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 = 'CF650E2' 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 = 'CF650E2' 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 UIEA200400206Mechanism · brokenAFTER TAKEOFF AT APPROX 2,500 FT, THE LT ENTRY DOOR (L1) DOOR LIGHT CAME ON. ACCOMPLISHED CHECK LIST. THEN HEARD A LOAD NOISE WITH AIRCRAFT PRESS CLIMBING. RETURNED TO SFO. AFTER LANDING, FOUND DOOR LOCKING LUG BROKEN OFF. ACCOMPLISHED DETAILED INSPECTIONSDR UIEA200400204Switch · dirtyON TAKEOFF, WHEN GEAR RETRACTED, RED GEAR WARNING LIGHT CAME ON. F/E PANEL RT WING DOOR OPEN LIGHT WAS ON, BOTH PRIMARY AND ALT POSITIONS. DID FHB CHAPTER 3, GEAR HANDLE UP, LIGHT WHEN OUT. GEAR HANDLE OFF, LIGHTS ON AGAIN. LT HANDLE UP. INSPECTED AND FOUSDR UIEA200400203Connector · looseNR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CONNECTOR LOOSE ON L/E DRIVE UNIT. RESECURED CONNECTOR IAW MM. OPS CHECK OK, NORMAL. (K)SDR P5CA0401288Link · missingNR 4 ENGINE T/R BLOCKER DOOR LINK MISSING AT 4 O'CLOCK POSITION. REMOVED BLOCKER DOOR AND BROKEN LINK PER CDL 78-31-1. T/R LOCKED OUT PER DDPG 78-1.SDR P5CA0401287Regulator Valve · failedON TAXI OUT DUCT LOW PRESS LIGHT CAME ON WITH DROP IN DUCT PRESSURE ON GAGE. ISOLATED LEFT WING PRESS LESS THAN 15 PSI. REPLACED PRESSURE REGULATOR VALVE ON ENGINE NR 2 PER MM 36-1114. PERFORMED ENGINE RUN PER MM 71-00-00. OPS CHECK OK.SDR UIEA200400202Shutoff Valve · leakingDURING CRUISE, LOSS OF FLUID NR 4 HYD SYSTEM. SYSTEM DEPRESSURIZED AT 2.0 GALS QUALITY. EDP TO SUPPLY OFF. FOUND NR 4 RUDDER CONTROL SHUTOFF VALVE FAILED. (LEAKED) REMOVED AND REPLACED NR 4 RUDDER SHUTOFF VALVE. OPS AND LEAD CHECK GOOD IAW MM. (K)SDR UIEA200400201Structure · missingPOST FLIGHT INSPECTION, FLT EK4979, 07/DEC/2004. DURING INSPECTION, FOUND NR 4 ENGINE AFT CENTER BODY CRACKED OFF. MISSING, LAST 20 INCHES FROM T/E. REMOVED AND REPLACED NR 4 ENGINE AFT CTR BODY IAW MM 78-11-02. INSPECTED AREA AFT OF NR 4 ENGINE FLAPS, WINSDR UIEA200400200Sensor · failedIMMEDIATELY AFT T/O, STALL WARNING, STICK SHAKER ACTIVATED ASSOCIATED WITH STALL WARNING. (POWER OFF) LIGHT ILLUMINATION ON PILOTS OVERHEAD PANEL. REMOVED AND REPLACED LT ANGLE OF ATTACK SENSOR. OPS CHECK NORMAL IAW MM.SDR 746002Engine · failedON TAKEOFF, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL. CREW SHUT DOWN ENGINE, DUMPED FUEL AND RETURNED TO BASE. ENGINE BOROSCOPED WITH NO DEFECTS NOTED. FOUND METAL IN TAILPIPE. ENGINE IS BEING REPLACED AT THIS TIME.SDR UIEA200400198Actuator · leakingDURING CLIMB-OUT, NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON WITH A DROP OF SYSTEM QUANTITY OIL FROM 8.5 TO 2.5, SYSTEM WAS SHUTDOWN. QUANTITY REMAINED AT 2.5. TURNED ADP TO CONTINUOUS, QUANTITY STARTED DROPPING, SYSTEM SHUTDOWN. REF: LOG PAGE 537018,SDR UIEA200400192Skin · crackedDURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSY FORWARD ANGLE FRAME OF THE NR 2 PYLON LT AND RT SIDE WERE FOUND CRACKED. