N652UA

Service difficulty reports · 303

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 = 'N652UA' 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 CALA2013110592661Light · inoperativeCAPTAINS EXECUTE LIGHT ON FMS IS BURNED OUT.Nov 3, 2013 · N652UA · Boeing 767322 · Flight Management Computing Hardware SystemSDR CALA2013100391692Shade · damagedLT EMERGENCY EXIT WINDOW SHADE DAMAGED. STOWED IN THE OPEN POSITION. PLACED ON DF0082.Oct 2, 2013 · N652UA · Boeing 767322 · Passenger Compartment EquipmentSDR CALA2013092591458Control Panel · faultyCREW REPORTS RT FLIGHT DIRECTOR INOPERATIVE. DEFERRED IAW MEL. MAINTAIN INSTRUCTION SOURCE SELECT SWITCH IN OPERATIVE POSITION FOR ALL PHASES OF FLIGHT. RT FLT DIRECTOR WAS DEFERRED BEFORE CREW REPORTED MCP PROBLEM. MODE CONTROL PANEL REPLACED. RT FLT DIRESep 25, 2013 · N652UA · Boeing 767322 · Flight Management Computing Hardware SystemSDR CALA2013092591433Autopilot Sys · malfunctionedMODE CONTROL PANEL FREEZES AT POWER TRANSFER & RT FLIGHT DIRECTOR DISAPPEARS. REPLACED MODE CONTROL PANEL IAW AMM & TESTED IAW AMM. FOUND ALL WORKING EXCEPT CENTER AUTO PILOT. DEFERRED CENTER AUTO PILOT IAW MEL 2210C. PERFORMED MCDP TEST FOR FCC LT, RT, BSep 25, 2013 · N652UA · Boeing 767322 · Autopilot SystemSDR CALA2013092491392Module · faultyR & L REV ISOLATION VALVE EICAS ILLUMINATED WITH THROTTLE QUAD LIGHT ON. REPLACED THRUST REVERSER RELAY MODULE IAW 78-36-03, OPERATIONS CHECKED GOOD.Sep 22, 2013 · N652UA · Boeing 767322 · Engine Thrust ReverserSDR CALA2013092391378Charger · inoperativeMAIN BATTERY CHARGER INOPERATIVE. R & R MAIN BATTERY & BATTERY CHARGER IAW AMM.Sep 22, 2013 · N652UA · Boeing 767322 · Battery/Charger SystemSDR CALA2013091191216Solenoid Valve · faultyLOST ELECTRICAL POWER & APU FAULT EICAS MESSAGE. R&R DEOIL SOLENOID VALVE, OPERATIONS CHECKED GOOD.Sep 9, 2013 · N652UA · Boeing 767322 · APU Oil SystemSDR CALA2013090290933Fan · faultyFORWARD EQUIPMENT BAY EXHAUST FAN STATUS MESSAGE AT GATE WILL NOT ERASE. R & R FORWARD EQUIPMENT BAY EXHAUST FAN, FAN CONTROL CARD M990 & K1009 CONTROL RELAY. EQUIPMENT BAY EXHAUST FAN STATUS MESSAGE CLEARED & SYSTEM OPERATIONS NORMAL.Sep 1, 2013 · N652UA · Boeing 767322 · Air Distribution FanSDR CALA2013082290662Valve · inoperativeRT INTEGRATED DRIVE GENERATOR VALVE STATUS MESSAGE. RT ENGINE INTEGRATED DRIVE GENERATOR VALVE INOPERATIVE. NIL TIME TO T-S. MEL COMPLIED WITH.Aug 21, 2013 · N652UA · Boeing 767322 · AC Generator-AlternatorSDR CALA2013081490455Seal · leakingCAPTAIN`S SIDE WINDOW HAS AN AIR LEAK IN AFT UPPER VERTICAL FRAME. FOUND AFT UPPER SEAL DAMAGED. R & R NR 2 CAPT'S OPENABLE WINDOW IAW AMM.Aug 14, 2013 · N652UA · Boeing 767322 · Flight Compartment WindowsSDR CALA2013081390427Microphone · damagedF/O HAND MICROPHONE STRAIN