Boeing 767-338
Service difficulty reports · 1,328
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 = '767338' 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 = '767338' 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 AU510001870Skin · crackedRT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT THROUGH RIVET HOLE. CRACK IS LOCATED IN INTERNAL DOUBLER AS WELL. CRACK WAS CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 63.5MM (2.5IN).SDR AU510001749Hose · worn(AUS) LOSS OF RT HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND NR 3 BRAKE HYDRAULIC HOSE CHAFED THOUGH. (CASA NR 510001749)SDR AU510001747Pump · faulty(AUS) RT FWD BOOST PUMP SUSPECT FAULTY. CB POPPED. ON DISASSEMBLY INVESTIGATION FOUND SEVERE SCORING WAS ON PUMP HSG IMPELLER BORE INSIDE DIAMETER, SHAFT AND ROTOR ASSY WAS SCORED ON BRG JOURNAL AREA. SEVERE SCORING COULD BE CAUSED BY FOD PASSING THROUGH PUMP.SDR AU510001741Shutoff Valve · failedFLAP/SLAT SHUTOFF VLV LOCATED IN RT W/W LEAKING. INSPECTION FOUND CAP P/N 732-18718 HAD AN OPEN CRACK AT LAST/OUTERMOST THREAD RUNNING 270 DEGREES AROUND ITS CIRCUMFERENCE (CRACKED THROUGH). HEX-NUT END OF ALUMINUM CAP HAD LIFTED BY 0.1 INCHES UNDER HYD PRESSDR AU510001650Actuator · leakingRT HYDRAULIC SYSTEM QUANTITY DECREASING. INVESTIGATION FOUND RT NO7 SPOILER ACTUATOR FILTER CAP PNO 1542615 LEAKING.SDR AU510001649Anti-Ice Valve · failedLT ENGINE ANTI-ICE VALVE FAILED.SDR AU510001647Light · failedSTRONG BURNING ODOR IN CABIN FORWARD GALLEY AREA. INSPECTION FOUND A BURNT FLUORESCENT TUBE ABOVE SEAT 2JK.SDR AU510001565Rod End · corroded(AUS) IB AFT FLAP DEFLECTION CONTROL ROD PULLED OUT OF IB RODEND. INSPECTION FOUND RODEND BADLY CORRODED AND THREAD STRIPPED.SDR AU510001553Actuator · faultyLEADING EDGE SLAT DISAGEE MESSAGE. INVESTIGATION FOUND THAT THE INBOARD LEADING EDGE SLAT BYPASS VALVE ROTARY ACTUATOR WAS INTERMITTENT IN OPERATION.SDR AU510001551Screw · missingLT THRUST REVERSE LEVER COULD BE LIFTED WITH FORWARD THRUST LEVER OFF IDLE. THE THRUST LEVER TOP COVERS WERE REMOVED AND IT WAS FOUND THAT THE AFT TWO FASTENERS OF THE LEFT THRUST LEVER BAULK RAIL INSTALLATION WERE MISSING. THIS ALLOWED THE LEFT THRUST REVERSDR AU510001550Torque Tube · shearedINBOARD LEADING EDGE DRIVE SHAFT/TORQUE TUBE SHEARED. DRIVE SHAFT SHOWED SIGNS OF SEVERE CHAFING DAMAGE DUE TO WATER SUPPLY LINE AND ADJACENT CLAMP. TORQUE TUBE HAD BEEN WORN THROUGH BY MORE THAN 50 PERCENT OF THICKNESS PRIOR TO FAILURE DURING MAINTENANCE.SDR AU510001505Compressor · overheatedFUMES IN CABIN PRIOR TO BOARDING. INVESTIGATION FOUND POTABLE WATER COMPRESSOR EXTREMELY HOT. INVESTIGATION FOUND THAT ON REMOVAL OF THE CAPS AND COVER BOTH STAGES HAD WATER IN BELLOWS AND VALVES. THE SECOND STATE (HIGH-PRESSURE) REED WAS FRACTURED AT THE OUSDR AU510001508Pump · faultyRT