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 = 'CF343A1' 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 = 'CF343A1' 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 SWIA2014062338267Mount · damagedLEFT ENGINE, FRETTING WEAR AT AFT MOUNT RIB. COMPLIED WITH REO. INSPECTED MAX ALLOWABLE GAP OF PYLON OTBD MOUNT RIB, AND FOUND TO BE WITHIN LIMITS.SDR CA140611002Autopilot Sys · failed(CAN) CREW DISCOVERED AN UNUSUAL PITCH UP MOVEMENT AND CHECKED THE SPEED BUG WHICH HAD MOVED FROM 252 KNOTS TO AROUND 50 KNOTS.SDR CA140522017Throttle Cable · broken(CAN) ACFT EXPERIENCED AN UNRESPONSIVE LT ENGINE THROTTLE. THE EVENT OCCURRED DURING APPROACH. THE CREW FOLLOWED THE QRH AND THE ENGINE WAS SHUTDOWN AND THE FLIGHT LANDED WITHOUT INCIDENT. UPON INVESTIGATION IT WAS DISCOVERED THAT THE LT ENGINE THROTTLE CABSDR CA140506005Engine · vibration(CAN) AIRCRAFT WAS IN CRUISE WHEN THEY HEARD A LOUD BANG AND ACFT STARTED TO SHUTTER. RIGHT ENGINE VIBRATION GUAGE TURNED YELLOW THEN RED. CAPTAIN RETARDED THE THRUST LEVER AND SHUTDOWN THE ENGINE. INVESTIGATION TURNED UP DAMAGE IN THE HOT SECTION OF THE ESDR CA140502005Adapter · failed(CAN) FREQUENCY CONVERTER BLOW OUT ON TEST. THE BREAKER NEVER TRIPPED.SDR CA140521003Pseu · failed(CAN) PILOTS REPORT, AFTER ACFT TAKEOFF AND GEAR LEVER SELECTION TO THE UP POSITION, ON EICAS WERE OBSERVED FOLLOWING WARNING MESSAGE "GEAR DISAGREE". DURING ALL THE FLIGHT GEAR WAS IN NOT SAFE INDICATION, ALL 3 RED LIGHTS, WITH "GEAR DISAGRE" MESSAGE. LANDINSDR CA140417002Windshield · cracked(CAN) AFTER TAKEOFF, RT WINDSHIELD CRACKED. FLIGHT ABORTED. RETURN AND LANDING AT ORIGIN AIRPORT. MAINTENANCE REPLACED THE WINDSHIELD.SDR CA140303005Cable · frayed(CAN) RECEIVED AN O/H THROTTLE CONTROL GEAR BOX, PN 2100140-010, TO REPLACE UNSERVICEABLE UNIT, ON RT ENGINE. DURING INSTALLATION OF THE O/H GEARBOX ASSY, THE AUTO THROTTLE RETARD, ATR, CABLE WAS FOUND FRAYED, WHERE THE INNER FITTING IS SWAGED. THIS GEARBOXSDR CA140226013Priority Valve · failed(CAN) FOLLOWING SDR 20140226012, ON FEB 22, 2014, AFTER 3 SUCCESSFUL FLIGHTS THE ACFT EXPERIENCED A SECOND GEAR DISAGREE MESSAGE WITH CONFIRMATION THAT THE NLG DID NOT EXTEND. NLG ALTERNATE EXTENSION WAS USED AGAIN SUCCESSFULLY AND ACFT LANDED WITHOUT INCIDENTSDR CA140226012Selector Valve · failed(CAN) DURING APPROACH, ACFT EXPERIENCED THE GEAR DISAGREE MESSAGE DURING EXTENSION. IT WAS NOTED THAT THE NLG DID NOT EXTEND. NLG ALTERNATE EXTENSION WAS USED AND THE ACFT LANDED WITHOUT INCIDENT. MECHANICS TROUBLESHOT THE ACFT