N738US

Service difficulty reports · 272

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 = 'N738US' 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.

SDR USAA2011081500003Floorbeam · corrodedC11, SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y-464.8. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y-464.8 IAW A319 SRM 51-72-11AND EA 200589.Aug 6, 2011 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011081500002Floorbeam · corrodedC11, SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y-765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y-765 IAW A319 SRM 51-72-11, 53-41-14 AND EA 200589.Aug 6, 2011 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2010032990656Lens · missingFLT 805 - PIT-PHL - EMERGENCY LIGHTS - DOOR 1R IS MISSING AN EXIT SIGN. INSTALLED MISSING LENS DOOR 1R.Mar 28, 2010 · N738US · Airbus A319112 · Emergency LightingSDR USAA2009071891877Selector Valve · failedLOGPAGE:8648088 - FLT 867 - PHL-PUJ - AIR TURN BACK - LANDING GEAR CONTROL AND INTERFACE UNIT (LGCIU) 1 FAULT DURING CLIMB. RETURNED TO PHL. REMOVED AND REPLACED LANDING GEAR DOOR SELECTOR VALVE 41GA PER MAINTENANCE MANUAL 32-31-34. OPERATIONAL AND LEAK CHEJul 16, 2009 · N738US · Airbus A319112 · Landing Gear SelectorSDR USAA920081178Oil Cooler · inoperativeFLT 1744 CLT - PHL - ELECTRICAL POWER LOSS - AIRCRAFT DEPARTED CLT WITH THE NR1 IDG ON MEL. CREW REPORTED APU AUTO SHUTDOWN AT FL 330. RESTARTED AT FL 290 AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU OIL COOLER. OJun 5, 2008 · N738US · Airbus A319112 · APU Oil SystemSDR SA07071Engine · malfunctionedRIC FLT 1673 - EN ROUTE RIC TO CLT. AT APPROXIMATELY FL190, THE FLIGHT EXPERIENCED EXTREME VIBRATION COMING FROM THE NUMBER ONE ENGINE. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. UPON REACHING THE GATE, IT WAS REPORTED THAT PASSENGERSOct 30, 2007 · N738US · Airbus A319112 · Engine (Turbine/Turboprop)SDR SA06045Idg · lowDFW FLT 1002 EN-ROUTE CLT TO PHX. WHILE IN FLIGHT, THE AIRCRAFT INTERMITTENTLY INDICATED A NR 2 IDG LO OIL PRESSURE. THE CREW STARTED THE APU AND HAD AN APU AUTO SHUTDOWN. THE CREW DECIDED TO DIVERT TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCEJun 21, 2006 · N738US · Airbus A319112 · AC Generator-AlternatorSDR USAA051219Floorbeam · corrodedLEFT AFT ENTRY SILL BEAM (FR 66 & Y1492) HAS CORROSION. DOUBLERS INSTALLED PER SRM 53-41-14, DEFECT SIZE: 1.5 X 1 INCH AREA.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA051217Floorbeam · corrodedAT SPLICE PLATE Y1292 FR 66 TO 68 FLOORBEAM; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: .030 TO .060 INCH DEEP.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA051216Frame · corrodedAROUND CLIP NUT HOLE ON AFT SERVICE DOOR (RT) SILL BEAM AT FR 66 CORRODED. INSTALLED REPAIR ANGLES & FILLED PER SRM 53-41-14; CORROSION, LEVEL 2; TASK JA-260-53500, DEFECT SIZE: 0.500" X 0.500".Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, FrameSDR USAA051213Floorbeam · corrodedY505, FRAME C-12 TO C-16; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED & REPLACED FLOORBEAM PER SRM 53-11-14, DEFECT SIZE: 1 X 4 INCH.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA051215Floorbeam · corrodedY1292 BEAM AT SPLICE AT FR 66; CORROSION LEVEL 2; TASK JA-260-53500. REMOVED & REPLACED PER SRM 51-72-11, IPC 53-41-04, DEFECT SIZE: 2 X 4 X .030 INCH DEEP.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA051214Floorbeam · corrodedY1162 BEAM AT SPLICE FR 68 & 69; CORROSION LEVEL 2; TASK JA-260-53500. REMOVED & REPLACED PER SRM 51-72-11 & IPC 53-41-04, DEFECT SIZE: 3 X 3 X .030 INCH DEEP.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA051218Shear Web · corrodedLT SIDE SHEAR WEB BETWEEN FR 69 & 70; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00, DEFECT SIZE: .75 INCH DIA AREA.Oct 19, 2005 · N738US · Airbus A319112 · Fuselage Main, StructureSDR SA05085Turbine · damagedEN-ROUTE, CLT TO PHL. AFTER DEPARTURE, THE NR 1 ENGINE HAD A DOUBLE COMPRESSOR STALL, FOLLOWED BY AN IMMEDIATE EGT OVERTEMP. THE CREW FOLLOWED PROCEDURE AND SHUT DOWN THE NR 1 ENGINE. FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENJul 15, 2005 · N738US · Airbus A319112 · Turbine SectionSDR SA05073Computer · failedON FINAL APPROACH, AT 500 FEET AGL, THE CAPTAIN'S AIRSPEED INDICATOR READ 25 KNOTS SLOWER THAN THE FIRST OFFICER'S INDICATION. JUST BEFORE LANDING, THE POWER SURGED TO TOGO WITHOUT PILOT INPUT. THE PILOT FLYING PULLED THE POWER BACK TO IDLE AND LANDED WITHOUJun 14, 2005 · N738US · Airbus A319112 · Pitot/Static Anti-Ice SystemSDR SA04113Windshield · crackedPUJ FLT 799 EN ROUTE CLT TO PUJ, THE F/O'S WINDSHIELD CRACKED ON DESCENT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CRACKED WINDSHIELD. OK FOR SERVICE.Dec 7, 2004 · N738US · Airbus A319112 · Flight Compartment WindowsSDR USAASA04012Power Supply · inoperativeDCA - THE EMERGENCY LIGHTS DO NOT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID RIGHT CABIN POSITION. (M)Feb 7, 2004 · N738US · Airbus A319112 · Emergency LightingSDR USAASA03020Power Supply · inoperativeCLT - AN 'INT LOAD EMERG L' FAULT WAS GENERATED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)Feb 28, 2003 · N738US · Airbus A319112 · Emergency LightingSDR USAASA02066Power Supply · inoperativeTPA - THE EMEREGNCY LIGHT TEST SHOWS 'L EPSU LOAD FAULT FORWARD'. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)Jul 22, 2002 · N738US · Airbus A319112 · Emergency LightingSDR USAASA01036Power Supply · faultyCLT - RECEIVED 'EPSU INT LOAD EMER L' MESSAGE ON THE CABIN INTERCOMMUNICATIONS DATA SYSTEM DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT (11WL). OPS CHECKED OK. (M)Jul 18, 2001 · N738US · Airbus A319112 · Emergency LightingSDR USAASA00034Power Supply · inoperativeCLT - THE EPSU INT LOAD EMER L MESSAGE CAME ON DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. LIGHT TEST CHECKS NORMAL. (M)Sep 13, 2000 · N738US · Airbus A319112 · Emergency Lighting
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