Boeing 767-322
Service difficulty reports · 11,768
Newest first. General aviation reporting is voluntary.
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 = '767322' 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 = '767322' 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 UALA2010020100413Cable · damagedAPU GEN WILL NOT STAY ON LINE. FIELD LIGHT FOR APU GEN LIGHT ON P-61 TRIED MANY TIMES TO RESET, NO JOY. TRIED NEW GCU, NO HELP. FOUND GEN FEEDER CABLES BROKEN AT LUG T2 TERM BLOCK, STUDS ON GEN LOOSE, MAY NEED TO REPLACE 4 LUGS FOR GEN FEEDER CABLES. PULLED SDR UALA2010020100414Connector · burnedCTR HYD PUMP NR1 EICAS MESSAGE AND LOW PRESSURE LIGHT ON WITH MOVEMENT OF FLAPS AND FLIGHT CONTROL MESSAGE. FOUND BURNED SOCKET ON CONNECTOR D482. CONTACT POSITION IS C. REPLACED CONNECTOR D482 IAW WDM. R & R PUMP DUE TO BURNED PIN ON MAIN AC CONNECTOR, LEAK CSDR UALA2010020100398Pressure Switch · unknownPUMP OFF AND LP LGT ON BUT NO EICAS MSG. TRIED S72 PRESSURE SWITCH NO HELP, TRIED OVERHEAD PANEL, NO HELP, REPLACED K190 CONTROL RELAY NO HELP. ISOLATED CIRCUIT BETWEEN S5 TO S72 & BOTH EICAS CMPTS, WIRES CHKS OK. REF FIM 28-22-00 FIG 111 BOX 2, 28VDC PRESENTSDR UALA2010020100383Circuit Card · malfunctionedIDLE DISAGREE EICAS LTN1 30 PERCENT RT 38 PERCENT N1 EQUAL W/ENG AI ON. INTEGRATED BOTH LT-RT PIMUS, IDENTIFIED LEFT ENGINE NUMEROUS FAULTS. REPLACED LT ENGINE SPEED CARD IAW MM. GRD TEST CARD OK.SDR UALA2010020100407Pump · overheatedRT EDP HYD PUMP 'OVHT' LIGHT ILLUMINATED WITH ASSOCIATED STATUS MSG. DISPLAY ELEC- HYD PG AND NOTICED A STEADY RISE IN RT HYD TEMP. REPLACED EDP AND REPLACED PRESSURE FILTER. PERFORMED LEAK CHECK ALL OK. RAN ENG AND ALL INDICATIONS GOOD.SDR UALA2010012800360Wire Harness · burnedFWD CARGO LOADING SYS INOP. WHILE ID PARTS, RESET SYS CB & SEVERAL BREAKERS POPPED. OPENED FLOOR PANEL TO INSP FOUND BURNED INSULATION & WIRE BUNDLE. STARTED REPAIR TO WIRE BUNDLE. WIRES REPLACED, TEMPORARILY MARKED NR S50 TO NR 59 & PULLED TIED TOGETHER ASDR UALA2010012800343Shutoff Valve · malfunctioned1 SPAR VALVE LIGHT REMAINED ILLUMINTATED WITH FUEL CONTROL SWITCH SELECTED (CUTOFF, RICH, RUN). EICAS MSG (L,R) SPAR VALVE DISPLAYED. POS(01=L,02=R) AFTER LT ENGINE START SPAR VALVE AND FUEL VALVE LIGHT ILLUMINATED ENGINE SHUTDOWN. REPLACED NR1 ENG FUEL SHUSDR UALA2010012600321Actuator · leakingFUEL LEAKING FROM LT WING FUEL JETTISON TUBE AFTER FUELING OF AC. ACTUATOR FOUND LEAKING. REPLACED FUEL JETTISON VALVE ACTUATOR. OPS