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY SDR UIEA200400193Frame · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD UPPER ASSY FRAMES CRACKED. STOPPED DRILLED THE CRACK ENDS IAW SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FSDR UIEA200400194Fairing · delaminatedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 2 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM THE OB SKIN SIDE AND REPLACEMENT CORE AND SKIN WERE SPLICED BY BONDING IAW SRM 51-40-06. IT WAS FURTHERSDR UIEA200400195Fairing · delaminatedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 4 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM BOTH IB AND OB SIDES WITH REPLACEMENT CORE, SKIN AND DOUBLERS BONDED IAW SRM 51-40-06. PERFORM DETAILEDSDR UIEA200400197Spar · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 16 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FISDR UIEA200400196Spar · crackedD-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 15 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FISDR UIEA200400191Strap · crackedDURING SCHEDULED MAINTENANCE, FOUND CRACK NR 4 PYLON AT AFT MOUNT BULKHEAD FRAME STRAP. SUBJECT CRACK WAS LOCATED ALONG THE STRUT UPPER SKIN ASSY LOWER EDGE. CRACK AFT END WAS CONTAINED WITH A STOP HOLE IN THE STRAP. THE REPAIR AREA WAS NDT INSPECTED, INCLUSDR UIEA200400190Pdu · failedDURING CLIMB-OUT, NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 LE PDU. OPS CHECK OK IAW MM 27-81-03. PDU OFF PN 126344-17-1, SN 22337, TOTAL MAINT DELAY, 3 HRS, 17 MIN. NOTE: NO FUEL WAS DUMPED.SDR UIEA200400189Rib · crackedDURING SCHEDULED MAINTENANCE. FOUND CRACK AT RT VARIABLE CAMBER FLAP HINGE RIB ASSEMBLY. TRIMMED THE FLANGE TO REMOVE THE DAMAGE. HFEC THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. THE REPAIR AND RESTORATION WAS ACCOMPLISHED TO RESTORE TO THE ORIGINALSDR P5CA0401269Sensor · malfunctionedSTICK SHAKER ACTIVATING INTERMITTENTLY IN STEADY STATE CRUISE FLIGHT, C/B PULLED. REPLACED LT AOA SENSOR PER AMM 27-32-01, OPS CHECK OK PER AMM 27-32-00.SDR UIEA200400187Precooler · crackedEK9971 ICN/ANC (ATB) FIRE WARNING: NR 4 ENGINE FIRE LIGHT CAME ON IN-FLIGHT NACELLE INDICATOR WAS ABOUT 3 TO 3.5 EGT APPROX 900 DEGREE HIGH STAGE BLEED LIGHT CAME ON JUST BEFORE FIRE LIGHT AND BELL. FIRE LIGHT CAME ON ABOUT FL 24.2 ENGINE S/D A/WITH FHB. INSDR P5CA0401263Fuel Cell · overservicedFUEL SPILL RIGHT WING. FOUND NR 4 MAIN OVER FILLED. DRAINED RIGHT SURGE TANK IAW 28/21/00, RESET SYSTEM & CONTINUED FUELING. CHECK OF VOLUMETRIC SYSTEM IAW 28-21-00 SATISFACTORY.SDR P5CA0401260Igniter · failedNR 3 ENGINE IGNITION INOP ON START. REPLACED BOTH IGNITER PLUGS PER AMM 74-21-02 & SYSTEM OPS TEST OK PER AMM 74-00-00/501.SDR P5CA0401259Duct · rupturedNR 4 ENGINE FIRE/FAULT LOOPS A&B BOTH SHOWED A CONTINUOUS RISE IN TEMP, CLOSED BLEED AIR VALVE, TEMPRATURE DROPPED TO NORMAL. RETARDED THROTTLE TO IDLE. T/S & FOUND S-DUCT IN PYLON RUPTURED. REPLACED DUCT & CLAMPS PER AMM 36-11-00, NO LEAKS NOTED.SDR UIEA200400179Inu · failedON CLIMB OUT, NR 1 