Boeing 767-338

Service difficulty reports · 1,328

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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 = '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.

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).Dec 12, 2005 · Boeing 767338 · Nacelle/Pylon, Plate/SkinSDR AU510001749Hose · worn(AUS) LOSS OF RT HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND NR 3 BRAKE HYDRAULIC HOSE CHAFED THOUGH. (CASA NR 510001749)Dec 12, 2005 · Boeing 767338 · BrakeSDR 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.Dec 12, 2005 · Boeing 767338 · Fuel Boost PumpSDR 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 PRESDec 12, 2005 · Boeing 767338 · Flight Control SystemSDR AU510001650Actuator · leakingRT HYDRAULIC SYSTEM QUANTITY DECREASING. INVESTIGATION FOUND RT NO7 SPOILER ACTUATOR FILTER CAP PNO 1542615 LEAKING.Dec 12, 2005 · Boeing 767338 · Drag Control ActuatorSDR AU510001649Anti-Ice Valve · failedLT ENGINE ANTI-ICE VALVE FAILED.Dec 12, 2005 · Boeing 767338 · Air Intake Anti/De-Ice SystemSDR AU510001647Light · failedSTRONG BURNING ODOR IN CABIN FORWARD GALLEY AREA. INSPECTION FOUND A BURNT FLUORESCENT TUBE ABOVE SEAT 2JK.Dec 12, 2005 · Boeing 767338 · Passenger Compartment LightingSDR AU510001565Rod End · corroded(AUS) IB AFT FLAP DEFLECTION CONTROL ROD PULLED OUT OF IB RODEND. INSPECTION FOUND RODEND BADLY CORRODED AND THREAD STRIPPED.Dec 12, 2005 · Boeing 767338 · Trailing Edge Flap Control SystemSDR AU510001553Actuator · faultyLEADING EDGE SLAT DISAGEE MESSAGE. INVESTIGATION FOUND THAT THE INBOARD LEADING EDGE SLAT BYPASS VALVE ROTARY ACTUATOR WAS INTERMITTENT IN OPERATION.Dec 12, 2005 · Boeing 767338 · Leading Edge Slat ActuatorSDR 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 REVERDec 12, 2005 · Boeing 767338 · Standard Practices/StructuresSDR 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.Dec 12, 2005 · Boeing 767338 · Leading Edge DevicesSDR 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 OUDec 12, 2005 · Boeing 767338 · Potable Water SystemSDR 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 THDec 6, 2005 · Boeing 767338 · Fuel Boost PumpSDR AU510002041Pneumatic System · faultyLT ENGINE PRV WARNING WHEN TAKEOFF THRUST SET. MESSAGE CLEARS WHEN THRUST REDUCED. INVESTIGATION CONTINUING.Nov 10, 2005 · Boeing 767338 · Pneumatic Distribution SystemSDR AU510001782Fuel Sys · faultyUNCOMMANDED INFLIGHT FUEL TRANSFER. INVESTIGATION COULD NOT FIND ANY MECHANICAL CAUSE FOR THE DEFECT.Nov 8, 2005 · Boeing 767338 · Aircraft Fuel Distribution SystemSDR 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 CYLINOct 8, 2005 · Boeing 767338 · AC Generator-AlternatorSDR AU510001602Anti-Ice Valve · faultyRT WING ANTI-ICE MESSAGE. THERMAL ANTI-ICE VALVE FAULTY.Oct 7, 2005 · Boeing 767338 · Airfoil Anti/De-ice SystemSDR AU510001597Bearing · collapsedNR 1 AFT GALLEY CHILLER FAULTY. WORKSHOP INVESTIGATION FOUND THE FAN BLOWER MOTOR BEARINGS COLLAPSED.Oct 7, 2005 · Boeing 767338 · Buffet/GalleysSDR AU510001507Valve · faultyLT BLEED ISOLATION VALVE FAULTY. WORKSHOP INVESTIGATION FOUND THE FAILURE WAS DUE TO AN WORN AND INOPERATIVE MOTOR ASSEMBLY.Oct 6, 2005 · Boeing 767338 · Pneumatic Distribution SystemSDR AU510001592Switch · faulty(AUS) SPOILER WARNING ON TAKEOFF. SUSPECT FAULTY POSITION SWITCH. (CASA NR510001592)Sep 7, 2005 · Boeing 767338 · Drag Control SystemSDR 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.May 10, 2005 · Boeing 767338 · Engine Fuel DistributionSDR AU510001844Circuit Card · faultyEICAS SIGNAL CONSOLIDATION CARD (SCC) FAILED.May 9, 2005 · Boeing 767338 · Central WarningSDR AU510001962Filter · contaminatedRT ENGINE FUEL FILTER CONTAMINATED.Apr 10, 2005 · Boeing 767338 · Engine Fuel DistributionSDR AU510001690Computer · faultyLT ENGINE INDICATION AND CREW