Boeing 767-383
Service difficulty reports · 647
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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 = '767383' 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 = '767383' 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 RYNA201204240020Connector · looseEMERGENCY FLOOR LIGHTING INOP BETWEEN ROWS 17-22 ON THE LEFT SIDE. FOUND SEVERAL CONNECTIONS THAT WERE LOOSE. RE-ATTACHED CONNECTIONS PER SWPM 20-60-00. OPS CHECK NORMAL.SDR ABXA20120128159Handle · lack of lube52 71 X1 01 L FWD ENTRY DOOR ARMING HANDLE REQUIRED EXTERNAL HANDLE TO BE PUSHED FLUSH TO ARM. LUBRICATED AND OPS CHECK DOOR IAW B767 AMM 52 11 00, OPS CHECK GOOD AT THIS TIME, AWG.SDR RYNA201201020001Light · brokenDURING TAXI WHILE BEING MARSHALLED IN AT YQB THE RIGHT WING TIP CONTACTED LIGHT (UTILITY) POLE. REMOVED FORWARD RIGHT WING POSITION LIGHT, INSPECTED FOR FURTHER DAMAGE IAW AMM 05-51-59. NO FURTHER DAMAGE NOTED. REMOVED AND REPLACED RIGHT FORWARD WING POSITISDR ABXA20110929108Stiffener · crackedNOSE WHEEL WELL STIFFENER BS 287 LBL 25 IS CRACKED. CUT & REMOVED PORTION OF EXTRUSION. FABRICATED REPAIR PLATES. REPAIRED DAMAGE IAW SRM 51-70-12 FIG 1.SDR ABXA20110929109Stiffener · crackedNOSE WHEEL WELL CHORD STA 287 RBL 25 IS CRACKED. REPAIRED NOSE WHEEL WELL CHORD STA 287 RBL 25 IAW B767 SRM 51-70-12 FIG 1 AWG.SDR RYNA2011040400011Slide · unwanted deployRT OVERWING SLIDE BLOWN. INSTALLED SERVICEABLE SLIDE ASSEMBLY IAW AMM 25-65-05.SDR 2011FA0000003Charger · failedRT WING SLIDE EMERGENCY LIGHT L391 INOP. R & R POWER SUPPLY BATTERY CHARGER.SDR ANCF2010101000070Pdu · out of adjustEICAS STATUS MESSAGE FLAP/SLAT ELEC. IN ACCORDANCE WITH AMM 27-81-11 PAGE 401 THE SLAT OUTBOARD POS NR 2 MS48 WAS CHECKED BY RIGGING VALVE FOUND IN 8,67V, IN ADDITION IAW AMM 27-51-00 PAGE 201 THE OPERATIONAL TEST OF FLAP /SLAT SYSTEM WAS PERFORMED CHECK AND SDR RYNA2010007020019Unknown · malfunctionedAFTER TAKEOFF, FORWARD EQUIPMENT OVERHEAT. RAN FIM 21-58-00 FIG 115. ITEMS 1-3-4-12-25 MESSAGES CLEARED AIR-FLOW RE-ESTABLISHED, SYSTEM OPERATES NORMAL. OK FOR SERVICE AMM 21-51-17-401.SDR RYNA2010006020015Wire Harness · disconnectedTHREE (3) LEFT MOST FORWARD EMERGENCY FLOOR LIGHTS INOPERABLE. FOUND WIRING DISCONNECTED AT 3RD LEFT LIGHT ASSEMBLY, RECONNECTED WIRING. OPS CHECK OK. REFERENCE AMM 33-51-10.SDR RYNA2010005210013Idg · failedRT ENGINE GEN DRIVE LIGHT GAME ON IN