESSURE LIGHT ILLUMINATED EICAS MESSAGE LT ENG OIL PRESSURE. OIL PRESSURE WAS ZERO. OIL QTY ZERO. ENGINE SHUTDOWN, FLIGHT DIVERTED. ACFT LANDED SAFELY. AFTER ENGINE INSPECTION, A CONSIDERABLE QUANTITY OF OIL SPREAD IN ENGINE EXHAUST AREA. SDR USAA2011080100031Pressure Switch · malfunctionedVCE - FLT 715 VCE TO PHL. ABOUT 10 MINUTES AFTER TAKEOFF, CREW RECEIVED "R ENG FUEL FILTER" EICAS INDICATION. THE FLIGHT RETURNED TO FIELD VCE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED THE FUEL FILTER. NO CONTAMINATION FOUND. REPLACED THE SDR USAA2011071100039Pressure Switch · faultySJU - FLT 1043 EN ROUTE STT TO CLT. ON T/O FROM STT, L ENG FUEL FILTER LIGHT ON EICAS ILLUMINATED. THE FLIGHT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL FILTER, AND LEFT ENGINE FUEL FILTER BYPASS SWITCH.SDR USAA20110616BB056Pressure Switch · faultyVCE - FLT 715 VCE TO PHL. CREW RECEIVED EICAS MESSAGE RT ENGINE FUEL FILTER DISPLAYED ON LIFT OFF. FUEL FILTER CHECKED, NO CONTAMINATION FOUND. FUEL FILTER REPLACED. FUEL FILTER DIFF PRESSURE SWITCH REPLACED. CHECKED FOR LEAK OK.SDR TAMF2011FA0000161Rotary Actuator · corrodedDURING CLIMBING STAGE L/E SLAT ASSY APPEARS. AIR TURNBACK. GROUND INSP FINDINGS: DURING VISUAL INSP WAS FOUND SLAT NR 12 HANGING DOWN FROM ONE SIDE. THE SLAT REMAINS SUPPORTED FROM 1 TRACK WHICH CAUSED HOLES OF SOME PANELS OF WING AND ANTI-ICE TUBES DEFLECTIOSDR 2011F00072Pin · installedEICAS MESSAGE GEAR DISAGREE DISPLAYED WITH WITH GEAR HANDLE UP, NOSE GEAR GREEN DN LGT FAILED TO EXTEND DOORS AMBER LIGHT WAS EXT & GEAR LIGHT ILLUMINATED. PERFORMED NLG INSPECTION CHECK AND IT WAS FOUND THE LANDING GEAR NOSE PIN INSTALLED. REMOVED IAW AMM 3SDR 2011FA0000158Oil System · low pressureLT ENGINE LOW PRESS, LOW 13 PSI. ENGINE IFSD. FLIGHT DIVERSION. ENGINE WAS R & R. REMOVED ENG WILL BE SENT TO INVESTIGATE THE CAUSE OF OIL ENG SYS FAILURE.SDR 2011FA0000155Oil System · contaminatedFLT 601 RT ENGINE OIL QUANTITY ZERO, ENGINE OIL PRESSURE WAS LOW. RT ENGINE SHUTDOWN WAS DIRECTED BY CHECKLIST. INFLIGHT RT ENGINE SHUTDOWN WAS PERFORMED. OIL PRESS WAS ALWAYS ABOVE 10PSI. FLIGHT DIVERTED. PERFORMED FIM 71-05-00 FIG 119 BLOCK 1 TO 6 AND 25SDR 2009FA0000724Engine · auto shutdownDURING CRUISE LEVEL AT FL 360, 65 NM MILES SOUTH OF INTERSECTION, THE RT ENG OIL FILTER EICAS ANNUNCIATION DISPLAYED. ACCORDING TO CHECK LIST, REDUCED THRUST TO IDLE, THE ANNUNCIATION REMAIN DISPLAYED. FOLLOWING CHECK LIST, THE RT ENGINE WAS SHUTDOWN AFTER COOSDR TAMF20090031SFitting · crackedDURING (SC3) CHECKS INSP WAS FOUND NACELLES/PYLON THRUST REVERSER FITTING AT 5 O´CLOCK WITH CRACK REPAIRED ACCOMPLISHED IAW EWO 767-54-031,SDR CNMA20090014Sensor · false indicationAT 1330Z, FLT LEVEL 34, 000 FT, NR 2 ENG OIL TEMP BEGAN TO RISE. WENT INTO YELLOW BAND. ACCOMPLISHED QRM PROCEDURES AND SHUT ENG DOWN AFTER 15 MINUTES. REMOVED AND REPLACED NR 2 OIL TEMP BULB IAW MM 79-32. ENGINE OPS AND LK CK GOOD IAW JRH. REMOVED AND REPLSDR USAA20090217BB037Sensor · faultyPHL - FLT 886 EN ROUTE CLT TO PHL. THE LT ENGINE ROLLED BACK TO IDLE WHILE