N212UA
Service difficulty reports · 186
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 = 'N212UA' 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 = 'N212UA' 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 CALA2016012895049Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 942 - 995. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.244, BLEND OUT REMAIN 0.236. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895048Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 863 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.284. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895047Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT NEAR SPAR, BETWEEN WS 864 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.350, BLEND OUT REMAIN 0.319. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTIOSDR CALA2016012895046Skin · corrodedRIGHT LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 810 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-0. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.241. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CSDR CALA2016012895045Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1182 - 1209. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & 51-20-01. SKIN ORIGINAL THICKNESS 0.155, BLEND OUT REMAIN 0.131. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895044Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1021 - 1074. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.220, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSSDR CALA2016012895043Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 995 - 1047. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.310 & BLEND OUT REMAIN 0.286. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895042Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER 14, WS 960 - 1000 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.245, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED SDR CALA2016012895041Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1095 - 1105 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.256, BLEND OUT REMAIN 0.247. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUSDR CALA2016012895040Skin · corrodedRIGHT WING CTR TANK MEASURING STICK 1, SURROUNDING SKIN FOUND CORRODED. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.557, BLEND OUT AREA REMAIN 0.511. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUT, NO DEFECTSDR CALA2016012895039Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1270 & WS 1280 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.106, BLEND OUT REMAIN 0.091. HFEC INSPECSDR CALA2016012895038Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE, FOUND CORROSION AT REAR SPAR, WS 1065 - WS 1080 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.268, BLEND OUT REMAIN 0.226. HFEC INSPESDR CALA2016012895037Skin · corrodedLEFT WING LOWER SKIN, EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 1020 & WS 1050. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.300, BLEND OUT REMAIN 0.290. HFEC INSDR CALA2015081394215Unknown · malfunctionedELEC BACKUP SYS A FAILURE IN THE BACKUP ELECTRICAL SYSTEM HAS OCCURRED THAT CANNOT BE ATTRIBUTED TO A BACKUP GEN. SATUS MSG 01 LATCHED CRUISE MODE DEPENDENT, BACKUP GEN RT VOLTAGE IS LOW. BACKUP CONVERTER MSG 02 LATCHED CRUISE MODE DEPENDENT, BACKUP GEN LT VSDR CALA2015061893993Connector · unsecurePER A CHECK, SEAT EEL FROM 26G TO 37G INOPERATIVE. SECURED CONNECTOR. OPERATIONS CHECKED OK.SDR CALA2015061893992Connector · unsecurePER A CHECK, SEAT EEL FROM 26C TO 37C INOPERATIVE. SECURED CONNECTOR. OPERATIONS CHECKED OK.SDR CALA2015061893991Battery · dischargedPER A CHECK, CEILING EMER LIGHTS INOPERATIVE FROM 27AB TO 35AB. REPLACED BATTERY. OPERATIONS CHECKED OK.SDR CALA2014080691733Sealant · missingFIRST OFFICERS SLIDING WINDOW HAS LOUD SQUEAL, LE TOP THIRD SEALANT MISSING AT TOP OF WINDOW. RESEALED, ALSO RESEALED BOTTOM FWD CORNER IAW AMM 56-11-00. LEAK CHECKED OK.SDR CALA2014061691280Control Unit · malfunctionedDOOR 1L FLIGHT ATTENDANT PANEL NOT FULLY POWERED. RESET ZMU, CHECKED GOOD.SDR CALA2014051391009Status Message · false activationAPU START SYS STATUS MSG ON START UP. RESTARTED APU, MSG GONE.SDR CALA2014040390747Status Message · activatedFIRE LOOP 1 ENG LT ON STATUS. MEASURED INDIVIDUAL LOOP RESISTANCE AS FOLLOWS, M26004 2.5 OHM, M26005 7.7 OHM & M26006 5 .1 OHM ALL WITHIN LIMITS IAW FIM26-11-808. UNABLE TO PROPERLY CHECK RESISTANCE TO GND OF LOOPS & WIRING DUE TO MEGGER 25577 OUT FOR CAL & SDR CALA2014022590478Fseu · malfunctionedFLAPS PRIMARY FAIL EICAS REPLACED FSEU & FLAP PRIMARY LOW SPEED SOLENOID, MAT GND TEST PASSED HIGH LIFT SYS IAW MM 27-51-05, 27-51-00.SDR CALA2013121893784Valve · malfunctionedLT FUEL VLV DOES NOT OPEN, SMG25-20050 SHOWN. CYCLE CB FOR FQPU IAW FIM2 8-41 TASK 801. BACK TO NORMAL., ALL FUEL VLV OPEN.SDR CALA2013121393670Warning Message · false activationAPU BLEED AIR STATUS MSG. FOUND MSG 49-11180, APU SURGE CONTROL VLV NOT IN COMMAND POSITION. BLEED VLV IS WORKING THROUGH SCHEMATIC, OPERATING BOTH AIR CONDITION PACK & MOTORING BOTH ENGS AS NORMAL. APU BLEED AIR CONSIDER A NUISANCE MSG & BLEED VLV IS VERIFSDR CALA2013112693261Apu · malfunctionedON APU START, EGT OVER TEMPED TO OVER 900 DEGREES, APU OBVIOUSLY DID NOT HAVE A SUCCESSFUL START. FIRST START ATTEMPT WAS NOT TOGGLED CORRECTLY, SECOND START ATTEMPT WAS ABORTED DUE TO REPORTED FLAME OUT EXHAUST. TROUBLE SHOT IAW FIM 49-7 0 TASK 81. CREW SHSDR CALA2013102492345Sliding Window · delaminatedLT NR 2 WINDOW HAS LARGE DELAMINATION ALONG LOWER EDGE APPROXIMATELY 11 IN BY 2- 2.5 IN. REPLACED WINDOW IAW MM, OPERATIONS CHECKED OK.SDR CALA2013102192209Wire · damagedDURING SECURITY CHECK, FOUND THREE BROKEN TERMINAL STRIPS ON BOTTOM SIDE OF MID GALLEY TABLE TOP. FOUND COVER INDEX 415 MISSING. ALL STRIPS FEED POWER TO FLOOR PROXIMITY LIGHTING. REPLACED ALL THREE TERMINAL STRIPS & INSTALLED WIRING IAW WDM 25-32-21 & WSDR CALA2013101592087Idg · faultyINBD TO GUM FLT 201 15O CT LT ENG GEN FAILED. FOUND MX MESSAGE 24-31551 IAW FIM 24-11TASK 803. R & R NR 1 ENG IDG IAW AMM 24-11-01. SEE LOG002 FOR OPERATIONS & LEAK CHECK.SDR CALA2013101191981Amplifier · failedSATCOM VOICE DATA LOST. REPLACED HPA FOR HGA IAW MM, GROUND TEST PASSED.SDR CALA2013100391714Satcom · faultySATVOICE LOST SATCOM VOICE SYSTEM LOGS OFF. REPLACED SATELLITE DATA UNIT & SATCOM RADIO FREQ UNIT IAW AMM. OPERATIONS TESTED IAW AMM.SDR CALA2013092491420Connector · damagedFOUND CONNECTOR D5251P ON OEU AT ROW 23 CENTER, CAUSING CIRCUIT BREAKER C23420 "OEU ZN 2 XFR BUSS" TO TRIP. REPLACED DAMAGED CONNECTOR IAW SWPM 20-72-22, WDM23-33-43 & 23-33-46, PSS. OP CHECKED NORMAL.SDR CALA2013092491416Seal · looseRT GEAR STRUT DOOR, FWD EDGE SEAL DAMAGED TWO PLACES. REPLACED DAMAGED BULB SEAL ON RT GEAR STRUT IAW GMM 5-30-06.SDR CALA2013090290925Circuit Card · faultySELECTION INDICATOR