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 = '767' 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 = '767' 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 UIEA2021031500568Aileron · damagedLH OTBD AILERON HAS STATIC DISCHARGE EVIDENCE ON OTBD TRAILING EDGE UPPER CORNER(<P ><SPAN>LH OTBD AILERON HAS BEEN / INSPECTED AND REPAIRED IAW B767 SRM 57-60-0201-1, 57-60-02-1A-1, 57-60-02-2R1, / 51-70-17</SPAN></P>)SDR UIEA2021031600596Warning Message · false indicationON TAXI OUT CTR L AND R FUEL PUMP MSG CAME ON WITH 2,000LBS FUEL IN CTR TANK(<P>4,000LBS OF FUEL ADDED TO CENTER TANK. PERFORMED OPS CHECK OF CTR L & CTR R FUEL PUMPS PER AMM 28-22-00. BOTH PUMPS OPS CHECKED GOOD.</P>)SDR 2LCF20210227Adi · odorON FEBRUARY 27, AIRCRAFT N542LA DURING THE CRUISE PHASE ON THE MIA - CJC ROUTE (UC-1307) MOMENTARILY TURNED OFF THE ADI OF THE CAPTAIN'S POSITION AND FOLLOWED BY A SHORT-CIRCUIT NOISE AND SMELL OF SMOKE IN THE CABIN; THE CREW MADE THE DECISION DIVERT TO PTY’S SDR DALA2022090906005None · noneSHIP 1806 DURING CCK AT STAG, A CRACK WAS FOUND ON THE #2 PYLON FWD UPPER SPAR WEB. ER/A 588456-14 SECTION I WAS ACCOMPLISHED. CORRECTIVE ACTION: 88456-14 NOW AT REVISION A. 12 MONTH DT LIMIT CAN BE CANCELED. (1656970)SDR DALA2022041902698None · noneSHIP 1815 ERA 585398-14 ISSUED FOR REPAIR TO #1 ENGINE PYLON FWD UPPER SPAR CHORD AT NAC STA 230. FOLLOW ON ACTCION IS REQUIRED. CORRECTIVE ACTION: REMOVED SEALANT AND CLEANED AREA FOR INSPECTION PER ERA 585398- 14 REV. ORIGINAL. ORIGINAL AND B767 NDT MANUAL PSDR DALA2020012400586Wedge · delaminatedPD: T/E WEDGE DELAMINATED ON UPPER SURFACE I/B. REPAIRED REF. 767-300 SRM 51-70-10, REF. 57-43-02-2R-1.SDR 2019FA0000372Connector · disconnectedEMERGENCY LIGHT ABOVE SEAT 25 H & J INOP DURING TEST. FOUND CONNECTOR D22096 DISCONNECTED. OPS CK NORMAL AFTER RECONNECTINGSDR FDEA20191213688Skin · damagedMDIS 144 27-80 1755 20MAR19 MEM OPEN U #6 SLAT DAMAGED BY BIRD IMPACT. SHGN 20MAR19 05:04 MEM U #6 SLAT L/E SKIN IS OUT OF LIMITS IN REF. TO B767 SRM 57-43-01-1A FIG 101 FACT 23MAR19 18:10 MEM SDR DALA2019050890004Link · damagedPD: WHILE INSPECTING THE PN 310T1032-3 LINK, DAMAGE WAS FOUND COMMON TOTHE BEARING BORE THAT WAS BEYOND THE LIMITS. CA:PRI 576880-14 WAS ISSUED TO MACHINE THE SUBJECT BORE TO COMPLETELY. REMOVE THE DAMAGE. PART WAS FPI'ED AND SLEEVES WERE MANUFACTURED AND INSTSDR DALA2022041902699None · noneSHIP 1818 B767-300 / FUSELAGE SKIN / STA 1654, S-13AR / MULTIPLE SRM REPAIRS / DEVIATIONS - SUPPLEMENTAL INSPECTION REQUIREMENTS, CORRECTIVE ACTION: CURRENT REVISION LEVEL OF ER/A 566343-14 IS REV. A. AT OR PRIOR TO 30,000 TOTAL AIRCRAFT CYCLES AND REPETITIVELSDR DALA2018072390004Sleeve · damagedPD:BEARING