Boeing 767-222

Service difficulty reports · 956

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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 = '767222'
  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 2003UALA00141Cover · missingEEL LIGHT STRIP FORWARD OF DOOR 2 LEFT IS INOPERATIVE AND COVER IS MISSING. SECURED POWER FEEDER. OPS CHECK OK. INSTALLED NEW LIGHT LENS COVER.Feb 3, 2003 · N605UA · Boeing 767222 · Emergency LightingSDR 2003UALA00136Throttle Cable · bindingNR 1 ENGINE THROTTLE CABLE BINDING. LEFT THROTTLE LEVER WILL NOT PROCEED PAST IDLE. NO THROTTLE RESPONSE AT 20 KTS. PUSH-PULL CABLE FOUND BINDING. CABLE WAS REPLACED. DELAY 2:48. PULL CHECK AND INSPECTION DONE AT C-CHK. NO KNOWN PREVIOUS INCIDENTS.Feb 2, 2003 · N619UA · Boeing 767222 · Power LeverSDR 2003UALA00106Wire Harness · chafedDURING TAKEOFF ROLL AT 110 KTS, AN AMBER LIGHT ENG NR 1 EICAS MESSAGE CAME ON. THE CAUSE WAS A CHAFED WIRE AT SWITCH S167. THIS IS THE ENGINE 1 RT REVERSER DEPLOY PROXIMITY SENSOR. THE WIRE WAS REPAIRED. WIRE HARNESS STAYS WITH THE REVERSER AND IS NOT CHANGJan 28, 2003 · N601UA · Boeing 767222 · Engine Thrust ReverserSDR 2003UALA00027Bearing · failedAIRCRAFT LOST NR 4 RIGHT AFT MLG WHEEL. RETURNED TO FIELD. WHEEL LOSS BELIEVED DUE TO BEARING FAILURE. INSPECTION OF RECOVERED PARTS REFLECT LACK OF LUBRICATION OF INBOARD WHEEL BEARING. NR 4R WHEEL AND BRAKE REPLACED. NR 3R MATE REPLACED, REAR AXLE REPLAJan 6, 2003 · N615UA · Boeing 767222 · Wheel/Ski/FloatSDR 2003UALA00006Skin · bulgedLOWER EXTERNAL FUSELAGE SKIN BULGING STATION 720 STRINGER 38R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.Dec 24, 2002 · N606UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2003UALA00005Skin · crackedRIGHT HAND BELLY SKIN, 20 INCHES AFT OF SECTION 41 BUTT JOINT, 18 INCHES OUTBOARD OF E&E EXHAUST PORT CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED.Dec 24, 2002 · N606UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2003UALA00004SkinLOWER FUSELAGE SKIN HAS PILLOWING AT STRINGER 39R TWO EACH AREAS MKD STATION 588 TO 610. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR INSTALLED.Dec 24, 2002 · N606UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2002UALA01864Seal · leakingLEFT BLEED DUCT LEAK EICAS MESSAGE. RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE LEFT ENGINE ANTI-ICE VALVE SEAL (S) LEAKING AT CLAMP. SEALS REPLACED, NO OTHER ACTION REQUIRED,Dec 17, 2002 · N619UA · Boeing 767222 · Air Intake Anti/De-Ice SystemSDR 2002UALA01854Compressor · stalledNR 2 ENGINE COMPRESSOR STALL, UNSUCCESSFUL RESTART. VANES WOULD NOT TRACK. EVBC REPLACED. DISASSEMBLY OF EVBC SHOWED EVACUATED BELLOW DEFECTIVE.Dec 16, 2002 · N603UA · Boeing 767222 · Turbine Engine Compressor SectionSDR 2002UALA01842Fuel Control · failedLOSS OF POWER TO NR 2 ENGINE. ENGINE RESTARTED. ENGINE WOULD NOT GO ABOVE IDLE. FCU CHANGED. BENCH CHECK SHOWED ACCEL & DECEL SCHEDULE UNDER LOW LIMITS, PROBABLE CAUSE OF POWER LOSS AT ALT 41K.Dec 9, 2002 · N615UA · Boeing 767222 · Fuel Control/Turbine EnginesSDR 