N643UA

Service difficulty reports · 451

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N643UA' AND registry_match = 'registration'
  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 UALA2013040502266Connector · damagedWIRE EXPOSED PIGTAIL POSITION P51. REPAIRED PIGTAIL P51 PLUG BACK SHELL, OPS OKAY.Apr 5, 2013 · N643UA · Boeing 767322 · Equipment/Furnishings WiringSDR UALA2013040502267Flashlight · inoperativeEMERGENCY TORCH AT LEFT OVERWING POSITION HAS BROKEN SEAL AND LED IS NOT FLASHING. LEFT OVERWING EMERGENCY FLASHLIGHT DEFERRED IAW MEL. REPLACED AS REQUIRED PER MM 25-00.Apr 4, 2013 · N643UA · Boeing 767322 · Emergency EquipmentSDR UALA2013032501818Guard · brokenAILERON TRIM SWITCH GUARD BROKEN. REMOVED AND REPLACED AILERON, RUDDER TRIM PANEL LIGHT PLATE PER MM.Mar 22, 2013 · N643UA · Boeing 767322 · Indicating/Recording SystemSDR UALA2013031101401Transmitter · faultedABOUT SIX HOURS INTO FLT, CALC FUEL WENT FROM 3000 HIGHER THAN TOTALIZER TO 4000 HIGHER ON PROG 2. REPLACED FUEL FLOW TRANSMITTER MM.Mar 10, 2013 · N643UA · Boeing 767322 · Fuel Indicating SystemSDR UALA2013030101242Door Actuator · leakingHYD LEAK IN LEFT WHEEL WELL. APPEARS TO BE FROM CEILING AREA. REPLACED LEFT GEAR DOOR ACTUATOR. PRESSURIZED SYSTEM AND CYCLED DOOR NUMEROUS TIMES, FOUND NORMAL.Feb 26, 2013 · N643UA · Boeing 767322 · Landing Gear Door ActuatorSDR UALA2013022701188Cylinder · damagedRIGHT OVERWING ESCAPE SLIDE CABLE BALL IS NOT IN THE MIDDLE AND IS BELOW RETAINER SPRING. REPLACED CYLINDER IAW AMM 25-65-02 STEP 2C (2).Feb 26, 2013 · N643UA · Boeing 767322 · Escape SlideSDR UALA2013022701187Cylinder · damagedLEFT OVERWING ESCAPE SLIDE INFLATION CYLINDER CABLE BALL IS NOT IN THE MIDDLE AND BELOW RETAINER SPRING. REPLACED CYLINDER IAW AMM 25-65-02 UP TO STEP 2C (2).Feb 26, 2013 · N643UA · Boeing 767322 · Escape SlideSDR UALA2013021901005Outflow Valve · failedOUTFLOW VALVE INDICATOR MOVES RANDOMLY. REMOVED AND REPLACED OUTFLOW VALVE, OPS CHECKED GOOD.Feb 19, 2013 · N643UA · Boeing 767322 · Pressure Regulator/Outflow ValveSDR UALA2013021200850Computer · failedDURING TAXI, LT EICAS COMPUTER FAILED. REPLACED LEFT EICAS & LOADED SOFTWARE PER MM, GROUND CHECKED NORMAL.Feb 10, 2013 · N643UA · Boeing 767322 · Central ComputersSDR UALA2013012900548Engine · surgesNR 1 ENGINE SILENT SURGE CHECKS. ECM DETECTED A 'SILENT' SURGE AT OR NEAR TOP OF DESCENT AT LOW POWER ON FLT 959-28. ECM DOES NOT SHOW ANY PARAMETER SHIFTS BEFORE THE SURGE. THIS IS THE SECOND SURGE WITHIN A WEEK.Jan 28, 2013 · N643UA · Boeing 767322 · Engine (Turbine/Turboprop)SDR UALA2013010700075Actuator · faultyAILERON LOCKOUT. REPLACED LEFT AILERON LOCKOUT ACTUATOR PER MM, OPS TESTED GOOD. NO MESSAGES NOTED.Jan 6, 2013 · N643UA · Boeing 767322 · Aileron Control SystemSDR UALA2013010700074Pin · missingFWD GALLEY FIRE EXTINGUISHER MISSING PIN. REPLACED FWD GALLEY FIRE EXTINGUISHER.Jan 5, 2013 · N643UA · Boeing 767322 · Fire Bottle, PortableSDR UALA2013010300030Computer · faultyFMC CALC FUEL > TOTALIZER AFTER TO THRU 10000FT AND > 3000 LBS ON LANDING. REFERENCE PTT SEQ 9592015, LEFT EICAS REPLACED PER CH4778. PER FIM 28-41 FAULT TREE 838 PAGE 125, SYSTEM OK IF LESS THAN 4500 LBS DIFFERENCE WHEN INITIAL FUEL LOAD IS GREATER THAN 119Jan 2, 2013 · N643UA · Boeing 767322 · Fuel Quantity IndicatorSDR UALA2012122707406Densitometer · faultyPOSSIBLE FUEL LEAKS. REF CH4688, ITEM(3). NEED TO REMOVE AND REPLACE LEFT AND RIGHT MAIN TANK DENSITOMETER ELECTRONICS UNIT. REPLACED BOTH LEFT AND RIGHT MAIN TANK DENSITOMETER ELEC UNITS.Dec 26, 2012 · N643UA · Boeing 767322 · Fuel Indicating SystemSDR UALA2012122707418Light · inoperativeEMERGENCY CEILING LIGHT AT 29AB INOPERATIVE. RELAMPED, OPS NORMAL.Dec 25, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012121207168Hydraulic Line · damagedLEFT MAIN LANDING GEAR BRAKE LINE HAS BRAIDING EXPOSED WHERE IT WAS WRAPPED. REMOVED AND REPLACED RT GEAR TILT ACT HYD LINE.Dec 7, 2012 · N643UA · Boeing 767322 · Hydraulic System, MainSDR UALA2012112006710Circuit Breaker · faultyAPU GEN DEF INOPERATIVE. ACP VISUAL CHECK OF WIRING PER SVC TIP MM24-21-01 PG200A. THIS SYSTEM HAD WIRE ISSUES (SEQ 1062012,1062011), IF NO DEFECTS NOTICED, REPLACE THE AUX POWER BREAKER (C905)PER MM. REPLACE APU GEN PER MM. DO NOT SIGN THIS DF ITEM AS CHNov 19, 2012 · N643UA · Boeing 767322 · Electrical Power SystemSDR UALA2012111306540Compressor Blade · damagedWHILE ACCOMPLISHING EM3658, FOUND DISTRESS BEYOND MM72-00-00-601 LIMITS TO THE 5TH, 6TH, AND 7TH STAGE HPC BLADES. NUMEROUS NICKS, DENTS, TEARS, AND ONE THIRD OF A 7TH STG HPC BLADE MISSING. RVI PICS POSTED. REPLACED NR 1 ENGINE, S/N 727948.Nov 12, 2012 · N643UA · Boeing 767322 · Turbine Engine Compressor SectionSDR UALA2012111206518Bpcu · faultyAIRPLANE WILL NOT ACCEPT APU POWER. REPLACED BPCU AND GCU AS PER MM. APU POWER NOW OK, SYS CHECK NORMAL.Nov 11, 2012 · N643UA · Boeing 767322 · External Power SystemSDR UALA2012110906456Processor · faultyCREW REPORTS THAT 5 HRS INTO FLIGHT, THAT THE FUEL USED AND THE OVERHEAD INDICATION IS OFF BY 1000LBS. IT STARTED OUT AS MUCH AS 2800LBS, 15 MIN LATER IT WAS 1500LBS. IT APPEARS THAT THE TOTALIZER IS INCONSISTENT. REF MM 28-41-00. ACP'D BITE OF FQIS AND NONov 8, 2012 · N643UA · Boeing 767322 · Fuel Indicating SystemSDR UALA2012110806427Indication Sys · malfunctionedFUEL DISAGREE PROG 2-TOTALIZER 35.9 CALCULATED 39.0-BOTH WINGTANKS SAME QUANTITY. DRIPSTICKS READING PERFORMED BEFORE AND AFTER REFUELING AS PER AMM. UPLIFT FUELER OK