AND REPLACED THE NLG SELECTORSDR CA140213004Windshield · damaged(CAN) F/O`S WINDSHIELD CRACKED AND HAS DELAMINATION.SDR CA140128010Seal · leaking(CAN) FLIGHT DIVERTED DUE TO LT ENGINE OIL TEMPERATURE INDICATION LOW AND FLUCTUATING. ENGINE HAD THE LT IDG CARBON SEAL REPLACED DUE TO AN OBSERVED LEAK AFTER THE EVENT.SDR CA131230006Bracket · bent(CAN) UPON SELECTING LANDING GEAR UP AFTER DEPARTURE, ONLY THE MAIN GEAR RETRACTED. THE NOSE GEAR STAYED DOWN AND LOCKED. CREW RETURNED FOR AN UNEVENTFUL LANDING. FAULT TRACED TO THE NLG CENTERING SENSOR BRACKET, PN CSK6217, IPC REF 32-20-00-2-29, WHICH IS BESDR CA131209010Cabin Pressure · failed(CAN) DURING CRUIZE AT FL340, FLIGHT CREW HAS REPORTED CAUTION "CABIN ALT" COMING ON ACCOMPANIED WITH GRADUAL DELTA P DECREASE AND CABIN ALT CLIMB. WHILE PILOTS WERE LOOKING FOR ABNORMAL PROCEDURES IN AFM THE CABIN ALT RAPIDLY REACHED 10000 FT AND "CABIN ALT"SDR CA130719003Windshield · cracked(CAN) F/O WINDSHIELD CRACKED IN FLIGHT AT FL270.SDR CA130806002Bulkhead · cracked(CAN) DURING C-CHECK, AFTER ZONAL NDT INSPECTION, FOUND 2 CRACKS ON RT SIDE BULKHEAD FS 559 BETWEEN RBL9 AND RBL18.SDR CA130708007Fire Bottle · discharged(CAN) AFTER TAKEOFF, CREW RECEIVED A CARGO BOTTLE, LOW CAUTION MESSAGE. ACFT RETURNED TO THE FIELD. CREW REPORTS THAT THEY DID NOT DISCHARGE THE BOTTLE AND RECEIVED NO OTHER COCKPIT INDICATIONS. F/A AND PASSENGERS REPORTED THEY DID NOT SMELL SMOKE OR NOTICSDR CA130617009Selector Valve · failed(CAN) DURING APPROACH ON LDG EXTENSION, GEAR DISAGREE. MLG DOWNLOCKED, NLG REMAINED UNLOCKED. GO AROUND MANEUVER PERFORMED BY FLIGHT CREW. ALTERNATE LANDING GEAR EXTENSION PERFORMED. ACFT LANDED AT DESTINATION AIRPORT. MAINTENANCE REPLACED THE NLG DOOR SELSDR CA130610002Landing Gear · failed(CAN) GEAR DISAGREE, W, ON APPROACH. LANDING GEAR EXTENSION SELECTION WITH NLG UNLOCKED INDICATION. ALTERNATE LDG EXTENSION PERFORMED. NO CODES RETRIEVED FROM PSEU. MAINTENANCE PERFORMED VARIOUS LANDING GEAR RETRACTION/EXTENSION FUNCTIONAL TESTS. ALL PASSEDSDR CA130521017Windshield · failed(CAN) CAPTAIN`S WINDSHIELD SHATTERED IN FLIGHT CAUSING DEPRESSURIZATION. IT IS REPORTED THAT FOLLOWING INITIAL CRACKING OF THE WINDSHIELD, AS THE CREW WAS EXECUTING A CHECKLIST, THE OPENING ENLARGED, CAUSING THE ACFT TO DEPRESSURIZE AND CABIN OXYGEN MASKS TO SDR CA130424004Bulkhead · cracked(CAN) DURING C-CHECK, SEVERAL CRACKS WERE FOUND ON REAR PRESSURE BULKHEAD FWD FACE FS621.SDR CA130429002Trim System · malfunctioned(CAN) PILOT EXPERIENCED A TRIM MOVEMENT THAT WAS