N503UA
Service difficulty reports · 79
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 = 'N503UA' 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 = 'N503UA' 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 2008UALA01225Unknown · malfunctionedDOOR NR 4 EMERGENCY ESCAPE SLIDE LAMP NOT ILLUMINATING, CHANGE LAMP, NO HELP. PERFORMED OPS TESTS OF EMER DOOR 4L AND SLIDE, ALL OPS CHECKS WERE NORMAL.. NO REPEATS.SDR 2007UALA03855Handle · stuckGEAR HANDLE WOULD NOT RAISE AFTER TOUCH & GO LANDING. WHEN SPOILER HANDLE WAS LOWERED ON LANDING ROLL THE AIRCRAFT ROLLED RIGHT.SDR 2007UALA03854Lamp · inoperativeLEFT OVERWING EMERGENCY LIGHT IS INOP.SDR 2007UALA03736Door · openBOTH LEFT & RIGHT OVERWING SLIDE SERVICE ACCESS DOORS PROTRUDING INTO AIRSTREAM. RIGHT SIDE HINGE IS CRACKED, LEFT SIDE HAS BROKEN SPRINGS. 10-9-07 INTERIM REPAIR MADE, RECHECKED DAILY AT FIRST MAINTENANCE. REPLACED BOTH OF THE ACCESS DOOR HINGE ASSEMBLISDR 2007UALA03657Truck · failedRTFL DUE TO LANDING GEAR RETRACTION FAILURE. 10-11-07 ACTUATOR DID NOT EXTEND WHEN HYDRAULIC LINES MOVED. BLOCK 25 CALLS FOR ACTUATOR REPLACEMENT. REPLACED MLG TRUCK POSITIONER ACTUATOR ASSEMBLY. AUTO SPEED BRAKE EICAS MESSAGE WAS DISPLAYED WHEN GEAR WSDR 2007UALA03017Warning Light · illuminatedEICAS MESSAGE -GEAR DOORS & GEAR DISAGREE- DISPLAYED WITH GEAR HANDLE UP. DOORS & GEAR AMBER LIGHTS ILLUMINATED. GEAR MOVEMENT WAS SO SLOW THAT EICAS MESSAGES "GEAR DOORS AND GEAR DISAGREE" WERE DISPLAYED DURING GEAR RETRACTION. ALL GEAR INDICATION "GREESDR 2007UALA01341Skin · damagedFUSELAGE DAMAGE TO AFT CARGO PIT DOOR THRESHOLD AND SURROUNDING STRUCTURE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN. MFG & INSTALLED FILLER AND DOUBLER REPAIR. INSTALLED NEW CENTER THRESHOLD PLATE AND NEW FWD CORNER PLATE. SEALED ALL EDGES.SDR 2006UALA01883Warning Message · illuminatedDIVERTED DUE TO APU OIL SERVICE INDICATION AND INOPERATIVE LEFT ENGINE GENERATOR. R GEN DF'D INOP AND APU OIL WAS SERVICED PRIOR TO DISPATCH. APU STARTED TO HAVE HIGH OIL CONSUMPTION LATER IN FLIGHT DUE TO LEAKS. NO EXTERNAL LEAKS OR REPORTS OF OIL FROM SESDR 2006UALA00994Squib · no testFOUND EMERGENCY ESCAPE (RT) SQUIB DOES NOT TEST.SDR 2005UALA00883Slide · separatedTHE RIGHT SLIDE BUMPER SEPARATED DURING OVERPRESSURE. INTERNAL SEAM FAILURE CAUSED BUMPER PROFILE TO DISTORT. ANALYSIS BY OEM OF BUMPER INTERNAL SEAM FAILURE SHOWED PROPER SEAM ASSEMBLY. INFLATABLE WAS REPLACED.SDR 2005UALA00527Attach Angle · crackedFWD NOSE AREA STA 202 BULKHEAD, RT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER REAR SIDE OF BULKHEAD, RBL 30-36. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U2 AND INSTALLED PER SRM 51-40-2.SDR 2005UALA00526Attach Angle · crackedFWD NOSE AREA, STA 202 BULKHEAD, LT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER SIDE LBL 36 AREA, REAR SIDE OF BULKHEAD. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U1 AND INSTALLED PER SRM 51-40-2SDR 2005UALA00524Floorbeam · corrodedRIGHT SIDE BS 1640 FLOORBEAM, RBL 0 - RBL 60, TOP CAP IS CORRODED. DAMAGE DUE TO CORROSION IN TYPICAL WET AREA. REMOVED CORRODED REPAIR STRAP AND INSTALLED NEW REPAIR STRAP.SDR 2005UALA00523Floorbeam · corrodedFLOORBEAM CORRODED AT STA 367, RBL 56 UPPER SURFACE. REPLACED SUPPORT 141N5161- 52 PER SRM 51-40-02.SDR 2005UALA00505Frame · dentedAFT PIT LT SIDE STA 1440 FRAME HAS A DENT ON INBOARD FLANGE BETWEEN STR 25L AND 26L. REPAIRED FRAME WITH A FABRICATED PRODUCTION SPLICE ANGLE DOUBLER PER TIMCO REO(EVA) G10548, REV B.SDR 2005UALA00504Frame · dentedAFT PIT STA 1480 FRAME HAS DENT ABOVE STR 26L ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED NESTED J-ANGLE PER TIMCO REO(EVA) G-10556, REV. C.SDR 2005UALA00502Frame · dentedAFT PIT LT SIDE AT STA 1460, FRAME HAS DENT ON INBOARD FLANGE BETWEEN STR 25L-26L. REPAIRED FRAME WITH FABRICATED PRODUCTION SPLICE ANGLE-DOUBLER PER TIMCO REO(EVA) G10547, REV. B.SDR 2005UALA00492Stringer · crackedLT FUSELAGE STRINGER 16L IS CRACKED AT STA 610. REMOVED DAMAGE AND FABRICATED NEW STRINGER SECTION PER SRM 53-30-03.SDR 2005UALA00052Skin · damagedEXTERIOR FUSELAGE AT STA 1420 BETWEEN STR 28R AND 30R, SKIN IS CREASED. FRAME SHEAR TIES WERE REPLACED.SDR 2005UALA00051Skin · damagedLEFT EXTERIOR FUSELAGE AT STA 620, STR 16L, REPAIR DOUBLER IS DENTED. REMOVED EXISTING DOUBLER AND REPLACED SKIN DOUBLER REPAIR.SDR 2003UALA00785Skin · gougedEXTERNAL FUSELAGE SKIN HAS 2EA GOUGES AT BOTTOM OF 3 INCH LONG BY 2 INCH HIGH DENT, AT STA 770 BETWEEN STR 15L AND 16L.SDR 2003UALA00399Fitting · separatedDOOR 3R GIRT BAR SHOE FITTING SEPARATED FROM GIRT BAR ASSEMBLY. REINSTALLED SHOE ASSY.SDR 2001UALA01008Skin · gougedFUSELAGE SKIN GOUGED STA 760-780, STR 16L. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS REPAIR AND INSTALLED NEW DOUBLER.SDR 2001UALA00658Actuator · failedLEADING EDGE LIGHT ON AND EICAS L/E SLAT DISAGREE MESSAGE. *S/D* LEADING EDGE SLAT ROTARY ACTUATOR NR 2 FAILED, WHICH CAUSED THE SLAT SYSTEM TO LOCKOUT AND ILLUMINATE THE DISAGREE LIGHT AND MESSAGE. REPLACED ACTUATOR NR 2, 3 AND 10 DUE TO OVERLOAD INDICATORSDR 99UAL900418Pump · brokenLANDED DEN UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* ENGINE DRIVEN PUMP SHAFT SHEARED. POSSIBLE BEARING FAILURE. REPLACED PUMP.SDR 99UAL900292Skin · damagedDURING THE HEAVY MAINTENANCE VISIT, THE FUSELAGE CROWN SKIN AREA BETWEEN BS 600 AND BS 660 AND BETWEEN S-4L AND S-4R WAS FOUND TO HAVE DAMAGE. A MAJOR REPAIR IS REQUIRED TO CORRECT DAMAGED AREA. *S/D* CAUSE NOT IDENTIFIED. REPAIRED CROWN WITH EXTERNAL DOUSDR 98UAL900083Axle · crackedAIRCRAFT AT MAINTENANCE BASE FOR GEAR CHANGE. NEW RT MLG AFT INBD AXLE SHEARED AFTER DE-JACKING OF AIRCRAFT. *S/D* HEAT DAMAGE INDUCED BY OEM FINISH GRINDING ON THE OD CHROME PLATE, 19.25 INCHES FROM AXLE THREADED END. REPLACED AXLE AND INSPECTED REMAININGSDR 97UAL900682Circuit Breaker · trippedAPU INOP AT DEPARTURE TIME. *S/D* RESET APU CIRCUIT BREAKER AND STARTED APU. OBSERVED BATTERY VOLTS AND CHARGER OUTPUT, ALL INDICATIONS NORMAL. LEFT APU RUNNING, AND AFTER 20 MINUTES APU STILL OPERATED NORMAL. NO OTHER CAUSES FOUND.SDR 95UAL900338Battery Pack · dischargedEMERGENCY LIGHTS IN BULLNOSE AT ROWS 30 AND 33 GO OUT AFTER 30 SECONDS. BATTERY PACK LOW. REPLACED BATTERY PACK.
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