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 2005UALA01246Battery · inoperativeEEL OVERHEAD LIGHTS AT SEATS 8B, 6B, 5B, 1B AND FWD OF 1B PLUS FWD LAV EEL LIGHT BAR INOP. *S/D* RESEATED BATTERY ON THE POWER SUPPLY.SDR 2005UALA01216Pump · overheatedCANCELLED DUE TO INBOUND HYDRAULIC PUMP OVERHEAT AND LOSS OF HYDRAULIC SYSTEM PRESSURE. MAINTENANCE REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP AND CASE DRAIN AND PRESSURE FILTERS. PERFORMED ENGINE RUN AND REQUIRED OP CK. ALL OK.SDR 2006UALA01175Housing · crackedLT O/W SLIDE DISCONNECT HOUSING IS CRACKED. REPLACE DISCONNECT HOUSING IAW 767MM 25-65-98.SDR 2006UALA01177Latch · wornR/W, O/W SLIDE COMPARTMENT, NR 4 AND 3 LATCHES ARE WORN. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98.SDR 2006UALA01176Latch · failedRIGHT OFF-WING SLIDE LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98.SDR 2006UALA01174Latch · failedLEFT OFFWING SLIDE DOOR LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW B767 MM 25-65-98.SDR 2005UALA01162Shear Tie · corrodedCORROSION ON AFT SIDE OF FRAME BS 1562 FROM BL 0 TO RBL 10 ON SHEAR TIE.SDR 2005UALA01161Frame · corrodedAFT CARGO COMPARTMENT, LOWER LOBE DRAIN HOLE IN FRAME AT BS 1562, BL 0, IS CORRODED.SDR 2005UALA01158Seat Track · crackedCABIN SEAT TRACK AT GALLEY 4A FWD ATTACH POINT IS CRACKED, OUTBOARD SEAT TRACK.SDR 2005UALA01157Intercostal · corrodedCORROSION ON UPPER SURFACE OF INTERCOSTAL AT STA 852 AND LBL 54.SDR 2005UALA01156Attach Angle · crackedFWD CARGO DOOR SILL ATTACHING ANGLE HAS A CRACK AT BS 610.SDR 2005UALA01138Flap System · malfunctionedLANDED ORD UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP INDICATION PROBLEM.SDR 2005UALA01134Frame · damagedFOUND SMALL AREA OF ELECTRICAL ARCH DAMAGE TO VERTICAL FRAME RT FLANGE APPROX 1.5 INCHES ABOVE BASE.SDR 2005UALA01133Battery · dischargedDOOR 1LH AND 1RH EMERGENCY EXIT LIGHTS INOP REPLACED POWER SUPPLY. REPLACED POWER SUPPLY.SDR 2005UALA01126Windshield · crackedCAPTAINS WINDSHIELD CRACKED. FLIGHT DIVERTED TO LHR.SDR 2005UALA01119Cable · inoperativeLT FWD LAV EEL LIGHT BAR INOPERATIVE. FOUND LIGHT CABLE BROKEN AND REPAIRED.SDR 2005UALA01118Cable · inoperativeRT SIDE A-ZONE EEL INOPERATIVE. REPAIRED DAMAGED EEL FEEDER CABLE.SDR 2005UALA01087Sill · corrodedFWD PIT LWR DOOR SILL AT APPROX RBL 40 IS CORRODED. STRAP WAS REPLACED.SDR 2005UALA01089Slide · malfunctionedBOTH SPOILER AND SLIDE SQUIBS DO NOT TEST ON BOTH LEFT AND RIGHT OVERWING EXITS. REPLACED BOTH OFF-WING SLIDE BATTERIES. TEST OK AFTER CHANGE OUT.SDR 2005UALA01042Skin · damagedSHARP DENT AND GOUGES IN BELLY SKIN 1 INCH AFT OF STA 1263 FRAME, BETWEEN 39L AND 39R STRINGERS. FUSELAGE DAMAGE AT STA 1264 LOWER CENTERLINE BEYOND LIMITS DEEP DENT AND SEVERAL GOUGES ACROSS SKIN AND FASTENERS. CONTACT DAMAGE TO LOWER AFT BELLY SKIN. REPAISDR 2005UALA01036Door · separatedDIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4SDR 