FORWARD BOOST PUMP TRIPPED CIRCUIT BREAKER WHEN PUMP SWITCHED `ON`. INVESTIGATION FOUND THE BOOST PUMP FAILED. WORKSHOP INSPECTION FOUND THAT THE IMPELLER FINS HAD EXCESSIVE WEAR FROM RUBBING IN THE PUMP HOUSING. THE HOUSING ALSO HAD SEVERE EROSION ON THSDR AU510002041Pneumatic System · faultyLT ENGINE PRV WARNING WHEN TAKEOFF THRUST SET. MESSAGE CLEARS WHEN THRUST REDUCED. INVESTIGATION CONTINUING.SDR AU510001782Fuel Sys · faultyUNCOMMANDED INFLIGHT FUEL TRANSFER. INVESTIGATION COULD NOT FIND ANY MECHANICAL CAUSE FOR THE DEFECT.SDR AU510001774Idg · failed(AUS) RT INTEGRATED DRIVE GENERATOR (IDG) FAILED. INITIAL INVESTIGATION FOUND BENT PINS 2, 9 AND 10 ON ELECTRICAL CONNECTOR (B). STRIP AND INVESTIGATION FOUND THE LT AND RT FIXED END CYLINDER BLOCKS TO PORT PLATES MATING FACES WERE SCORED. THE CONTROL CYLINSDR AU510001602Anti-Ice Valve · faultyRT WING ANTI-ICE MESSAGE. THERMAL ANTI-ICE VALVE FAULTY.SDR AU510001597Bearing · collapsedNR 1 AFT GALLEY CHILLER FAULTY. WORKSHOP INVESTIGATION FOUND THE FAN BLOWER MOTOR BEARINGS COLLAPSED.SDR AU510001507Valve · faultyLT BLEED ISOLATION VALVE FAULTY. WORKSHOP INVESTIGATION FOUND THE FAILURE WAS DUE TO AN WORN AND INOPERATIVE MOTOR ASSEMBLY.SDR AU510001592Switch · faulty(AUS) SPOILER WARNING ON TAKEOFF. SUSPECT FAULTY POSITION SWITCH. (CASA NR510001592)SDR AU510001999Filter · contaminatedRT ENGINE FUEL FILTER CONTAMINATED WITH BLACK SOOTY DEPOSITS. FURTHER INVESTIGATION FOUND A LESSER DEGREE OF THE SAME DEPOSITS IN THE LT ENGINE FUEL FILTER. EXTENSIVE FUEL DRAINS FOUND TO BE CLEAR. INVESTIGATION CONTINUING.SDR AU510001844Circuit Card · faultyEICAS SIGNAL CONSOLIDATION CARD (SCC) FAILED.SDR AU510001962Filter · contaminatedRT ENGINE FUEL FILTER CONTAMINATED.SDR AU510001690Computer · faultyLT ENGINE INDICATION AND CREW ALERT SYSTEM (EICAS) COMPUTER FAULTY.SDR AU510002111Mec · leakingLT ENGINE MAIN ENGINE CONTROL (MEC) LEAKING AT THE FORWARD ATTACHMENT FLANGE.SDR AU510001871Skin · crackedRT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT AND THROUGH RIVET HOLE. CRACK CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 58.4MM (2.3IN). CRACK ALSO EXISTS IN INTERNAL DOUBLER AS WELL.SDR AU510001555Engine · bird ingestionRT ENGINE BIRDSTRIKE. THREE FAN BLADES DAMAGED BEYOND LIMITS LAID DOWN IN MAINTENANCE MANUAL.SDR AU510001554Controller · failedLT ENGINE PNEUMATIC SYSTEM PRESSURE REDUCING VALVE (PRC) CONTROLLER FAILED. INVESTIGATION CONTINUING.SDR AUS20040510Wire Harness · worn(AUS) PASSENGER SERVICE UNIT (PSU) LOOM WORN AND SPARKING. PSU LOCATED AT SEAT 44JK.SDR AUS20040495Oxygen Mask · misinstalled(AUS) PASSENGER OXYGEN MASKS INCORRECTLY PACKED INTO PASSENGER SERVICE UNITS (PSU). OXYGEN MASK HOSES CAUGHT BETWEEN DOOR AND MASK HOUSING CAUSING HOSES TO BECOME KINKED AND THE DOORS TO BULGE WHEN CLOSED. UNITS