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 aircraft_model_key = '747338' 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 aircraft_model_key = '747338' 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 AU510002178Panel · missing(AUS) NR 4 ENGINE VIGV ACCESS PANEL MISSING. INVESTIGATION ALSO FOUND THE LP COMPRESSOR ACOUSTIC LINING DAMAGED AT THE 6 O`CLOCK POSITION WITH A HOLE APPROXIMATELY 150MM BY 100MM (6IN BY 4IN) IN THE SKIN. VIGV CONTROLLER PANEL SUPPORT STRUCTURE ALSO DAMAGED. (SDR AU510002110Solenoid · corrodedLT WING LANDING GEAR UPLOCK ACTUATOR SOLENOID CORRODED. A CORROSION LIKE SUBSTANCE WAS FOUND AROUND THE CANNON PLUG AND PART OF THE OPERATING SOLENOID OUTER CASE WAS CORRODED AWAY.SDR AU510001843Interphone · unserviceableCABIN INTERPHONE SYSTEM FAULTY. INVESTIGATION CONTINUING.SDR AU510001830Frame · crackedFOUND FUSELAGE INNER CHORD RING CRACKED. CRACK LOCATED AT FASTENER HOLE LBL 33.5 AND WL 153 BS 140 FPB (REAR FACE). FOUND DURING INSPECTION IAW AD/B747/159 AND EI 747-053-0215.SDR AU510001829Intercostal · crackedINTERCOSTAL CRACKED. CRACK LOCATED AT FORWARD FACE OF BS 140 FPB AT LBL 20 AT 2 O`CLOCK POSITION LOOKING AFT. FOUND DURING INSPECTION IAW AD/B747/159 AND EI 747-053-0215.SDR AU510001717Trunnion · crackedRT WING LANDING GEAR AFT TRUNNION CRACKED ON INTERNAL SURFACE OF THE SPIGOT BORE LOCATED APPROX 241.3MM (9.5IN) FORWARD OF THE AFT FACE BETWEEN THE 6 O`CLOCK AND 9 O`CLOCK POSITIONS. CRACK CONFIRMED USING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION. FOUND SDR AU510001639Frame · scratched(AUS) FORWARD PRESSURE BULKHEAD AFT FACE OUTER CHORD SCRATCHED IN BEND RADIUS LOCATED AT LBL46/WL235 AND RBL24/WL268. SUSPECT A SHARP OBJECT WAS USED TO REMOVE SEALANT. FOUND DURING INSPECTION IAW AD/B747/159. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA NSDR AU510001595Tire · damagedNR 3 REAR TIRE ASSEMBLY CONTAINED A DEEP CUT. INVESTIGATION FOUND CUT TO BE OUT OF LIMITS.SDR AU510002016Pump · failedNR 3 ENGINE FUEL PUMP LOW PRESSURE IMPELLER SHEARED. INVESTIGATION FOUND THE FAILURE OF THE PUMP WAS CAUSED BY VIBRATIONS THAT WERE INTRODUCED BY THE INTERACTION OF THE IMPELLER SYMMETRICAL SUPPORT PINS WITH THE SPACER TUBE. THESE VIBRATIONS CAUSED A LOSS OFSDR AUS20040443Indicator · faulty(AUS) LT OB TRAILING EDGE FLAP INDICATOR FAILED.SDR AUS20040390Bolt · incorrect(AUS) LT WING LANDING GEAR TO LANDING GEAR DOOR TIE ROD BOLTS INCORRECTLY FITTED. BOLTS WERE FITTED UPSIDE DOWN. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040353Wire · broken(AUS) ENGINE AIRBORNE VIBRATION MONITOR INDICATION MODULE SELECTOR SWITCH WIRE FROM PIN 19 OF CONNECTOR DM162 BROKEN.SDR AUS20040127Blanket · deteriorated(AUS) APU DUCT INSULATION BLANKET BURNED AND IN POOR CONDITION.SDR AUS20031255Ballast · failed(AUS) LIGHTING BALLAST LOCATED AT SEAT 19JK FAILED.SDR AUS20031205Wire Harness · worn(AUS) WIRING LOOM LOCATED AT BS 1000 BEHIND OVERHEAD LOCKERS CHAFED THROUGH INSULATION BLANKET AND CONTACTED FUSELAGE FRAME CAUSING BURNING OF WIRES AND DAMAGE TO THE INSULATION BLANKET AND FRAME. AREA OF DAMAGE TO FRAME WAS APPROXIMATELY 4.762MM BY 2.381MM(0.SDR AUS20031038Control Cable · worn(AUS) NO3 ENGINE THRUST CABLE T3A-4 WORN AT LOCATION ILES 564. FOUNDDURING INSPECTION IAW EI 743-076-0002R02 (FAA AD 2000-05-30 AND CASA AD/B747/229).SDR AUS20030882Tire · failed(AUS) NR 5F TIRE TREAD SEPARATED FROM CASING. TIRE REMAINED INFLATED. NIL DAMAGE EVIDENT TO REST OF AIRCRAFT. SUSPECT CAUSED BY FAILURE OF TREAD TO BOND TO CASING DURING RETREAD.SDR AUS20030655Wire · damaged(AUS) ELECTRICAL WIRING CHAFED AND BURNED IN AREA LOCATED ABOVE TOILET CEILING.SDR AUS20030634Slide · failed(AUS) DOOR NR 1 RT SLIDE RAFT FAILED.SDR AUS20030518Radio · failed(AUS) DUAL HF SYSTEM FAILURE. ON ARRIVAL IT WAS REPORTED THAT