VERIFIED WITH OPBLM. FQIS BITE PERFORMED NO FAULTS. FMC FUEL TOTAL EQUAL WITH TOTAL FUEL Nov 6, 2012 · N643UA · Boeing 767322 · Fuel Quantity IndicatorSDR UALA2012110506314Lamp · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE, CEILING BETWEEN ROWS 21 AND 22 RIGHT. REPLACED LAMP, OPS NORMAL.Nov 4, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012110506313Lamp · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE CEILING ROW 6 RIGHT. REPLACED LAMP, OPS NORMAL.Nov 4, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012110506312Lamp · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE DOORWAY 1 RIGHT. REPLACED LAMPS, OPS NORMAL.Nov 4, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012110506311Lamp · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE CEILING BETWEEN ROWS 34 AND 35 LEFT. REPLACED LAMPS, OPS NORMAL.Nov 4, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012110506310Lamp · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE CEILING ROW 29 LEFT. REPLACED LAMPS, OPS NORMAL.Nov 4, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012101805963Structure · dentedDENT ON LOWER FWD EDGE OF DOOR 2R. DENT IS LOCATED BOTTOM EDGE 16INS FROM BOTTOM AND 6.5INS FROM FWD EDGE DEPTH .020INS. 3INS LONG AND 1 IN WIDE. FREE OF SHARP CREASES.Oct 17, 2012 · N643UA · Boeing 767322 · Service DoorsSDR UALA2012091905305Computer · faultyWHILE ACP CAT 3 CHECK HAVE FAULT AIL SERVO RT FAIL. REPLACED RIGHT FCC, AIL TESTED OK.Sep 17, 2012 · N643UA · Boeing 767322 · Autopilot ComputerSDR UALA2012083104902Fan · faultyCREW REPORTED SMOKE AND FUMES IN CABIN FOLLOWED BY A LEFT RECIRC FAN EICAS MESSAGE. FAN TURNED OFF AND SMOKE-FUMES BEGAN TO DISSIPATE. FLIGHT ATTENDANT REPORTED SMOKE FUMES MOST PRONOUNCED AT MID CABIN LEFT SIDE AREA. SUSPECT BAD LEFT RECIRC FAN. FAN MADE Aug 31, 2012 · N643UA · Boeing 767322 · Air Distribution FanSDR UALA2012090404939Unknown · smokeCREW REPORTED SMOKE AND FUMES IN CABIN FOLLOWED BY A LEFT RECIRC FAN EICAS MESSAGE.Aug 31, 2012 · N643UA · Boeing 767322 · Air Distribution SystemSDR UALA2012082904864Slide · out of positionFLIGHT ATTENDANT UNABLE TO DETERMINE IF L2 DOOR IS DISARMED. REPOSITIONED L2 DOOR SLIDE PER AMM. DOOR OPERATION AND SLIDE ARM CHECKED CONFIRMED SAFETY PINS REMOVED AND ALL LANYARDS ATTACHED. VERIFIED L2 DOOR SLIDE PACK INSTALLATION IAW AMM 25-66-01.Aug 28, 2012 · N643UA · Boeing 767322 · Escape SlideSDR UALA2012080604211Connector · damagedAPU GENERATOR FEEDER CABLES BULKHEAD CONNECTOR DISCONNECTED. WIRES FOUND BURNED AND WELDED TOGETHER. APU GCU CIRCUIT BREAKER COLLARED. INSTALLED APU GEN CABLE 6F16610-501 HARNESS FROM GEN TO BULKHEAD REF MM 24-21-01-409. DISCONNECTED HARNESS IN STAB COMPARAug 2, 2012 · N643UA · Boeing 767322 · AC