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.
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
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 UALA2012051102755Valve · malfunctionedUNABLE TO CONTROL CABIN TEMP. CYCLED CB C33 PER TOMC AND REGAINED CAB TEMP CONTROL. FOUND MID TRIM MODULATING VALVES IN OPEN POSITION. AS PER DF0690 CLOSED AUX MID AND MID MODULATING VALVES.SDR UALA2012032601906Panel · damagedLEFT WING FIXED T/E UPPER OTBD PANEL HAS DAMAGE. REF IPC 57-51-65-002 REMOVED AND ROUTED TO SHOP 273 FOR DELAM REPAIR ON R62260.SDR UALA2012031501721Panel · damagedLT WING PANEL ISSUE, FLIGHT DIVERTED. THE L/E IS UP INTO THE AIRSTREAM APPROX 2-3 INCHES. NO CONTROL OR VIBRATION PROBLEMS. REMOVED PANEL. REPAIRED IAW EC-RA NR 5700-03044SDR UALA2012030601427Cable · shortedP62 PIGTAIL SPARKS WHEN DISCONNECTED. COLLARED CB. REPLACED SHORTED PIGTAIL CABLE AND RESET C-B.SDR UALA2012011900412Control Unit · faultyFLAP-SLAT MSG. TRBLSTG PER FIM. NEW FSEU, NO HELP. FAULTING M548 OTBD SLAT POS XDCR. ON AOG, E5555 ETA 0450. DMM 0240. REPLACED FSCU PER MM. SYSTEM OPERATED NORMAL. NO EICAS OR STATUS MSG. PRESENT.SDR UALA2012010300042Igniter · failedNO EGT RISE ON RT ENG WITH NR 2 IGNITION START OK ON BOTH IGNITORS. REPLACED NR 2 IGNITER PLUG IAW MM, ENGINE STARTED OK PER JRH 2-6-1.SDR UALA2012010300060Wire · brokenCENTER FCC FAILS INTERFACE TEST 04. FOUND WIRE W011-770-22 BROKEN AT CONNECTOR D479. REPINNED WIRE REF BOEING STANDARD PRACTICES MANUAL 20-10-13. CTR FCC TEST NORMAL. ACP CAT III TEST PER MM, TEST PASSED. AIRCRAFT RETURNED TO CAT III STATUSSDR UALA2012010300059Selector Knob · brokenHEADING SELECT KNOB BROKEN BUT USEABLE. REPLACED MCP PER MM.SDR UALA2011121906930Panel · looseFOUND DURING WALK AROUND THE RT ANTI-ICE DUCT FAIRING PANEL JUST OUTSIDE OF THE ENGINE REAR PART HANGING DOWN. REMOVED PER CDL 57EE. DOOR ASSY IS LOST. REPLACED PANEL.SDR UALA2011120606720Controller · faultyAFT CABIN TEMP EICAS MESSAGE WITH INOP LIGHT ON. RESET ZONE TEMP CONTROLLER - NO HELP. CW MEL. REPLACED ZONE TEMP CONTROLLER PER MM, OPS CHECK GOOD. NO EICAS MESSAGES OR FAULTS.SDR UALA2011111106162Wire · damagedCREW ABORTED TAKEOFF AT APPROXIMATELY 80 KNOT DUE TO NR 1 GEN DRIVE LIGHT AND ASSOCIATED EICAS MSG. ACCOMPLISH HIGH ENERGY STOP CHECK PER MM 05-51-14 201. ITEM ROLLED FORWARD. ACP'D INSP PER AMM. NO DEFECTS NOTED. DUE TO RECENT REPORTS OF THE NR 1 ENG IDGSDR UALA2011092005081Pressure Switch · faultyLEFT HYD DEMAND PUMP FAILED TO OPERATE IN AUTO WITH ENGINE OFF. WORKS OK IN ON POSITION. -RDF-T :RPL S27 ELEC HYD PUMP L CONTROL PRESSURE SWITCH, NO HELP. REPLACED RELAYS K130, K134, & K131 NO HELP. REPLACED L DEMAND PUMP SWITCH ASSY S5, NO HELP.