LIGHTS ON LEFT AUDIO PANEL AND LEFT RADIO TUNING PANEL WILL NOT DIM. REPLACED M33002 PER AMM.SDR CALA2013082690737Socket · wornENGINE FUEL FILTER RT DIFFERENTIAL PRESSURE ACROSS RIGHT FUEL FILTER APPROACHES BYPASS CONDITION. MESSAGE INTERMITTENT ON TAKE OFF & INITIAL CLIMB MSG-7350922 INACTIVE CL MODE MSG-7360912 INACTIVE IC MODE. ACCOMPLISHED MEL CHECKED OK. FUEL FILTER CLEAR. PERSDR CALA2013082690780Connector · damagedFOUND CONNECTOR D5251P ON OVERHEAD ELECTRONICS UNIT AT ROW 23 CENTER, CAUSING CIRCUIT BREAKER C23420 "OEU ZN 2 XFR BUS" TO TRIP. READING LTS 22-27 DEFG INOPERATIVE ON ACCOUNT OF DAMAGED CONNECTOR AT 23F. CAPPED OFF POWER WIRES TO PIN15 & PIN 06 IAW SWP MANUSDR CALA2013080790207Probe · inoperativeTOTAL FUEL QTY INDICATION INOPERATIVE. REPLACED RT TANK PROBE NR 17. NO ABNORMALITIES NOTED UNDER FUELING PANEL GAUGES.SDR UALA2013071204875Coupling · leakingELECTRICAL BACKUP GENERATOR FAILED. FOUND GENERATOR LOST OIL DUE SERVICE COUPLING LEAKING AND UNABLE TO RESET TO CLOSE. REPLACED COUPLING AND NO LEAKS NOTED. SERVICED GENERATOR. NR 2 BACK UP GENERATOR CHECKED NORMAL IAW AMM 24-25-00.SDR UALA2013070804714Actuator · failedMAINTENANCE MESSAGE FOR FUEL CROSSFEED FWD DISPLAYED ON STATUS PAGE. TRIPPED CIRCUIT BREAKER L23. REPLACED FWD FUEL CROSSFEED ACTUATOR IAW AMM.SDR UALA2013060503902Valve · faultyTRIM AIR PRSOV RT. R & R RT TRIM AIR PRSOV IAW AMM 21-62-01. INSTALLATION TEST PASSED. LEAK CHECKED OK.SDR UALA2013052103513Control Panel · brokenEXIT LIGHT PANEL BROKEN LOCATION 663. SECURED EXIT LIGHT PANEL.SDR UALA2013042302811Sensor · failedSTATUS MESSAGE FOR BLEED FAMV R MAINT. MESSAGE 36-10320. REPLACED MANIFOLD DUAL TEMP SENSOR PER MM, OPS CHECKED GOOD.SDR UALA2013041802685Liner · missingACOUSTIC INSULATION AT 2 O'CLOCK IS MISSING A PIECE ON RIGHT ENGINE 1.5 INCHES DIAMETER PIECE MISSING IN RIGHT ENGINE FRONT FAN CASE RUB STRIP. REPAIRED RUB STRIP PER MM.SDR UALA2013040402211Spring · missingRIGHT GEAR FWD UPLOCK SPRING MISSING.SDR UALA2013040102060Rod End · wornAFT APU MOUNT ROD ENDS WORN. REPLACED ROD ENDS.SDR UALA2013032802016Apu · leakingDUE TO HISTORY OF APU HOC, AND CONSULTATION WITH TOMC, FILL APU OIL LEVEL TO FULL, RAN APU FOR TWO HOURS WITH APU BLEED OFF. APU BURNED 1 QT OF OIL. NO LEAKS FROM LUBE DRAINS. DID FIND OIL LEAKING FROM SURGE VALVE COUPLING DUCT AT AFT DUCT MOUNT POINT. APUSDR UALA2013032601927Slide · low pressureR1 DOOR SLIDE PRESSURE GAUGE OUT OF GREEN BAND. REPLACED DOOR SLIDE PER MM, OPS CHECKED GOOD.SDR UALA2012122107328Switch · faultyFUEL PUMP FAILURE, FLT DIVERTED. FOUND MAINT MSG 23-43770 REPLACED (R) CTR KORRY FUEL SWITCH ON P5 PNL. PER FIM TASK 28-22 TASK 805. OP'S TEST REF; 28-42-01.SDR UALA2012121207172Module · faulty"FMC L" MSG ON LWR EICAS. "SATCOM SYS" INOP. UNABLE TO ACCESS SATCOM SYS ON CDU'S. SATCOM SYS FAILS GRD TEST, MAT FAULTS LEFT AIMS MODULE M002 -- MAINT MSG 31-5023. REF DF0323 FOR CORRELATED FAULT. REPLACED LEFT AIM M002 PER AMM, AIM RESET TEST PASS.SDR UALA2012112806823Valve · faultyFAMV-RIGHT DISPLAYED. REPLACED NR 2 ENG FAMV. PERFORMED AIR SUPPLY TEST FOR NR 2 ENG FAMV. OP CHECKED GOOD.SDR UALA2012111206496Gasket · leakingUPON ARRIVAL AT ORD 200-09NOV EVIDENCE OF OIL LEAK NR 2 ENGINE, HISTORY. SAMC TEXT: PERFORM ENGINE CHECK NR 7-OIL LEAKS PER FIM TASK 71-08 TASK 819 TO IDENTIFY SOURCE OF LEAK. OPBLM-EMC :EVIDENCE OF WETTING AT 1 O'CLOCK TO 6 O'CLOCK INTERMEDIATE CASE AREA. C
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