INS WARNING LIGHT CAME ON. ON CLIMB OUT NR 1 INS WARNING LIGHT CAME ON. NR 1 ADI AND HEADING FAILED. SELECTED NR 3 ATTITUDE AND COMPASS. APPROX 3 MINUTES LATER NR 3 INS WARNING LIGHT CAME ON. BOTH SCREENS WENT BLANK AND SHUT DOWN. REMOSDR P5CA0401230Warning Light · activated(ANT FAULT): MESSAGE ON BOTH NR 1 AND NR 2 WX RADARS. TRANSFERED TO DMI NR 33183 IAW MEL NR 34-23B.SDR UIEA200400156Line · brokenAFTER TAKEOFF NR 4 ENGINE FIRE WARNING SOUND. PEAK EGT 976 FOR 11 SECONDS. GOT A RED BALL, SHUTDOWN THE ENGINE IAW FHB FIRE INDICATION WENT OUT WHEN NR 4 ENGINE FIRE SWITCH WAS PULLED. PERFORMED NR 4 ENGINE VISUAL INSPECTION NO EVIDENCE OF FIRE. PERFORMED SDR P5CA0401181Engine · malfunctionedDURING T/O AFTER ROTATION NR 2 ENG TEMP ROSE INTO THE YELLOW BAND & THE NACELLE TEMP WAS RISING RAPIDLY, THE THROTTLE WAS RETARDED & TEMP CAME DOWN. ENG FAILURE CHECK ACCOMPLISHED. NR 2 ENGINE REMOVED & REPLACED.SDR P5CA0401180Relief Valve · malfunctionedNR 2 ENG INDICATE A FIRE AT 13:50- 6 MINUTES AFTER TAKEOFF. NACELLE TEMP IN THE FIRE ZONE. ENGINE FIRE PROCEDURE WAS ACCOMPLISHED, PULLED FIRE HANDLE, DID NOT DISCHARGE FIRE BOTTLES. OIL PRESSURE NORMAL. REMOVED AND REPLACED NR 2 ENG PRESSURE RELIEF VALVE SDR P5CA0401179Controller · out of adjustNR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. ADJUSTED MAIN ENGINE CONTROL PER AMM 73-00-00.SDR P5CA0401174Transducer · failedAUTO BRAKES INOP. REPLACED ANTI-SKID TRANSDUCER NR 3 POSITION, SPIN CHECK NORMAL (NO LIGHT ILLUMINATE PER MM 32-43-00).SDR P5CA0401137Connector · looseRUDDER RATIO LIGHT CAME ON DURING CLIMBOUT, 220KTS, FLAPS 1 DEGREE. RESEATED CONNECTOR TO RUDDER RATIO CONTROLLER AND SERVO ACTUATOR IAW AMM 27-21-00..SDR P5CA0401136Comparator · inoperativeRUDDER RATIO LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED RUDDER RATIO COMPARATOR.SDR P5CA0401133Pressure Valve · inoperativeDURING ENGINE START NR 3 ENGINE ROTATION WAS SLOW, LIGHT OFF NORMAL BUT WOULD NOT ACCELERATE PAST 30 PERCENT. REPLACED NR 3 ENGINE PRESSURE RELIEF VALVE, OPERATIONAL CHECK GOOD IAW MM 36-11-00.SDR P5CA0401131Valve · malfunctionedAFTER ENGINE START NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. ALL INSTRUMENTS INDICATED ENGINE AT IDLE POWER. CLEANED CDP LINE, NO HELP, REPLACED CIT SENSOR, ENGINE NOW RUNS HIGH EGT, FOUND PYLON VALVE AT FAULT, OPENED DMI NR 36-5-2.SDR P5CA0401120Seal · leakingNR 1 ENGINE OIL QTY DROPPED FROM 5.3 GALLONS AFTER TAKEOFF, QTY DROPPED TO 1.25 GALLONS, OIL PRESSURE CLIMBED FROM 50 PSI TO 75 PSI & TEMP 110C. REMOVED AND REPLACED NR 1 ENGINE GENERATOR & GENERATOR SEAL, ALSO REPLACED NR 1 ENGINE CSD SEAL. OPS CHECK OK IAWSDR P5CA0401173Charger · smokeSMOKE IN COCKPIT. MAIN BATTERY CHARGER FAULTY. SWAPPED MAIN CHARGER WITH APU CHARGER, OPS CHECK OK PER AMM 24-31-00. DEFERRED APU BATTERY CHARGER PER MEL 24-24.SDR UIEA200400123Bulb · failedPO380/10 DXB/CGK LOWER CARGO AFT FIRE LIGHT CAME ON DURING TAKEOFF: LOWER CARGO AFT FIRE LIGHT CAME (ON) AT ROTATION. APPROPRIATE DRILLS