N722US

Service difficulty reports · 299

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 = 'N722US' 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 USAA2011080400013Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011080200013Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D534-72780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200012Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200011Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y254. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y254 IAW A319 SRM 51-72-11 AND AIRBUS DRAWINGS D53472750 AND D53472780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200010Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11AND AIRBUS DRAWING 53472780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200044Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+15 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+15 INCHES, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53480505.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011080200043Floorbeam · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1540. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1540 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200040Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER AFT CORNER FITTING AT R2 DOOR AT FR68, S23R. REPLACED LOWER AFT CORNER FITTING AT R2 DOOR AT FR68, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011080200036Shear Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING 53474180.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011080200034Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, S23R, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011080200033Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y465 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534 72816.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200032Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1235. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1235 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200031Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1235. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, Y1235 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200030Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D534-72780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200029Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162 IAW A318 SRM 51-72-11 & AIRBUS DRAWING 53472780.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011080200017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53110900.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011072200024Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WEB BETWEEN FR16 TO FR12, -Y1652. REPLACED RIGHT WEB BETWEEN FR16 TO FR12, -Y1652 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53114392.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011072200023Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WEB BETWEEN FR20 TO FR24, Y1652. REPLACED LEFT WEB BETWEEN FR20 TO FR24, Y1652 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011072200022Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, -Y1652. REPLACED WEB BETWEEN FR20 TO FR24, -Y1652 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53114392.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011072200021Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, Y512 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2011072200020Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011072200019Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112831.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2011072200018Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y189. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111406.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011072200017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011072200016Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11.Jul 8, 2011 · N722US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2011080900037Skin · damaged2S CHECK - BLEND OUT ON EXTERNAL SKIN LOCATED BETWEEN FR29 TO FR30 AND BETWEEN S19L TO S20L UPPER FUSELAGE. REPAIRED FUSELAGE EXTERNAL SKIN BETWEEN FR29 TO FR30 AND BETWEEN S19L TO S20L IAW A319 SRM 53-21-11.Jul 7, 2011 · N722US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2011081100003Access Panel · cracked2S CHECK - 4 EA CRACKS ON LEFT PYLON ACCESS PANEL 413DL. REPAIRED LEFT PYLON ACCESS PANEL 413DL IAW EA 133733.Jul 6, 2011 · N722US · Airbus A319112 · Nacelle/Pylon, Plate/SkinSDR USAA2011041191395Flashlight · inoperativeFLT 1982 - CLT-BOS - EMERGENCY LIGHTS - EMERGENCY FLASHLIGHT FORWARD FLIGHT ATTENDANT STATION NO FLASHING RED LIGHT. REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT.Apr 8, 2011 · N722US · Airbus A319112 · Emergency LightingSDR USAA2009060491400Pin · corrodedPIT - GEAR CHANGE - CORROSION & PITTING ON MAIN LANDING GEAR RIGHT REAR PINTLE PIN. REPLACED