ALERT SYSTEM (EICAS) COMPUTER FAULTY.Mar 8, 2005 · Boeing 767338 · Central ComputersSDR AU510002111Mec · leakingLT ENGINE MAIN ENGINE CONTROL (MEC) LEAKING AT THE FORWARD ATTACHMENT FLANGE.Feb 11, 2005 · Boeing 767338 · Fuel Control/Turbine EnginesSDR 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.Feb 9, 2005 · Boeing 767338 · Nacelle/Pylon, Plate/SkinSDR AU510001555Engine · bird ingestionRT ENGINE BIRDSTRIKE. THREE FAN BLADES DAMAGED BEYOND LIMITS LAID DOWN IN MAINTENANCE MANUAL.Feb 7, 2005 · Boeing 767338 · Engine (Turbine/Turboprop)SDR AU510001554Controller · failedLT ENGINE PNEUMATIC SYSTEM PRESSURE REDUCING VALVE (PRC) CONTROLLER FAILED. INVESTIGATION CONTINUING.Feb 7, 2005 · Boeing 767338 · Pneumatic Distribution SystemSDR AUS20040510Wire Harness · worn(AUS) PASSENGER SERVICE UNIT (PSU) LOOM WORN AND SPARKING. PSU LOCATED AT SEAT 44JK.Jun 11, 2004 · Boeing 767338 · Equipment/Furnishings WiringSDR 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, 1EFJun 4, 2004 · Boeing 767338 · Passenger Oxygen SystemSDR 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 May 30, 2004 · Boeing 767338 · Emergency ExitsSDR AUS20040488Valve · faulty(AUS) RT ENGINE BLEED SYSTEM PRESSURE REDUCING VALVE (PRV) SUSPECT FAULTY. LIMITED INFORMATION PROVIDED.May 25, 2004 · Boeing 767338 · Pneumatic Distribution SystemSDR 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.May 25, 2004 · Boeing 767338 · Engine Thrust ReverserSDR AUS20040391Door · missing(AUS) NR 2 ENGINE NACELLE/STRUT OB ACCESS DOOR MISSING.May 10, 2004 · Boeing 767338 · Nacelle/Pylon, Main FrameSDR AUS20040382Tire · deflated(AUS) LT MAIN LANDING GEAR NR 5 TIRE DEFLATED. NO DAMAGE TO TIRE EVIDENT.May 3, 2004 · Boeing 767338 · TireSDR 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.Apr 29, 2004 · Boeing 767338 · Engine Oil CoolerSDR 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.Apr 27, 2004 · Boeing 767338 · Leading Edge DevicesSDR AUS20040352Battery · faulty(AUS) EMERGENCY LIGHTING SYSTEM POWER SUPPLY AND BATTERY M1395 FAULTY.Apr 27, 2004 · Boeing 767338 · Emergency LightingSDR 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.Apr 26, 2004 · Boeing 767338 · Engine Thrust ReverserSDR AUS20040297Latch · faulty(AUS) LT OFFWING SLIDE DOOR NR 3 LATCH GUIDE PIN, BUSH AND SPRING MISSING.Apr 20, 2004 · Boeing 767338 · Emergency ExitsSDR AUS20040342Selector · faulty(AUS) CABIN PRESSURE SELECTOR FAULTY.Apr 18, 2004 · Boeing 767338 · Cabin Pressure ControllerSDR AUS20040296Bolt · faulty(AUS) LT AND RT VERTICAL FIN FORWARD ATTACHMENT BOLTS FAILED TORQUE TEST.Apr 18, 2004 · Boeing 767338 · FastenersSDR AUS20040341Indicator · faulty(AUS) TRAILING EDGE FLAP DISAGREE INDICATION.Apr 7, 2004 · Boeing 767338 · Trailing Flap Position Indicating SystemSDR AUS20040258Valve · faulty(AUS) LT ENGINE PRESSURE REGULATING VALVE (PRV) FAULTY.Apr 7, 2004 · Boeing 767338 · Pneumatic Distribution SystemSDR AUS20040442Pump · failed(AUS) LT ENGINE DRIVEN HYDRAULIC PUMP FAILED DUE TO LOSS OF HYDRAULIC FLUID.Mar 15, 2004 · Boeing 767338 · Hydraulic Pump (Electric/Engine), MainSDR AUS20040201Control System · faulty(AUS) FLAPS FAILED TO MOVE FROM 20 TO 30.Mar 9, 2004 · Boeing 767338 · Trailing Edge Flap Control SystemSDR AUS20040170Actuator · cracked(AUS) NR 6 SPOILER POWER CONTROL ACTUATOR FILTER HOUSING SPLIT. LOSS OF HYDRAULIC FLUID.Mar 7, 2004 · Boeing 767338 · Drag Control ActuatorSDR AUS20040194Fan · failed(AUS) FORWARD EQUIPMENT COOLING FAN SEIZED. FUMES IN COCKPIT.Mar 3, 2004 · Boeing 767338 · Air Distribution FanSDR 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.Feb 28, 2004 · Boeing 767338 · Air Supply (Water Pressure System)SDR AUS20040160Probe · failed(AUS) TAT PROBE FAILED.Feb 28, 2004 · Boeing 767338 · Outside Air Temperature Indicator/Sensor
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