CHECKED SDR UALA2011092005080Transceiver · weakHF TRANSMISSION AND RECEPTION ARE INOP, WEAK,GARBLED INTERMITTENT, ETC AT ALL CREW STNS. (1 = L HF, 2 = R HF). MAINT TEXT: LEFT HF INOP PER CREW. NO TIME TO TROUBLESHOOT. COMPLIED WITH MEL. REPLACED LEFT HF TRANSCEIVER PER AMM, OPS CHECKS GOOD.SDR UALA2011083104675Control Valve · faultyAFT CARGO OVERHEAT LIGHT ON. REPLACED AFT CARGO HEAT CONTROL VALVE PER MM, OPS CHECKED NORMAL.SDR UALA2011080304013Fairing · missingDURING RAMP CHECK FOUND PANEL MISSING ON AFT TOP OF RIGHT LANDING GEAR BODY DOOR AREA. ACCOMPLISH REPAIRS PER EVA 81169. RT WING MLG SIDE STRUT SWIVEL FAIRING ASSEMBLY TEMPORARY FAIRING INSTALLED AS PER EVA-8 1169. VERIFICATION REQUIRED BEFORE EACH FLIGHT SDR UALA2011072203733Aileron Sys · bindingCREW REPORTS DURING THE FLIGHT CONTROL CHECK BOTH CAPT AND F/O FELT BINDING IN THE LEFT AND RIGHT AILERON CONTROL CHECK. AILERON CONTROL BINDING. MM INSPECTED CABLES AND BEARINGS PER MM. LUBED LEFT FEEL AND CTR MECH AND LEFT OUTBOARD AILERON PER MM. DISCONSDR UALA2011071903655Fitting · missingSTRANGE NOISE AROUND ROW 19A. SOUNDS LIKE OBJECT FLAPPING IN WIND STREAM CLOSE TO FUSELAGE. FOUND LEFT AFT OVERWING DOOR STEP CHORD DISCONNECTED, REPLACED MISSING CIRCLIP AND SECURED CHORD TO STEP, ALL CHECKS NORMAL.SDR UALA2011052402535Wire · brokenMCP FAULT. FOUND AUTOPILOT ANNUNCIATOR LIGHT L19 FAULTING. TRIED GOOD UNIT FCC L & R PASSED TEST 1. C FCC FAULTING NO INFC FCC C MCP A-P EN G DISC AND NO INFC FCC C MCP A-P ARM IN. PER FIM 28 V DC PRESENT AT PINS 7 ALL CONNECTORS. ACCOMPLISHED WIRING CHECKS SDR UALA2011050202129Unknown · odorCREW REPORTS BURNING RUBBER SMELL AT ROWS 31 TO 33. CALL LIGHT ON AT SEAT 33C WITHOUT CALL BUTTON, SEAT VIDEO 33C WENT BLANK AND SMELL DISSIPATED. CREW REPORTED CALL LIGHT WAS ABLE TO BE RESET. CHECKED VICINITY OF ROWS 31C THRU 33C ALL PCU AND VIDEO FUNCTISDR UALA2011041801886Pump · defectiveNR 1 ENG FUEL PUMP NEEDS TO BE OP AND LEAK CHECKED. FUEL PUMP CHANGED BY AMT. PERFORM IDLE RUN TO OPS CHK FUEL FILTER CONNECTOR NR 1 ENGINE. ACP'D FIVE MINUTE IDLE NR 1 ENGINE, OPS CHK OKAY. NO MESSAGES.SDR UALA2011041501842Connector · looseNR 1 ENG MAIN FUEL FILTER SENSOR CANNON PLUG IS LOOSE. REPLACED CONNECTOR D10996.SDR UALA2011041101758Floor Panel · crackedAROUND ROW 20 RT FLOOR SOFT HAS SLIGHT INDENTATION. FLOOR PANEL HAS 18 IN CRACK DOWN CENTER. ACCOMPLISHED INTERIM REPAIR IAW EVA 80757.SDR UALA2011040401611Pressure Sensor · failedL FUEL OVERRIDE PUMP CIRCUIT BREAKER IS OUT. MEL COMPLIANT. REPLACED LEFT OVERRIDE PUMP PER AMM. NO PUMP PRESSURE. CHECKED PRESSURE SWITCH, OVERRIDE PUMP FOUND FAILED. REPLACED PCN AS PER MM. OP'S NORMAL NOW.SDR UALA2011032101339Relay · faultyLEFT HYD ELEC DEMAND PUMP IN AUTO CAUSES PRESS AND SYS PRESS LTS TO ILLUMINATE. WORKS IN ON. DEFERRED LEFT HYD ELEC DEM AND