CHKS ARE NORMAL. FOUND GAMA COUPLING DOWNSTREAM OF JETTISON VALVE LEAKING WHEN WING TANK WAS FULL. REPLACED PACKINGS ON COSDR UALA2010012500312Indicator · faultySTATUS MSG FLAP-SLAT ELEC WHEN FLAPS SELECTED TO 5 ON TAXI. REPLACED FLAP INDICATOR. RAN FLAPS THROUGH CYCLE. OPS NOW SATISFACTORY. MESSAGE CLEARED. NEED TO ACCOMPLISH BIT TEST ON FSEU IAW MM. NO FAULTS ON BITE, REPLACED FSEU.SDR UALA2010012500307Battery · faultyAPU WILL NOT START. HANGS AT 40 PERCENT THEN SHUTS DOWN WITH FAULT LT 777 EGT. REPLACED APU BATTERY AND APU DOOR ACTUATOR IAW MM, OPS CHECKED GOOD.SDR UALA2010012500284Light · missingSEAT 1B FWD EMERGENCY LIGHT MISSING. REPLACED SEAT 1B EMERGENCY LIGHT STRIP. CHECKS OK.SDR UALA2010012500308Controller · faultyBOTH PACKS CYCLE FROM 0 TO 110 DEGREES APPROX EVERY 30 MIN WITH PACK OPERATED INDIVIDUALLY AND BOTH SAME TIME, RESPONSE BEFORE PACK TEMP STABILIZED WERE BETWEEN 20 TO 30 MINS. REPLACED ZONE TEMP CONTROLLER. AFTER ZONE TEMP CONTROLLER CHG RAN BOTH PACKS, PACKS SDR UALA2010012200267Window · unknownCAPTAIN REPORTED JUST AFTER LIGHTNING STRIKE, ODOR OF BURNING ELECTRICAL WAS PRESENT IN COCKPIT. CHECK WINDOW HEAT WIRING AROUND CAPTAINS WINDSHIELD FOR EVIDENCE OF OVERHEATING WHEN WINDOW IS REMOVED. DOES NOT PASS WINDOW HEAT CHECK PER MM. REMOVED WINDOW.SDR UALA2010012200273Structure · damagedRT WING LE STA ISS 308 HAS DAMAGE. CRACKS STOP DRILLED. VERIFIED NO CRACKS BEYOND STOP DRILL. REMOVED CRACKED SECTION AND REPAIRED IAW DWG. ACCOMPLISHED INSPECTION OF REPAIR INSTALLATION IN COMPLIANCE WITH DWG. OK IAW INSPECTOR SIGN OFF.SDR UALA2010012100261Circuit Breaker · trippedAPU INOP ACCT FIRE DISCHARGE LIGHT ILLUMINATED. THIS CONDITION INDICATES A BAD PRESSURE SWITCH AND THE APU FIRE EXTINGUISHER BOTTLE SHOULD BE REPLACED. REPLACED BOTTLE ASSY, NO HELP. CREW REPORTS CB C796 APU REMOTE FIRE INDICATOR CIRCUIT BREAKER POPPED. PULSDR UALA2010012000246Unknown · odorELECTRICAL SMOKE ODOR INTERMITTENT AROUND SEATS 21H&J. TURNED OFF L&R RECIRC FANS. FIXED IT. ACP VISUAL AND ODOR CHECK OF AREAS. REMOVED CEILING PANELS NEAR AREA AND CHECK E/E DOOR HEATER FOR EXCESSIVE HEAT. NO EVIDENCE OF ODOR OR BURNED WIRING. TALKED TO CRSDR UALA2010012000244Shutoff Valve · malfunctionedRT ENG BLEED OFF EICAS AFTER ENG START. VALVE FOUND INADEQUATE. REPLACED PRSOV AND RAN ENG, OPS CHECKED NORMAL.SDR UALA2010011900236Shutoff Valve · malfunctionedR-HPSOV MSG DISPLAYED ON EICAS. LAX REPORTS BITE FAULTED RT HPSOV & PRESS SENSOR. REPLACED RT HPSOV, ENG