NOT AS INTENDED. DECLARED AN EMERGENCY AND RETURNED TO AIRPORT OF DEPARTURE. INVESTIGATION ON GOING. SUSPECTING A QUALITY ESCAPE.SDR CA130408003Actuator · failed(CAN) CREW REPORTED ON SHORT FINAL, ACFT PITCHED DOWN AND NEITHER YOKE COULD BE PULLED BACK. AUTOPILOT HAD BEEN DISENGAGED 500 FT EARLIER. AT 200 AGL F/O`S YOKE RELEASED AND BANG WAS FELT THROUGH FLOOR.SDR CA130327006Latch · cracked(CAN) CREW REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. CREW HAD TO HAVE RAMP ASSIST IN CLOSING THE CABIN DOOR. AFTER THEY GOT IT CLOSED THEY COULD NOT GET IT OPENED. PASSENGERS HAD TO BE DEPLANED FROM THE SERVICE DOOR. MAINTENANCE FOUND THE LATCH/SDR CA130320004Flap System · failed(CAN) ON APPROACH, FLAPS FAIL, UPON FLAPS SELECTION TO 8 DEGREES WITH FLAPS NOT MOVING FROM 0 DEGREES. ABORTED APPROACH. FLIGHT DIVERSION DUE TO WEATHER CONDITIONS AT ORIGINAL DESTIINATION. ACFT LANDED SAFELY. MAINTENANCE DEFERRED IAW PART V. DISPATCH FOLSDR 2013FA0000109Uplock · misriggedACFT RETURNED TO BASE AFTER THE CREW RECIEVED A RT MLG DISAGREE ON RETRACTION WHILE DEPARTING. THE CREW FOLLOWED THE EMERGENCY PROCEDURE IN THE QRH AND CONDUCTED AN ALTERNATE EXTENSION. SUBSEQUENTLY, THE GEAR EXTENDED, INDICATED DOWN AND LOCKED, AND A NORMALSDR CA130214008Actuator · failed(CAN) MAIN CABIN DOOR CLOSED ITSELF WITH CREW AND PASSENGERS INSIDE THE ACFT UPON ARRIVAL. THE CREW POWERED DOWN THE ACFT AND WERE ABLE TO KEEP DOOR OPEN LONG ENOUGH TO PULL UP THE JET BRIDGE. ACFT POWER WAS THEN RESTORED, AT WHICH TIME THE DOOR AGAIN ATTEMPTSDR CA130128018Bearing · corroded(CAN) LT ELEVATOR PARTIAL JAM DURING TAXI. PROBLEM HAS BEEN ISOLATED TO THE SUPPORT ASSY ON THE HORIZONTAL STABILIZER REAR SPAR. PIVOT FITTING APPEARS TO HAVE DAMAGED/CORRODED BEARINGS AS NO PHYSICAL BLOCKAGE WAS NOTED.SDR CA130125002Actuator · failed(CAN) DURING THE APPROACH, FLIGHT CREW RECEIVED A FLAP FAIL, CAUTION MESSAGE AFTER FLAP SELECTION OUT OF ZERO. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT FURTHER INCIDENT. FLAP ELECTRONIC CONTROL UNIT (FECU) CODES WERE DOWNLOADED AND ANALYSED SUGGSDR CA130116001Detector · failed(CAN) DURING THE APPROACH, FLAP FAILED AT 30 DEGREES. THE APPROACH WAS CONTINUED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TRAVELLED TO THE AIRCRAFT LOCATION AND FOUND THE 2 SKEW DETECTION UNIT, SDU, FAULT LIGHTS ILLUMINATED. THE SDU WAS RSDR CA130114005Landing Gear · malfunctioned(CAN) FLIGHT CREW RECEIVED A GEAR DISAGREE MESSAGE AS THE NLG DID NOT RETRACT. THE MESSAGE WAS IMMEDIATE AND REMAINED