BORE WAS FOUND WITH DAMAGE THAT EXCEEDED CMM LIMITS.BORE WAS MACHINED FOR SLEEVE REPAIR. SLEEVE AND REPLACEMENT BEARING WAS INSTALLED PER ER/A 569038-14.SDR DALA2020020490508Skin · debondedPD:1)LOWER SKIN FWD PANEL. INNER SKIN DIS-BONDED. APROX 170 INCHES FROMINBD END. 2)GOUGE, FLAP ATTACH PLATE LOCATED 292" FROM INBD3)EDGE DAMAGE CA:1)REPAIRED PER SRM 767-300 51-70-10 12-15-2019.2)COMPLIED WITH ERA 583012-14 REV ORG.3)COMPLIED WITH ERA583012-14SDR DALA201711107901Flap · damagedDAMAGED MAIN FLAP LOWER PANEL AND TRAILING EDGE FLAP. REPAIRED PER ERA 563106-14, ERA 563009-14, ERA 563016-14, ERA 563078-14 AND ERA 563067-14.SDR CALA2014051691041Frame · corrodedFORWARD CARGO FLOOR STATION 742 FRAME CHORD HAS CORROSION UNDER NUTPLATES AT APPROXIMATELY LBL 10. R & R UPPER CHORD AT STATION 742 IAW DWG 143T1214 & SRM 51-40-02.SDR DALA201302150358Skin · damagedTHE SUBJECT AILERON WAS FOUND WITH A CRACK AND DELAMINATION IN THE UPPER AND LOWER SKINS AND CORE. REF ERS 511351-14, REV ORIG FOR REPAIR.SDR CALA2012082000516Skin · crackedRT WING NR 9 SLAT OTBD MAIN TRACK FITTING L/E SKIN ONE FASTENER HOLE FOUND CRACKED. REPAIRED IAW SRM 57-43-01. REPAIR 2 FIG 201 AND HFEC NO CRACK FOUND ATTACH MX WORK SHEET FORM 44.0008, ITEM 1-18 ACCOMPLISHED.SDR 2012F00110Slide · misoverhauledDURING PACKING OF THE EVACUATION RAMP/SLIDE, NOTED INCORRECT SHEAR-PIN RESTRAINTS INSTALLED DURING PREVIOUS MX. THERE WERE THREE SHEAR-PIN RESTRAINTS INCORRECTLY INSTALLED, TWO 170LB SHEAR-PIN RESTRAINTS, INSTALLED BUT SHOULD BE TWO 70LB SHEAR-PIN RESTRAINTSSDR L4PR20110824001Manifold · damagedRECEIVING INSPECTION OF BOEING PART NUMBER 332T4326-1, MANIFOLD ASSEMBLY, FOUND A PORTION OF THE VALVE ASSEMBLY, P/N S210T120-111 IMBEDDED INTO THE MANIFOLD DUCT HALF. THE MANIFOLD ASSEMBLY WAS SENT IN FOR REPAIR FROM NORTHWEST AIRLINES REFERENCE SERVICE ORDESDR 5PHR20110831001Plug · misinstalledEVALUATION CONDUCTED BY MFG. REPAIR ACTIONS AND HISTORY PRIOR TO INVESTIGATION, TO BE PROVIDED BY OPERATOR OR ITS SUPPLIER. HISTORY OF OVERTEMP/ENGINE SHUTDOWN. UNIT WAS REPAIR AT OPERATOR, VENDOR GA TELESIS. THE VALVE FAILED TO OPERATE DURING RECEIVING TESTSDR IPXA09656397Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND PUNCTURED AT STA 1580 LBL 28. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R FIG 201 REV 44.SDR 2008FA0000466Computer · failedAIR TURNBACK DUE PILOT REPORT 4273256-1; EICAS MSG L FMC FAIL DISPLAYED. FIM 34-61-00 FOLLOWED L FMC PWR RESET ALL INDICATIONS NORMAL. PLS MONITOR FURTHER. AS A PREVENTIVE ACTION DURING OVERNIGHT; IAW AMM 34-61-01/401 WAS REMOVED AND REPLACED THE FLIGHT MANASDR HALA0800255Seat Track · corrodedLEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1273, AREA