NEEDS TO BE RUN AT HIGHER POWER SETTING DUE TO EICAS MSG ON TAKEOFF ROLL.SDR UALA2010011800226Actuator · faultyNEED TO DISC NR 7 SLAT INBD CONTROL ROD TO FACILITATE MAN MOVEMENT OF SLAT TO CK FOR FREEDOM OF MOVEMENT, PRIOR TO ROTARY ACTUATOR & G-BOX REPLACEMENT. DISC SLAT DRIVE CONTROL RODS, MANUALLY MOVED SLAT, THEN RECONNECTED AND MOVED SLAT MANUALLY WITH TORQUE TUBSDR UALA2010011900228Light · unsecureSEAT 6H EMERGENCY LIGHT HANGING LOOSE. SECURED SEAT EMERGENCY EXIT LIGHTING. LIGHT OPERATES NORMAL.SDR UALA2010011800224Unknown · odorHEAVY RUBBER ODOR IN AFT CABIN NEAR SEAT 25 & AFT. TURNED OFF BOTH UTILITY ON SHORT FINAL. IAW CAPTAIN THE BURNED ODOR WAS NOTICED ON THE FLIGHT DECK. IAW THE F/A THE ODOR WAS ON THE RT SIDE OF THE CABIN AND DISSIPATED AFTER CAPTAIN TURNED OFF THE UTILITY BUSSDR UALA2010011800210Priority Valve · faultyRIGHT ENG PRV VALVE EICAS ON TAXI IN. UNABLE TO RUN ENGINE IN KOA. LOCKED OUT PRV VALVE. REPLACED RT ENG PRV.SDR UALA2010011900238Controller · faultyFLT DECK TEMP CONTROL FAILED TO CONTROL DESIRED TEMP IN 'AUTO' OR 'MAN'. CREW COMMENTS: FLT DECK IS IN FULL HOT MANUAL & IT IS JUST BARELY COMFORTABLE. REPLACED FLIGHT COMPARTMENT TRIM MODULATING VALVE. DID NOT FIX PROBLEM. VALVE SHOWS FULL HOT, WITH COLD AIRSDR UALA2010011900237Static Inverter · malfunctionedFLIGHT CREW REPORTS STANDBY INVERTER MESSAGE DISPLAYED. MSG IS INTERMITTANT, REPLACED STATIC INVERTER. ACCMP'D OP CK PASSED.SDR UALA2010011800207Transmitter · faultyFLAP-SLAT ELEC LIGHT INTERMITTENT ON TAXI IN. UNABLE TO VERIFY THE PROBLEMS, REPLACED FSEU AS PRECAUTION AND SYS CHECKED NORMAL. PROBLEM RECURRED. ACCOMPLISHED BITE ON FSEU AND HAD M489 FAULT. RPLC'D NR 8 FLAP POSITION TRANSMITTER. SYS CHECKS OK AT THE PRSDR UALA2010011500199Module · leakingHYD LEAK RT MLG W/W FROM BOTTOM OF FLAP SLAT HYD S/O VLV MODULE. REPLACED MODULE. OPS AND LEAK CK GOOD. REPLACED MODULE. OPS AND LEAK CHECKED GOOD.SDR UALA2010011500197Transmitter · faultyNR 2 ENG HIGHER FUEL FLOW. CREW REPORTS RT TANK IS FEEDING RT ENG WITH 17K IN CTR TANK. CTR TANK QTY 40K LT, 36.7K RT POSS CTR BOOST PUMP. TROUBLESHOOTING. REPLACED THE NR 2 ENGINE FUEL FLOW TRANSMITTER. REPLACED RT AUX OVERRIDE PUMP. WITH CTR PUMPS ON FUELSDR UALA2010011500189Switch · faultedLT ENG FUEL FILTER EICAS, RTFL. REPLACED FILTER AND FUEL DIFFERENTIAL PRESSURE SWITCH RAN ENG, LEAK AND OPS CKS OK.SDR UALA2010011500196Line · leakingNR 2 ENG FUEL OIL COOLER LINE LEAKING. FOUND A COMBINATION FLEX HARD LINE LEAKING