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 DL764050321Battery Pack · dischargedL3 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK.SDR CALA0500118Light · inoperativeFLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACE EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01.SDR AUS20040458Pipe · worn(AUS) LT HYDRAULIC SYSTEM PIPE WORN THROUGH BY BROKEN CLAMP LOCATED IN LT PYLON. LOSS OF HYDRAULIC FLUID.SDR CA040427004Windshield · failed(CAN) DURING CRUISE, FIRST OFFICER WINDSHIELD NON STRUCTURAL OUTER PANE SHATTERED. WINDSHIELD TOTAL TIME 9,854 HRS. AIRCRAFT TOTAL TIME 50,585 HRS.SDR AUS20040210Filter · failed(AUS) NR 1 HYDRAULIC SYSTEM FILTER MODULE PRESSURE FILTER BOWL SHEARED OFF. LOSS OF HYDRAULIC FLUID.SDR AUS20040072Battery · discharged(AUS) NR 3R DOOR ESCAPE SLIDE EMERGENCY LIGHTING FAILED TO ILLUMINATE. INVESTIGATION FOUND THE BATTERY FLAT.SDR AUS20031329Receiver · failed(AUS) LT INSTRUMENT LANDING SYSTEM (ILS) RECEIVER FAILED. LT ILS CIRCUIT BREAKER TRIPPED.SDR AUS20031307Thrust Reverser · faulty(AUS) ENGINE THRUST REVERSER FAULTY. LIMITED INFORMATION PROVIDED.SDR ANCF200300029Duct · contaminatedDURING CRUISE, BOTH RECIRCULATION FANS WERE TURNED OFF FOR AIR RECIRCULATION JUST AFTER THAT A ELECTRICAL SMOKE ODOR BEGAN IN ALL THE AIRPLANE IMMEDIATELY RECIRCULATION FANS WERE TURNED ON AND ODOR DISAPPEAR. WERE CHECKED FWD APU AIR DUCTS AND CHECK VALVE APUSDR ANCF200300027Apu · leakingSMOKE ODOR THROUGH THE PASSENGER CABIN WITH NO SMOKE EVIDENCE. SMOKE DETECTORS ACTIVATED ON THE AFT AND FORWARD LAVATORIES. UTILITY BUSES WERE TURNED OFF WITH NO HELP ON THE SITUATION. LT AND RT RECIRCULATING FANS WERE TURNED OFF AS WELL AS THE RIGHT HAND. SDR AUS20031222Filter · damaged(AUS) LT HYDRAULIC FLUID DISCHARGED THROUGH DELTA (P) FITTING IN HYDRAULIC PUMP PRESSURE MODULE.SDR AUS20031134Compressor · damaged(AUS) LT ENGINE HAD SPARKS AND FLAMES WITH EGT APPROXIMATELY 50 DEGREES HIGHER THAN THE RT ENGINE. BOROSCOPE INSPECTION OF THE HPC FOUND SIGNS OF DAMAGE TO FIRST AND SECOND STAGES.SDR AUS20031028Engine · malfunctioned(AUS) RT ENGINE FAILED TO ACHIEVE TAKEOFF POWER. THRUST SHORTFALL REQUIRED WAS 1.73 BUT ONLY 1.71 WAS ACHIEVED WITH ASSOCIATED EICAS MESSAGE RT ENGINE RPM LIMIT. TAKE OFF WAS ABORTED AT 110 KNOTS GROUND SPEED.SDR AUS20030993Controller · faulty(AUS) RT ENGINE STALLED. ENGINE MOVED INTO RED ZONE (115 PERCENT N1). INVESTIGATION FOUND VIGV CONTROLLER FAULTY. LT AND RT VIGV ACTUATORS ALSO FAULTY.SDR AUS20030633Fairing · failed(AUS) RT ENGINE FAIRING FAILED. FAIRING WAS LOCATED ON THE STRUT AT THE 6 O'CLOCK POSITION. A SMALL AMOUNT OF DAMAGE WAS NOTED ON SEVERAL BLOCKER DOORS AND ONE CASCADE SEGMENT.SDR AUS20030560Wire · burned(AUS) ELECTRICAL WIRING LOCATED IN THE MEC AT THE REAR OF THE E3 PANEL ARCED AND BURNED. CAUSED BY PANEL RETAINING SCREW CHAFING ON 115 VOLT AND 28 VOLT WIRING OF THE LEFT TRU.SDR DL764030384Bulb · burned outDOOR 4R SLIDE ARM LIGHT INOPERATIVE. RELAMPED SAMESDR DL764030366Engine · stalledJUST PRIOR TO LIFT OFF ATL 27 RT, LT