FLIGHT. REMOVED AND REPLACED RT ENG IDG PER MM 24-11-01, GEN RUN OPS CHECK GOOD.SDR RYNA2010005210012Wire · looseEXTERNAL EMERGENCY LIGHT AT R4 DOOR AND RT FUSELAGE AFT OF WING INOP. EMERGENCY FLOOR LIGHTS LT SIDE ROWS 7-19 NOT WORKING. CONNECTOR LOOSE WIRE AT LT ROW 9 FLOOR LIGHT ASSY & EMERGENCY LIGHT OPS CHECK GOOD PER MM 33-51-00. RELAMPED R4 DOOR SLIDE LIGHT AND SDR RYNA2010004010011Battery Pack · dischargedFLOOR EMERGENCY LIGHT IN ON RIGHT SIDE FROM ROW 8-15 ON LEFT SIDE FROM ROW 1-15. REMOVED AND REPLACED BATTERY AND CHARGER ON RIGHT SIDE ADDITIONALLY FOUND LOOSE WIRE ON LEFT SIDE.SDR RYNA2010003260007Light · saturatedEXTERIOR EMERGENCY LIGHTS AT AFT RT ENTRY DOOR FILLED WITH WATER. DRAINED WATER CLEANED AND SEALED LIGHT LENS EMERGENCY LIGHT TEST GOOD PER AMM 33-50-00.SDR RYNA201000325006Wire · brokenDURING INSPECTION AND TESTING OF THE EMERGENCY LIGHTING SYSTEM THE RT SIDE OF THE CABIN THE EMERGENCY LIGHTS BETWEEN SEAT ROWS 10H/J AND 32H/J WERE NOTED TO BE INOPERATIVE. REPAIRED BROKEN WIRE AND SHORTED PINS AT SEAT ROWS 20J/H CROSS AISLE AND REPLACED ASSOSDR ANCF2009071600051Connector · dirtyGROUND TURNBACK. PILOT REPORT: DURING ENG START AFTER IDG OR GENERATOR STABILIZER EICAS MSG L ENG, FUEL VAL AND ENG VALVE LIGHT ILLUM WITH FUEL CONTROL SWITCH IN RUN POSITION ENG SHUTS DOWN BY ITSELF. CLEANED CONNECTOR TO THE LEFT ENG FUEL SHUT OFF VALVE. SDR ANCF200800022Drive Assy · intermittentAIR TURN BACK DUE REPORT: "WXR FAIL DISPLAYED ON HSI WITH 02=R SYSTEM SELECTED. WXR FAIL ANTENNA ON HSI. NOTE: PREVIOUSLY REPORTED ON FLIGHT 020 OF 8/30/2008. SWEEP (GHOST IMAGE WITH) ON HSI, WEATHER DISPLAY WITH 03=R BOTH SYSTEM SELECTED. NOTE: PREVIOUSLY REPSDR ANCF200700009Contactor · failedAPU FAILED TO START FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED, ADDITIONAL START ATTEMPTS UN SUCCESFULL. VISUALLY SMOKE WAS DETECTED IN THE APU AREA AND APU FIRE EXTINGUISHER SYSTEM WAS USED. IN ACCORDANCE WITH WDM 49-41-11 PAGE 1 THE WIRES W020-0SDR ANCF200600049Window · damagedWITH HANDLE POSITION HANDLE CLOSED, (LATCH HANDLE) OPERATING CRANK IN CLOSED POSITION AND WINDOW INDICATOR CLOSED, FO`S WINDOW WENT OPEN ON THE BACK OF WINDOW, JUST AFTER TAKEOFF, IAW AMM 56-11-02 PAGE 401 THE RT WINDOW WAS REMOVED AND REPLACED.SDR NOCA21406Spring · corrodedLEFT WING INBOARD AILERON OUTBOARD DROOP QUADRANT SPRINGS ARE CORRORED INTERNALLY. REMOVED AND REPLACED SPRINGS, RIGGED SPRINGS PER