NR 1 HF SYSTEM WANDERS OFF FREQUENCY AND BECOMES GARBLED. NR 2 HF WOULD NOT TUNE TO THE FREQUENCY SELECTED. THE NR 1 SYSTEM WAS RE-RACKED AND OPERATED NORMALLY. THE NR 2 SYSTEM TRANSCEIVER AND COUPSDR AUS20030453Valve · faulty(AUS) STRUT OVERHEAT WARNING. HIGH STAGE VALVES AND PYLON VALVES REPLACED. LIMITED INFORMATION PROVIDED.SDR AUS20021149Pump · failed(AUS) NR 2 ENGINE DRIVEN FUEL PUMP FAILED.SDR AUS20020994Engine · failed(AUS) NR 1 ENGINE FAILED. EXCESSIVE VIBRATION INDICATIONS. INSPECTION FOUND METAL IN TAILPIPE.SDR AUS20020787Bolt · fractured(AUS) RT AILERON PCU RODEND BOLT HEAD BROKEN.SDR AUS20020646Switch · failed(AUS) FLAP SWITCH S315 HAD HIGH RESISTANCE. FOUND DURING FUNCTIONAL TEST IAW TST 018632.SDR AUS20020513Charger · faulty(AUS) APU BATTERY CHARGER FAULTY.SDR AUS20020380Engine · failed(AUS) ON ROTATION A LOUD BANG WAS HEARD AND NR 4 EPR INDICATION DROPPED AND SPARKS WERE REPORTED FROM THE NR 4 ENGINE. THE ENGINE WAS SHUT DOWN.SDR AUS20020305Handle · out of adjust(AUS) L5 DOOR HANDLE RIGGING OUT OF ADJUSTMENT.SDR AUS20020131Panel · debonded(AUS) NR 1 ENGINE ICE IMPACT PANEL DISBONDED.SDR AUS20020118Engine · stalled(AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES.SDR AUS20020089Actuator · faulty(AUS) RUDDER RATIO ACTUATOR FAULTY.SDR AUS20020074Hose · leaking(AUS) LT BODY LANDING GEAR STEERING SYSTEM FLEXIBLE HYDRAULIC HOSE LEAKING. LOSS OF NR 1 HYDRAULIC SYSTEM FLUID.SDR AUS20020067Coupling · misrigged(AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED.SDR AUS20020054Engine · vibrates(AUS) NR 2 ENGINE VIBRATION EXCESSIVE.SDR AUS20020039Pcu · faulty(AUS) RT INBOARD AILERON POWER CONTROL UNIT (PCU) FAULTY.SDR AUS20020032Control Unit · faulty(AUS) NR 2 ENGINE VIBRATION SIGNAL CONTROL UNIT SUSPECT FAULTY.SDR AUS20011437Bolt · sheared(AUS) H11 BOLT LOCATED AT STN 1241/LBBL 127/WL 163 SHEARED. FOLLOWING REMOVAL OF THE BOLT CORROSION WAS FOUND IN THE BULKHEAD FITTING BORE. FOUND DURING ULTRASONIC INSPECTION.SDR AUS20011381Bolt · loose(AUS) NR 1 ENGINE FUEL FLOW REGULATOR (FFR) TO FUEL PUMP PIPE LEAKING. INVESTIGATION FOUND A LOOSE PIPE RETAINING BOLT ON THE FFR.SDR AUS20011362Crosstube · damaged(AUS) NR 3 FLAP TRACK CARRIAGE AFT BOGIE CROSSTIE ASSEMBLY DAMAGED DUE TO INTERFERENCE WITH THE FLAP TRACK.SDR AUS20011348Control Valve · leaking(AUS) HYDRAULIC OIL WAS FOUND LEAKING FROM THE LOWER RUDDER PCU TRANSFER VALVE.SDR AUS20011200Transceiver · faulty(AUS) WEATHER RADAR TRANSCEIVER FAULTY.SDR AUS20011178Line · damaged(AUS) HYDRAULIC LINE DAMAGED BY CONTACT FROM THE RT WING LANDING GEAR RETRACTION ACTUATOR. LOSS OF NR 4 HYDRAULIC SYSTEM FLUID.SDR AUS20011132Control Cable · seized(AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED.SDR AUS20011075Ballast · failed(AUS) LIGHT BALLAST LOCATED AT SEAT 70HJK BURNT.SDR AUS20011066Transformer · burned out(AUS) TWO LIGHTING TRANSFORMERS Y7NT02 AND Y7NT03 BURNT. INVESTIGATIONFOUND THAT THE OVERHEATING WAS CAUSED BY INCORRECT PART NUMBERLAMPS FITTED IN TWO LOCATIONS. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR AUS20011016Cable · distorted(AUS) NR 3 ENGINE THRUST CABLE KINKED IN THE AREA OF THE STRUT TO WING INTERFACE.SDR AUS20011084Video Display · faulty(AUS) VIDEO MONITORS LOCATED AT SEAT 2A AND 17B BURNT INTERNALLY. INVESTIGATION FOUND OVERHEATING TRANSISTORS CAUSING THE PCB AND PROTECTIVE LAYER TO BURN.SDR AUS20010995Video Display · failed(AUS) VIDEO SCREEN LOCATED AT SEAT 2A SMOKING. MONITOR AT SEAT 17B HAD BURNING SMELL.SDR AUS20010928Cover · cracked(AUS) LT AND RT ENGINE THRUST CABLE GUARD COVERS LOCATED IN AREABETWEEN BS960 TO BS1000 DETERIORATED AND CRACKED. FOUND DURING INSPECTION IAW EI 743-076-0002R02.SDR AUS20010883Engine · vibrates(AUS) NR 2 ENGINE VIBRATION EXCESSIVE.
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