2002UALA01791Fitting · looseRIGHT GENERATOR DRIVE LIGHT AND EICAS MSG DISPLAYED WHEN POWER SET ON TAKEOFF. ABORTED TAKEOFF AT 65 KTS. LOOSE OIL LINE FITTING IN IDG EXTERNAL OIL CIRCUIT CAUSED LOSS OF OIL RESULTING ILLUMINATION OF IDG DRIVE LIGHT DUE TO LOW OIL PRESS. OIL LINE TIGHTENEDec 1, 2002 · N601UA · Boeing 767222 · Engine Oil Distribution (Airframe Furnished)SDR 2002UALA01784Warning System · malfunctionedRIGHT ENGINE BLEED LIGHT ILLUMINATED AND EICAS MSG. ABORTED TAKEOFF AT 110 KNOTS. ACCOMPLISHED BITE OF RIGHT PNEU SYSTEM, NO FAULTS FOUND. NO MAINTENANCE ACTION TAKEN, AND NO SUBSEQUENT PROBLEMS IN RIGHT PNEUMATIC SYSTEM HAVE BEEN REPORTED.Nov 26, 2002 · N617UA · Boeing 767222 · Pneumatic Indicating SystemSDR 2002UALA01639Valve · failedUNABLE TO PRESSURIZE THE CABIN. FLIGHT RETURNED TO FIELD. THIS AIRCRAFT HAD A SIMILAR PROBLEM ON 10/24/02. THE GROUND EQUIPMENT COOLING EXHAUST VALVE FAILED OPEN. THE VALVE WAS FOUND TO HAVE WORN BEARINGS AND INTERNAL PARTS CAUSING INTERMITTENT OPERATION.Oct 30, 2002 · N619UA · Boeing 767222 · Air Distribution SystemSDR 2002UALA01637Oil Filter · failedNR 2 ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED. ALL OTHER ENGINE PARAMETERS NORMAL. SUPPLEMENTAL DATA UPDATE ENGINE LEASED FROM AIR CANADA. OIL FILTERS AND CHIP DETECTORS CHECKED OK.OIL FILTER DIFFERENTIAL SWITCH CHECKED OKOct 30, 2002 · N607UA · Boeing 767222 · Engine Oil Indicating SystemSDR 2002UALA01635Engine · failedCOMPRESSOR STALL NR 2 ENGINE AT 2,500 FEET. ENGINE SHUTDOWN, RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE POST FLIGHT EXAM SHOWED N2 SYSTEM FROZEN. CHIP DETECTORS FULL . ENGINE WAS LEASED FROM AIR CANADA, 97 HRS OUT OF A FULL OVERHAUL. ENGINE RETURNED TO LOct 30, 2002 · N607UA · Boeing 767222 · Engine (Turbine/Turboprop)SDR 2002UALA01630Flap · crackedLEFT WING INBOARD TRAILING EDGE FLAP, MID SUPPORT CRACKEDAT OUTBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FLAP TO MID FLAP SUPPORT HINGE.Oct 26, 2002 · N603UA · Boeing 767222 · Trailing Edge FlapsSDR 2002UALA01628Valve · malfunctionedUNABLE TO CONTROL CABIN ALTITUDE. CABIN AT 9400 FT, AIRCRAFT AT 11000 FT. THE SAME IN AUTO 1 AND AUTO 2. IN MANUAL, CABIN ALTITUDE INCREASED BY 200 FPM. RETURNED TO FIELD. THE LEFT AND RIGHT OUTFLOW VALVES ACTUATORS AND THE CABIN PRESSURIZATION ALTIMETEROct 24, 2002 · N619UA · Boeing 767222 · Air Distribution SystemSDR 2002UALA01629Pump · fluctuatesFROM TAKE OFF TO ABOUT 6000 FT AT REDUCED CLIMB THRUST, NR 1 ENGINE FLUCTUATED ABOUT 4 PERCENT (N1). STABILIZED AFTER THAT. SUPPLEMENTAL DATA UPDATE FUEL CONTROL AND FUEL PUMP REPLACED PER MM. ENGINE RUN, CHECKED OK. FP AND FCU ROUTED TO OSV.Oct 24, 2002 · N615UA · Boeing 767222 · Fuel Injector NozzleSDR 2002UALA01618Web · mislocatedRIGHT HAND WHEEL WELL UPPER PRESSURE WEB HAS A MISLOCATED DRAIN HOLE FROM PREVIOUS INSTALLATION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WEBOct 22, 2002 · N603UA · Boeing 767222 · Fuselage Structure (General)SDR 2002UALA01617Engine · bird strikeBIRD STRIKE TO RIGHT ENGINE. RETURNED TO FIELD. THE