RELIEF PULLED OUT OF PLUG. REPLACED HAND MIC.Aug 12, 2013 · N652UA · Boeing 767322 · Communications SystemSDR CALA2013080990293Warning Light · false activationRIGHT OIL FILTER EICAS CAME ON MOMENTARILY 2-3 TIMES.Aug 8, 2013 · N652UA · Boeing 767322 · Turbine Engine Oil SystemSDR CALA2013080790233Connector · dirtyRT PIMU MESSAGE, FOUND A CHANNEL RESISTANCE LOW AND FLUCTUATING. FOUND DEBRIS IN CONNECTOR W5J12. CLEANED CONNECTOR AND SECURED. PERFORMED EEC STATIC CHECK IAW MM 71-00-00. OPS CK GOODAug 6, 2013 · N652UA · Boeing 767322 · Engine Fuel System WiringSDR CALA2013072990026Fairing · crackedFLAP CANOE FAIRING, 571DB HAS 1 INCH CRACK INBD SIDE. PERFORMED PERMANENT REPAIR IAW SRM 57-53-70, 1 PAGE, 103 NOTE A.Jul 28, 2013 · N652UA · Boeing 767322 · Trailing Edge FlapsSDR UALA2013072605253Controller · failedLEFT ENGINE PRIORITY VALVE EICAS MESSAGE. R & R NR 1 ENGINE PRESSURE REGULATOR VALVE CONTROLLER IAW AMM. ACCOMPLISHED ENGINE IDLE RUN, NO BLEED FAULTS.Jul 26, 2013 · N652UA · Boeing 767322 · Pneumatic Distribution SystemSDR UALA2013071204898Heat Exchanger · failedLEFT IDG VALVE STATUS MESSAGE. REPLACED IDG AIR-OIL HEAT EXCHANGER IAW MM. OPS TESTED IAW AMM, TESTED GOOD, IDG OPS NORMAL.Jul 9, 2013 · N652UA · Boeing 767322 · AC Generator-AlternatorSDR UALA2013071204897Switch · failedAPU START SWITCH DOES NOT SPRING RETURN FROM "START" TO "ON". REPLACED APU START SWITCH AND OPS NORMAL.Jul 9, 2013 · N652UA · Boeing 767322 · APU Start/Ignition SystemSDR UALA2013070904787Pressure Switch · failedFUEL SYSTEM PRESSURE EICAS MESSAGE, FLT DIVERTED. REPLACED THE LEFT AFT BOOST PUMP PRESSURE SWITCH.Jul 7, 2013 · N652UA · Boeing 767322 · Fuel Boost PumpSDR UALA2013070504704Pump · failedLEFT FWD FUEL PUMP EICAS MESSAGE. NO ASSOCIATED PRESSURE LIGHT IN LT FWD FUEL PUMP SWITCH. FOUND P6 CIRCUIT BREAKER FWD BOOST PUMP OPEN. REPLACED LT FWD BOOST PUMP. LEAK AND OPS CHECKED GOOD.Jul 3, 2013 · N652UA · Boeing 767322 · Fuel Boost PumpSDR UALA2013061704161Outflow Valve · malfunctionedRECEIVED A CABIN ALTITUDE WARNING IN AUTO 1 - CABIN ALTITUDE REACHED 10,000 FT, MANUAL CONTROL AND AUTO 1 OK, NOW CONTROL OK AND AUTO 1 OK. NOW SHOWING GRADUAL CLIMB IN AUTO 1 EVEN THOUGH DIFFERENTIAL PRESSURE IS LESS THAN 8 PSI. CREW SELECTED MANUAL AND REJun 14, 2013 · N652UA · Boeing 767322 · Pressure Regulator/Outflow ValveSDR UALA2013050903247Audio Panel · weakFIRST OFFICER`S AUDIO PANEL VOLUME WEAK ALL CHANNELS SPEAKER VOLUME OK HEADSET WEAK. REPLACED MINITEL.May 9, 2013 · N652UA · Boeing 767322 · Audio Integrating SystemSDR UALA2013050603144Circuit Breaker · trippedCREW REPORTED CIRCUIT BREAKER G17 ON P11 TRIPPED SHORTLY AFTER TAKEOFF. G17 FOR 1R CSEU AC PWR SUPPLY. RESET NOT ATTEMPTED DUE TO POWER SUPPLY 2R POWERING THE CSEU. RERACK CSEU POWER SUPPLY AND