ILLUMINATED. FLIGHT CREW WERE CONSULTING THE QRH AND SHORTLY THEREAFTER, THE NLG RETRACTED ON ITS OWN, THE GEAR HANDLE WAS IN THE UP POSITIOSDR CA130107005Socket · failed(CAN) RT AFTER DEPARTURE THE F/A ADVISED THE CREW THAT SMOKE WAS PRESENT IN THE CABIN ALONG WITH AN ELECTRICAL SMELL. ACFT RETURNED TO DEPARTURE AIRPORT. EMERGENCY WAS DECLARED. F/A TURNED OFF CABIN LIGHTS AND ODOR STARTED TO CLEAR. CREW REPORTED WHEN MAINTSDR CA121126010Actuator · failed(CAN) CAPTAIN STATED THAT AT FL250 THEY HAD A HARD RUDDER KICK AND THE YAW DAMPER NR 2 KICKED OFF-LINE. THE AFT SPEED WAS SLOWED AND TRIMMED WHEN A SHORT TIME LATER THE RUDDER KICKED AGAIN UNCOMMANDED. THE YAW DAMPER SYS AND AUTO PILOT WAS DISENGAGED. A SHOSDR 2012FA0000758Unknown · odorAPU ON MEL, PERFORMED AN AIR START OF BOTH ENGINES. SHORTLY AFTER BRINGING PACKS ONLINE AND CLOSING PASSENGER DOOR COCKPIT AND CABIN FILLED WITH A HAZY SMOKE AND TOXIC ODOR. ODOR WAS NOT TYPICAL OF OIL IN PACKS. PASSENGER DOOR WAS OPENED AND PACKS TAKEN OFFLSDR 2012FA0000760A/C Pack · failedACFT EXPERIENCED A LT ACM FAILURE ON SHORT FINAL. CREW REPORTED A STRONG BURNED OIL ODOR OR VAPOR ENTERING THE COCKPIT THROUGH THE ECS SYSTEM. BOTH PACKS WERE TURNED OFF AND THE ODOR DISSIPATED. MX CONFIRMED THAT THE LT PACK HAD LOST OIL QUANTITY AND FAILSDR CA121113004Control Lever · failed(CAN) FLAP FAIL AT 30 ON APPROACH 714855, FLAP FAIL EVENT. REPLACED OF FLAP CONTROL LEVER. SYSTEM FUNCTION TESTS CARRIED OUT AND NO FAULTS. SYSTEM CHECKS SERVICEABLE.SDR CA121108010Bushing · worn(CAN) CREW DID A REJECTED TAKE OFF AT 135 KNOTS DUE TO A SPOILER CONFIG WARNING MESSAGE. THE LH FLIGHT SPOILER AND LINK ASSY WAS FOUND WITH WORN BUSHINGS. THE LT FLIGHT SPOILER AND LINK ASSY WAS REPLACED.SDR MASA2012081335034Engine · failedLEFT ENGINE WAS SHUT DOWN DUE TO HIGH ITT AND LOW OIL PRESS WARNING. THIS EVENT HAPPENED WHILE CLIMBING THROUGH 6000 FEET. THERE WAS SMOKE IN THE COCKPIT GENERATED BY THE EVENT. THE SMOKE DISSAPATED WHEN THE ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO FIESDR CA120710007Hsi · failed(CAN) ACFT DIVERTED DUE TO LOSS OF VSI ON BOTH SIDES, GS ON BOTH SIDES WENT TO DASHES, HSI LOST ALL DATA ON BOTH SIDES, CIRCLE OF THE COMPASS ROSE IS ALL THAT REMAINED, LOST FMS, FD AND AS RED FLAGS ON BOTH SIDES. THIS HAPPENED AT FL270 WITH AP ON AND CONTINUSDR 2012FA0000386Thrust Reverser · bindingDURING TAXI OUT, SUBSEQUENT TO THRUST REVERSER AND ANTI-ICE OPS CHECKS, THRUST REVERSER ON RT ENGINE FAILED TO DEPLOY WHEN COMMANDED. RETURNED TO HANGAR AND FOUND KNOB