BIRD STRIKE CAUSED THE FAILURE OF A FAN BLADE. THE TIP OF THE FAN BLADE LIBERATED INBOARD OF THE MIDSPAN SHROUD, WHICH CAUSED ABNORMAL VIBRATION AND OVERTEMP. THE ENGINE WAS SHUT DOWN AND RETURNED TO FIELOct 19, 2002 · N607UA · Boeing 767222 · Turbine Engine Compressor SectionSDR 2002UALA01555Flap · crackedRIGHT WING INBOARD FLAP HINGE FITTING FLANGE IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE.Oct 7, 2002 · N606UA · Boeing 767222 · Trailing Edge FlapsSDR 2002UALA01554Doubler · damagedEXTERNAL FUSELAGE, LEFT HAND SIDE SKIN DOUBLER HAS POPPED RIVET AND BULGED SKIN AT BODY STATION 742-744, STRINGER 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER.Oct 7, 2002 · N606UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2002UALA01493Stringer · crackedAFT CARGO PIT AT BODY STATION 1080-1087, STRINGER 33L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER.Sep 25, 2002 · N605UA · Boeing 767222 · Fuselage Main, Longeron/StringerSDR 2002UALA01489Blade · failedLEFT ENGINE COMPRESSOR STALL. SINGLE STG 8 HPC BLADE FAILED .75 INCH FROM BLADE TIP. FATIGUE FAILURE ORIGINATING FROM SMALL FOD/DOD NICK AT LE. MINOR TIP DMG TO REMAINDER OF STG 8. NO OTHER DMG STG 7,8 & 9 HPC BLADES ARE INSTALLED NEW AT EACH HPC DEBLADESep 20, 2002 · N602UA · Boeing 767222 · Turbine Engine Compressor SectionSDR 2002UALA01451Battery Pack · intermittentEXIT PATH LIGHTING FLICKERING OFF AND ON. REPLACED BATTERY PACK.Sep 14, 2002 · N606UA · Boeing 767222 · Emergency LightingSDR 2002UALA01419Wire Harness · faultyONE EEL LIGHT INOP ON RIGHT SIDE OF SEAT 1F. ALSO, DOOR 1R LOWER EXIT LIGHT INOP. MAJOR REPAIR ACCOMPLISHED. REPLACED POWER LEAD CABLE, END CAPS, AND COVER.Sep 8, 2002 · N606UA · Boeing 767222 · Light System WiringSDR 2002UALA01351Battery Pack · disconnectedNUMBER 1 SPOILER SQUIB AND NUMBER 2 ESCAPE SLIDE WILL NOT TEST. FOUND EMERGENCY ESCAPE BATTERY PACK ON RIGHT SIDE M962 DISCONNECTED. THE CONNECTOR WAS RECONNECTED AND THE SYSTEM OPERATED OK.Aug 23, 2002 · N620UA · Boeing 767222 · Emergency EquipmentSDR 2002UALA01332Engine · bird ingestionAT TAKEOFF COMPRESSOR STALL ON NR 1 ENGINE. BIRD STRIKE CONFIRMED. COMPRESSOR BORESCOPED PER MM. NO DAMAGE. ENGINE CONTINUED IN SERVICE.Aug 21, 2002 · N603UA · Boeing 767222 · Engine (Turbine/Turboprop)SDR 2002UALA01300Bearing · failedRIGHT ENGINE OIL FILTER MESSAGE DISPLAYED. RIGHT ENGINE SHUTDOWN BEFORE LANDING. FAILURE OF THE NUMBER THREE BEARING. ENGINE WAS 85 HOURS TSO. FAILURE BEING INVESTIGATED BY ENGINE OVERHAUL OSV AND BEARING OSV.Aug 12, 2002 · N615UA · Boeing 767222 · Engine (Turbine/Turboprop)SDR 2002UALA01287Blade · failedRIGHT ENGINE COMPRESSOR STALL - HIGH EGT ON CLIMB OUT. SEVENTH STAGE COMPRESSOR BLADE FAILURE. ON TEARDOWN, FIVE EACH BLADES WERE COMPLETELY MISSING FROM THE DISK.Aug 8, 2002 · N611UA · Boeing 767222 · Turbine Engine Compressor SectionSDR 2002UALA01288Valve · failedMID CABIN LAV TOILET OVERFLOWED, WATER SHUTOFF. RINSE VALVE ON TOILET ASSY FAILED IN THE OPEN POSITION. REPLACED TOILET ASSEMBLY.Aug 8, 2002 · N620UA · Boeing 767222 · Waste Disposal SystemSDR 2002UALA00959Battery · dischargedEMERGENCY FLOOR LIGHTS STAYED ON SEATS 16-32 LT SIDE. REPLACED BATTERY PACKS AND OVERHEAD PANEL ON-OFF-ARMED SWITCH.Jun 5, 2002 · N609UA · Boeing 767222 · Emergency LightingSDR 2002UALA00924Skin · corrodedAFT EXTERNAL FUSELAGE, AFT WATER DRAIN MAST, CORROSION AROUND BASE, BODY STATION 1417, STRINGER 35R. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN WITH EXTERNAL DOUBLER.May 28, 2002 · N604UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2002UALA00929Fitting · crackedRIGHT HAND WING FRONT SPAR OUTBOARD PITCHLOAD FITTING CRACKED AT THE FORWARD UPPER RADIUS ABOVE FITTING LUG, CRACK FOUND AND CONFIRMED. MAJOR REPAIR ACCOMPLISHED. REPLACED OUTBOARD PITCHLOAD FITTING.May 27, 2002 · N604UA · Boeing 767222 · Wing, Control SurfacesSDR 2002UALA00857Fan · failedELECTRIC SMELL THROUGHOUT CABIN. FOUND LEFT RECIRC FAN MAKING LOUD GRINDING NOISE, CYCLED SWITCH FAN FAILED TO TURN ON. CABIN FILLED WITH SMOKE. REPLACED LEFT RECIRC FAN PER SMC 09-MM 21-25-01. FAN WAS REPLACED. NO FURTHER EVENTS OF SMOKE OCCURRED. RECIMay 11, 2002 · N601UA · Boeing 767222 · Air Distribution FanSDR 2002UALA00764Pressure Switch · defectiveLEFT ENGINE OIL FILTER EICAS CAUTION ILLUMINATED ON CLIMBOUT. REPLACED ENGINE MAIN OIL PRESS DIFFERENTIAL SWITCH PER MM.Apr 28, 2002 · N607UA · Boeing 767222 · Engine Oil PressureSDR 2002UALA00763Pcu · malfunctionedIN CRUISE THE RUDDER TRIM FROZE. ATTEMPTS TO TROUBLESHOOT WITH THE CAPTAIN WERE UNSUCCESSFUL. DIVERTED TO ORD. NO EMERGENCY DECLARED. REPLACED CENTER PCU, REPLACED RUDDER TRIM MODULE AND RUDDER TRIM POSITION INDICATOR, REPLACED RUDDER TRIM ACTUATOR. REPAIApr 25, 2002 · N609UA · Boeing 767222 · Rudder Tab Control SystemSDR 2002UALA00521Cover · out of positionLEFT WING EMERGENCY SLIDE DEPLOYED. THE AMT INVESTIGATED A VERBAL REPORT FROM THE INBOUND CREW THAT THE PLASTIC COVER HAD FALLEN OFF THE LEFT OVERWING DOOR RELEASE HANDLE. IT WAS DETERMINED THAT THE HANDLE GRIP WAS ROTATED 90 DEGREES FROM ITS CORRECT POSITIOMar 21, 2002 · N609UA · Boeing 767222 · Emergency ExitsSDR 2002UALA00316Actuator · out of rigAFTER T/O PROIR TO POWER REDUCTION LT ENG SURGED 1.3 TO 1.9 EPR FOR 30 SECONDS, THROTTLES STEADY, ALL NORM UNTIL TOP OF CLIMB, AT LEVEL OFF, THROTTLES STEADY, SMALL SURGE 15 SECONDS, LATER IN CRUISE SMALL OSCILLATIONS IN EPR FRM 1.28 TO 1.30. DIVERTED TO ORD.Feb 24, 2002 · N606UA · Boeing 767222 · Compressor Bleed ControlSDR 2002UALA00796Strap · crackedDURING C-CHECK FOUND CRACK IN FAIL-SAFE STRAP. CRACK IN THE FAIL-SAFE STRAP AT STA 955.1 ON THE LEFT SIDE WAS CAUSED BY FATIGUE. OTHER CONTRIBUTING FACTORS TO THE CRACK ORIGINATION ARE BEING DETERMINED BY THE OEM WITH FURTHER ANALYSIS OF THE CRACKED PART. TFeb 6, 2002 · N609UA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2002UALA00207Bleed Valve · out of rigLEFT ENGINE COMPRESSOR STALL WITH EGT PEAKING AT 698 DEGREES. ATC REPORTED FLAMES FROM REAR OF ENGINE. RETURNED TO JFK. ACCOMPLISHED THE EVBC (ENGINE VANE & BLEED CONTROL) AND 3.0 BLEED TRIM. THE 3.0 BLEED WAS FOUND OUT OF