CHECK PINS ALL OK RESET CIRCUIT BREAKER. CIRCUIT BREAKER STAYMay 3, 2013 · N652UA · Boeing 767322 · AC Power Distribution SystemSDR UALA2013042202753Actuator · leakingRUNNING HYD LEAKAGE FROM VERTICAL STABILIZER. INDENTIFIED LEAKING COMING FROM RUDDER RATIO ACTUATOR (RRCA) ROD END. RRCA NEED REPLACEMENT REF AMM 27-21-15.Apr 22, 2013 · N652UA · Boeing 767322 · Rudder Tab Control SystemSDR UALA2013041502542Contact · dirtyAFT CARGO FIRE EXTINGUISHER ARM LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. CLEANED AND RESEATED CONTACTS ON ARM LIGHT. OPS TESTED NORMAL.Apr 12, 2013 · N652UA · Boeing 767322 · Fire Protection System WiringSDR UALA2013041202524Hook And Loop · looseLIFE VEST POUCH ON CAPT SEAT IS LOOSE. REPLACED VELCRO ALL OPS OK.Apr 12, 2013 · N652UA · Boeing 767322 · Emergency EquipmentSDR UALA2013040302178Pump · failedFUEL CONFIGURATION LIGHT ON DURING CRUISE. ALL PUMPS ON. NO LIGHTS. PERFORMED FUEL PROCESSOR BITE FOUND FAULTS RM DENS SENSOR FAILURE A01, AND RM DENS SENSOR OPEN AT SPAR A01. VERIFIED MFQ OF RT AND LT TANKS TO BE WITHIN LIMITS VIA STICK READINGS AND PER FApr 2, 2013 · N652UA · Boeing 767322 · Fuel Indicating SystemSDR UALA2013032802008Blocker Door · damagedNR 1 ENGINE HAS A DAMAGED BLOCKER DOOR ON THE INNER THRUST REVERSER HALF AT THE 4.30 TO 5 O'CLOCK POSITION. REMOVED BLOCKER DOOR AND DRAG LINK PER CDL AND MM78-31-14 AND 15. REPLACED BLOCKER DOOR.Mar 27, 2013 · N652UA · Boeing 767322 · Engine Thrust ReverserSDR UALA2013032601896Liner · dentedNR 1 ENGINE INBOARD THRUST REVERSER HALF HAS THREE DENTS IN THE ACOUSTIC LINER IN THE INNER C DUCT. REPAIRED IAW SRM 54-00-01 REPAIR 1 AND 2.Mar 25, 2013 · N652UA · Boeing 767322 · Engine Thrust ReverserSDR UALA2013022701195Control Unit · failedACFT RETURNED TO BLOCKS WITH C1 ELECTRIC HYDRAULIC PUMP INOPERATIVE. NO HYD PRESSURE ON EICAS PAGE. FOUND PUMP TO OPERATE NORMAL FOR ABOUT 10 MINUTES AND THEN SHUTOFF UNCOMMANDED WITH NO UNUSUAL MESSAGES. REPLACED ELCU PER MM 29-11-14. RAN PUMP FOR 30 MINUFeb 26, 2013 · N652UA · Boeing 767322 · Hydraulic System, MainSDR UALA2013012500476Probe · failedLT ENGINE EEC MODE ILLUMINATED, FLT DIVERTED. REPLACED PT2 TT2 PROBE REF MM 73-21-03 ACCOMPLISHED PT2 SYSTEM LEAK TEST NO14 REF MM 71-0 0-00 AND EEC IDLE TEST NO6 REF MM 71-00-00 ALL CHECKED OK.Jan 25, 2013 · N652UA · Boeing 767322 · Fuel Control/Turbine EnginesSDR UALA2013012800492Wire Harness · chafedCREW REPORTED WHEN LEFT ENGINE START SELECTED, CBS D19 (LT ENG START CONT) AND D28 (STBY ENG IND) ON P11. MAINTENANCE FOUND BENT PIN AT CONNECTOR D7982P ON P61 AND DAMAGED WIRES ON START VALVE HARNESS REF WDM80-11-11. FOUND WIRE BUNDLE TO STARTER VALVE CHAFEJan 25, 2013 · N652UA · Boeing 767322 · Engine Starting System WiringSDR UALA2013012500461Start Valve · faultyWHEN