WAS HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PER SRM.SDR DL764071164Sensor · malfunctionedRTB DUE TO R ENG BLEED OVERHEAT AND PRSOV STATUS MSG, T/S PER FIMM 36-20-00 FAULT 36-10510. REPLACED TM1 SENSOR OPS/LK CK GOOD RAN ENG. COULD NOT DUPLICATE.SDR 2007FA0001091Manifold · fracturedMANIFOLD CRACKED IN THE FILTER BOWL AS DESCRIBED IN BETWEEN WHAT IS DESCRIBED IN THE SERVICE LETTER AND THIS UNIT FRACTURED COMPLETELY. VISUAL INSPECTION APPEARS TO SHOW THAT THE CRACK ORIGINATED IN THE THREAD ROOT AT THE THINNEST AREA OF THE HOUSING. THE CRSDR NOCA04407Light · inoperativeE-PATH LIGHTING AT SEAT 6AB CEILING LIGHT INOP. REPLACED LIGHT AS PER MM 33-51-00.SDR HALA0600868Connector · disconnectedEMERGENCY TRACK LIGHTS FROM SEAT ROW 2H THROUGH 16H INOP. RECONNECTED CONNECTION AT LIGHT ASSY NEXT TO SEAT 2H ALL EMERGENCY LIGHTS CK GOODSDR HALA0600867Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM - FUEL TEMP DISPLAY INACCURATE. REP FUEL TEMP SENSOR IAW AMM 28-43-01-004-001-001 AND AMM 28-43-01-404-050-001 CKS GOOD.SDR 2006FA0001000Pump · crackedPART HAS CRACK IN FILTER BOWL PORT, UNIT LEAKING. (K)SDR NOCA13806Target · missingDURING TAKEOFF ROLL AT 60 KNOTS MASTER WARNING AND EICAS (MESSAGE FLAPS). ABORTED TAKEOFF AND PERFORMED LOW ENERGY STOP. PERFORMED T/O WARNING SYSTEM TEST IAW FIM 31-51-00 FIG 107, OPS CHECK. TE FLAPS IAW AMM 27-58-00 PERFORMED PSEU BITE PROCEDURE IAW FIM 32SDR NOCA12506Flashlight · inoperativeEMERGENCY FLASHLIGHT AT R4 INOP. REMOVED AND REPLACED FLASHLIGHT.SDR CA060829005Slide · no test(CAN) DURING SCHEDULED INSPECTION OF OFF-WING SLIDE COMPARTMENT DOOR LATCHES AND DISCONNECT HOUSING IAW SB 767-25A0260, BOTH OFF-WING SLIDES WERE INFLATED WITHOUT THE ASSOCIATED SLIDE COMPARTMENT DOOR BEING COMMANDED OPEN. AS A RESULT THE COMPARTMENT DOORS, SDR 2006FA0000915Cylinder · damaged(REF NR: 209609/QN1) PIN HOLE THROUGH CYLINDER WALL. PRESSURES CYCLES AND MATERIAL DEFECT. (K)SDR ANCF200600026Oil Cooler · defectiveLT ENGINE OIL TEMP HIGH 180 GRADES; IAW FIM 79-21-00 PAGE 109 FIG 104 THE BLOCKS 1,2,3 WERE ACCOMPLISHED. THE AIRCRAFT IS AOG, OIL COOLER WAS REPLACED AND ADDITIONAL CHECKS ARE BEEN ACCOMPLISHED BY TROUBLESHOOTING.SDR NOCA10706Power Supply · dischargedEXIT SIGN BY L4 AND R4 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY ASSY IAW MM 33-51-07.SDR NOCA10306Light · inoperativeEMERGENCY PATH LIGHT INOP 1GH. REPLACED LIGHT BULB, OPS NORMAL.SDR NOCA08806Light · inoperativeE-PATH LIGHTS AFT L2 DOOR, SEATS 36AB & 3AB INOP. REPLACED LENS AND RELAMPED.SDR FWT2006F00001Relay · malfunctionedAFTER 00:25 FLYING MINUTES, RETURNED TO GROUND DUE TO 1-30-32-03-01 EICAS MSG L AOA PROBE DISPLAYED. L AOA PROBE HEAT LIGHT ILLUM. 