FROM FUEL OIL COOLER, PART AOG'D J3857, LINE IN HAND. LEAK APPEARED TO BE ON THE FLEX PART OF THE LINE APPROX 6 INCHES FROM THE FUEL PUMP CONNECTION. R & R FUEL PUMP INLET TUBSDR UALA2010011500188Pressure Switch · damagedFUEL PRESSURE SWITCH PROBLEM. DURING EC6251-1 ACCOMPLISHMENT FOUND FUEL DIFFERENTIAL PRESSURE SWITCH CONNECTOR (D2064) LOOSE AND GETTING APART. FURTHER INVESTIGATION REVEALED SWITCH AND CONNECTOR THREADS ARE DAMAGED. REPLACED FUEL DIFFERENTIAL SWITCH, IDLE LESDR UALA2010011500179Skin · damagedLT OTBD AILERON UPPER OTBD EDGE HAS METAL BOND PATCH PEELED BACK AND TORN APPROX 8 INCHES BACK FROM FRONT EDGE. FOUND BY DEICE CREW. TRIMMED AND REPAIRED LIGHTNING STRIKE PICTURE FRAME ON LT OTBD UPPER AILERON SURFACE. REPAIR GOOD UNTIL NEXT CK OR 5000H.SDR UALA2010011500178Unknown · leaking38E, OVRHEAD BIN, STILL DRIPPING WATER, SEEMS TO BE ONLY IN FLIGHT. REPLACED SEVERAL CROWN ARE A INSULATION BLANKETS THAT WERE FOUND WET WITH CONDENSATION. REPLACED CEILING PANELS.SDR UALA2010011500177Light · inoperativeEMERGENCY LIGHT INOP AT: 4B AFT, 5B AFT. REPLACED EMERGENCY LIGHT ASSY., 4B AFT, 5B AFT, CHECKED NORMAL ON GROUND.SDR UALA2010011500174Monitor · faultyNR 2 ENG N1 VIB INDICATION FLUCTUATES WITH EPR CHANGE. NO VIBES FELT IN STABLE CRUISE. NO ACTUAL VIB FELT, CREW FELT ISSUE TO BE FAULTY IND. REPLACED AVM UNIT.SDR UALA2010011300172Sensor · malfunctionedT/E FLAP DISAGREE ON FINAL WITH 15 FLAPS. SUGGEST CK ALL T/E FLAP ROTARY ACTUATORS FOR TRIPS. ROTARY ACTUATORS OK. BITE CHECK FSEU NO FAULTS. OPERATED FLAPS THROUGH FULL CYCLES AND OPS NORMAL. FLAP DISAGREE WAS TROUBLESHOT TO THE M548 MODULE FOR THE OTBD SDR UALA2010011300159Unknown · unknownCABIN EXCESSIVELY COOL, CARGO HOT MESSAGES MOST OF FLT.SDR UALA2010011500190Processor · malfunctionedUNWANTED FUEL TRANSFER. PROCESSOR FOUND DEFECTIVE. REPLACED FQIS PROCESSOR. OP CHECKS NORMAL.SDR UALA2010011300161Regulator Valve · leakingTRIM AIR SUPPLY NOT AVAIL IN ANY MODE OR CONFIG AS EVIDENCED BY SUPPLY DUCT TEMPS ON ECS PAGE. TRIM AIR REGULATING VALVE FOUND LEAKING THRU CAB PRESSURE PORT. VALVE REPLACED. RAN PACKS AND PRESSURIZED AIRCRAFT TO 4 PSI. ALL OPS NORMAL WITH HEAT AVAILABLE THROSDR UALA2010011200151Bleed Valve · faultyLT BLEED ISOLATION LIGHT CAME ON AND LO BLEED DUCT PRESSURE LT NEEDLE READS 10 PSI. VALVE FOUND FAULTY. REPLACED LT ISOLATION VALVE. NORMAL OPS.SDR UALA2010011200147Battery Pack · faultyEMERGENCY LIGHTS INOP LT SEAT ROWS 1-6, FWD GALLEY FLOOR TRACKS 2EA AND DR 1L LWR EXIT SIGN. REPLACED BATTERY PACK. BATTERY PACK NO HELP. FOUND L901 SHORTED, DISCONNECTED EMERGENCY LIGHT STRIP AT DR 1L LAV. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED NORSDR UALA2010011100137Actuator · faultyFLAP DISAGREE MSG. FOUND "ALT FLAP PWR" CB POPPED. RE-SET AND SYS OP NORMAL. FOUND FLAP ROT ACT OVERLOAD IND ON ACT NR 1, NR 3 AND NR 8 POPPED. REPLACING ALL 3 ACT. NR 8 REPLACED. STARTING NR 1. REPLACED NR1 T-E ROTARY ACTUATOR. REPLACED NR 3 ROTARY ACTUASDR UALA2010011100145Controller · inoperativeCOCKPIT TEMP SELECTOR INOP LIGHT ON IN AUTO. INSTALLED NEW ZONE TEMP CONTROLLER. INOP LIGHT EXTINGUISHED. OPS NORMAL.SDR UALA2010011100136Anti-Ice Valve · faultyRT WING ANTI-ICE IS INOP. DURING TROUBLESHOOTING VALVE FOUND DEFECTIVE. REPLACED RT WING A/I VALVE. OPS CKS ARE NORMAL.SDR UALA2010011100126Pump · malfunctionedFUEL IMBALANCE. REPLACED RT JETTISON PUMP AND DIFFUSER. OPS CHECK OK AND NO LEAKS.SDR UALA2010011100125Bleed Valve · faultyAPU BLEED BLEED AIR ON WITH SWITCH OFF. APU VALVE LOCK CLOSED. SUSPECT THE APU BLEED SWITCH AT FAULT. REPLACED VALVE, OPS TEST NORMAL.SDR UALA2010011100122Oxygen Mask · unsecureOXYGEN MASK COMPARTMENTS FELL OPEN AT 35A & 35B. REPACKED OXYGEN MASKS, INSPECTED OXYGEN GENERATOR AND CLOSED AND SECURED OXYGEN MASK DOOR IAW MM.SDR UALA2010011100140Module · faultyCTR SYS WILL NOT TRIM NOSE DOWN. ACFT WILL NOT TRIM NOSE DOWN WITH CTGTR SYS, NOSE UP OK. SINGLE CHANNEL CHECKS OK, LT SYS TRIMS NORMAL, ALT TRIMS NORMAL. OPS CHK INDICATES RT WILL NOT TRIM IN PRIMARY AND ALTERNATE. REPLACED RT STAB TRIM LOCKOUT MODULE. ACFSDR UALA2010010700100Skin · gougedRT INBD AILERON IS GOUGED ON LOWER SURFACE. DAMAGE MEASURES .5" BY 10" IN LENGTH. PREPPING TO REMOVE AILERON. DURING THE RT INBD AIL OPS TEST, ACFT FAILS TEST. ALL OTHER TEST REQUIREMENTS CK NORMAL. ACCOMPLISHED REMOVAL AND INSTALLATION OF ROBBED AILERON IAW MSDR UALA2010010700079Skin · corrodedLEFT HIGH GAIN BEAM STEERING ANT AT FUSELAGE SKIN CORROSION DUE TO INADEQUATE SEALING. DURING SEALANT REMOVAL FOR CORROSION INSP FOUND SCRIBE MARKS AROUND 30 PERCENT OF ANTENNA PERIMETER. REPAIRED IAW SRM. ACCOMPLISHED HFEC AND ULTRASOUND, ALL FOUND OK. ALODSDR UALA2010010700097Shutoff Valve · malfunctionedL ENG HPSOV ON AND BLEED LIGHT ON. RETARDED THROTTLES TO IDLE. GOT LT ENG HPSOV EICAS MSG AND OVERHEAD PANEL BLEED LIGHT ILLUMINATED. SECURED LT HPSOV CLOSE POSITION. REPLACED HPSOV. OP CHECKS NORMAL.
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