Generator-AlternatorSDR UALA2012072303957Filter · warning lightRT ENGINE FUEL FILTER, RETURNED TO FIELD, REPLACED FUEL PUMP FILTER PER MM. RAN ENGINE, LEAK CHECKED GOOD AND NO FILTER MESSAGE.Jul 20, 2012 · N643UA · Boeing 767322 · Fuel Injector NozzleSDR UALA2012070103507Gcu · failedNR 2 ENGINE GENERATOR WILL NOT STAY ON LINE. REPLACED RIGHT ENGINE GCU AND ENG CONTROL BREAKER C903. RAN ENGINE TWICE GEN OPERATED NORMAL.Jun 29, 2012 · N643UA · Boeing 767322 · AC Generator-AlternatorSDR UALA2012062203341Window · crackedCAPTAIN'S WINDSHIELD'S VISIBILITY IS IMPAIRED, REPLACEMENT IS REQUESTED. CREW COMMENTS: AT FL360 LOUD POP AND CAPT FWD WINDOW SHATTERED. NO AIR LEAKS. FORWARD VISION IMPAIRED. REPLACED CAPTAINS WINDOW PER AMM.Jun 17, 2012 · N643UA · Boeing 767322 · Flight Compartment WindowsSDR UALA2012051102729Valve · faultyRIGHT BLEED LIGHT AND HIGH STAGE (OVERHEAT) LIGHT ILLUMINATED. DESCENDING FROM FL380. ACCOMPLISHED QRH ITEMS. BLEED OVERHEAT AND RT PACK OFF LIGHT REMAINED ON. ACCOMPLISHED AN OPERATIONAL TEST PER MM. ACCOMPLISHED BITE CHECK OF AIR SUPPLY BLEED MODULE IAWMay 10, 2012 · N643UA · Boeing 767322 · Pneumatic Distribution SystemSDR UALA2012051102728Indicator · faultyVHF 1 RIGHT DISPLAY, HUNDREDS DIGIT FAINT. REPLACED NR 1 VHF COMM CONTROL PANEL PER MM, OPS NORMAL.May 10, 2012 · N643UA · Boeing 767322 · VHF Communications SystemSDR UALA2012041702322Connector · faultyR ENG A-O VALVE STATUS MSG. PERFORMED BITE ON PIMU, FOUND MSG. EEC CH A, AOC TR CHECK FAIL AND AOC T, M W, A FAIL. PERFORMED CONT CHECK AND INSPECTED AND CLEANED CONNECTORS W3P17 AND W1P 6. ALL CHECK NORMAL. RAN ENG. NO FURTHER FAULT.Apr 16, 2012 · N643UA · Boeing 767322 · Turbine Engine System WiringSDR UALA2012041502278Control Panel · faultyACFT HAS HOT MIC. REMOVED & REPLACED VHF CONTROL PANEL PER AMM, OPS CHECKED GOOD.Apr 13, 2012 · N643UA · Boeing 767322 · VHF Communications SystemSDR UALA2012030501409Control Unit · faultyAPU FAULT LIGHT ON START UPON LANDING. REPLACED APU CONTROL UNIT, STARTS & RUNS NORMAL.Mar 4, 2012 · N643UA · Boeing 767322 · APU ControlsSDR UALA2012022701193Eec · malfunctionedENG EXPERIENCED A 'SILENT SURGE'. PLEASE REPLACE THE EEC MR73412 PCN 480-9191. REF MM 73-21-04 P4XX. PUT EG ALERT TAG ON REMOVED EEC. WRITE RMVL REASON AS "ROUTE TO HS FOR PB SENSORS RPLMNT. REF HS SB EEC131-73-62 DUE SURGE". REPLACED LT ENG EEC PER MM, Feb 26, 2012 · N643UA · Boeing 767322 · Fuel Control/Turbine EnginesSDR UALA2012021700960Control Valve · vibrationVIBRATION STILL FELT ON 6 MINUTE CYCLE. CAN BE FELT IN COCKPIT FLOOR. ALL CRUISE ALTITUDES. FWD CARGO HEAT DUCTING IN RT AC BAY IS SECURED. WILL NEED TO INSPECT PICCOLO DUCT IN FWD CARGO PIT FLOOR. NOT ENOUGH TIME TO DISASSEMBLE FWD CARGO PIT FLOOR PANELSFeb 