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 = 'CF348C1' 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 = 'CF348C1' 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 ASOA2012070901873Floor Support · corrodedAFT CARGO RT FLOOR SUPPORT IS CORRODED BETWEEN FS 1015 - 1031. REMOVED CORROSION DAMAGE IAW SRM DAMAGE IAW SRM 51-21-06-001-001-A01 AND FOUND AREA TO OUT OF LIMITS IAW SRM 51-61-43-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSDR ASOA2012062801832Floor Panel · crackedRIGHT ELECTRICAL BAY FLOOR AT FS 193 IS CRACKED. CUT OUT CRACK IAW REO 670-53-11-509. COMPLIED WITH STEP 11 OF EC/TC REO 670-53-11-509 IAW NDTM PART 1, 51-20-006. NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALLED DOUBLER IAW REO 670-53-11-509.SDR ASOA2012070301850Angle · corrodedREMOVED AND REPLACED FOUR CORRODED ANGLES FROM UPPER ASD JUST BELOW HINGE IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS A MINOR.SDR ASOA2012070301851Floor Support · corrodedFLOOR SUPPORT AT FS 280.00 IS CORRODED. PERFORMED CUT-OUT IAW REO 670-53-21-139 STEP 1 & 2. COMPLIED WITH STEP 3 OF REO 670-53-139 IAW NDTM PART 1, 51-20-006, NO INDICATIONS NOTED. INSTALLED REPAIR IAW WITH REO 670-53-21-139.SDR ASOA2012070901869Floorbeam · corrodedFLIGHT COMPARTMENT FLOORBEAM ANGLE AT FS 280 IS CORRODED AROUND NUTPLATES. REMOVED CORROSION, OUT OF ALLOWABLE LIMITS IAW SRM 51-21-06-001-001-A01, & 53-00-00-101-001-A01. REMOVED CORRODED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-06-001SDR ASOA2012071001879Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN FS 319 - 333. REMOVED CORROSION IAW SM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED EXISTING HOLES IN NEW STRINGER IAW SDR ASOA2012071301890Support · corrodedFWD JACKING POINT SUPPORT IS CORRODED BETWEEN FS 265-280 AND S26L-26R. FOUND FWD JACKING POINT SUPPORTS OUT OF LIMITS, REPLACED LT & RT SUPPORTS IAW SRM 51-42-06-001-001 & 51-42-21-001-001.SDR ASOA2012071301891Stringer · corrodedAVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN FS 333-349. REMOVED CORROSION IAW SRM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW STRISDR MASA2012052234804Plug · missingEMERGENCY DECLARED DUE TO ENGINE NR 2 LEAKING OIL. INSPECTED EDP SPLINE PLUG AND IT WAS NOT INSTALLED. MAINTENANCE INSTALLED SPLINE PLUG. SERVICED ENGINE OIL AND NO LEAKS NOTED.SDR CA120518006Tire · failed(CAN) ON DEPARTURE, AND SLIGHTLY AFTER V1, THE FLIGHT CREW FELT A MILD VIBRATION. THE NOSE TIRES WERE OFF THE RUNWAY AT THIS POINT, GIVEN WE WERE IN THE MIDDLE OF ROTATION. BASED ON THE VIBRATION AMOUNT, ONE OF THE SHIMMY DAMPERS WAS SUSPECTED. THEY CONTINUE SDR CA120515003Cable · damaged(CAN) DURING ROUTINE SCHEDULED MAINTENANCE A DEFECT AILERON CONTROL CABLE WAS FOUND. THE DEFECTIVE CABLE CONNECTS THE AILERON AUTOPILOT SERVO WITH THE RT REAR QUADRANT. THE CABLE HAD SOME DAMAGE, TORN WIRE STRINGS. THE AILERON SERVO AND THE SERVO MOUNT WERE SDR CA120518005Line · chafed(CAN) FOLLOWING TAKEOFF, THE CREW OBSERVED