PUMP AUTO FUNCTION IAW MEL. REPLACED K130 RELAY. LEFT HYD DEMAND PUMP OPERATES NORMAL IN AUTO.SDR UALA2011032101348Connector · unsecureFWD GALLEY CROSSAISLE EEL LIGHT STRIP INOP. SECURED POWER FEEDER CONNECTOR, OPS CHECKED OK.SDR UALA2011032101329Holder · defectiveRT OVERWING SLIDE AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPHOLDER ASSY PER MM, OP CHECKS NORMAL.SDR UALA2011022800965Actuator · leakingHYD LEAK COMING FROM VERTICAL STABILIZER MID AREA. SWING RUDDER BACK AND FORTH, WITH RIGHT HYD SYSTEM,LEAK INTENSIFED. REPLACED RT RUDDER PCA REF MM.SDR UALA2011022500956Heat Shield · brokenREPLACED THE OIL TANK HEATSHIELD ON NR 2 ENGINE DUE TO LOWER SECTION BROKEN AND SEPARATING, WHICH HAS DAMAGED THE WIRE BUNDLE BELOW. REPLACED NR 2 OIL TANK HEAT SHIELD IAW MM.SDR UALA2011022200899Idg · faultyRIGHT IDG DRIVE LIGHT CAME ON STEADY DURING CLIMB AT APPROX 10,000 TO 12,000 FT. WHEN THE DRIVE LIGHT CAME ON IT WAS ACCOMPANIED BY A VIBRATION. WHEN THE IDG WAS DISCONNECTED THE VIBRATION ENDED. REPLACED OVHD PUSH BUTTON SWITCH & RT IDG.SDR UALA2011022200898Heat Exchanger · faultyDUE TO HISTORY OF RT IDG DRIVE LIGHT ON IN FLIGHT AND POSSIBLE FUEL CONTAMINATION AT TERMINATION OF FLT REPLACE IDG AIR-OIL HEAT EXCHANGER AND VALVE. (HEAT EXCHANGER AND VALVE SHOULD BE REPLACED AS AN ASSY). AIR OIL COOLER REPLACED IAW MM.SDR UALA2011022100854Idg · overservicedRT IDG DRIVE LIGHT, RTFL. CAME ON RT AFTER TAKEOFF. CREW REDUCED POWER AT 10,000 AND THE DRIVE LIGHT WENT OUT. CREW STARTED CLIMB & AT 12,000 FT, DRIVE LIGHT CAME BACK ON AND WOULD NOT GOT OUT. CREW DISCONNECTED IDG. CHECKED OIL LEVEL IN RIGHT IDG AFTER LASDR UALA2011022100853Idg · overservicedRT ENG IDG EICAS, RTFL. RIGHT IDG DRIVE LIGHT ILLUMINATED ON CLIMB. CREW REDUCED THE POWER ON THE RIGHT ENGINE AND THE DRIVE LIGHT WENT OUT. AT THIS TIME THE IDG IS NOT DISCONNECTED. FOUND IDG OVERSERVICED. REPLACED NR 2 ENG IDG. REPLACED NR 2 ENG IDG DRIVE OSDR UALA2011022200897Idg · faultyRT GEN DRIVE LIGHT ON AND CREW DISCONNECTED GEN. FOUND RT IDG OVER SERVICE DRAINED 1.5 QTS. REPLACED RT GCU IAW MM. RAN BOTH ENGS FOR 5 MIN IAW JRH, ALL INDICATION ARE NORMAL, AFTER RUN CHECK IDG OIL SERVICE, FOUND NORMAL.SDR UALA2011021700830Idg · faultyCREW REPORTS RT GENAERATOR DRIVE LIGHT ILLUMINATED. CREW DISCONNECTED RT GENERATOR. RT ENGINE IDG REPLACED. IDLE RUN ACCOMPLISHED BY CREW, GENERATOR OPS NORMAL. IDG SERVICED WITH 2197 OIL.SDR UALA2011021100740Probe · leakingLOUD SQUEAL FROM BEHIND CAPT INST PANEL - REPEAT. TROUBLESHOT AND FOUND LT UPPER AND LOWER PITOT PROBE LEAKING, LT TAT PROBE AND RADOME HINGE ATTACHMENT BOLTS LEAKING. SEALED AS REQUIRED. PERFORMED LEAK CHECK, NO LEAKS NOTED.SDR UALA2011011000135Valve · inoperativeON SHORT FINAL HAD C HYD DEM PUMP EICAS AND PUMP PRESSURE LIGHT 2 TIMES FOR ABOUT 10 SECONDS EACH. CENTER