2005UALA01039Warning System · activatedABORTED TAKE OFF DUE TO FLAP CONFIGURATION MESSAGE.SDR 2005UALA01016Warning Light · illuminatedRETURNED TO SFO DUE TO LEADING EDGE SLAT ASYMMETRY PROBLEM.SDR 2005UALA00996Slat System · malfunctionedRETURNED TO HNL DUE TO A SLAT ASYMMETRY MESSAGE.SDR 2006UALA01173Housing · crackedLT O/W SLIDE COMPARTMENT DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 25-65-98.SDR 2005UALA00832Stiffener · crackedFWD NOSE SECTION BS 246 FLOORBEAM, FWD SIDE AT LBL 40 VERTICAL STIFFENER IS CRACKED. FINDING AND REPLACING CRACKED VERTICAL STIFFENERS IS WITHIN THE SCOPE OF ROUTINE INSPECTION OF THIS AREA, PER FAA-APPROVED BOEING SERVICE BULLETIN 767-53-0093. STIFFENER WASSDR 2005UALA00804Stiffener · crackedFWD NOSE SECTION, BS 246 FLOORBEAM, FWD SIDE APPROX LBL 17, VERTICAL STIFFENER CRACKED. ROUTINE INSPECTION IN PLACE TO FIND AND FIX THESE CRACKED STIFFENERS. THIS IS A KNOWN ISSUE ADDRESSED BY BOEING SERVICE BULLETIN AND UA MAINTENANCE PROGRAM.SDR 2005UALA00803Skin · gougedFWD LOWER FUSELAGE, E/E DOOR SKIN IS GOUGED ON THE FWD RT CORNER. THE GOUGE IS AN ISOLATED INCIDENT AND NOT SYSTEMIC TO FLEET. PRODUCTION BLENDED AND FOUND IT TO BE OUT OF THE SRM, SRM 52-40-01 LIMITS. A DOUBLER WAS FABRICATED PER SRM 52-40-01 AND INSTALLEDSDR 2005UALA00923Slide · damagedUPON INFLATION OF THE UNIT, UPPER TUBE IS NOTED WITH TEAR ON THE FABRIC ABOUT .25 INCH LOCATED CLOSE TO PRESSURE RELIEF VALVE. HOLE GOES THROUGH ON TOP AND BOTTOM PART OF THE UPPER TUBE. THE PRESSURE RELIEF VALVE BAND CLAMP SCREW IS NOTED WITH SHARP EDGES THSDR 2005UALA00792Light · inoperativeLEFT SIDE FIRST CLASS EEL STRIPS INOP.SDR 2005UALA00751Skin · puncturedRAMP REPORTED A PUNCTURE IN THE AFT MANUAL PIT DOOR. MEASURES APPROXIMATELY .5 BY .25 IN AN "L" SHAPE. AFTER INTERIM REPAIR WAS REMOVED, A HFEC INSPECTION WAS ACPL AND NO CRACKS WERE FOUND. REPAIR DOUBLER WAS INSTALLED PER SRM 51-20-05 AND 51-40-02. WORK WSDR 2005UALA00742Failsafe · damagedSTATION 1395 FAIL/SAFE CHORD LOWER FLANGE IS DAMAGED BETWEEN STRINGERS 37L AND 38L AND ALSO BETWEEN STRINGERS 38R AND 39R. LOWER AFT FUSELAGE STRUCTURE DAMAGED BY MOVING BAGGAGE CART. DAMAGED STRUCTURE INCLUDED SKIN, STRINGERS, FRAME, TEAR STRAP. COMBINATIOSDR 2005UALA00717Piston Rod · crackedCRACKED PISTON IN THE NOSE LANDING GEAR RETRACT ACTUATOR. ON WALKAROUND FOUND NOSE LANDING GEAR ACTAUTOR ROD NEAR ROD END CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED NOSE GEAR ACTUATOR PER MM 32-34-01. HYDRAULIC QUANTITY WAS OK.SDR 2005UALA00651Power Supply · dischargedEMERGENCY LIGHTS L900, L908 AND L976 ON WITH SW IN ARMED POSITION. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK.SDR 2005UALA00647Engine · overheatedRETURNED TO THE FIELD DUE TO HIGH OIL TEMPERATURE ON NR 2 ENGINE. REPLACED FUEL/OIL COOLER BYPASS VALVE SOLENOID. TESTED OK AFTER REPLACEMENT.SDR 2005UALA00716Piston Rod · crackedCRACKED PISTON IN NOSE LANDING GEAR RETRACT ACTUATOR. ON WALKAROUND FOUND NOSE LANDING GEAR ACTUATOR ROD NEAR ROD END CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED NOSE GEAR ACTUATOR PER MM 32-34-01. HYDRAULIC QUANTITY WAS OK.SDR 2005UALA00612Engine · surgesRETURNED TO IAD DUE TO NR 1 ENGINE COMPRESSOR STALL. SURGE ON POWER REDUCTION AT 5500 MSL. EPR = 1.128. TWO ADDITIONAL SURGES AT EPR < 1.128. NOT GROUP-3 SURGE. TEST-21 NOT REQUIRED. IAD HPC BSI: OK. IAD REPLACED: 2.9 BLEED SOLENOID & RELAY, HP BLEED CONSDR 2005UALA00625Lamp · inoperativeEEL LIGHT RIGHT OF MID GALLEY INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK.SDR 2005UALA00624Lamp · inoperativeEEL LIGHT ADJACENT DR 2R INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK.SDR 2005UALA00605Light · inoperativeEEL INOP AT SEAT ROW 26 TO 36 RT SIDE. FOUND SEAT EEL HARNESS AT 35HJ RIPPED OUT OF ITS MOLEX CONNECTORS UNDER THE SEAT AND FROM THE SIDEWALL CONNECTOR. WIRING WAS REPAIRED. OKSDR 2005UALA00601Hinge Fitting · damagedLT INBD FLAP CENTER HINGE FITTING LINE INBD SIDE DAMAGED. LEFT INBOARD FLAP CENTER HINGE FITTING FOUND DAMAGED ON INBOARD SIDE. REPAIRED PER SRM 57-53-02.SDR 2005UALA00600Skin · corrodedBS 955 CENTER WING BOX UPPER SKIN AT RBL 3 AT AFT SPAR CORRODED, SKIN SPLICE FITTING AND AFT SPAR. CORROSION CAUSED BY MOISTURE IN THE AREA. BLENDED WING SKIN, FABRICATED REPAIR SHIM BETWEEN SKIN AND FITTING, BLENDED SPAR CHORD, AND FABRICATED MODIFIED FITTSDR 2005UALA00593Skin · dentedDENT IN BULK CARGO DOOR, .5 INCHES BELOW EXISTING EXTERNAL REPAIR DOUBLER. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILESDR 2005UALA00582Apu · shutdownDIVERTED DUE TO AUXILIARY POWER UNIT AUTO-SHUTDOWN WITH LEFT GENERATOR DEFERRED INOPERATIVE. UPON LANDING APU FOUND 4.0 QUARTS LOW. MM ADDED OIL. ENGINEERING MONITORING OIL CONSUMPTION. TO DATE CONSUMPTION IS .014 QT/HOUR. LIMIT IS .20 QT/HR. SAMC REQUESTEDSDR 2006UALA01172Latch · wornLT O/W SLIDE DOOR LATCH FAILS EDGE MARGIN CHECK (NR 3 LATCH). REPLACE LATCH IAW 767, MM 25-65-98.SDR 2005UALA00552Bearing · brokenDURING PACKING PROCEDURES, 6 BEARINGS BROKE WHEN TENSION PUT ON BAR. AIRFRAME MANUFACTURER IS AWARE OF THIS ISSUE AND IS EVALUATING CHANGE TO MORE DURABLE BEARING MATERIAL. IN THIS CASE, ALL OF THE BROKEN BEARINGS WERE REPLACED.SDR 2005UALA00483Adc · failedFAILURE OF F/O AIR DRIVEN COMPUTER AND ALTIMETER. RT AIR DATA COMPUTER RPL, MR41190, NO DASH, BUT S/N=88041280. A/C HAD PREVIOUS HISTORY ON 18 MAY. NO UNIT HISTORY AVAILABLE IN CIDER FOR THIS S/N, SUSPECT THIS IS 1ST REMOVAL.SDR 2006UALA01170Latch · failedLT O/W DOOR LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES REF UAL B767 MM-25-65-98.SDR 2005UALA00468Slide · defectiveDURING REMOVAL OF THE LEFT OVER WING SLIDE IT WAS FOUND TO BE DEFECTIVE.SDR 2006UALA01169Keeper · frozenLT O/W HATCH SLIDE DOOR HAS 1 KEEPER FROZEN. REPLACE KEEPER IAW 767 MM 25-65-98.
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