N345UA
Service difficulty reports not matched to an aircraft · 31
They name N345UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N345UA' AND registry_match IS NULL 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 = 'N345UA' AND registry_match IS NULL 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 2002UALA01315Skin · dentedDENT FOUND IN RIGHT HAND SIDE OF FUSELAGE BELOW FWD LAV SERVICE PANEL AND ABOUT 3 INCHES AFT OF RED STEERING LIMIT STRIPE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.SDR 2002UALA01310Bear Strap · damagedAFT PIT DOOR CUTOUT SKIN BEAR STRAP BLENDED BEYOND LIMITS AT STATION 796 STR 21-24R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR 2002UALA01293Web · gougedAFT PIT DOOR SILL VERTICAL WEB GOUGED BETWEEN STATION 793 - 821 RBL 23 (APPROX) BELOW FLOOR TRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB.SDR 2002UALA01284Doubler · gougedEXTERNAL EXISTING FUSELAGE SKIN REPAIR STATION 845, 1 INCH BELOW STR 22R GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2002UALA01274Skin · damagedEXTERNAL FUSELAGE GOUGED STATION 299 BETWEEN STRINGER 25R AND 26R. ALSO GOUGED STATION 305 BETWEEN STRINGER 25R AND 26R. LIGHTNING STRIKES STATION 313 AT STRINGER 25R, AND STATION 308 STRINGER 25R AND 26R. FUSELAGE DENTED STATION 288 BETWEEN STRINGER 24R ANSDR 2002UALA01269Door Frame · crackedCABIN, STATION 294, FUSELAGE STUB FRAME CRACKED AT UPPER DOOR STOP FITTING, AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STUB FRAME.SDR 2002UALA01259Frame · crackedCABIN BODY FRAME INBOARD CHORD IS CRACKED BODY STATION 294, RBL 53, WL 209. MAJOR REPAIR ACCOMPLISHED. SPLICED FRAME INBOARD CHORD.SDR 2002UALA01258Floorbeam · corrodedAFT CABIN LEFT HAND SIDE FLOORBEAM UPPER SURFACE CORRODED AROUND NUT PLATE HOLES STATION 927 BETWEEN LBL 14 AND LBL 44. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED ANGLE DOUBLER AND FILLER.SDR 2002UALA01247Frame · damagedSTATION 294.5 FRAME JUST INBOARD OF STRINGER 4R IS BLENDED BEYOND LIMIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA01228Floorbeam · damagedCABIN STATION 947.5 BETWEEN LBL 5 & LBL 20 UPPER SURFACE OF FLOORBEAM HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIRS & FILLERS.SDR 2002UALA01227Frame · crackedSTATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME DOUBLER.SDR 2002UALA01216Frame · crackedCABIN BODY FRAME WEB IS CRACKED BODY STATION 440 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB.SDR 2002UALA01215Frame · crackedCABIN STATION 827 STRINGER 4R FRAME WEB WAS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR.SDR 2002UALA01214Frame · crackedCABIN STATION 847 FRAME WEB AT STRINGER 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR.SDR 2002UALA01213Frame · crackedCABIN STATION 887 FRAME WEB CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR.SDR 2002UALA01212Frame · crackedSTATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR 2002UALA01211Frame · crackedSTATION 440 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR 2002UALA01209Frame · crackedSTATION 480 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA01208Frame · crackedSTATION 520 FUSELAGE FRAME CRACKED IN WEB AND INBOARD FLANGE RADIUS BELOW STRINGER 14R OUT OF INSULATION STANDOFF HOLE JUST BELOW FRAME SPLICE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.SDR 2002UALA01068Flap · malfunctionedAFTER DEPARTURE ON FLAP RETRACTION FROM FLAPS 1 TO FLAPS UP, THE FLAPS SPLIT ACCORDING TO THE FLAP POSITION INDICATOR. RETURNED TO THE FIELD AND MADE A FLAPS UP LANDING.SDR 2002UALA00010Bulkhead · crackedWEB CRACKED AT BODY STATION 178, WL 218, LBL 12. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.SDR 2002UALA00002Bulkhead · crackedBODY STATION 178, WL 211, LBL 17 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.SDR 2002UALA00001Bulkhead · crackedBODY STATION 178, WL 200, LBL 5.7 WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.SDR 2000UALA00621Fuel Cell · leakingSUSPECTED FUEL LOSS FROM NUMBER 2 MAIN TANK. *S/D* FOUND CENTER SHIELDED CONNECTOR SHIELD BROKEN ON NR 2 MAIN FUEL GAUGE. REPLACED SHIELDED SOCKET AND CENTER PIN. REPLACED FUEL BOOST PUMP AND LOW PRESSURE SWITCH. AIRCRAFT OPS CHECKED GOOD. FUEL PUMP P/N:SDR 2001UALA00638Control Rod · chafedRUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. OFF UNIT FOUND TO BE WITHIN LIMITS PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISSUE SDR 2000UALA00328Sensor · malfunctionedYELLOW LEADING EDGE FLAP TRANSIT LIGHT REMAINED ON AND LEFT INBOARD FLAP INDICATOR GREEN LIGHT ON. EXCEEDED 230KTS BY 5-10 KTS. *S/D* REPLACED LEADING EDGE FLAP NUMBER 2 EXTEND SENSOR, S171, PER AMM 27-8 8-11.SDR 99UAL900271Sensor · failedEXHAUST FAN INOP. *S/D* EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED EQUIPMENT COOLING LOW FLOW SENSOR, OPS CHECK OK.SDR 98UAL900133Eau Fork · fracturedBOTH THRUST REVERSER UNLOCK LIGHTS ILLUMINATED AFTER TAKEOFF. *S/D* FOUND ENGINE ACCESS UNIT RETAINING FORK ON RADIO RACK FRACTURED AND MISSING PIN. EAU WAS LOOSE IN RACK. REPLACED FORK AND PERFORMED EAU OPS CHECK, OPS CHECK GOOD.SDR 97UAL900420Fire Loop · out of positionEXPERIENCED RT WING BODY OVERHEAT WARNING. OVERHEAT LIGHT ON INTERMITTENT DURING CLIMB. *S/D* THE CAUSE WAS ATTRIBUTED TO THE POSITIONING OF THE FIRE DETECTION LOOP ELEMENTS 35564-4-310 (RT LEADING EDGE OVERHEAT) AND 35560-4-310 (RT ENGINE STRUT CAVITY OVERSDR 97UAL900276Charger · failedEEL LIGHT FLOOR STRIPS INOP AT ROW 11 THROUGH 17. AFT EMERGENCY EXIT INDICATOR LIGHT INOP. BULLNOSE EMERGENCY EXIT LIGHT INOP. THE EEL LIGHTS AT ROWS 11 THROUGH 17, THE EMERGENCY EXIT INDICATOR, AND BULLNOSE EMERGENCY EXIT LIGHTS WERE INOPERATIVE, DUE TO ASDR 96UAL900585Actuator · brokenTHE LEADING EDGE FLAPS TRANSIT LIGHT IS ON AND THE NR 6 SLAT LIGHT IS ON STEADY. REPLACED SLAT ACTUATOR. SHOP FOUND THE ACTUATOR ROD END BROKEN. SENT ROD END TO BOEING FOR EVALUATION.
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