GROUND SELECTED FOR LT ENGINE START, CIRCUIT BREAKER D28 AND D19 TRIPPED. REPLACED LEFT ENGINE START VALVE.Jan 25, 2013 · N652UA · Boeing 767322 · Engine Start Valves/ControlsSDR UALA2013010700079Anti-Ice Valve · damagedHMG HAS BEEN DEF IN COMPLIANCE WITH MEL CARD. REPLACED NUMBER 1 ENGINE COWL TAI VALVE REF AMM, NO HELP. ENG ANTI- ICE VALVE REPAIRED AND HMG SYSTEM HAS BEEN RESTORED PER MEL CARD. RAN CHECK & HMG CHECKED NORMAL. PERFORMED LEFT ENGINE ANTI-ICE VALVE TEST AJan 7, 2013 · N652UA · Boeing 767322 · Engine Anti-Icing SystemSDR UALA2013010400051Hydraulic Line · leakingRIGHT HYDRAULIC SYSTEM QTY READS .81 ON ARRIVAL LHR. HYDRAULIC LINE LEAKING IN AREA BELOW RIGHT INBD SPOILER ACTUATOR. FOUND HYDRAULIC LINE WITH IMPACT DAMAGE. SEE IPC REF 29-11-77-005 ITEM 560. REPLACEMENT TUBE SECTION IAW AMM 20-10-09 REV 75 & GPM 1-0-13Jan 3, 2013 · N652UA · Boeing 767322 · Hydraulic System, MainSDR UALA2012111306537Hinge · brokenLEFT WING THERMAL ANTI-ICING DUCT SEAL DOOR ASSY AFT HINGE BROKEN AND AFT OUTBD. CORNER OF PANEL SHEET METAL TORN. REMOVED DAMAGED DOOR ASSEMBLY AND HARDWARE AND PLACED IN BULK PIT. REMOVED DAMAGED ERODED EDGE STRIP AND APPLIED LAY-UP REPAIR PER SRM 57-41-0Nov 13, 2012 · N652UA · Boeing 767322 · Wing Miscellaneous StructureSDR UALA2012111306538Skin · crackedLEFT WING NR 5 LEADING EDGE SLAT HAS A CRACK IN THE LOWER SURFACE OF THE SLAT SKIN AT THE TAB INBOARD OF THE ANTI ICING DOOR ASSEMBLY. CRACK STARTS AT AFT EDGE OF TAB AND EXTENDS 1 INCH TO RIVET. COMPLIED WITH SRM 57-43-01 PAGE 104 ITEM P. ALL ITEMS IN AREANov 12, 2012 · N652UA · Boeing 767322 · Leading Edge DevicesSDR UALA2012111206510Pressure Sensor · defectiveFLT DECK DOOR CKT BREAK POPPED. TROUBLESHOT SYSTEM FOUND PRESSURE SENSOR BAD. INSTALLED ROBBED SENSOR. GROUND FUNCTIONAL TEST NORMAL IAW WD 52-51-11. NEW SENSOR ON AOG L4650 RESET CB NORMAL.Nov 10, 2012 · N652UA · Boeing 767322 · Fixed Inner DoorsSDR UALA2012102306076Computer · faultyLT ENG HYD LEAK, FLIGHT DIVERTED. CREW REPORTS AUTOTHROTTLE DISCONNECT. WOULD NOT RESET. REPLACED THRUST MANAGEMENT COMPUTER PER MM. HYDRAULIC L ENG PUMP SUPPLY CB POPPED. LOCATION OVHD PANEL D29. LEFT ENG HYD SHUT-OFF VALVE IS LEAKING AT UPPER MATING FLOct 22, 2012 · N652UA · Boeing 767322 · Auto Throttle SystemSDR UALA2012092105368Transmitter · faultyINBOARD AILERONS DO NOT EXTEND SYMMETRICALLY WHEN FLAPS ARE LOWERED; RT SIDE DROPS LOWER. FOLLOWED FIM 27-18-00 FIG 106 FOR INDICATOR FAILS TO RETURN TO ZERO WITH CONTROL WHEEL ZERO. FOLLOW "NO" ON DIAGRAM AND NEXT STEP STATES TO EXAMINE AILERON CABLE SYSTEM.Sep 20, 2012 · N652UA · Boeing 767322 · Aileron Control SystemSDR UALA2012090605034Transmitter · faultyFLAP SLAT ELEC STATUS MSG. DUE TO REPEAT FLAP SLAT ELEC STATUS EICAS MESSAGES AND NOTHING FOUND WHEN