ADP PUMP HAS BEEN RENDERED INOP PER MEL. FOUND HPSOV BITE FAILS. REPLACED NR 1 HPSOV IAW MM.SDR UALA2011011000134Bonding Jumper · brokenNR 1 ENG HPSOV BONDING JUMPER BROKEN AT LUG. REPLACED BROKEN BONDING JUMPER ON HPSOV AND SAME ON HP-IPSOV.SDR UALA2010121604594Connector · failedWINDOW MESSAGE DISPLAYED ON EICAS. INOP LGT ILLUM. INOP LGT EXTINGUISHED WHEN SW WAS RECYCLED TO OFF THEN ON. POSN 4 (1=L FWD, 2=L SIDE,3=R FWD,4=R SIDE) FRM 30 41 01. CREW COMMENTS: LT SIDE WINDOW HEAT FAILED 3X - RESET EACH TIME FOR SEVERAL HOURS. REPLACESDR UALA2010121304533Adc · faultyCAPTAIN ALT CONSTANTLY MOVES UP AND DOWN 60' AT CRUISE. ALSO TEMPORARILY WENT UP IN DESCENT. ALL FLIGHT CONTROLS FELT UNUSUALLY HEAVY ON FINAL AND LANDING. IAW CREW HEAVY FORCES WERE NOTICED ON AIL AND ELEV. LT ADC REPLACED. ACP BITE CHK OF ALL CSEU UNITSSDR UALA2010112204306Amplifier · inoperativeSATCOM HI GAIN INOPERATIVE. AMPLIFIER FOUND DEFECTIVE. REPLACED HIGH POWER AMPLIFIER.SDR UALA2010110504104Actuator · leakingLT WING AFT OF PYLON SAIL TAIL AREA HAS EVIDENCE OF HYD LEAK. LEAK IS AT LT INBD AILERON INBD ACTUATOR ON ACT ROD SEAL. LEAK IS MEASURED AT 4 DROPS PER MIN. COMPLETED ACTUATOR REPLACEMENT.SDR UALA2010110104040Actuator · bypassingOPERATED HYD & TURNED CONTROL WHEEL LEFT, CAN FEEL SHUTTER, VIBRATION IN COCKPIT AIRFRAME, CONTROL WHEEL & FROM INBD AILERON TO OTBD AILERON WHILE IT STILL HELD IN LT TURN. ISOLATED TO CTR HYD SYS. NO VIB IN RT & LT HYD SYS ON. RT WING AILERON OK NO VIBS. ISDR UALA2010102103896Pressure Switch · faultedLEFT FWD BOOST PUMP LOW PRESSURE LIGHT INOPERATIVE. CLEANED CONNECTOR AND BLEED PRESSURE SWITCH LINE, NO HELP. DEFERRED PUMP INOPERATIVE. REPLACED LT FWD FUEL BOOST PUMP PRESSURE SWITCH (S70) IAW MM. CHECKED GOOD, NO LEAKS.SDR UALA2010090303255Controller · inoperativeLT WINDOW SIDE HEAT INOPERATIVE. REPLACED M192 WINDOW HEAT CONTROLLER, WINDOW HEAT OPERATION RESTORED.SDR UALA2010081903056Line · leakingHYD FLUID LEAKING FROM LT PYLON INBD DRAIN.SDR UALA2010081703015Line · leakingHEAVY HYD LEAK NR 1 PYLON. SUPPLEMENTAL DATA UPDATE HYDRAULIC FLUID LEAKING FROM LEFT PYLON INBD DRAIN WHILE REVERSER DEPLOYED AND LEFT HYDRAULICS PRESSURIZED. LINE IS LOCATED BETWEEN RESERVOIR AND INTO A BULKHEAD, EXTREMELY TIGHT ACCESS. LINE REMOVAL IS IN PSDR UALA2010081602998Isolation Valve · defectiveLEFT ISOLATION VALVE WOULD NOT OPEN. REPLACED LT ISOLATION VALVE. OPS CHECK NORMAL.SDR UALA2010081202941Cdu · failedRH FMC/CDU FAILURE, FLIGHT DIVERTED. 1ST OFFICER'S CONTROL DISPLAY UNIT FOUND FAULTY. REPLACED F-O'S CDU PER AMM. RT CDU CHECKS SATIS.SDR UALA2010063002338Entertain Sys · inoperativeENTIRE PASSENGER ENTERTAINMENT SYSTEM IS INOPERATIVE.SDR UALA2010051001582Tire · unknownTIRE DEBRIS ON T/O ROLL, RTFL. REPLACED TIRE.
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