IN CRUISE DESCENT. THE AUTO-THROTTLES WERE ENGAGED AT THE TIME AND THE ANTI-ICE WAS OFF. THE THROTTLES REMAINED TOGETHER DURING THE EVENT. THE ENGINE REGAINED POWER ON ITS OWN. THSDR UIEA200900007Engine · seizedENGINE 2 FAILED IN FLIGHT. AUTO SHUTDOWN, UNABLE TO AIR START ENG. FLIGHT LEVEL 380. NORMAL FLUID QUANTITIES AND ENGINE INDICATIONS AT THE TIME JUST BEFORE SHUTDOWN. MASTER CHIP DETECTOR FOUND CLEAN. FOUND ENGINE WOULD NOT TURN. REMOVED AND REPLACE ENGINE.SDR UPS08B53921Hmu · malfunctionedINSPECTION TYPE:N/A ENG NR 1 FAILURE ON FINAL WITH SUCCESSFUL AUTO RELIGHT. NR 1 FAILED AGAIN ON GROUND WITH ENG 1 CONTROL MESSAGE. WIND ON FINAL APPROACH TO 26L WAS OUT OF NORTH UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ENG HMU IAW MM 73-21-14, REMOVED ANDSDR USAABB08133Pressure Switch · failedYQX FLT 716 EN ROUTE PHL TO MXP. DURING CRUISE, THE FLIGHT RECEIVED EICAS MESSAGE "LT ENG FUEL FILTER." THE FLIGHT DIVERTED TO YQX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT ENG FUEL DIFFERENTIAL PRESSURE SWITCH. OPERATIONALLY AND LEASDR USAABB08111Pressure Switch · faultyPHL FLT 710 EN ROUTE PHL TO ZRH. THE FLIGHT RETURNED TO FIELD DUE TO A NR 2 ENGINE FUEL FILTER MESSAGE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENG FUEL PRESSURE SWITCH. OPERATIONAL AND LEAK CHECKS OK. (S)SDR TAMF20080017SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER CHORD STA 779.44 AND 784.44. (2) RIBS WERE FABRICATED AND INSTALLED IAW P0214296 AND P0214326, AND DRAWINGS 114T2217 AND 114T2218 AND SRM 51-40-02 PG 1-7.SDR TAMF20080012SSplice · crackedDURING C2 CHECK INSPECTION WAS FOUND A CRACK ON SPLICE PLATE FRONT SPAR LOWER CHORD STA ISS 256.15 261.26 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767 57-041 AND MFG SERVICE REQUEST 1-789000676. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUSDR P5CA0801545Carbon Seal · leaking"ENG 4 OIL PRESSURE" ENG 4 SHUT DOWN DUE TO ZERO OIL QUANTITY/LOW PRESS AFTER SHUT DOWN OIL PRESS REMAINED 7PSI. SERVED ENG OIL WITH 25 QTS ACCOMPLISHED ENG MOTORING AND FOUND LEAK ON IDG DRAIN PORT. REPLACED NR 4 ENG IDG CARBON SEAL. ACCOMPLISHED ENG RUN ASDR TAMF20070038SSkin · damagedDURING TRANSIT CHECK THE AIRPLANE WAS HIT AT FUSELAGE WITH A STAIRWAY. SECTION 43, STA 347, STRINGER 31 RT. DAMAGED AREA WAS REPAIRED IAW SRM 53-00-01 REPAIR 1 AND EWO 767-53-061. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR. PERMANENT REPAIR WAS PERFORMED SDR TAMF20070033SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=25 ON SKIN STA 1307-1329 STR 32-33 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-052 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20070024SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 873.13 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-028 AND SERVICE REQUEST 1-527347746. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 81SDR TAMF20070025SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-027 AND SERVICE REQUEST 1-526643882. THIS REPAIR IS CONSIDERED A MAJOR REPAIR. FORM 810SDR TAMF20070018SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=20 ON FUSELAGE SKIN AT STA 1506, STR 31-32 -LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-048 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20070019SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=40 ON LAP SKIN STA 1536 STR 36 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-049 AND SRM 53-00-01 REPAIR 12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20070023SCowling · damagedDURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2. DAMAGED AREA WAS REPAIRED IAW CV07-1781-01 AND EWO 767-54-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20070028SSkin · dentedDURING INSPECTION OF (C2) CHECK WERE FOUND SEVERAL DENTS ON FUSELAGE SKIN STA 1417-1436 STRINGER 33 -36-LT. DAMAGED AREAS WERE REPAIRED IAW EWO 767-53-055 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVSDR TAMF20070029SSill · corrodedFWD CARGO COMPARTMENT LOWER MAIN SILL, THE UPPER EXTERIOR EXTRUDED SECTION HAS CORROSION AT STA 610. REMOVED AND REPLACED MAIN SILL IN FWD CARGO COMPARTMENT UPPER EXTERIOR EXTRUDED SECTION STA 610 IAW SRM 51-40-02 PAGE 2-3 AND SRM 51-40-02 PAGE 4-7.SDR TAMF20070031SSkin · wrinkledDURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-029 AND MFG SERVICE REQUEST 1-527377149. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVINGSDR TAMF20070032SSkin · chafedDURING INSPECTION OF (C) CHECK WAS FOUND A WEAR ON RUB STRIPS SKIN STA 1725.50 STRINGER 22 - RT/LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-054 AND MFG SERVICE REQUEST 1-524791119. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THSDR TAMF20070030SFairing · corrodedDURING C CHECK INSPECTION WAS FOUND A CORROSION ON HORIZONTAL STABILIZER TIP LT NOSE IB - LT.DAMAGED AREA WAS REPAIRED IAW EWO 767-57-030 AND MFG SERVICE REQUEST 1-524791300. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIRSDR TAMF20070016SSkin · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND CORROSION OVER REPAIR DOUBLER AT SKIN STA 456, STR 31-32 -RT. THE DOUBLER NEEDS TO BE REPLACED. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-046 AND SRM 53-00-01 REPAIR 14.THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR TAMF20070022SSkin · dentedDURING INSPECTION OF C2 CHECK WAS FOUND A DENT ON LAP SKIN STA 212.5, STR 30-RT. DENT ON LIMITS IAW EWO 767-53-051 AND MFG SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR TAMF20070011SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-084-01-2) WAS FOUND WEAR ON STRUT SKIN STA 148.50. THE MINIMUM THICKNESS IS 0.047 INCH. CF6-80C2 ENGINE NR 2. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-017 AND MFG SERVICE REQUEST 1-512263744. THIS REPAIR CONSTITUTESSDR TAMF20070014SFairing · crackedDURING C-CHECK INSPECTION WAS FOUND NR 2 NACELLE STRUT NR 446CL ACCESS PANEL DELAMINATED AND CRACKED. ACCESS PANEL WAS FABRICATED AND INSTALLED IAW MFG SERVICE REQUEST 1-50853397 AND DRAWING 015T0563-8.SDR TAMF20070006SSpar · crackedDURING C-CHECK INSPECTION (MFG TASK CARD 06-099-01-1) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-499965004 AND EWO 767-57-021. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 SDR TAMF20070010SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N:224-2301-517, S/N: 0115 WITH ELONGATED HOLE AT FRAME STA NAC 294, ENGINE NR 2.DAMAGED AREA WAS REPAIRED IAW EWO 767 54-016 AND AUTHORIZATION CV07-1674-01.SDR TAMF20070013SStructure · corrodedDURING C-CHECK INSPECTION (MFG TASK CARD 53-456-00) WAS FOUND A CORROSION ON FWD CARGO COMPARTMENT CARGO DOOR UPPER SURFACE, INNER CHORD AT MAIN SILL LARGE CARGO DOOR, BETWEEN STA 544-566. DAMAGED AREA WAS BLENDED OUT AND CORROSION REMOVED IAW SRM 51-10-02 PASDR TAMF20070007SWeb · wornDURING (C) CHECK INSPECTION (TASK CARD 57-592-00) WAS FOUND WORN OUT OF LIMITS ON IB AILERON LT - OB CLOSURE RIB WEB. DAMAGE WAS REPAIRED IAW BOEING SERVICE REQUEST 1-500301558 AND EWO 767-57-024. ALSO, FAIL-SAFE FITTING PN 113T6145-11 WAS FABRICATED AND INSTSDR TAMF20070003SSkin · corrodedDURING C-CHECK INSPECTION (TASK CARD 57-500-00) WAS FOUND A CORROSION ON SLAT NR 2 LOWER SKIN STA OSS 953.48 LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025537 AND EWO 767-57-022. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUSDR TAMF20070012SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 57-666-00) WAS FOUND A LIGHTNING STRIKE ON WING UPPER SKIN STA 1018.2 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-490432776 AND EWO 767 57-023. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSDR TAMF20070005SBeam · corrodedDURING C-CHECK INSPECTION (TASK CARD 53-426-00) WAS FOUND CORROSION ON NLG W/W BULKHEAD, STA 287, CENTER BEAM PN 141T2939. CORRODED AREA WAS REMOVED IAW SRM 51-10-02 PAG 12-13 AND IT WAS FOUND OUT OF LIMITS (MAX 0.190 IN, MIN 0.160 IN) IAW SRM 53-10-14 FIGURESDR UIEA200700069Pump · unserviceableHYD QTY LOW NR 2 EICAS MSG QTY 0. FOUND HYD FLUID LEAKING FROM NR 2 EDP (FLUID STILL IN SYSTEM). REMOVED AND REPLACED NR 2 EDP PER MM 29-11-08, OPS, LEAK CHECK OK AND ALL INDICATION ON PRESSURE NORMAL. REMOVED AND REPLACED NR 2 CASE DRAIN FILTER PER MM 29-1SDR DL76G061071Computer · unserviceableA/C RTO AT 125KTS DUE TO A INCORRECT EGT EXCEDANCE OF THE LT ENGINE. THE LT EICAS COMPUTER DISPLAYED A RED EGT BOX AT 831 DEGREES C DURING TO ROLL. THE EGT EXCEEDANCE PARAMETER IS ABOVE 960 FOR THE CF680C2. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICASDR USAABB06081Slide · failedDURING OPERATIONAL CHECK OF THE L1 DOOR ESCAPE SLIDE, THE ESCAPE SLIDE INFLATED PROPERLY BUT THE SLIDE MOUNTED LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE ASSEMBLY.SDR USAABB06080Engine · surgesPHL FLT 1707 EN ROUTE FROM DUB TO PHL, CREW REPORTED RIGHT ENGINE SURGES AND LOW CLIMB POWER. RIGHT ENGINE THRUST LEVER IS 3/4 KNOB WIDTH FORWARD OF LEFT AT FL380. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PHL. MAINTENANCE ACCOMPLISHED FIM PSDR BB06074Slide · failedDURING ACCOMPLISHMENT OF L1 DOOR ESCAPE SLIDE OPERATIONAL CHECK, SLIDE INFLATED NORMALLY BUT THE LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY.
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