BITING THE FSEU, INSTALL A -63 FSEU PCN 481-9266 PER MM. CREATED A CF ITEM STATING THAT THE -63 IS INSTALLED AND TO BE REMOVED AT A LATER DATE. REPLACED FSESep 6, 2012 · N652UA · Boeing 767322 · Trailing Flap Position Indicating SystemSDR UALA2012090404978Inverter · faultySTANDBY INVERTER STATUS MESSAGE . REPLACED STANDBY INVERTER IAW MM.Sep 1, 2012 · N652UA · Boeing 767322 · AC InverterSDR UALA2012081604551Wire · chafedAFT VACUUM BLOWER (LAV SYS 1) CIRCUIT BREAKER POPPED. TROUBLESHOT AS PER WD 38-32-11. FOUND NO POWER AT PINS 2 AND 3 ON D1266, HAVE 115V AC AT PINS 22 2 0 24 ON D6314 NEED TO CHECK FROM D1266 BACK. NO FURTHER TIME DUE TO AC MOVEMENT BLOWER SYSTEM DEACTIVATEAug 14, 2012 · N652UA · Boeing 767322 · Vacuum System WiringSDR UALA2012072303982Duct · damagedAPU COOLING AIR DUCT DAMAGED. REPLACED COOLING AIR DISCHARGE DUCT AND SECURED WITH CLAMPS PER AMM.Jul 23, 2012 · N652UA · Boeing 767322 · Pneumatic Distribution SystemSDR UALA2012072303992Pressure Switch · failedLOW OIL PRESSURE SWITCH FAULTED. REPLACED LOW OIL PRESSURE SWITCH RAN APU. APU AUTO SHUTDOWN AFTER 90 SEC.Jul 21, 2012 · N652UA · Boeing 767322 · APU Oil SystemSDR UALA2012072303985Control Unit · faultyAPU AUTO SHUTDOWN AT THE GATE. REPLACED CONTROL UNIT PER MM. OPERATED APU PER JRH 2-6-15 WITH PNEUMATIC AND ELEC LOAD APPLIED. RUNS NORMAL.Jul 21, 2012 · N652UA · Boeing 767322 · APU ControlsSDR UALA2012072303994Filter · faultyFOUND APU GENERATOR LUBE SYSTEM FILTER DIFFERENTIAL PRESS IND POPPED. REPLACED APU GENERATOR LUBE SYSTEM FILTER AND RESET DIFFERENTIAL PRESSURE INDICATOR.Jul 19, 2012 · N652UA · Boeing 767322 · APU Oil SystemSDR UALA2012071903934Pressure Switch · failedAPU AUTO SHUTDOWN. APUC BITE TEST SHOWED LOP. REPLACED LOW OIL PSI SWITCH. REPLACED APU DEOIL SOLENOID AND FLOW SENSING MODULE-NO HELP. FOUND DIFFERENTIAL PRESS IND POPPED FOR GENERATOR LUBE FILTER.Jul 18, 2012 · N652UA · Boeing 767322 · APU Oil SystemSDR UALA2012071103700Brake · fireLEFT MAIN GEAR AFT INBD BRAKE TEMP WENT TO 7. GROUND CREW NOTED FLAME AND DISCHARGED POWDER TYPE FIRE EXTINGUISHER. TIRE FUSE DID NOT RELEASE. CDG FIRE DEPT WAS CALLED AND SPRAYED WATER ON LEFT MAIN BRAKES. WHEEL AND BRAKE REPLACED LEFT MAIN GEAR AFT INBD Jul 9, 2012 · N652UA · Boeing 767322 · Landing Gear Brake SystemSDR UALA2012070503600Access Panel · out of adjustLEFT WING FUELING PANEL WILL NOT STAY OPEN. SUPPLEMENTAL DATA, FUELING PANEL DOOR HOLD OPEN EYELET ADJUSTED TO SIT CORRECTLY IN RETAINING HOLE. NOW OPERATES NORMALLY.Jul 3, 2012 · N652UA · Boeing 767322 · Wing, Plate/SkinSDR UALA2012070203512Brake · fireHOT BRAKES, RAMP SAW FLAMES COMING FROM BRAKE. ACCOMPLISHED INSPECTION MM.Jun 28, 2012 · N652UA · Boeing 767322 · Brake Anti-Skid Section
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