AMM 27-11-38-404-046. INSTALLED QUADRANT PER AMM, RIGGED CHECKED GOOD, OPS CHECKED GOOD.SDR ANCF200600036Engine · flamed outLT ENG SHUTDOWN, RESTARTING NOT ATTEMPTED DUE TO HIGH EGT (652 DEGREES) HIGH VIBRATION AND NO OIL PRESS, AIRPLANE WAS ON CRZ AT 36000 WITH SPEED MACH 0.79. NO APPARENT REASON FOR FLAMEOUT. WAS PERFORMED VISUAL AND BOROSCOPE INSPECTION AND CHECK, THE DIGITAL FSDR ANCF200600029Warning Message · illuminatedAFTER TAKEOFF, EICAS MESSAGE (FWD CGO EX VALS) DISPLAYED. NORMAL PRESURIZATION. WITHOUT PILOT REPORTS, THIS ITEM WAS DIFFERED PREVIOUSLY TO DMI 227; IAW MEL 21-28-1. THAT EVENT HAS NOT ADITTIONAL MAINTENENCE ACTIONS.SDR ANCF200600027Outflow Valve · failedFWD CRGO GDD EX VALS DISPLAYED AFTER T/O AIRPLANE DID NOT NOT PRESSURIZE. SEE DMI 227 IAW MEL 21-28-1 PREVIOUSLY OPENED. MEL PROCEDURE WAS ACCOMPLISHED DEACTIVATING BACKUP VALVE.SDR CA051125007Coffeemaker · burned(CAN) FAULT: IN CRZ VENTRE GALLEY COFFEE MAKER GAVE A FLASH AND ASH DEPOSITED ALL AROUND, ELECTRIC FUMES SMELT BY F/AS, ALL CB'S IN AREA PULLED UNTIL BUSSES DEPOWERED. DIVERTED YYT FOR MTCE/SAFETY CHECK. FOUND LOWER C/M MID GALLEY HEATING ELEMENT INSULATION BSDR CA051111002Radio · intermittent(CAN) FAULT: WHEN ATTEMPTING TO TUNE NR 1 HF (LT) STRONG ACRID ODOR/HEATING SMELL RT HF INTERMITTENT FOR TRANSMITTING BOTH HF'S SELECTED OFF C/B'S FOR BOTH HF'S PULLED SMELL DISSIPATED FLT OP ADVISED ACTION: LT HF T/R REPLACED IAW AMM 23-11-03-406 RT HF T/R RSDR ANCF200400013Controller · malfunctionedEICAS MESSAGE. LT ENGINE BLEED OFF AND BLEED LIGHT ILLUMINATED. REMOVED AND REPLACED TEMP SENSOR FAN MODULATING VALVE. IAW AMM 36-11-17 PG 401 TEST SATISFACTORY. CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATE EICAS MSG CABIN ALTITUDE WAS UNABLE TO RESTORE. SDR ANCF200400012Shutoff Valve · failedDURING WING AND ENGINE ANTI-ICING USE CABIN CONTROL WITH AUTO 1 SELECTED, WITH 7.0 UNITS OF DIFFERENT TO LAND, 9500 OF ALTITUDE WITH STRONG PRESSURIZATION SURGE. THIS CONDITION WAS PRESENTED AT 35.000 FT WITH CABIN 2 SELECTED INDICATIONS WERE NORMAL. WAS REMOSDR 200300286Attach Fitting · brokenLEFT WING OUTBOARD T/E FLAP, OUTBOARD FLAP TRACK SUPPORT ATTACH FITTING BROKEN OFF AT REAR WING SPAR.SDR AUS20030701Line · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP CASE DRAIN LINE LEAKING. LOSS OF HYDRAULIC FLUID.SDR ANCF200300018Pin · bentPILOT REPORT: DURING FLIGHT WAS PRESENTED ENTRY DOORS LIGHT