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 = 'CF348C5' 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 = 'CF348C5' 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 MASA2013032125455Engine · damagedIN CRUISE CREW FELT STRONG AIRFRAME VIBRATION FOLLOWED BY EICAS INDICATION OF FLAME OUT AND ENGINE DEGRADED MESSAGES. THE SYSTEM THEN PERFORMED AN AUTOMATIC RELIGHT. THIS SEQUENCE OF EVENTS OCCURED TWICE. AFTER SECOND RELIGHT THE CREW RETARDED THROTTLE LEVESDR CA130321002Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE OTBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORDS TO BE REPLACED IAW CMM 30-11-07.SDR CA130320001Baffle · fractured(CAN) DURING A SCHEDULED BOROSCOPE INSPECTION OF THE LT ENGINE COMBUSTION LINER AND STAGE 1 NOZZLE ASSY, A SECTION OF BAFFLE WAS FOUND MISSING. FURTHER INSPECTION REVEALED SIGNIFICANT DAMAGE TO SOME OF THE HP TURBINE FIRST STAGE BLADES. ENGINE CHANGE CURRENTLYSDR CA130308003Pin · broken(CAN) AFTER GAINING ACCESS INSIDE THE COCKPIT, THE F/A COULDN`T REOPENED THE DOOR. AFTER MANY UNSUCCESSFUL ATTEMPTS TO UNLOCK/OPEN THE DOOR, F/A STAYED INSIDE THE COCKPIT FOR THE REMINDER OF THE FLIGHT. CABIN DUTIES WERE PERFORMED BY THE OTHER F/A. UPON ARRISDR CA130307006Pitch Control · malfunctioned(CAN) UNCOMMANDED PITCH UP. AUTOPILOT HAS BEEN DISCONNECTED AUTOMATICALLY WITH NO POSSIBILITY TO RE-ENGAGE.SDR CA140728013Line · cracked(CAN) AFTER OPENING AN RFC 3000069664, AS A RESULT OF A CUSTOMER QUALITY INVESTIGATION REQUEST, QIR SROS-NDAR-13-00052 DATED MARCH 6TH 2013, REGARDING THE OXYGEN BOTTLE FILL LINE LEAKING, CONDUCTED A FRACAS REPORT AND IDENTIFIED 78 CASES IN SERVICE WHICH MAY RSDR CA130225012Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE LT WING L/E. THE SAME WAS FOUND AT THE INBD AND OTBD RT WING L/E LOCATIONS. THE CHAFED SPIRAL CORDS WILL BE REPLACED IAW CMM 3SDR CA130219002Pump · leaking(CAN) DURING DESCENT THROUGH 10,000 FT, THE NR 2 EDP HYDRAULIC PUMP CAUTION BEGAN CYCLING. NR 2 HYDRAULIC SYS PRESSURE WAS RESTORED WITH THE 2B ACMP HOWEVER THE FLUID QTY DROPPED TO 5 PERCENT AT WHICH POINT NR 2 HYDRAULIC SERVICES WERE LOST. THE NR 2 EDP WAS SDR SWIA201332811Torque Shaft · crackedUPON STOWING THRUST REVERSER RT ENGINE FLAMEOUT MESSAGE ILLUMINATED AND ITT SPIKED. AFTER CLEARING AND ITT RETURNED TO NORMAL. RT ENGINE REMAINED FLAMED-OUT. (FLT 4605) REPLACED THE RT ENGINE I/B AND O/B VG TORQUE SHAFTS IAW AMM.SDR CA130214005Feeder Cable · chafed(CAN) DURING MAINTENANCE INSPECTION CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORD HARNESSES WERE REPLACE IAW CMM 30-11-07.SDR CA130220004Link · failed(CAN) UPON STOWING THRUST REVERSER RT ENGINE FLAME OUT MESSAGE ILLUMINATED AND ITT SPIKED, AFTER CLEARING ACTIVE RUNWAY MESSAGE CLEARED AND ITT RETURNED TO NORMAL. RIGHT ENGINE REMAINED FLAMED-OUT. MAINTENANCE R & R THE RT ENGINE INBD AND OTBD VG TORQUE SHAFTSDR CA130214016Oil System · overheated(CAN) HIGH RIGHT OIL TEMP FOLLOWED QRH PERFORMED IN-FLIGHT ENGINE SHUTDOWN.SDR CA130201003Cable · broken(CAN) WHILE CARRYING OUT MAINTENANCE TASK RJ9-52-830-101, DETAILED INSPECTION OF THE PASSENGER DOOR LATCH MECHANISM