16, 2012 · N643UA · Boeing 767322 · Air Distribution SystemSDR UALA2012021600949Indicator · faultyAIRFRAME VIBRATION FELT EVERY 6 MIN, LASTING 1 MIN. CABIN RATE -500FPM AT BEGINNING & CONT. REPLACED CABIN PRESS INDICATOR PER AMM. VERIFIED REMOTE DIFFERENTIAL PRESS SENSOR WAS COMPATIBLE.Feb 15, 2012 · N643UA · Boeing 767322 · Cabin Pressure Control SystemSDR UALA2012021400877Battery · dischargedEMERGENCY LIGHT SIGN AT 19A AND EMERGENCY LIGHT STRIP, BY LT MID LAV CAME ON FOR ABOUT 30 MIN IN FLT THEN FLICKERED AND WENT OUT. DISCONNECT AND RECONNECTED EMERGENCY BATTERY PACK PER MM AND TESTED PER MM. ACP FIM 33-51-00-108 SYS PASSED OK, NO FAULTS FOUND.Feb 14, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012013000580Light · intermittentEMERGENCY PATH LIGHTS BY WINDOW EXIT LEFT SIDE 19A-B FLASH ON & OFF. CHECKED EEL FAULT. COULD NOT REPRODUCE, OK DURING GROUND CHECK.Jan 28, 2012 · N643UA · Boeing 767322 · Emergency LightingSDR UALA2012012400485Bearing · faultySUSPECT NOSE GEAR DOOR SLIGHTLY DROOPING AS FEEL LIGHT VIBRATION IN CRUISE FL 340 MACH .820. SAMC TEXT: CREW NOTICED RUMBLING MORE PRONOUNCED ON MID CABIN LEFT SIDE. TURNED OFF FWD GALLEY EQUIPMENTS, INCREASE & DECREASED AIR SPEED, NO CHG. ENG'S PNEUMATIC Jan 22, 2012 · N643UA · Boeing 767322 · Landing Gear DoorsSDR UALA2012011600346Wire Harness · defectiveRIGHT VIBRATION GAUGE INDICATES 0 BOTH N1 AND N2. REPLACED NR 2 ENGINE ACCELEROMETER. ACP'D IDLE RUN AND N1 SHOWED 0.0 TO 0.1, N2 STAYED AT 0.0. IDLE RUN INCONCLUSIVE. REPLACED WIRE HARNESS FROM PLUG D8836P TO ACCELEROMETER D10994 DUE TO OPEN WIRE W3504-01TJan 15, 2012 · N643UA · Boeing 767322 · Engine Indicating System WiringSDR UALA2012011600319Apu · faultyAPU FIELD OFF LIGHT ON AFTER APU REPLACEMENT DURING OPS CHECK. REPLACED APU FUEL CONTROL, NO HELP. APU AUTO SHUTDOWN FAULT LIGHT ON OVERTEMP ECU MESSAGE. MR49305 ON-86 OFF159. TRIED TWO FUEL CONTROL UNITS. SAME RESULT. SWAPPED APU CONTROL UNIT (ECU) AND Jan 14, 2012 · N643UA · Boeing 767322 · APU Core EngineSDR UALA2012011200271Eec · failedIDLE DISAGREE EICAS, RTFL. REPLACE RT ENGINE EEC FOR TROUBLESHOOTING. REPLACED EEC PER AMM, ACCOMPLISHED ENG RUN PER TASK 6 MM 71-00-00-501, NO HELP. CARRIED OUT PIMU BITE TEST FOUND CHANNEL A & B MESSAGES, EEC UNIT FAIL-EEC CTRL- EEC CAT 1 AND EEC CAT 2 MESSJan 11, 2012 · N643UA · Boeing 767322 · Fuel Controlling SystemSDR UALA2011122907155Floorbeam · corrodedCORROSION UNDER FASTENER HOLES IN AFT CARGO FLOORBEAM AT BS 1197.132 LBL 6.5 TO LBL 10. FOUND CORROSION TO BE OUT OF LIMITS AFTER BLENDING. REMOVED FLOORBEAM TEE IAW SRM. FABRICATED NEW FLOORBEAM TEE IAW SRM 53-00-07 AND 51-42-05. ALODINED AND PRIME AND TOP CDec 28, 2011 · N643UA · Boeing 767322 · Fuselage Main, Floor Beam
Back to N643UA