2-30-33-06-00 EICAS MSG TAT PROBE DISPLAYED, TAT PROBE HEAT LIGHT ILLUM. 3-30-31-09-00 EICAS MSG PROBE HEAT DISPLAYED 2 OR MORSDR NOCA07206Light · inoperativeE-PATH AT 2G INOP. REPLACED BULB, OPERATION NORMAL.SDR CA060516007Windscreen · failedLOCATION APPROX 30 DEGREES WEST AT FL 320 - IAS M .8 AS REPORTED BY THE FLIGHT CREW: WHILE IN CRUISE THE FLIGHT CREW NOTICED A CRACK STARTING IN THE UPPER LEFT CORNER OF THE CAPTAINS FORWARD WINDOW (NR 1) WITH IN A FEW MINUTES THE CRACK HAD SPREAD ALMOST ALL TSDR ABXA060162Flight Dir · malfunctionedALL 3 FLIGHT DIRECTORS FAILED ON DESCENT INTO MIAMI AFTER LANDING FD'S CAME BACK. A/C IN MIA FOR C-CHECK DUE OUT 5/9/06. SCHEDULED FOR MOD AT IAI ON 5/28/06, DUE OUT 10/07/06.SDR NOCA01606Battery Pack · intermittentEMERGENCY LIGHTS FROM 26AB TO 36AB INTERMITTENT.SDR 2006FA0000271Housing · cracked(203230/FXS) HOUSING CRACK AT THE PRESSURE (INLET) PORT FOR THE CHECK VALVE BORE. PROBABLE CAUSE: FATIGUE. REDESIGN HOUSING. (K)SDR NOCA0606Charger · burned outL2 DIVIDER AND ROW 10 AB THROUGH 14AB EMERGENCY LIGHT INOPERATIVE.SDR NOCA0706Fan · burned outLT RECIRCULATION FAN WRITTEN UP FOR HAVING AN ELECTRICAL BURNING SMELL, FAN WAS DEFERRED IAW MEL 21-25-01.SDR FWT2006F00000Warning System · activatedFWD EQUIPMENT OVERHEAT DISPLAYED AND OVERHEAT LIGHT REMAINED EXTIN AFTER SELECTOR WAS POSITIONED TO STBY. ABORTED TAKEOFF AT 90KNTOS. PERFORMED FIM, OPS CHECK SYSTEM FOUND GOOD AND PERFORMED AIRCRAFT INSPECTION OF HIGH ENERGY STOP ABORTED TAKEOFF IAW AMM. AISDR AU510001748Oven · faulty(AUS) NR 5 REAR GALLEY OVEN FAULTY. SMOKE AND FUMES IN CABIN. SUSPECT CAUSED BY SHORTED/BURNED OVEN FAN MOTOR. (CASA NR 510001748)SDR AU510001563Idg · failed(AUS) RT INTEGRATED DRIVE GENERATOR (IDG) FAILED. INVESTIGATION FOUND PUMP AND MOTOR ASSEMBLY CYLINDER BLOCKS WORN BEYOND LIMITS AT VARIOUS PISTON AND SLIPPER BORES. NUMEROUS OTHER COMPONENTS ALSO SEVERELY WORN. SUSPECT CAUSED BY OIL CONTAMINATION. IDG SCAVENSDR AU510002042Control Rod · separatedRT INBOARD FLAP OUTBOARD FAIRING ATTACHMENT ROD SEPARATED. INVESTIGATION FOUND THE CONTROL ROD FROM FLAP LOWER SURFACE TO THE AFT LINKAGE OF THE FAIRING HAD BECOME DETACHED AND THE LOWER BEARING HAD PULLED OUT OF THE ROD.SDR HALA0500914Line · leakingCENTER HYD QTY DROPPED TO .24 AND MAY HAVE LEAKED FROM RIGHT MAIN AREA. GROUND CONTROL REPORTED FIRE FROM 45 MAIN AREA WHICH WAS PUT OUT BY FIRE TRUCKS. FOUND PIN HOLE LEAK ON HYD LINE. REPLACED BOTH HYD FLEX LINES TO RIGHT MLG POSITIONER ACT. ACCOMP HEAT SDR PU3R200500001Piston · crackedPISTON CRACKED AT ROD END. ROD END AND PART OF PISTON ALMOST COMPLETELY SEPARATED FROM THE REST OF THE ACTUATOR.
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