AFFECTED WERE LOCATED AT 39DEF , 37DEF,5JK, 1EFSDR AUS20040461Door · sticking(AUS) LT OVERWING EMERGENCY DOOR PREVENTED FROM COMPLETELY OPENING BY THE TARGET FOR THE LT SLIDE COMPARTMENT DOOR CLOSED SENSOR (S218) CATCHING ON THE TAIL OF A SCREW NUT INSTALLED ON THE PACKBOARD. FURTHER INSPECTION REVEALED THAT THE LATCH CONTROL ROD THE SDR AUS20040488Valve · faulty(AUS) RT ENGINE BLEED SYSTEM PRESSURE REDUCING VALVE (PRV) SUSPECT FAULTY. LIMITED INFORMATION PROVIDED.SDR AUS20040477Thrust Reverser · faulty(AUS) LT ENGINE THRUST REVERSER FAILED TO OPERATE ON SELECTION DURING LANDING. INVESTIGATION AND ENGINE GROUND RUN COULD NOT FAULT SYSTEM. SUSPECT CAUSED BY ICING.SDR AUS20040391Door · missing(AUS) NR 2 ENGINE NACELLE/STRUT OB ACCESS DOOR MISSING.SDR AUS20040382Tire · deflated(AUS) LT MAIN LANDING GEAR NR 5 TIRE DEFLATED. NO DAMAGE TO TIRE EVIDENT.SDR AUS20040364Bolt · loose(AUS) LT TANK FUEL QUANTITY APPROXIMATELY 800 KILOGRAMS LOWER THAN RT TANK. INVESTIGATION FOUND THE FUEL/OIL COOLER FORWARD BASKET BOLTS LOOSE BUT ASCERTAINED THIS WAS NOT THE CAUSE OF THE APPARENT FUEL LOSS. INVESTIGATION CONTINUING.SDR AUS20040359Skin · delaminated(AUS) RT LE SLAT T/E WEDGE DELAMINATED ON IB END UPPER FACE. AREA OF DELAMINATION APPROXIMATELY 70 SQ IN. FOUND DURING INSPECTION IAW AD/767/73.SDR AUS20040352Battery · faulty(AUS) EMERGENCY LIGHTING SYSTEM POWER SUPPLY AND BATTERY M1395 FAULTY.SDR AUS20040313Brake Assy · failed(AUS) RT ENGINE THRUST REVERSER LT AND RT ELECTROMECHANICAL BRAKES FAILED SYSTEM TORQUE CHECK. FOUND DURING INSPECTION IAW AD/B767/182 AND AD/B767/83.SDR AUS20040297Latch · faulty(AUS) LT OFFWING SLIDE DOOR NR 3 LATCH GUIDE PIN, BUSH AND SPRING MISSING.SDR AUS20040342Selector · faulty(AUS) CABIN PRESSURE SELECTOR FAULTY.SDR AUS20040296Bolt · faulty(AUS) LT AND RT VERTICAL FIN FORWARD ATTACHMENT BOLTS FAILED TORQUE TEST.SDR AUS20040341Indicator · faulty(AUS) TRAILING EDGE FLAP DISAGREE INDICATION.SDR AUS20040258Valve · faulty(AUS) LT ENGINE PRESSURE REGULATING VALVE (PRV) FAULTY.SDR AUS20040442Pump · failed(AUS) LT ENGINE DRIVEN HYDRAULIC PUMP FAILED DUE TO LOSS OF HYDRAULIC FLUID.SDR AUS20040201Control System · faulty(AUS) FLAPS FAILED TO MOVE FROM 20 TO 30.SDR AUS20040170Actuator · cracked(AUS) NR 6 SPOILER POWER CONTROL ACTUATOR FILTER HOUSING SPLIT. LOSS OF HYDRAULIC FLUID.SDR AUS20040194Fan · failed(AUS) FORWARD EQUIPMENT COOLING FAN SEIZED. FUMES IN COCKPIT.SDR AUS20040478Thermostat · failed(AUS) POTABLE WATER COMPRESSOR OVERHEATING. INVESTIGATION FOUND THAT THE COMPRESSOR MOTOR HAD SEIZED DUE TO THE OVERHEAT THERMOSTAT (THERMAL PROTECTOR) PN 45618-380 FAILING IN A CLOSED POSITION CAUSING THE MOTOR TO CONTINUALLY OPERATE AND FINALLY SEIZE.SDR AUS20040160Probe · failed(AUS) TAT PROBE FAILED.
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