LOCK JAMMED. MANUALLY CRANKED T/R TOWARDS OPEN/DEPLOYED DIRECTION AND LOCK FREED UP. OPS CHSDR CA120507016Brace · cracked(CAN) OPERATOR WAS INCORPORATING AN SB AND ON REMOVAL, THE MLG SIDE BRACE SHAFT FITTINGS WERE FOUND HEAVILY CORRODED AND CRACKED.SDR CA120502007Skin · punctured(CAN) DURING A SCHEDULED NR 1 ENGINE CHANGE, THE UPPER CORE COWL WAS FOUND WITH A1" PUNCTURE IN IT. INVESTIGATION REVEALED THAT THE CORE COWL WAS IN CONTACT WITH THE TOP OF THE OIL TANK LEVEL SENSOR ON THE REMOVED ENGINE. A NEW CORE COWL WAS INSTALLED ON THE SDR CA120410003Drag Brace · cracked(CAN) DURING REMOVAL OF NLG ASSY, THE UPPER DRAG BRACE TRUNNION CASTING WAS FOUND CRACKED AROUND .7500 OF THE CIRCUMFERENCE. REF IPC 32-21-05, FIG 1, ITEM 5. CMM 32-70-04, FIG 5 ITEM 35, PN 16414-1 SHOWS UPPER LEG.SDR CA120308001Gcu · failed(CAN) SHORTLY AFTER ROTATION, FLIGHT CREW OBSERVED AN AC UTIL 1 OFF AND A AC UTIL 2 OFF ON THE ENGINE INDICATION AND CREW ALERTING SYSTEM, EICAS, DISPLAY FOLLOWED BY AN EMERGENCY POWER ONLY RED WARNING MESSAGE AND THE ACFT LOST ALL ELECTRICAL POWER. THE AIR DRSDR CA120307007Heat Exchanger · failed(CAN) CABIN DO NOT PRESSURIZE CORRECTLY. CREW ELECTED TO CONTINUE FLIGHT AT FL 110 TO DESTINATION. ACFT LANDED AT DESTINATION AIRPORT. MAINTENANCE FOUND PACK NR 1 DUCT BETWEEN PRIMARY HX AND PRECOOLER DISCONNECTED. DUCT AND PRIMARY HX CONNECTION DAMAGED. RSDR CA120214003Selector Valve · failed(CAN) GEAR DISAGREE ON APPROACH.SDR CA120208006Light · shorted(CAN) SIDEWALL LIGHT 4F SHORTED OUT AND SPARKED CAUSING SLIGHT SMOKE IN CABIN. CONSIDERABLE CONDENSATION NOTICED. RESOLVED ON WO: 323780 TASKCARD: NR-00001, SIDEWALL LIGHT ASSY, PN, BCI -0065-003, AT ROW 4DF REPLACED AND TESTED SERVICEABLE. LIGHTING FIXTURESDR CA120410002Flap System · failed(CAN) ACFT WAS EXECUTING AN INSTRUMENT APPROACH. WHILE ON BASE LEG THE CREW RECEIVED A FLAP FAIL ANNUNCIATOR MESSAGE. THE FLAPS WERE VERIFIED TO BE AT ZERO DEGREES. THE CREW NOTIFIED ATC AND REQUESTED THAT ARFF STANDBY. THE DESCENT WAS DISCONTINUED. ACFT LASDR CA120209007Adg · unwanted deploy(CAN) ADG DEPLOYED ON CLIMB. NO AC OR DC GENERATION LOSS ON EICAS. CREW ELECTED TO RETURN TO FIELD. MAINTENANCE UNABLE TO DUPLICATE OR FIND FAULT, STOWED ADG, AND ACFT RETURNED TO SERVICE.SDR CA120221004Actuator · failed(CAN) FLAPS FAIL C ON APPROACH - FLAPLESS LANDING. MAINTENANCE APPLIED TC AD CF2007-10R1, PART V. ALL FLEXSHAFT WERE INSPECTED, CLEANED AND LUBRICATED. RT OTBD FLAP ACTUATORS WERE REPLACED.
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