ILLUMINATED STEADY AND EICAS MSG. RT AFT ENTRY DOOR DISPLAYED STEADY. LOCK PIN ENGAGED. FLIGHT RETURNED. AFT ENTRY SERVICE DOOR LATCH PIN WAS FOUND BENT AND IT WAS REPLACED IAW AMM 521115 PAGE 401 SDR ANCF200300015Switch · malfunctionedLT PACK INOPERATIVE, LIGHT ILLUM. EICAS MSG L PACK TEMP DISPLAYED. LIGHT DID NOT EXTIN WHEN STBY SELECTED AND RESET PUSHED. AIRCRAFT RETURNED. LT PACK TEMPERATURE CONTROL (PTC) BITE PROCEDURE WAS PERFORMED IAW FIM 21-51-00 FIG 103, COMPRESSOR OUTLET OVERHEASDR ANCF200300012Heat Exchanger · contaminatedCABIN ALT & CABIN ALT LIGHTS ILLUM, EICAS MESSAGE CABIN ALTITUDE WAS DISPLAYED. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE, O2 MASKS DEPLOYED. ALSO WAS PRESENTED EICAS MSG FWD CARGO A/C AND FWD CARGO A/C INOP LIGHT ILLUM WHEN THE FLT ARRIVED LT PACK WAS SDR ANCF200300010Controller · malfunctionedDURING FLIGHT APPEARED: "LT PACK INOP IN AUTO AND STANDBY", EICAS MSG "R ENG HPSOV" AND "R ENG BLEED LIGHT". FLIGHT RETURNED TO BOGOTA. LT PACK TEMPERATURE CONTROLLER AND HPSOV CONTROLLER WERE REPLACED IN ACCORDING WITH AMM 21-51-14 PAG 401 AND AMM 36-11-08 SDR CA030313005Fan · failed(CAN) SMOKE IN COCKPIT, DISSAPATED AFTER LANDING WITH A STATUS MESSAGE 'FWD EQ EXH FAN' AND FOUND C/B H21 LWR EQUIPEMENT PANEL 'FWD EXH EQUIP COOL FAN' POPPEDSDR CA030304003Cooling Fan · failed(CAN) SMOKE IN COCKPIT . STOPPED AFTER 20 SECS. AFTER LANDING IN ANC STATUS MSG. 'FWD EQ EXH FAN' AND C/B H21 LWR EQUIP PANEL 'FWD EXH EQUIP COOL FAN ' TRIPPED.FWD EQUIPMENT COOLING FAN REPLACED AS PER AMMSDR ANCF200300003Windshield · crackedDURING FLIGHT WAS FOUND 1L WINDOW CRACKED (windshield outer panel). AIRCRAFT RETURNED TO BOGOTACORRECTIVE ACTION:1L WINDOW WAS REPLACED IN ACCORDING TO AMM 56-11-01 PAG 401 TO 411, AND WINDOW HEATING SYSTEM CHECKED IAW AMM-30-41-00/501 WITH SATISFACTORY RESULTSDR ANCF200300002Outflow Valve · inoperativeDURING CLIMB THROUGH 35000 FT, MASTER WARNING AND CABIN ALTITUDE ALARM WERE PRESENTED; EMERGENCY DESCENT WAS STARTED TO 21000 FT. CHECK LIST WAS PERFORMED. DURING MANUAL TEST PROCEDURE IAW AMM 21-31-00 PAGE 507 WAS FOUND THAT OUTFLOW VALVE WAS NOT WORKING WHSDR CA020801001Actuator · binding(CAN) SPOILER LEVER FEELS TO HAVE MORE TENSION (BINDING) WHEN DEPLOYING AND RETRACTING. REPLACED SPEEDBRAKE MECHANISM AND TESTED PER AMM 27-62-04-002-114SDR ANCF200200013Outflow Valve · failedAT FL 350 CABIN ALT ALERT PRESENTED ON EICAS, CABIN