THE PRESSURE VENT FLAP ICE BREAKER CABLE WAS FOUND TO BE DAMAGED. APPROXIMATELY 90 PERCENT OF CABLE STRANDS FRAYED/BROKEN. CABLE TO BE REPLACEDSDR CA130204009Compressor · damaged(CAN) THE FOLLOWING LANDING EVENT OCCURRED: RECEIVED LT ENGINE BLEED CAUTION MSG FOLLOWED BY LEFT ENGINE DEGRADED CAUTION MSG DURING FINAL, UPON LDG LT ENG FLAMED OUT, FLAMEOUT, CAUTION MSG WAS RECEIVED. THE CAPTAIN REPORTED THAT DURING APPROACH FLIGHT, THEY SDR MASA2013012752392Engine · dirtyFOUL ODOR DURING TAKEOFF AT FULL THRUST. PERFORMED ENGINE WATER WASH. RAN ENGINE FOR PERFORMANCE, ODOR AND OIL CONSUMPTION. NO FAULTS NOTED, ALL PARAMETERS WITHIN LIMITS.SDR CA130124018Window · cracked(CAN) 4000 FT, RT SIDE WINDOW CRACK APPEARS FOLLOWED BY R WINDOW HEAT, C, ON ED1. RT SIDE WINDOW WINDOW: NP139322-12, RT SIDE WINDOW CONTROLLER 1659-1-1.SDR CA130122002Turbine · damaged(CAN) DURING THE CLIMB THROUGH 8600 FT THE CREW HEARD A POPPING SOUND AND FELT CONSIDERABLE ENGINE VIBRATION. THE EICAS SHOWED FLAMEOUT FOR THE RT ENGINE AND THE CREW COMPLETED THE SHUTDOWN CHECKLIST AND RETURNED TO THE DEPARTURE AIRPORT. INITIAL INVESTIGATIOSDR CA130118010Blades · damaged(CAN) RT ENGINE APR ON N1 GAUGE MESSAGE ON TAKEOFF ROLL, REJECTED TAKEOFF AT BETWEEN 80-100 KNOTS, WAS A NOTICABLE SHUTTER IN THE AIRFRAME WHEN MESSAGE OCCURRED, NO OTHER ABNORMALITIES WITH PARAMETERS NOTED BY CREW, DAMAGE FOUND ON COMPRESSOR BLADES, ENGINE RSDR CA130118005Cabin Pressure · failed(CAN) AFTER THE TAKEOFF, CABINE PRESSURE CLIMBING TO 2,700 CABIN RATE FT/MIN AND FLIGHT LEVELED AT 100FL, CABIN ALT WARNING APPEARS ASSOCIATED WITH PRIOR EICAS MESSAGE ODOR OF SMOKE IN THE COCKPIT.SDR CA121211016Windshield · cracked(CAN) LEFT CRACKED WINDSHIELD.SDR CA121130001Fan · failed(CAN) DURING TROUBLESHOOTING OF A DEFERRED DEFECT RECIRCULATING FAN FAULT MESSAGE. DEBRIS WAS DISCOVERED BLOCKING A SCREEN IN A UNDERFLOOR SUPPLY DUCT AT FS 677-682, ABOUT MID CABIN AND RESTRICTING AIRFLOW. THE FOD WAS REMOVED AND THE SYS WAS FUNCTION CHECKESDR CA121130002Turbine Blades · damaged(CAN) CLIMBING THROUGH 8000 FT, FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY A YAW TO THE RT. RT ENGINE PARAMETERS INDICATED THE ENGINE WAS SPOOLING DOWN. FLIGHT CREW SECURED THE ENGINE, DECLARED AN EMERGENCY, TURNED BACK AND LANDED WITHOUT FURTHER INCIDENT. SDR CA121109008Line · leaking(CAN) WHILE APPLYING TO POWER AT THE START OF THE TO ROLL THE 1 EDP CAUTION MESSAGE CAME ON AND THE NR 1 HYDRAULIC QTY WENT TO ZERO. MAINTENANCE INVESTIGATION FOUND A CHAFED HYDRAULIC LINE IN THE AFT EQUIPMENT BAY THAT WAS LEAKING. THE LINE HAD CHAFED AGAINST SDR CA121102004Feeder Cable · chafed(CAN) DURING MAINTENANCE INSPECTION CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE O/B TELESCOPIC DUCT OF THE L/H WING LEADING EDGE. THE SAME WAS FOUND AT THE LH IB LOCATION AND THE RT IB LOCATION. ALL HARNESSES WERE REPLACED IAW CMM 30-1SDR CA121024002Skin · dented(CAN) ON APPROACH, THE ACFT SUSTAINED SEVERAL BIRD STRIKES. AFTER LANDING THE ACFT WAS INSPECTED AND A LARGE DENT WAS FOUND JUST BELOW THE F/O SIDE WINDOW. THE DAMAGE AREA WAS MAPPED AND ALLEVIATION WAS RECEIVED