N714US

Service difficulty reports · 252

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 = 'N714US' 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 USAA2011020490512Fitting · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR27 & BETWEEN S43L TO S43R. REPLACED CLEAT AT FR27 & BETWEEN S43L TO S43R IAW A319 SRM 51-72-11.Jan 17, 2011 · N714US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011012890388Rod · out of adjustSAL - EES - S4 CHECK - DIMENSION A BETWEEN FINGER AND STRIKER LEVER OF THE R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IS OUT OF TOLERANCE. ADJUSTED DIMENSION A BETWEEN FINGER AND STRIKER LEVER OF THE R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW A3Jan 17, 2011 · N714US · Airbus A319112 · Service DoorsSDR USAA2011012890387Dampener · low pressureSAL - EES - S4 CHECK - R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE IS LOW. SERVICED THE R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW A319 AMM 52-10-00-614-001.Jan 17, 2011 · N714US · Airbus A319112 · Service DoorsSDR USAA2011021490743Slide Raft · faultySAL - EES - S4 CHECK - DOOR 841 SLIDE RAFT PACK ASSEMBLY OVER INFLATED. REPLACED DOOR 841 SLIDE RAFT PACK ASSEMBLY IAW TASK CARD 26C841522006.Jan 15, 2011 · N714US · Airbus A319112 · Escape SlideSDR USAA2011021490742Slide Raft · faultySAL - EES - S4 CHECK - DOOR 842 SLIDE RAFT PACK ASSEMBLY OVER INFLATED. REPLACED DOOR 842 SLIDE RAFT PACK ASSEMBLY IAW TASK CARD 26C84252006.Jan 15, 2011 · N714US · Airbus A319112 · Escape SlideSDR USAA2011021490741Damper · low pressureSAL - EES - S4 CHECK - DOOR 832 CYLINDER DOOR DAMPER AND EMERGENCY OPERATION PRESSURE WAS LOW. REPLACED DOOR 832 CYLINDER DOOR DAMPER AND EMERGENCY OPERATION IAW A319 AMM 52-13-14.Jan 15, 2011 · N714US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2011020890609Hinge Fitting · wornSAL - MAJOR REPAIR - S4 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3 AT RIB 5. REPLACED RUDDER HINGE FITTING NR 3 AT RIB 5 IAW A319 SRM 51-72-11.Jan 15, 2011 · N714US · Airbus A319112 · Rudder StructureSDR USAA2011020890608Hinge Fitting · wornSAL - MAJOR REPAIR - S4 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4 AT RIB 6. REPLACED RUDDER HINGE FITTING NR 4 AT RIB 6 IAW A319 SRM 51-72-11.Jan 15, 2011 · N714US · Airbus A319112 · Rudder StructureSDR USAA2011020790565Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 11 TO RIB 12 & 1.8 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 11 TO RIB 12 & 1.8 INCHES FROM TRAILINGJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790564Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.5 INCHES FROM TRAILING EJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790563Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 6 TO RIB 7 & 3.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 6 TO RIB 7 & 3.5 INCHES FROM TRAILING EDGJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790562Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.2 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.2 INCHES FROM TRAILING EJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790561Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 12 TO RIB 13 & 2.8 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 12 TO RIB 13 & 2.8 INCHES FROM TRAILINGJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790560Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 13 & 2.7 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 13 & 2.7 INCHES FROM TRAILING EDGE IAW A319 SRM 55-21-11 & Jan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790559Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 7 & 3.3 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 7 & 3.3 INCHES FROM TRAILING EDGE IAW A319 SRM 55-21-11 & 51Jan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790558Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 8 & 4.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN SURFACE AT THS RIB 8 & 4.5 INCHES FROM TRAILING EDGE IAW A319 SRM 55-21-11 & 51Jan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790557Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE LEFT ELEVATOR UPPER SKIN SURFACE AT THS RIB 6 & 2.