ENGINE COMPRESSOR STALLED REPETITIVELY ABOUT 7 TIMES BEFORE THROTTLE WAS REDUCED AF TER TAKEOFF. FLT ATTENDANTS NOTED FLAMES COMING OUT OF LEFT ENGINE WHILE THIS POPPING WAS OCCURING. N1 AND EGT FLUCUATED. TAKEOFF POWER WASSDR DL764030357Bulb · burned out2L DOOR SLIDE LIGHT INOPERATIVE AT DEPARTURE. RELAMP OPS NOW CHECKS NORMAL.SDR ANCF200200015Coupling · damagedTRANSMISSION ON BOTH HF INOPERATIVE AT ALL STATIONS.CORRECTIVE ACTION:PERFORMED FIM 23-11-00 OPERATION FOUND NORMAL ON LH HF, ON RH SYSTEM WAS REPLACED HF COUPLER AND HF TRANCEIVER AS PER AMM 23-11-03 ANS 23-11-01, ACCOMPLISHED OPERATIONAL TEST ON BOTH SYSTEM SDR AUS20020976Bolt · missing(AUS) BRAKE ROD PIN RETAINING BOLT LOCK BOLTS MISSING. AIRCRAFT ISFIJIAN REGISTERED DQ-FJC. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020625Screw · missing(AUS) BRAKE RETAINING BOLT LOCK BOLTS MISSING. AIRCRAFT IS FOREIGNREGISTERED DQ-FJC. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020531Landing Gear · failed(AUS) LT MAIN LANDING GEAR FAILED TO RETRACT.SDR AUS20020501Actuator · faulty(AUS) LT MAIN LANDING GEAR SIDE BRACE ACTUATOR FAULTY.SDR AUS20020493Oil Tank · low(AUS) APU OIL QUANTITY LOW. NO EVIDENCE OF ANY LEAKS. TWO LITRES ADDED TO TOP UP THE OIL.SDR CALA0200073Power Supply · dischargedINSPECTION FOUND RT OVERWING EXIT DOOR EMERGENCY LIGHTS AND LAST THREE CENTER SEAT LIGHTS IN FIRST CLASS AISLE INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-07 AND OPERATION CHECKED GOOD.SDR ZW0A0111301Lamp · missingTHE EGRESS LIGHT AT CABIN SEAT 33B WAS MISSING. INSTALLED LAMP ASSEMBLY.SDR AUS20011171Apu · failed(AUS) APU FAILED TO START.SDR AUS20011100Apu · failed(AUS) APU SHUTDOWN.SDR ZW0A0107504Light · inoperativeTHE OUTSIDE EMERGENCY LIGHT AT THE RH SIDE NUMBER 2 CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP.SDR AUS20010912Spring · missing(AUS) NOSE LANDING GEAR OVERCENTRE LOCK SPRING MISSING.SDR AUS20010502Panel · separated(AUS) RH ENGINE BULLNOSE SECTION LOCATED AFT OF THE ACOUSTIC PANELMISSING FROM AREA BETWEEN NO4 AND NO7 BLOCKER DOORS. THE MISSINGPIECE WAS APPROXIMATELY 2 METERS (6FT) IN LENGTH. DAMAGE CAUSED TO THREE BLOCKER DOORS, COMBUSTOR FAIRING AND BLISTER FAIRING.SDR AUS20010478Extinguisher · damaged(AUS) FIRE EXTINGUISHERS LOCATED IN THE MID CABIN LT AND RT TOILETS AND AFT CABIN RT TOILET HAD IMPACT DAMAGE TO THE FUSEABLE TIP AREA. FOUND DURING INSPECTION IAW 767-A2-25-006.SDR AUS20010473Fairing · missing(AUS) NR 2 ENGINE LT A' FRAME TO FAN CASE AFT LOWER FAIRING MISSING.SDR DL764010612Actuator · malfunctionedTE FLAP DISAGREE ON TAKEOFF. FLAPS STOPPED RETRACTING AT 10DEG. FLAPS EXTENDED TO 20 DEG. WITH ALTN FLAPS SYSTEM. FOUND ROTARY ACTUATOR BRAKE TRIPPED ON RT OUTBOARD FLAP GEAR BOX ROTARY FLAP ACTUATOR ON INBOARD SIDE TRIPPED. REPLACED ROTARY ACTUATOR MFR. NBSDR 20010409CW008Connector · damagedDURING DISASSEMBLY OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNED AND IN SOME CASES COMPLETELY DETACHED FROM THE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED.SDR 20010409CW007Connector · damagedDURING DISASSEMBLIES OF 11 YAW DAMPNER ASSEMBLIES, FOUND ELECTRICAL CONNECTOR PINS FOR THE HYDRAULIC SOLENOID VALVE BURNED AND IN SOME CASES COMPLETELY DETACHED FROMTHE WIRE WITH THE CONNECTOR DAMAGED IN 5 OF THE 11 UNITS REPAIRED.SDR DL764010400Socket · corrodedDURING PRE-DEPARTURE CHECK FOUND LT OVERWING EXTERIOR EXIT EMERGENCY LIGHT BULB INOP. REPLACED BULB AND BULB HOLDER. OPS NORMAL. USED SPARE BULB HOLDER. BULB HOLDER AND BULB HAD CORROSION RENDERING LIGHT INOP.SDR DL764010072Lens · brokenEMERGENCY LIGHT LENS AT SEAT 44B BROKEN. REPLACED E-PATH LIGHT LENS LIGHT, OP CK GOOD. CAPT VERBAL REPRT ITEM FOUND BY FAA INSPTR.SDR 20010126CW006Housing · crackedHOUSING IS CRACKED BELOW THE RETRACT PORT. PROBABLE CAUSE: STRESS AND OR FATIGUE.SDR ANCF200000002Controller · malfunctionedDURING CRUISE, LT ENGINE BLEED OFF DISPLAYED AND ENGINE BLEED AIR VALVE OFF LIGHT ILLUMINATED, WITH SWITCH ON. DUCT PRESS WAS ZERO PSI, NACELLE ANTI-ICE OPERATION NOT CHECKED. DURING GROUND CHECK FAIL HPSOV AND EICAS MESSAGE. IAW AMM 36-11-07 PAGE 401, THE SDR 20001107SH019Sensor · inaccurateANGLE OF ATTACK SENSOR P/N 861CAB, CHANNEL 2, SET UP WRONG. UNITS FITTED TO BOEING 757/767. A DEFECT HAS BEEN FOUND IN WORKSHOP TEST EQUIP THAT ALLOWED UNITS TO BE RETURNED TO SERVICE WITH CHANNEL 2 SET UP WITH A 180 DEGREE ERROR. AN OPERATOR RETURNED 2 ANGSDR CA000519002Computer · faulty(CAN) LEFT EICAS COMPUTER PLUS LOSS OF FUEL USED AND CALCULAED FUEL. CB RESET AND PARTIAL INFO RETURNED. A/C DIVERTED FOR COMPUTER REPLACEMENT. LT EICAS COMPUTER REPLACED.SDR 20000608SH006Housing · crackedBODY IS CRACKED ALONG THE UP, DOWN, AND CLOSED PORTS. POSSIBLE CAUSE: FATIGUE, OVERSTRESSED AND/OR HIGH TIME ON UNIT. (X)SDR 20000505SH003Armature · failedTHIS PART WAS REPAIRED AND RETURNED TO SERVICE 6-3-99 WITH NO TIME IN SERVICE SINCE THAT DATE. INSTALLED ARMATURE IN MOTOR AND CONDUCTED TESTING PER OHM 24-09-02. MOTOR FAILED TESTING. UPON DISASSEMBLY, DISCOVERED THE COMMUTATOR IN THE CONDITION SHOWN IN THSDR 2000ZZZX495Reel · damagedPHONE REEL MELTED.SDR 98ZZZX4725Skin · delaminatedELEVATOR RECEIVED FOR WORK. UPON PRELIMINARY WORK, DISCOVERED THAT A PORTION OF THE UPPER SKIN IN THE INBOARD END AT THE SPAR WAS DELAMINATED EXPOSING THE PEEL PLY STILL ATTACHED. DISPOSTION PENDING.SDR 98ZZZX3581Filter · failedMALFUNCTION WAS CAUSED BY THE FAILURE OF AN EMI FILTER CAPACITOR. A SB WAS ISSUED TO CHANGE OLD STYLE FILTER TO THE NEW REPLACEMENT MODEL. SUBMITTER STATED THIS INCIDENT IS THE THIRD KNOWN INCIDENT OF OVER 4,500 UNITS IN OPERATION.SDR 98ZZZX3682Case · damagedDURING CLIMB FROM MIAMI, THE ENGINE (POS NR 1) EXPERIENCED TWO SURGES WITH EGT EXCEEDING 796 DEGREES CELSIUS FOR 15 SECONDS. AN IN-FLIGHT SHUT DOWN AND AIR TURN BANK EFFECTED. DISASSEMBLY INSPECTION AT PWORC REVEALS 360 DEGREE FAILURE OF THE HPT CASE WALL APSDR AU980822Radome · mismanufactured(AUS) RADOME FAILED TO MEET THE REQUIREMENTS OF RTCA/00-213 FOR A CLASS B RADOME. (TRANSMISSION EFFICIENCY).
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