ALTITUDE MODE SELECTED SWITCHED TO AUTO 1, CABIN CONTINUED DESPRESSURIZING, THEN SWITCHED TO MANUAL, VALVE CLOSED MANUALLY, CABIN CONTINUED CLIMBING AND REACHED 11000 FT, THEN WE DESCENT TO 12000 FT AND CABINSDR ANCF200200007Line · leakingDURING FLIGHT RT HYDRAULIC QUANTITY DECREASED FROM 1.03 TO ZERO, QUANTITY STABLE WITH EDP DEPRESSURIZED AND AC PUMP OFF. RT HYDRAULIC QUANTITY READS ZERO. DURING MAINTENANCE INSPECTION WAS FOUND HYDRAULIC LEAK FROM RT AC PUMP PRESSURE. LINE., ADJUSTED PRESSURSDR CA020502012Control Unit · failed(CAN) FLAP DISAGREE MESSAGE ON EICAS WHEN FLAP SELECTED TO RETRACT FROM 5 DEGREE TO 1 DEGREE ON TAKEOFF. ALTERNATE TE FLAP EXTENSION USED FOR LANDING. FOUND TO BE THE FSEU AT FAULT (FLAP SLAT CONTROL UNIT). REPLACED ELECT FLAP SLAT UNIT.SDR CA991007018Light · failed(CAN) NO INDICATION OF NOSE GEAR DOWN. REPLACED LAMPS, STILL U/S. FLY-BY CONFIRMED GEAR DOWN. NOSE GEAR LIGHT CONTACTS CLAEANED AND BULB REPLACED.SDR 98ZZZX4715Line · failedSKBO/KJFK - FLT 020 - DURING FLIGHT, RT HYDRAULIC SYSTEM WAS LOST. PILOTS REPORTED: 'RT HYD QTY READS ZERO. HYD QTY LIGHT ILLUMINATED AND EICAS MESSAGE DISPLAYED RT HYD QTY'. FOUND EDP PRESSURE LINE IN RT PYLON BROKEN. REPLACED PRESSURE LINE. ALSO CHANGESDR 99ZZZX657Controller · malfunctionedJFK/BOG - FLT 021 - EICAS MESSAGE. LEFT ENGINE, HPSOV DISPLAYED LEFT ENGINE BLEED LGT ILLUMINATED STEADY AT HIGH THRUST. DUCT PRESSURE NOT CHECKED. TAKEOFF WAS REJECTED AT 90 KNOTS. PERFORMED TROUBLESHOOTING ACCORDING TO 36-10-00 PG 127. HI PRESS VALVE FASDR ANCF9600002Door · unlockedAIR RETURN: DURING FLIGHT FROM SKGT TO SKBO AT 28,000 FEET, FWD ENTRY DOOR LIGHT ILLUMINATED WITH EICAS MESSAGE. FLIGHT ATTENDANT REPORTED THE DOOR HANDLE COMING OUT OF LOCKED POSITION AND STRONG NOISE. CABIN ALTITUDE INCREASED RAPIDLY, BUT WAS CONTROLLED ISDR ANCF9600001Brake · overheatedFLT 014 BOG-PAR. DURING T/O ROLL AFTER PASSING 80 KNOTS, THE BRAKE TEMP LIGHT CAME ON. WAS NECESSRY TO MAKE A REJECTED T/O. INSPECTION ACCOMPLISHED ACCORDING MM 32-42800. ALL NORMAL. TIRES NRS 1, 2, 6, 7, AND 8 WERE CHANGED. (X)SDR 96ZZZX2748Switch · malfunctionAFTER 7:15 HOURS FLY-TIME FROM GOB TO CDG, EICAS MESSAGE FOR LEFT ENGINE OIL FILTER CAME ON. MESSAGE REMAINED WHEN THRUST REDUCED. ENGINE SHUT DOWN. UNSCHEDULED LANDING MADE. INSPECTED LT ENGINE OIL CHIP DETECTOR AND OIL TANK AND GEARBOX FOUND NORMAL. REM
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