THE, INBD GROUND SPOILERS, IB BRAKE PRESS AND HYD 3 LO PRESS, MESSAGES ON THE EICAS WHILE ATTEMPTING TO RETRACT THE LANDING GEAR, FOLLOWED BY GEAR DISAGREE. THE LANDING GEAR REMAINED DOWN AND THE CREW NOTICED THAT TSDR CA120515004Cable · damaged(CAN) PILOT REPORTED DURING FLIGHT CONTROL CHECK HARD TO REACH FULL LT AILERON DEFLECTION, CHECK MAINTENANCE ACTIONS: FOUND CONTROL CABLE OF THE AILERON SERVO BROKEN ALSO FOUND SIGNS OF CORROSION AT THE CONTROL CABLE OF THE SERVO. AILERON SERVO MOUNT REMOVEDSDR CA120502010Control System · binding(CAN) ON APPROACH, THE PITCH CONTROL FELT STIFF FOLLOWING AUTOPILOT DISCONNECT PRIOR TO LANDING. AT ABOUT 400 FEET ALTITUDE, THE CREW DISCONNECTED THE AUTOPILOT. THE AIRCRAFT THEN PITCHED NOSE DOWN. THE CREW REPORTED THAT FOLLOWING THE PITCH DOWN THEY FAUGHT WSDR CA120328001Yaw Damper · failed(CAN) FLIGHT CREW REPORTED DURING CLIMBOUT AT 280 KTS, THE RUDDER STARTED TO OSCILLATE RT AND LT. AUTO PILOT WAS IMMEDIATELY DISCONNECTED. OSCILLATION CONTINUED LT AND RT. YDNR 1 INOPERATIVE STATUS, MSG APPEARED. TRIED TO DISCONNECT YD NR 2 BUT WOULD NOT DSDR CA120321003Door · separated(CAN) AFTER LANDING THE AFT NLG DOOR WAS FOUND SEPARATED FROM THE ACFT. THE FLIGHT CREW REPORTED HEARING A NOISE WHEN EXTENDING THE LANDING GEAR ON APPROACH NLG AFT DOOR CC670-33098-5.SDR CA120315001Aileron Sys · binding(CAN) CONTROL YOKE JAMMED AFTER DISCONNECTING THE AUTO PILOT. LIGHT TO MODERATE AILERON FORCE BROKE IT FREE WITH NO FURTHER PROBLEMS. MAINTENANCE REPORTED PERFORMING AN OPS CHECK AND DECLATED THE SYS TO BE SERVICABLE WITH NO NOTED FINDINGS.SDR ASOA201200644Fadec · inoperativeRT ENG DEGRADED-ALL ASSOCIATED INSTRUMENTS SHOWED SIGNAFICANT DROPS (N1, ITT, N2, FF, ECT) REPEATED - NOTICABLE YAW EVERY DEGRADED MSG (ENROUTE ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION) R & R RT FADEC IAW AMM 73-21-01. OPS CHECKED GOOD. SDR CA120206011Yaw Damper · failed(CAN) FLIGHT DIVERTED, DUE TO UNEXPECTED, UNCOMMANDED. MOVEMENT OF THE RUDDER IN FLIGHT. THE NR 1 YD WAS DEFERRED ON THE ACFT. THE F/O WAS IN COMMAND WITH AP ENGAGED. THE RUDDER APPARENTLY KICKED TO THE RT, CREW UNSURE OF DEGREE DISPLACEMENT. IN THE PROCESS OSDR CA120126010Sensor · failed(CAN) ACFT ON APPROACH WHEN THE CREW REPORTED A WING ANTI-ICE SYS FAILURE AND COULD NOT CONTINUE THE APPROACH DUE TO WEATHER. THEY REQUESTED TO BE TAKEN OUT OF THE APPROACH SEQUENCE INTO A CLEAR SPACE AND TO BE DIVERTED TO ANOTHER AIRPORT. THEY DECLARED AN ESDR CA120131006Wire Harness · failed(CAN) EMERGENCY DECLARED, ON SHORT FINAL ANTI-SKID INBD INOPERATIVE AND INBD FLIGHT SPOILER MESSAGES ON EICAS. RT INBD WIRING HARNESS IAW CMM 32-61-01. PERFORMED EXTENSION AND RETRACTION OF MLG IAW AMM 32-30-00. PERFORMED SPOILER TEST IAW AMM 26-61-00. NO DSDR SWIA201229119Bleed Valve · leakingLEFT ENGINE SMOKING ON APPROACH. (FLT 4723) FOUND OPERABILITY BLEED VALVE FITTING LEAKING. REPLACED OPERABILITY BLEED VALVE.SDR CA120103005Window · cracked(CAN) ON DESCENT, NOTICED CRACK IN CAPTAINS