TRIM. PROBLEMS WERE ENCOUNTEREFeb 2, 2002 · N606UA · Boeing 767222 · Compressor Bleed ValveSDR 2002UALA00184Cart · defectiveBURNT ELECTRICAL ODOR FROM INSIDE GALLEY CART IN THE RIGHT SECTION OF THE AFT GALLEY REPORTED BY FLIGHT ATTENDANTS. BURNT ODOR CAME FROM CART 404. CART REMOVED IN IND. POWERED UP ENTIRE GALLEY. CHECKED OPERATION OF ALL GALLEY COMPONENTS AND LIGHTS. CONFIRJan 31, 2002 · N601UA · Boeing 767222 · Buffet/GalleysSDR 2002UALA00131Warning System · malfunctionedCREW HEARD LOUD THUMPING ON LEFT SIDE OF AIRCRAFT, AND HAD L/E SLAT DISAGREE LIGHT ILLUMINATE. DIVERTED TO SLC. NUISANCE EICAS MESSAGE GENERATED BY PROXIMITY SWITCH SYSTEM. THERE IS NO HISTORY OF SLAT POSITION PROBLEMS ON THIS AIRCRAFT. PERFORMED PSEU BITEJan 20, 2002 · N614UA · Boeing 767222 · Leading Edge Slat Position Indicating SystemSDR 2002UALA00138Warning System · activatedEICAS MESSAGE LEADING EDGE SLAT DISAGREE DISPLAYED INTERMITTANTLY ALONG WITH CAUTION LIGHT ILLUMINATED. FLIGHT DIVERTED TO SLC.Jan 20, 2002 · N614UA · Boeing 767222 · Leading Edge Slat Position Indicating SystemSDR 2002UALA00109Relay · intermittentLIGHTS FLICKERING IN COCKPIT. POSSIBLE LOSS OF ALL INSTRUMENT LIGHTING. DIVERTED TO DEN. FOUND LOOSE WIRE AT TERMINAL BLOCK BEHIND P6 PANEL, SECURED WIRE. PROVIDES POWER TO CAPT FLOODLIGHT STBY POWER RELAY. OVERHEAD LIGHTS FLICKER-REPEAT. REPAIRED WIRINGJan 15, 2002 · N606UA · Boeing 767222 · Flight Compartment LightingSDR 2002UALA00062Module · faultyCREW REPORTED EICAS MSG FOR RUDDER RATIO, AILERON LOCKOUT, AND AUTOPILOT PROBLEMS. RETURNED TO SFO. AILERON LOCKOUT MESSAGE WAS GENERATED BY FAULTED STAB TRIM AILERON LOCKOUT MODULE (SAM). NOTE, SAM ALSO PROVIDES AIR DATA TO RUDDER RATIO CHANGER MODULE. REJan 10, 2002 · N601UA · Boeing 767222 · Stabilizer Control SystemSDR 2001UALA02503Valve · failedAFT MID LAV CONTINUOUSLY FLUSHING. LAV WATER OVERFLOWED AND FLOODED AREA INCLUDING MID GALLEY. AIRCRAFT DIVERTED TO ORD FOR REPAIR. TOILET RINSE VALVE FAILED IN THE OPEN POSITION. REMOVED AND REPLACED TOILET ASSY.Dec 31, 2001 · N608UA · Boeing 767222 · Waste Disposal SystemSDR 2001UALA02428Odor · detectedACRID ELECTRICAL BURNING SMELL AND FUMES COMING FROM DOOR 1R CEILING AREA. GALLEY CB U33 PULLED. GALLEY CIRCUIT BREAKER WAS PULLED. CABIN WAS AIRED OUT. ALL SYSTEMS WERE TURNED ON AGAIN. SMELL COULD NOT BE REPRODUCED. NO HISTORY OF ODOR IN CABIN.Dec 18, 2001 · N609UA · Boeing 767222 · Air Distribution SystemSDR 2001UALA02423Seal · defectiveCAPTAIN'S NR 2 SLIDING WINDOW HAS A VERY LOUD SQUEAL. CREW CONSIDERS IT UNACCEPTABLE FOR FURTHER FLIGHT. BULB SEAL WAS FOUND DEFECTIVE. OLD SEAL WAS REMOVED, SEAL CHANNEL CLEANED AND NEW SEAL INSTALLED AS OUTLINED IN MM 56-11-11 WITH APPROPRIATE CURE TIMES Dec 16, 2001 · N602UA · Boeing 767222 · Flight Compartment WindowsSDR 2001UALA02373Skin · crackedFUSE SKIN CRACKED AT STATION 1654 BETWEEN STRINGER 4R TO 5R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.Dec 6, 2001 · N602UA · Boeing 767222 · Fuselage Main, Plate/Skin
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