CARRIED OUT. AIRCRAFT RETURNED TO DEPARTURE. CHECKED LOWER AFT CARGO FOR FIRE OR DAMAGE, NO EVIDENCE. BULK CARGO IS EMSDR P5CA0401119Pdu · inoperativeNR 4 LEADING EDGE (AMBER) TRANSIT LIGHT ON WITH FLAPS EXTENDED. REMOVED AND REPLACED NR 4 EDGE PDU IAW MM 27-81-01, OPS CHECK NORMAL, ALSO REPLACED PDU ELECTRICAL CONNECTOR.SDR P5CA0401116Valve · malfunctionedON ENGINE START-UP NR 1 ENGINE PYLON VALVE WILL NOT OPEN DURING MANUAL ENGINE START. REPOSITIONED PYLON VALVE IN ORDER TO ACHIEVE ENGINE START, OPS CHECK GOOD IAW MM 36-11-04.SDR P5CA0401117Valve · malfunctionedDMI NR 32768, NR 1 PYLON VALVE INOPERATIVE, ALSO HIGH PRESSURE BLEED VALVE ON ENGINE NR 1. REMOVAL AND REPLACEMENT. REMOVED AND REPLACED PYLON VALVE DUE TO NOT CLOSING COMPLETELY , OPS CHECK AND LEAK CHECKS GOOD IAW MM 36-11-04.SDR P5CA0401118Switch · dirtyAFTER START AND TAXI, LE FLAPS NR 4L WOULD NOT EXTEND FROM AMBER, ALT SYSTEM ATTEMPTED, STILL REMAINED AMBER. NR 4L LE FLAP IND GREEN UNTIL TAKEOFF POWER SETTING APPLIED, IND WENT AMBER, ALSO TAKEOFF WARNING HORN SOUNDED. INSPECTED CLEANED IND SWITCH ASSEMBLSDR P5CA0401114Indicator · inoperativeFLIGHT OFFICER AIRSPEED INDICATOR INOPERATIVE, NO MOVEMENT. REPLACED INDICATOR OPS CHECK OK, IAW MM 34-17-03.SDR UIEA200400120Controller · failedGT 8237/03 RMS/DOV AUTO FAIL LIGHT CAME ON DURING FLIGHT: AUTO FAIL LIGHT CAME ON DURING CLIMB ABOUT 8000 FT A/C ALTITUDE OUTFLOW VALVES .2500 CLOSED USED MANUAL IAW ABNORMAL CHECK LIST TO CONTROL DIFFERENTIAL PRESSURE AT 4 PSID CONTINUED FLIGHT. GOING THROUSDR P5CA0401112Actuator · inoperativeBEFORE DEPARTURE COULD NOT LOCK LATCHES ON MAIN CARGO DOOR. REPLACED LATCH ACTUATOR, OPS CHECK OK AS PER MM 52-32-09.SDR UIEA200400119Indicator · malfunctionedDURING CLIMB, WHEN CLEARED INS WAYPOINT AND SELECTING INS MDU, CDI ON C/A AND F/O HSI WOULD NOT CENTER X WHEN CLEARED VOR AND SELECTING ON INS MDU, HSI SHOWED ABOUT 30 DEGREE DIFFERENCE IN UPDATE. EXCESSIVE DIFFERENCE IN DRIFT ON ARRIVAL . 23400 FUEL DUMPED.SDR P5CA0401109Coupler · damagedCAPTAIN COMPASS SYSTEM WOULD NOT SYNC. REPLACED COMPASS COUPLER, OPS CHECK NORMAL AS PER AMM 34-21-00.SDR P5CA0401108Manifold · rupturedNR 4 ENGINE 14TH STAGE MANIFOLD RUPTURE AT LEFT HAND SIDE CDP AIR SWIVEL JOINT. REPLACED 14TH STAGE MANIFOLD & CLAMP AS PER AMM 75-23-00. OPS CHECK & LEAK CHECK ACCOMPLISH AS PER AMM 71-00-00.SDR P5CA0401106Valve · failedNR 3 ENGINE FIRE WARNING CAME ON DURING CLIMB, A & B LOOPS READ 7 TO 10 UNITS, THAN STABILIZED TO 4 UNITS SCALE WHEN THROTTLE MOVED TO IDLE. FOUND NR 3 ENGINE HIGH-STAGE BLEED VALVE LEAK. REMOVED AND REPLACED NR 3 ENGINE HIGH STAGE BLEED VALVE AS PER MM 36-1SDR UIEA200400116Drive Unit · unserviceableDURING CLIMB LT L/E NR 2 AMBER LIGHT REMAINED ILLUMINATED. ALTERNATE PROCEDURES ACCOMPLISHED TO NO AVAIL. WITH NR 2 L/E DIRECTIONAL SW TO (UP), ALTERNATE L/E FLAP DRIVE C/B ON P6 TRIPS. 27000 KG FUEL DUMPED IAW FUEL JETTISON CHECKLIST AT FL140 TO MAX LANDIN
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