SIDE WINDOW. WINDOW, SIDE LT NP139322 & 8722, 11.SDR SIMA201135301Valve · inoperativeON FLIGHT 4655 THE CREW REPORTED THAT ON DESCENT FROM FL 400 THE CAPTAIN WAS PULLING THE THRUST LEVERS TO IDLE AND HEARD A "THUMP" FOLLOWED BY A RUMBLE FROM THE RIGHT ENGINE WITH BOTH N1 AND N2 SPOOLING DOWN WITH NO RELIGHT. MOVED THRUST LEVER TO IDLE. WHENSDR CA111212004Fire Warning · unknown(CAN) CLIMBING WHEN THE FWD LAVATORY FIRE ALERT ACTIVATED. THE CREW DECIDED TO RETURN FOR A SAFE LANDING. A PAX REPORTED ODOR OF SMOKE ON BOARD, A FIRE ALERT WAS HEARD FROM THE FWD LAVATORY. THE CAPTAIN ANNOUNCED THERE WAS AN UNIDENTIFIED PROBLEM WITH A FIRSDR CA111213004Windshield · cracked(CAN) DURING CRUISE FLIGHT CAPTAINS WINDSHIELD SINGLE PANE SHATTERED. ALL PRESS READINGS REMAINED STABLE. ACFT RETURNED TO DEPARTURE AIRPORT. WINDSHIELD LT 601R33033-13.SDR SWIA201128702Unknown · vibrationDURING CRUISE RIGHT N1 VIBES STARTED SLOWLY RISING TO 1.6 THEN UP TO 2.0, RAN QRH PROCEDURE, AND PULL BACK THE ENGINE TO ACCEPTABLE LEVELS TO HOLD ACCEPTABLE SPEED AT ALTITUDE N1 HAD TO BE AT 74 PERCENT. ENGINE VIBES SLOWLY DEGRADED. (FLT 5194) SHOOK BLADESSDR ASOA201102029Engine · fireWHILE TAXING TO GATE, RECIEVED LEFT ENGINE FIRE WARNING MESSAGE. FIRE WARNING EXTINGUISHED, TAXIED TO GATE. ENGINE WAS ALREADY SHUTDOWN AT TIME OF WARNING. R & R LEFT ENGINE ASSY. ACFT OK FOR SERVICE.SDR CA111025002Bleed Valve · damaged(CAN) WHILE TAXING TO GATE, RECEIVED LT ENG FIRE WARNING MESSAGE. PERFORMED IMMEDIATE ACTION ITEMS FOR LT ENG. SEVERE DAMAGE ON GROUND (QRH). FIRE WARNING CEASED. TAXIED TO GATE. ENGINE WAS ALREADY SHUTDOWN AT TIME OF WARNING. NOTED THAT CREW DID NOT DISCSDR MASA2011091463680Actuator · leakingFUEL LEAK RT ENG DRAIN MAST DURING PUSH. R2 SLAVE VG ACTUATOR.SDR CA110816005Line · leaking(CAN) ON TAKEOFF, EXPERIENCED A LEFT ENGINE FIRE. FLIGHT CREW REPORTEDLY HEARD TWO LOUD BANGS ON TAKEOFF, FOLLOWED BY AN EICAS FIRE WARNING FOR THE LT ENGINE, THERE WAS NO INDICATED LOSS OF POWER. FLIGHT CREW FOLLOWED PROCEDURES IAW THE QRH. BOTH FIRE BOTTLSDR MASA2011071103196Engine · vibrationRT ENG N1 VIBE 1.8 IN CRUISE. C/W RO MAX VIBE AFTER RUN 0.3.SDR CA110607001Engine · shutdown(CAN) ENGINE 1 -10 SEC AFTER START, AND AFTER STABILIZED ENGINE OPERATION, THE AUTOMATIC ENGINE SHUTDOWN OCCURRED. NO RESTART OF ENGINE POSSIBLE. REMAINING MSG. LT FADEC FAULT 1 + LT THROTTLE FAULT/STATUS MSGS. READ OUT OF THE MDC WAS REPORTED BY OUR MECHANSDR CA110607008Engine · power loss(CAN) DURING CLIMB LT ENGINE INDICATIONS REDUCED BY 50 PERCENT FOR APPROXIMATELY 3 SECS. AC YAWED THEN ENGINE RETURNED TO NORMAL. NO EICAS MSGS ENGINE DID NOT SHUTDOWN.SDR COMA2011042870011Warning Message · illuminatedON APPROACH, RECEIVED RT FADEC CAUTION MESSAGE. EMERGENCY DECLARED, ACFT LANDED SAFELY. PERFORMED FIM TASKS 73-21-00 AND 73-21-02. NO FUTHER DEFECTS NOTED.SDR MASA2011041102382Fluid · leakingLT ENG FLUID LEAK. MX RE-INSPECTED THE LEAK AND FOUND IT TO BE WITHIN LIMITS.SDR MASA2011041102378Unknown · leakingNR 2 ENG FUEL LEAK. MX PERFORMED DRY MOTOR AND RUNS, LEAK CHECK GOOD.SDR CA110331011Controller · failed(CAN) CONTROL OF CABIN PRESSURE IN AUTO AND MANUAL MODES WAS NOT POSSIBLE. MDC SHOWED INTERNAL PRESSURE SENSOR FAILURE. CPCP REPLACED. ACFT RETURNED IN SERVICE.SDR CA110328009Acm · failed(CAN) DURING THE FLIGHT PREPARATION BEFORE BOARDING AND AFTER SWITCHING ON THE RT AIR CONDITIONING PACK A CHEMICAL ODOR AND A BRIGHT SMOKE WAS NOTICED WITHIN THE CABIN. THERE UPON THE PIC SWITCHED OFF THE APU AND THE BATTERY MASTER SWITCH AND LT THE ACFT TOGESDR MASA2011030402057Actuator · leakingLEFT ENGINE LEAKING FUEL. MX R2 VG ACTUATOR ASSEMBLY.SDR MASA2011012001729Sensor · dirtyLEFT ENG DEGRADED CAUTION, CREW ABORTED TAKEOFF. MX CLEANED LT T2 SENSOR PLUG.SDR CA110106003Ballast · burnedSMOKE IN THE CABIN REPORTED BY PAX AND FLIGHT ATTENDANT WHILE CLIMBING THROUGH FL 200. RETURNED TO BASE. SMOKE WAS REPORTED AROUND THE VICINITY OF ROW 10. REMOVED AND REPLACED CEILING LIGHT BALLAST AT 12AB. OPS CHECKED A/C FOR 30 MIN. OPS CHECKED GOOD AT SDR QXEA2010122100926Seal · dirtyGALLEY SERVICE DOOR HARD TO OPEN. CLEANED AND LUBRICATED DOOR SEAL. C/W FUNCTIONAL TEST OF THE GALLEY SERVICE DOOR IAW AMM 52-41-00-720-801-A01. FUNCTION CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.SDR MASA2010121601471Blade · lack of lubeLEFT ENGINE VIBE IN YELLOW (3.8) DURING TAXI. MX C/W BLADE LUBE.SDR ASOA201001988Wire Harness · unserviceableNOSE WHEEL STEERING CAUTION MSG AFTER TAKEOFF WHEN GEAR RETRACTED. LANDED WITHOUT NWS. NOT AN OVERWEIGHT LANDING. UNABLE TO RESET ON GROUND WITH MX (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) R & R NWS HARNESS, OPS CHECK GOOD IAW AMM 32SDR SIMA201034905Engine · vibrationON FLIGHT 3879 THE CREW REPORTED THAT DURING CRUISE AT FLIGHT LEVEL 370 THE RIGHT ENGINE N1 VIBRATION AT 2.1 -AMBER RANGE- THRUST WAS 85 PERCENT. THE CREW REDUCED THRUST TO 70 PERCENT N1 WHICH GOT N1 VIBRATION INTO GREEN RANGE AT 1.7 N1 VIBRATION. THIS WAS NSDR QXEA2010121700903Computer · malfunctionedSTALL FAIL CAUTION MESSAGE DURING CLIMBOUT. EMERGENCY AND ABNORMAL CHECKLIST COMPLIED WITH; CAPT STALL PROTECTION SWITCH TURNED OFF. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R STALL PROTECTION COMPUTER AS A PRECAUTIONARY MEASURE. AMM TASKS 27-35-01-000-71SDR ASOA201001914Support · corrodedLT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 517.0 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-00-00 AND REO 670-53-31-189.SDR ASOA201001915Support · corrodedLT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 485 IS CORRODED. BLENDED CORROSION IAW SRM 51-21-06. MATERIAL LOSS OF .005 NOTED, ORIGINAL MATERIAL THICKNESS OF .056, REMAINING MATERIAL THICKNESS OF .049 NOTED, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.SDR ASOA201001916Seat Track · corrodedCORROSION ON LT SIDE SEAT RAIL APPROX 3 FT BEHIND OVERWING EXIT DOOR. BLENDED AND FOUND OUT OF TOLERANCE, R & R SEAT TRACK IAW AMM 53-00-49
Back to GE CF34-8C1