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.
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
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 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 2005UALA01133Battery · dischargedDOOR 1LH AND 1RH EMERGENCY EXIT LIGHTS INOP REPLACED POWER SUPPLY. REPLACED POWER SUPPLY.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 2006UALA01173Housing · crackedLT O/W SLIDE COMPARTMENT DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 25-65-98.SDR 2004UALA00545Control Unit · overheatedLOMBAR CONTROL SEAT 9A IS HOT AND MELTING. REPLACED SWITCH. THE BURNED BACK CYCLER SWITCH WAS AN OLDER, ORIGINAL UNIT. THE ORIGINAL BACK CYCLER SWITCH WAS UPGRADED IN 2001 DUE TO RELIABILITY PROBLEMS. AN IMPROVED, REPLACEMENT SWITCH WAS DEVELOPED AND INTRODUCSDR 2004UALA00399Light · inoperativeFWD GALLEY EEL STRIP IS INOPERATIVE. REPAIRED EEL FEEDER. CHECKS GOOD.SDR 2004UALA00280Battery Pack · dischargedEMERGENCY EXIT LIGHTS INTERMITTENT ROWS 15-18 LEFT SIDE. REPLACED EEL BATTERY POWER SUPPLY PACK.SDR 2004UALA00264Battery Pack · inoperativeRIGHT EMERGENCY LIGHT PATH INOP FROM 15 THROUGH ROW 18. REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKED OK.SDR 2004UALA00263Support · crackedRIGHT INBOARD FLAP, CENTER SUPPORT IS CRACKED ON THE LOWER INBOARD FLANGE AT THE MID FLAP ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR TO HINGE FITTING.SDR 2004UALA00262Fitting · crackedRIGHT INBOARD T/E FLAP, MAIN FLAP INBOARD T/E HINGE FITTING SUPPORT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCMENT REPAIR ANGLE TO HINGE FITTING.SDR 2004UALA00259Stiffener · crackedSTA 246 FLOORBEAM VERTICAL STIFFENER IS CRACKED AT LBL 23. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.SDR 2004UALA00258Hinge · crackedLEFT WING INBOARD FLAP MAIN TO AFT FLAP HINGE IS CRACKED ON BOTH SIDES. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIRS.SDR 2004UALA00133Light · inoperativeEMERGENCY EXIT LIGHT AT NR 2AB ROW INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT, OPS OK.SDR 2004UALA00118Jackscrew · failedFLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANICALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED.SDR 2003UALA00382Compressor · stalledCOMPRESSOR STALL ON NR 1 ENGINE. ENGINE SURGED ON CLIMB AND RECOVERED. BOROSCOPE FOUND CRACK ON 14TH STAGE STATOR AND BENT 14TH AND 15TH STAGE BLADES. ENGINE WAS REMOVED AND THE HPC WILL BE OVERHAULED. UPON DISASSEMBLY OF THE HPC NO STATORS WERE CRACKED AND THSDR 2002UALA01462Web · crackedNR 1 ENGINE PYLON CRACKED AT FORWARD TORQUE BOX, OUTBOARD DRAIN HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLERS AND FILLERS.SDR 2002UALA01461Fitting · crackedNR 1 PYLON INBOARD MID SPAR FITTING LOWER ANGLE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED LOWER HORIZONTAL ANGLE.SDR 2002UALA01460Bulkhead · crackedNR 2 PYLON WEB CRACKED, ACCESS THROUGH PYLON PANELS 446BL OR 446BR. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01459Bulkhead · crackedNR 2 PYLON AFT UPPER SPAR WEB, AFT INBOARD CORNER CRACKED FOR PNEUMATIC DUCT, ACCESS THROUGH RT WING PANEL 611PT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01458Bulkhead · crackedNR 1 PYLON UPPER WEB CRACKED AT IDG CABLE CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01457Bulkhead · crackedNR 1 PYLON UPPER WEB CRACKED AT MAIN ENGINE WIRE HARNESS CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01456Bulkhead · crackedNR 1 PYLON PNEUMATIC DUCT CUTOUT, UPPER WEB CRACKED AT INBOARD AFT CORNER WHERE FIRE PROTECTION LINES ATTACHES. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01455Bulkhead · crackedNR 2 PYLON WIRE HARNESS CUTOUT AT UPPER WEB CRACKED ACCESS THROUGH INBOARD PANEL 442BL. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH REPAIR DOUBLER.SDR 2002UALA01454Bulkhead · crackedNR 2 PYLON IDG WIRE HARNESS UPPER WEB CUTOUT HAS SEVERAL CRACKS. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER PYLON WEB WITH REPAIR DOUBLER SPLICE L ANGLE AND STIFFENER.SDR 2002UALA01420Skin · lightning strikeAFTER THE LIGHTNING STRIKE WAS REMOVED AT BODY STATION 1261 BETWEEN STRINGER 30-31 HAS TOO MUCH MATERIAL REMOVED FROM THE SKIN. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER AND FILLER.SDR 2002UALA01313Compressor · stalledCOMPRESSOR STALL ON LEFT ENGINE AT TAKEOFF. ENGINE EXPERIENCED A GROUP 3 (TAKEOFF) SURGE. REMOVED ENGINE FOR HIGH COMPRESSOR OVERHAUL.SDR 2002UALA01278Inverter · malfunctionedEICAS STATUS MESSAGE OF STANDBY INVERTER DISPLAYED. UNABLE TO CLEAR MESSAGE. SUPPLEMENTAL DATA UPDATE FOUND INVERTER POWER TRU CB OPEN, REPLACED STATIC INVERTER. OPS CHECK OK.SDR 2002UALA01205Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. ENGINE RECOVERED. NR 2 ENGINE HAD A GROUP 3 (TAKEOFF) SURGE. THE ENGINE SELF RECOVERED. ENGINE WAS REPLACED AT TERMINATION OF THE FLIGHT FOR COMPRESSOR REFURBISHMENT.SDR 2001UALA01630Relay · failedLEFT ENG DIFFICULT TO SHUTDOWN. DELAYED SHUTDOWN OF LEFT ENGINE AT GATE ARRIVAL. REPLACED FUEL/IGNITION CONTROL RELAY K-D4A019 IN P36 MISC ELECTRICAL EQUIPMENT PANEL.SDR 2001UALA01453Bulkhead · damagedMAJOR REPAIR ACCOMPLISHED TO AFT PRESSURE BLKHD 6:00 POSITION.SDR 2001UALA01433Bulkhead · damagedMAJOR REPAIR ACCOMPLISHED TO AFT PRESSURE BLKHD 6:00 POSITION.SDR 2001UALA01392Skin · dentedBULK PIT DOOR HAS SMALL DEEP DENT 14 INCHES FROM T/E AND 16 INCHES ABOVE DOOR HANDLE.SDR 2001UALA00095Circuit Board · failedON DEPARTURE FROM SFO AT APPROX 1500 FT FORWARD CARGO DOOR EICAS MESSAGE ILLUMINATED. WENT OFF AFTER APPROX FIVE MINUTES. DID NOT CHECK CARGO LIGHTS. *S/D* REPEAT NUISANCE MESSAGE WAS CORRECTED BY VERIFYING ADJUSTMENT OF FORWARD CARGO DOOR LOCK SENSOR, CLOSDR 2000UALA00704Battery Pack · failedEMERGENCY LIGHTS AT ROWS 20 - 26 ON THE RIGHT SIDE ON INTERMITTENTLY. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY PACK PER MM33-51-07. TESTED GOOD.SDR 2000UALA00649Light · inoperativeEMERGENCY EEL STRIP LIGHTING ON AT ROWS 20 TO 28 RIGHT SIDE. REMOVED AND RECONNECTED, COMES ON WITH SWITCH. WATCHED FOR 10 MINUTES DID NOT COME ON, WHEN ON GROUND.SDR 2000UALA00453Connector · looseLEFT FUEL QTY UNRELIABLE. FLUCTUATED BETWEEN 2000 LBS LOW WITH 10000 LBS IN CTR, BALANCED FUEL. LATER LEFT TANK INDICATING LBS HIGH. CHRONIC PROBLEM. AIRCRAFT REMOVED FROM ETOPS. *S/D* THE LEFT MAIN TANK FQIS TANK UNITS AND COMPENSATOR WERE CHECKED FOR SSDR 99UAL900633Indicator · malfunctionedHALF OF THE NOSE GEAR, RIGHT MAIN AND ALL LEFT MAIN GEAR LIGHTS REMAINED ILLUMINATED DIM AFTER RETRACTION. GEAR DID SEEM UP. FLIGHT RETURNED TO SFO.SDR 99UAL900223Fan · failed'FWD EQ EXH FAN' EICAS MESSAGE DISPLAYED. SMOKE ON FLIGHT DECK. CB H21 ON P6 PULLED AS PRECAUTION. SMOKE EVAC PERFORMED AND SMOKE DISSIPATED. *S/D* SMOKE IN FLIGHT DECK WAS PROBABLY CAUSED BY A BEARING FAILURE IN FORWARD EQUIPMENT EXHAUST FAN. THIS FAN WASDR 99UAL900179Oven · failedFORWARD GALLEY OVEN NR 12 GENERATED A SMALL AMOUNT OF SMOKE AND ELECTRICAL ODOR. OVEN ISOLATED AND SWITCHED OFF BY PULLING CB09 FOR OVEN NR 12.SDR 99UAL900149Actuator · brokenUNABLE TO RAISE LEFT MAIN LANDING GEAR. RETURNED TO FIELD. AMBER ALERT DECLARED. *S/D* TRUCK POSITION ACTUATOR FOUND LEAKING INTERNALLY AT PRESSURE RELIEF VALVE. REPLACED ACTUATOR.SDR 99UAL900081Compressor · stalledNR 1 ENGINE COMPRESSOR STALL. THROTTLE TO IDLE CLEARED STALL. *S/D* THIS ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. GROUP 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCES IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. THIS ENGINE WAS REMOVED SDR 98UAL900362Compressor · stalledNR 2 ENGINE HEAVY COMPRESSOR STALL AT 200 FEET AGL. REDUCED THRUST TO FLIGHT IDLE, JETTISONED FUEL. RETURNED TO MIA AMBER ALERT, OVERWEIGHT LANDING. *S/D* ENGINE SURGE WAS DUE TO GENERAL DETERIORATION OF THE HIGH PRESSURE COMPRESSOR. THE ENGINE WAS REMOVESDR 97UAL900652Lights · illuminatedAFTER LANDING ON TOUCHDOWN ROLL, EMERGENCY LIGHTS ILLUMINATED THROUGHOUT THE AIRCRAFT. *S/D* DEPOWERED ELECTRICAL POWER FROM AIRCRAFT. RESET EMERGENCY LIGHTS, OPS OK.SDR 97UAL900054Central Warning · malfunctionedON THREE OCCASIONS DURING FLIGHT, THE RADIO ALTIMETER AMBER LIGHT ILLUMINATED ON THE ATTITUDE DEVIATION INDICATOR (ADI). THE FLIGHT MANAGEMENT COMPUTER (FMC) WARNING CONFIGURATION LIGHT AND ALSO THE LANDING GEAR NOT DOWN LIGHT MOMENTARILY ILLUMINATED WITHOUTSDR 96UAL900534Idg · failedTHE NUMBER 2 INTEGRATED DRIVE GENERATOR FAILED. AIRCRAFT DIVERTED TO JFK. *S/D* A HYDRAULIC LOG FAILURE OCCURRED IN THE IDG. HEAVY CYLINDER BLOCK WEAR ALSO CONTRIBUTED TO A LOSS OF OIL CHARGE PRESSURE AND AN INABILITY TO MAINTAIN FREQUENCY. THE IDG WAS RESDR 96UAL900290Idg · failedLOST RIGHT INTEGRATED DRIVE GENERATOR AND RECEIVED RIGHT EEC MESSAGE. RESET RIGHT EEC, BUT IT REMAINED IN ALTERNATE MODE. *S/D* REPLACED RIGHT INTEGRATED DRIVE GENERATOR, GENERATOR CONTROL UNIT AND GENERATOR CONTROL BREAKER. IDG AND GCU WERE SHOP TESTED A
Back to N643UA