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN SURFACE AT THS RIB 6 & 2.5 INCHES FROM TRAILING EDGE IAW A319 SRM 51-77-13.Jan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790556Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.8 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 9 TO RIB 10 & 3.8 INCHES FROM TRAILING EDGJan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011020790555Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 8 TO RIB 9 & 3.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 8 TO RIB 9 & 3.5 INCHES FROM TRAILING EDGE Jan 15, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011021490733Angle · crackedSAL - MAJOR REPAIR - S4 CHECK - RIGHT EMERGENCY EXIT DOOR SEGMENT ANGLE CRACKED BETWEEN BEAM 1-3. REPLACED RIGHT EMERGENCY EXIT DOOR SEGMENT ANGLE CRACKED BETWEEN BEAM 1-3 IAW EO 52101228.Jan 14, 2011 · N714US · Airbus A319112 · Emergency ExitsSDR USAA2011020790544Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jan 14, 2011 · N714US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011020790554Skin · saturatedSAL - S4 - MAJOR REPAIR - TRAPPED WATER INDICATIONS FOUND ON THE LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 12 TO RIB 13 & 4.3 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN SURFACE BETWEEN THS RIB 12 TO RIB 13 & 4.3 INCHES FROM TRAILING EJan 13, 2011 · N714US · Airbus A319112 · Elevator, Plate/SkinSDR USAA2011021790774Sill · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON THE L2 DOOR CUTOUT LOWER SILL AT FR 66, S23L. REPAIRED THE L2 DOOR CUTOUT LOWER SILL AT FR 66, S23L IAW EA 133310.Jan 12, 2011 · N714US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2010120992934Reservoir · low pressureFLT 2186 - DCA-LGA - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ILLUMINATED AND WILL NOT RESET. FOUND LEFT OVERWING EXIT SLIDE RESERVOIR BOTTLE PRESSURE LOW. REMOVED AND REPLACED RESERVOIR BOTTLE ASSEMBLY PER AMM 25-62-46-O4. CIDS WARNING CLEARED.Dec 7, 2010 · N714US · Airbus A319112 · Escape SlideSDR USAA2010091491985Megaphone · inoperativeFLT 1276 - PHL-IND - EMERGENCY EQUIPMENT - FORWARD MEGAPHONE IS INOPERATIVE. REMOVED AND REPLACED FORWARD MEGAPHONE. OPERATIONAL CHECK WAS GOOD.Sep 13, 2010 · N714US · Airbus A319112 · Emergency EquipmentSDR USAA2009061191457Lens · missingFLT 1537 - DEN - EEL - SEATS 8C, 16C, 22C EMERGENCY LIGHT LENS COVERS MISSING. MAINTENANCE INSTALLED LENSES AS REQUIRED.Jun 10, 2009 · N714US · Airbus A319112 · Emergency LightingSDR USAA2009030290473Handle · brokenFLT 772 - PLS-CLT - EMERGENCY EQUIPMENT - 2R DOOR EMERGENCY ASSIST HANDLE BROKEN. MAINTENANCE REMOVED AND REPLACED HANDLE.Feb 27, 2009 · N714US · Airbus A319112 · Passenger/Crew DoorsSDR USAA920081567Coffeemaker · brokenFLT 1062 ABE CLT BURNING ODOR FORWARD COFFEEMAKER HAD ELECTRICAL ODOR. TURNED OFF AND PULLED CIRCUIT BREAKER. NO FURTHER PROBLEMS NOTICED.Aug 24, 2008 · N714US · Airbus A319112 · Buffet/GalleysSDR USAA920081564Light · inoperativeLOGPAGE 7896719 FLT848 PHL EEL ROW 16A SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY LIGHT ASSEMBLY. OPS CHECK WAS GOOD.Aug 24, 2008 · N714US · Airbus A319112 · Emergency LightingSDR USAA920081508Coffeemaker · smokeFLT 981, SMOKE CAME OUT FWD COFFEEMAKER WHEN TURNED ON. R & R FORWARD COFFEEMAKER. OPS CHECK WAS GOOD.Aug 8, 2008 · N714US · Airbus A319112 · Buffet/GalleysSDR SA08019Slide Raft · bulgedPIT - THE RIGHT, AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED A CLEARANCE CHECK. MAINTENANCE REPLACED THE RIGHT AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE. INSPECTED OK FOR SERVICE.Mar 22, 2008 · N714US · Airbus A319112 · Escape SlideSDR USAA920080697Slide Raft · deflatedPIT - EES - C11 CHECK - R2 DOOR SLIDE FAILED CLEARANCE CHECK. REPLACED R2 DOOR SLIDE IAW USAIRWAYS TASKCARD 26C84252002.Mar 22, 2008 · N714US · Airbus A319112 · Escape SlideSDR SA06021Odor · detectedAT 10,000 FEET DURING DESCENT INTO JAX, THE CABIN CREW DETECTED A BURNING ODOR AROUND ROW 17 LEFT. AFTER LANDING, THE CREW SHUT DOWN THE NR 2 ENGINE AND OPENED UP THE CROSS BLEED. THE ODOR DISSIPATED. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. Apr 3, 2006 · N714US · Airbus A319112 · Air Distribution SystemSDR SA05047Strut · lowPIT FLT 219 ENROUTE PIT - TPA, AFTER TAKEOFF, ECAM MESSAGE 'L/G SHOCK ABSORBER FAULT' DISPLAYED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT.Apr 28, 2005 · N714US · Airbus A319112 · Main Landing Gear Strut/Axle/TruckSDR USAA050520Floorbeam · corrodedPIT - FOUND BEAM CORRODED .25 INCH DIAMETER, RT OUTER SILL BEAM, FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00 DWG IED 53474180. (M)Apr 16, 2005 · N714US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA050519Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED .25 INCH DIAMETER SPOT, RT OUTBOARD SEAT TRACK, FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK NR JA-260-53500. (M)Apr 16, 2005 · N714US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA050521Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED, RT INBOARD SEAT TRACK AT FRAME 20. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M)Apr 16, 2005 · N714US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA050523Seat Track · corrodedPIT - FOUND SEAT TRACK BEAM CORRODED .25 INCH BY 1.5 INCH AREA, FRAME 66-68. DEFECTIVE PART REPLACED WITH IDENT PART NUMBER. (M)Apr 15, 2005 · N714US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA050498Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 1 FT BY 1.5 INCH FRAME 20. DEFECTIVE PART REPLACED WITH IDENT PART. (M)Apr 14, 2005 · N714US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA050499Floorbeam · corrodedPIT - FOUND FLOORBEAM ASSEMBLY .25 INCH BY .5 INCH CORROSION, FRAME 69L Y1440. DEFECTIVE PART REPLACED WITH IDENT PART. (M)Apr 14, 2005 · N714US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA050497Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 1 INCH IN DIAMETER, LT INBOARD SEAT TRACK BEAM AT FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART. CORROSION LEVEL 1, TASK JA 260-53500. (M)Apr 13, 2005 · N714US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA050500Frame · corrodedPIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH BY .072 INCH DEEP AREA, TOP SURFACE OF FRAME FROM C12-16, 12 INCHES LEFT OF C/L. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14 FIG 106. CORROSION LEVEL 1, TASK JA-220-53500. DEFECTIVE PART REPLACED WITHApr 10, 2005 · N714US · Airbus A319112 · Fuselage Main, FrameSDR SA05020Epsu · faultyTHE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY TESTS OK.Feb 10, 2005 · N714US · Airbus A319112 · Emergency LightingSDR USAASA04009Power Supply · inoperativeDCA - THE EMERGENCY LIGHTS WOULD NOT PASS THE SELF TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID CABIN, RIGHT HAND POSITION. OPS CHECKED OK. (M)Jan 28, 2004 · N714US · Airbus A319112 · Emergency LightingSDR USAASA03034Power Supply · failedTHE AFT EMERGENCY POWER SUPPLY UNIT SHOWS FAULT. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. SYSTEM CHECKS OK. (M)Apr 21, 2003 · N714US · Airbus A319112 · Emergency LightingSDR USAASA02045Control Unit · malfunctionedCLT - FLT 9202 - EN ROUTE PIT-CLT - THE LANDING GEAR DOORS DID NOT CLOSE AFTER GEAR RETRACTION. THE LANDING GEAR WAS RECYCLED AND THE LANDING GEAR DOORS CLOSED NORMALLY. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE CHECK OF THE LAMay 5, 2002 · N714US · Airbus A319112 · Landing Gear Door Retract SectionSDR USAASA02044Proximity Sensor · out of adjustPIT - FLT 132 - EN ROUTE DEN-PIT - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF IN DEN. WHEN THE LANDING GEAR WAS CYCLED, THE LANDING GEAR RETRACTED NORMALLY. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT GEAR FORWARD MAIN LANDIMay 4, 2002 · N714US · Airbus A319112 · Landing Gear Position and WarningSDR USAASA02043Proximity Sensor · faultyBOS - FLT 2143 - EN ROUTE MHT-BOS, AFTER DEPARTURE FROM MHT, THE NOSE LANDING GEAR WOULD NOT RETRACT. WHEN THE LANDING GEAR HANDLE WAS CYCLED, THE LANDING GEAR RETRACTED NORMALLY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PRMay 2, 2002 · N714US · Airbus A319112 · Landing Gear Position and WarningSDR USA2002F00003Proximity Sensor · faultyENROUTE, AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT. WHEN THE LANDING GEAR WAS RECYCLED, THE GEAR RETRACTED NORMALLY. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR PROXIMITY SENSOR 25GA. FUNCTIONALLYApr 30, 2002 · N714US · Airbus A319112 · Landing Gear Position and WarningSDR USAASA02019Connector · looseRDU - THE LEFT FORWARD ESCAPE SLIDE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE RECONNECTED LOOSE PLUG BEHIND THE SLIDE ASSEMBLY. OPERATIONALLY CHECKED OK. (M)Feb 9, 2002 · N714US · Airbus A319112 · Emergency Lighting
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