FROM THE OEM. THE ACFT WAS RETURNED TO SERVISDR SWIA201231984Engine · flamed outRIGHT ENGINE FLAMED OUT IN FLIGHT. (FLT 4469) REPLACED RIGHT ENGINE ASSEMBLY IN REFERENCE TO AMM. PN OFF: CF34-8C5 SN OFF 194594.SDR ASOA2012101802376Connector · damagedEXPERIENCED FUMES IN THE COCKPIT. DECLARED AN EMERGENCY, RAN QRH, RETURNED TO DEPARTURE. FOUND ELECTRICAL DAMAGE TO PL116P1 AND PL116J1, SEE WO 267716, FOR DETAILS OF REPAIR, PERFORMED OPS CK OF DC PWR IAW AMM 24-61-00-710-806, NO FAULTS FOUND AT THIS TIME.SDR CA121017008Bearing · failed(CAN) AILERONS DIFFICULT TO MOVE IN FLIGHT. FOUND BEARING FAILED.SDR CA121003013Window · cracked(CAN) IN THE CLIMB, AFTER DEPARTURE, THE F/O SIDE WINDOW CRACKED. THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT. CONTRACTED MAINTENANCE, DETERMINED THAT THE CENTER PLY WAS CRACKED. THE ACFT WAS FERRIED TO A MAINTENANCE BASE IAW SL 56-002. THE F/O SIDESDR CA121012013Generator · failed(CAN) ACFT TOOKOFF WITH APU OFF. APPROXIMATELY 40NM OUT, THE NR 2 GENERATOR WENT OF LINE AND SHOWED NR 2 GEN CAUTION LIGHT. DURING THE HANDLING OF THE QRH PROCEDURE, NR 1 GENERATOR WENT OFF LINE. DUE TO TOTAL AC-POWER LOSS THE ADG DEPLOYED AUTOMATICALLY. NSDR CA121002003Brake · failed(CAN) AFTER TAKEOFF AND DURING THE LANDING GEAR RETRACTION THE AURAL WARNING BRAKE OVERHEAT RINGS IN THE COCKPIT WITH THE EICAS MESSAGE BRAKE OVERHEAT. THE INDICATION OF THE BTMS NR 2 WAS OF LEVEL 20, MAXIMUM LEVEL. ONCE ON GROUND, THE PILOT INSPECTED THE AFFSDR CA120918017Line · split(CAN) AFTER ENGINE START THE NR 2 HYD QTY WENT TO 0 AND RAMP REPORTED SEEING MIST FROM THE NR 2 ENGINE. PN CN627-2005-001, FOUND SPLIT. REPLACED. ALSO FOUND QUICK DISCONNECT UNION SPLIT, PN AE99118H.SDR CA120918019Coupling · split(CAN) AFTER ENGINE START THE NR 2 HYD QTY WENT TO 0 AND RAMP REPORTED SEEING MIST FROM THE NR 2 ENGINE. FOUND QUICK DISCONNECT UNION SPLIT, PN AE99118H, REPLACED. ALSO FOUND EDP HYD SUCTION LINE SPLIT SDR 20120918017.SDR ASOA2012091402222Connector · disconnectedLT SIDE EXIT LIGHT OUTSIDE INOPERATIVE. RECONNECTED LIGHT BEHIND PASSENGER SIDE WALL, OPS CHECKED GOOD IAW AMM 33-51-00-710-801.SDR ASOA2012091402221Light · inoperativeRT OVERWING EMERGENCY EXIT LIGHT NOT WORKING. R & R EMERGENCY LIGHT ASSY IAW ESPM 20-16-05. OPS CHECKED GOOD, NO DEFECTS. OK FOR SERVICE.SDR CA120906006Duct · cracked(CAN) DURING ENGINE OIL SERVICING A BLEED LEAK WAS DISCOVERED. INSPECTION REVEALED A CRACKED BLEED-AIR CROSSOVER DUCT. RESOLVED ON W/O: 351549, TASKCARD: NR-00001, NEW DUCT INSTALLED AND LEAK TESTED IAW AMM TASK NO 36-19-09-400-801, PN GG670-80301-1, SN OFF:SDR ASOA2012082802122Wire · brokenRIGHT WING AFT EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE IAW ESPM 20-33-00.SDR ASOA2012082702110Charger · inoperativeRT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSY IAW AMM 33-51-17. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR ASOA2012082702108Circuit Breaker · trippedCIRCUIT BREAKER P2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE, ALL CABIN EMERGENCY LIGHTS WENT DARK AFTER 30 MINUTES LATER. RESET CIRCUIT BREAKER P2 U3 IAW FIM. NO FURTHER ACTION IS REQUIRED.SDR ASOA2012082702106Circuit Breaker · trippedBREAKER BB2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE RESET CIRCUIT BREAKER. PERFORMED OPERATION TEST OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00. OPS CHECKED GOOD.SDR CA120917024Overheat Loop · failed(CAN) DURING A SCHEDULED FLIGHT AND ON CLIMBOUT, PASSING THROUGH 30,000 FT, THE FLIGHT CREW REPORTED A LT BLEED DUCT WARNING MESSAGE AND THEN FOLLOWED BY THE LOSS OF CABIN PRESSURE CONTROL. THE FLIGHT CREW DIVERTED AND LANDED UNEVENTFULLY WITHOUT DECLARING ASDR CA120917023Duct · failed(CAN) DURING A SCHEDULED FLIGHT AT CRUISE ALTITUDE, THE FLIGHT CREW REPORTED A LT BLEED DUCT WARNING MESSAGE ANNUNCIATED AND THEN FOLLOWED BY A LOSS OF CABIN PRESSURE CONTROL. THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY AND LANDED UNEVENTFULLY.SDR ASOA2012081702075Light · inoperativeSTATUS MESSAGE: EMERGENCY LIGHTS ON, BREAKER U3 TRIPPED. R & R K198 RELAY IAW ESPM 20-39-00 AND R & R PS37, PS38 AND PS43 BATTERY CHARGERS AND PS37 BATTERY IAW AMM 33-51-17-000/400-801. PERFORMED OPERATIONAL TEST OF THE EPSU IAW AMM 33-51-17-710-801 NO DEFECSDR CA120809003Bpsu · failed(CAN) ON APPROACH, THE FLAPS STOPPED MOVING AT 30 DEGREES AND THE FLAP FAIL CAUTION MESSAGE WAS POSTED. AN UNEVENTFUL FLAP 30 LANDING WAS CARRIED OUT. THE LT BPSU WAS REPLACED AND THE SYS TESTED SERVICEABLE. PN 5913000, S/N A0508, IPC 27-52-03, FIG 1-5.SDR ASOA2012080302030Glowstrip · brokenPHOTO LUMINESCENT AROUND SERVICE DOOR IS BROKEN OFF. R & R TRIM PANEL ON LT SIDE OF SERVICE DOOR IAW AMM 25-26-07. NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.SDR CA120801008Tube · cracked(CAN) DURING TROUBLESHOOTING OF AN AIR CONDITIONING PROBLEM, MAINTENANCE FOUND THE RT RAM AIR WATER SPRAYER TUBE PART NR MM670-97132-001, IPC 21-52-02-01-030, LOOSE. FURTHER TROUBLESHOOTING REVEALED THAT 2 BRACKETS AND 1 CLAMP SECURING THE TUBE IN PLACE WERE BSDR CA120801006Fuel/Oil Cooler · failed(CAN) IN THE CLIMB THE RT OIL TEMP WENT TO 171C IN THE RED. THE CREW REDUCED POWER TO LOWER THE OIL TEMP AND THE ACFT RETURNED TO THE DEPARTURE AIRPORT. MAINTENANCE T/S DETERMINED THAT THE RT FUEL OIL COOLER WAS AT FAULT AND REPLACED THE UNIT. PN 4119T36P03SDR CA120830001Blades · broken(CAN) DURING CLIMB OUT THROUGH APPROXIMATELY 30000` A LOUD BANG WAS HEARD WHICH WAS FOLLOWED BY A YAW AND RT ENGINE INDICATIONS SPOOLED DOWN. ADDITIONALLY, AN AMBER RT ENGINE FLAME OUT MESSAGE WAS RECEIVED. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED ASDR CA120723014Holder · shorted(CAN) DURING CRUISE FLIGHT AT FL350 THE F/O CHART HOLDER BEGAN TO SMOKE AND SPARK. CB 2G6 TRIPPED AND THE SMOKE DISSIPATED ALMOST IMMEDIATELY. THE FLIGHT CONTINUED TO DESTINATION. MAINTENANCE INVESTIGATION FOUND A SMALL SCREW BEHIND THE LIGHT ASSY ON THE CHASDR CA120723012Ballast · failed(CAN) DURING INITIAL CLIMBOUT FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR AND ELECTED TO RETURN AND LAND. THE ACFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE COCKPIT ENTRANCE LIGHT BALLAST, PS91, AT FAULT. THE BALLAST WAS REPLACED, TESTED AND
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