MAIN LANDING GEAR RIGHT REAR PINTLE PIN IAW US AIRWAYS TASK CARD 26T00032001.May 30, 2009 · N722US · Airbus A319112 · Main Landing Gear Attach SectionSDR USAA920081378Line · crackedFLL-DCA-FLT 1712 - CREW RECEIVED A GREEN HYDRAULIC SYSTEM LOW MESSAGE. CREW DIVERTED TO BWI. AS A PRECAUTION, CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. CREW WAS ABLE TO EXIT THE RUNWAY BY DIFFERENTIAL BRAKING. ACFT WAS TOWED TO THE GATE. MX Jul 15, 2008 · N722US · Airbus A319112 · Hydraulic System, MainSDR SA08024Flashlight · inoperativePIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT.Apr 3, 2008 · N722US · Airbus A319112 · Emergency EquipmentSDR SA02024Flashlight · inoperativePIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT.Apr 3, 2008 · N722US · Airbus A319112 · Emergency EquipmentSDR SA07076Unknown · odorMCI FLT 1609 MCI - CLT. A STRONG ODOR WAS NOTED IN THE CABIN. MAINTENANCE ACTION PENDING.Nov 18, 2007 · N722US · Airbus A319112 · Air Distribution SystemSDR SA07056Epsu · malfunctionedPHL - THE EMERGENCY LIGHTS TEST INDICATED EMERGENCY BATTERY FAULT. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT.Aug 31, 2007 · N722US · Airbus A319112 · Emergency LightingSDR SA07040Epsu · dischargedCLT - THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT BATTERY SHOWS FAULT ON TEST. MAINTENANCE REPLACED THE BATTERY ON THE LEFT, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Jun 19, 2007 · N722US · Airbus A319112 · Emergency LightingSDR SA07033Battery Pack · dischargedDCA - THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY INDICATED A LOW CHARGE. MAINTENANCE REPLACED THE LEFT HAND, MID-CABIN EMERGENCY EXIT LIGHT BATTERY. OPERATIONALLY CHECKS OK.Jun 5, 2007 · N722US · Airbus A319112 · Emergency LightingSDR SA07027Epsu · faultyBDL - DURING THE EMERGENCY LIGHTS TEST, RECEIVED -EPSU FWD L- MESSAGE. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Apr 17, 2007 · N722US · Airbus A319112 · Emergency LightingSDR SA07026Epsu · faultyBDL - THE EMERGENCY LIGHT SYSTEM FAULTED WITH -EXT LOAD AFT L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Apr 17, 2007 · N722US · Airbus A319112 · Emergency LightingSDR USAA050867Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH DIAMETER HOLES AROUND NUT PLATES, -Y1200 BETWEEN FRAME 66/69. REPLACED 3 SECTIONS OF FLOORBEAM PER SRM 51-72-11. (M)Jul 13, 2005 · N722US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA050868Beam · corrodedFOUND BEAM CORRODED 8 INCHES BY 2 INCHES, BETWEEN FRAME 14 AND 16 Y 503.2. REPLACED BEAM BEAM PER SRM 51-72-11. (M)Jul 13, 2005 · N722US · Airbus A319112 · Fuselage Main, StructureSDR USAA050869Floorbeam · corrodedPIT - FOUND BEAM CORRODED 2 INCHES BY 1 INCH, FLOORBEAM FRAME 16, FRAME 16-Y254. REPLACED BEAM PER SRM 51-72-11. (M)Jul 13, 2005 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA050870Beam · corrodedPIT - FOUND BEAM CORRODED 10 INCHES BY 2 INCHES, BETWEEN FRAME 16 AND 20 Y254. INSTALLED BEAM PER SRM 51-72-11. (M)Jul 13, 2005 · N722US · Airbus A319112 · Fuselage Structure (General)SDR USAA050871Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 5 FEET, TOP OF BEAM FRAME 66 THROUGH FRAME 69. REPLACED FLOORBEAM AND A SPLICE PART PER SRM 51-72-11. (M)Jul 13, 2005 · N722US · Airbus A319112 · Fuselage Main, Floor BeamSDR SA05003Odor · detectedIN CRUISE FLT, CABIN CREW REPORTED A RUBBER/ELECTRIC ODOR AROUND ROW 18. THE VIDEO ENTERTAINMENT SYS TURNED OFF. ODOR SUBSIDED, BUT CAME BACK BRIEFLY. ODOR SUBSIDED AGAIN & REMAINED THAT WAY FOR THE REST OF THE FLIGHT. MX COULD NOT DUPLICATE THE ODOR. PLAJan 2, 2005 · N722US · Airbus A319112 · Air Distribution SystemSDR SA04112Wire · disconnectedTHE EMERGENCY EXIT LIGHT WIRING WAS FOUND DISCONNECTED AND THE MAIN ENTRANCE DOOR SLIDE COVER LOOSE. MAINTENANCE INSTALLED THE LOOSE SLIDE COVER AND CONNECTED THE EMERGENCY LIGHT WIRING. OPERATIONALLY CHECKS OK.Dec 3, 2004 · N722US · Airbus A319112 · Emergency LightingSDR SA04107Contactor · out of adjustTHE CABIN CREW REPORTED THAT THE LEFT OVERWING EXIT LIGHT DOES NOT ILLUMINATE WHEN NO PED SWITCH IS TURNED ON. MAINTENANCE ADJUSTED A CONTACT. OPERATIONALLY CHECKS OK.Nov 20, 2004 · N722US · Airbus A319112 · Emergency LightingSDR USAASA02038Wire · damagedBDL - THE EMERGENCY LIGHT ON SEAT 8C WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING AT CONNECTOR ON BOTTOM OF SEAT. OPERATIONALLY CHECKED OK. (M)Apr 23, 2002 · N722US · Airbus A319112 · Light System WiringSDR USAASA01013Power Supply · dischargedPHL - THE LT AND RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)Apr 21, 2001 · N722US · Airbus A319112 · Emergency LightingSDR USAASA00025Unknown · odorPHX-PHL - FLT 168 - AN ODOR BECAME PRESENT IN THE FORWARD GALLEY AFTER TAKEOFF. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GALLEY, COFFEEMAKER, CHILLERS, ELECTRICAL DEVICES, AND OTHER EQUIPMENT. ALSO, RAN ENGINE, APUJun 24, 2000 · N722US · Airbus A319112 · Air Distribution System
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