N704US

Service difficulty reports · 285

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 = 'N704US' 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 USAA2009070891726Girt Bar · damagedFLT 1651 - AFTER TAKEOFF 2R SLIDE ARMING HANDLE MOVES OUT OF ARMED POSITION, DISARMS SLIDE AND WILL NOT GO BACK INTO THE ARMED POSITION. MAINTENANCE REMOVED METAL SHAVING FROM GIRT BAR FITTING & CLEANED DEBRIS FROM SLIDE ASSEMBLY.Jul 7, 2009 · N704US · Airbus A319112 · Emergency EquipmentSDR SA06075Slide · tornIAD - A STRAP FROM THE L-1 DOOR ESCAPE SLIDE/RAFT TO THE SLIDE COVER WAS FOUND TORN OFF. MAINTENANCE REPLACED THE L-1 DOOR ESCAPE SLIDE/RAFT. OK FOR SERVICE.Sep 26, 2006 · N704US · Airbus A319112 · Escape SlideSDR USAA061105Skin · delaminatedFOUND SKIN DELAMINATION BOTTOM OF LEFT BLEV-18" FROM I/B END. REMOVED DAMAGE AND REPOTTED AREA PER SRM 55-21-11, DEFECT SIZE: 6" X 1.5".Aug 30, 2006 · N704US · Airbus A319112 · Elevator, Plate/SkinSDR USA2004F00064Strap · misroutedTHE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE LT FORWARD ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.Jun 3, 2004 · N704US · Airbus A319112 · Escape SlideSDR USAA040148Sill · corrodedBFM - FOUND DOOR SILL BEAM CORRODED 1.2 INCHES LONG BY .080 INCH WIDE BY .052 INCH DEEP, BETWEEN FRAME 66-68, Y1970, -Z240. REMOVED AND REPLACED PART PER SRM 51-74-00, 53-41-14, 53-42-11, 51-77-11, 51-42-11. (M)Apr 28, 2004 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAASA04039Slide · inoperativeCLT - THE MAIN CABIN ENTRY DOOR WOULD NOT ARM. THE SLIDE ARMED LIGHT WOULD FLASH ON AND OFF ON ECAM DOOR DISPLAY. ALSO, THE HANDLE WAS SPONGY. MAINTENANCE REPLACED THE MAIN CABIN ENTRY DOOR SLIDE/RAFT. OK FOR SERVICE. (M)Apr 28, 2004 · N704US · Airbus A319112 · Escape SlideSDR USAA040155Sill · corrodedBFM - FOUND SILL PLATE ASSEMBLY CORRODED 5 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP, L2 DOOR SILL PLATE ASSEMBLY, Y1732 FORWARD OF FRAME 66. REMOVED AND REPLACED PER SRM 53-41-14, 53-41-11. (M)Apr 27, 2004 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040157Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 2 INCHES BY 38.5 INCHES BY 13 INCHES AND .5 INCH BY 10 INCH AREA, PANEL NR 222FF, FRAME 16-20, Y=-1732, Z=-240. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-02-00. CORROSION LEVEL 2, TASK NR JA-220-53300. (M)Apr 24, 2004 · N704US · Airbus A319112 · Fuselage Floor PanelSDR USAA040158Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 36 INCHES, 1 INCH BY 12 INCHES, 1 INCH BY 10 INCHES, PANEL NR 221FF, FRAME 16-20, Y=1732, Z=-240. REMOVED AND INSTALLED NEW PANEL. CORROSION LEVEL 2, TASK NR JA-220-53300-001. (M)Apr 24, 2004 · N704US · Airbus A319112 · Fuselage Floor PanelSDR USAA040153Beam · corrodedFOUND BEAM CORRODED 1 INCH BY 1 INCH BY .023 INCHE DEEP, FRAME 66, -Y1292, -Z240. REMOVED AND REPLACED BEAM PE SRM 53-41-15, 51-74-00, 51-42-11. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040154Plate · corrodedBFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH BY 1.4 INCH BY .025 INCH, FRAME 69, -Y1732, -Z240. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-02-00, 51-77-10, 51-11-00, 51-72-11. CORROSION LEVEL 2, TASK NR JA-260-53500.(M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040156Floorboard · corrodedBFM - FOUND FLOORBOARD CORRODED 1.3 INCHES BY 1.125 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, -Y1732, -Z240. REMOVED AND REPLACED FLOORBOARD PER SRM 51-42-11, 51-74-00. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Floor PanelSDR USAA040149Beam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY .20 INCH BY .27 INCH DEEP AREA, FRAME 67, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15 51-42-11, 53-00-14, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040150Beam · corrodedBFM - FOUND BEAM ASSEMBLY CORRODED 1 INCH BY 1.2 INCH BY .035 INCH DEEP AREA, BETWEEN FRAME 64/65, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040151Beam · corrodedBFM - FOUND BEAM CORRODED 1.2 INCH BY 1 INCH BY .047 INCH DEEP AREA, BETWEEN FRAME 68 AND 69, Y1292,-Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040152Beam · corrodedBFM - FOUND BEAM CORRODED 2 INCHES BY 1.6 INCHES BY .058 INCH DEEP AREA, FRAME 68, -Y1732, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040159Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 1.5 INCH BY 2.5 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, Y1732, -Z240. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-42-11, 51-74-00. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage Floor PanelSDR USAA040147Seat Track · corrodedBFM - FOUND SEAT TRACK CORRODED 1.5 INCHES BY 2.4 INCHES BY .067 INCHES DEEP AREA, BETWEEN FRAME 67 AND 68, -Y1732, -Z24. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED SEAT RACK PER SRM 53-00-15, 51-74-00, 51-42-00, 53-00-14. (M)Apr 23, 2004 · N704US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040145Beam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY .65 INCH BY .045 INCH DEEP AREA, FRAME 20, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-11-14, 51-23-11. CORROSION LEVEL 2. TASK NR JA-220-53500. (M)Apr 21, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040144Crossbeam · corrodedBFM - FOUND CORSSBEAM CORRODED, 1 INCH BY .7 INCH BY .55 INCH DEEP, FRAME -Y254, CROSSBEAM C68 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M)Apr 20, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040115Shear Plate · corrodedBFM - FOUND SHEAR PLATE CORRODED 1.2 INCH BY 1.3 INCH BY .012 INCH AREA, BETWEEN C69-C70, Y-1292. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11, 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)Apr 19, 2004 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040146Beam · corrodedBFM - FOUND BEAM CORRODED 2.8 IN BY 1.2 INCH BY .050 INCH DEEP AREA, FRAME 16, -Y1292, -Z240. CORROSION LEVEL 2, TASK NR JA-220-53500. FABRICATED AND INSTALLED ANGLE, DOUBLER, FILLER PER SRM 53-11-14, 53-1-14, 51-42-11. (M)Apr 19, 2004 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040142Beam · corrodedBFM - FOUND BEAM CORRODED 1 INCH BY .75 INCH BY .024 INCH DEEP, FRAME 68, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 53-00-14. CORRODED LEVEL 2, TASK NR JA-260-53500. (M)Apr 16, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAA040143Crossbeam · corrodedBFM - FOUND CROSSBEAM CORRODED 1.3 INCHES BY 1.9 INCH BY .033 INCH AREA, C68, Y-765, AND -Z240. REMOVED AND REPLACED CROSSBEAM PER SRM 51-74-00, 53-00-15, 53-00-14. (M)Apr 16, 2004 · N704US · Airbus A319112 · Fuselage Main, StructureSDR USAASA03141Psu · inoperativePHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT POSITION FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)Dec 25, 2003 · N704US · Airbus A319112 · Emergency LightingSDR USAASA03024Battery Pack · inoperativePHL - THE EMERGENCY POWER SUPPLY UNIT, FORWARD BATTERY PACK, WAS INOPERATIVE IN THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACK. OPERATIONALLY CHECKS OK. (M)Mar 18, 2003 · N704US · Airbus A319112 · Emergency LightingSDR USAA020462Floorbeam · corrodedTPA - FOUND FLOORBEAM WITH 1 INCH SQUARE CORRODED AREA, UPPER SURFACE FLOOR SUPPORT BEAM Y765 AT FRAME 66. REMOVED AND REPLACED FLOORBEAM PER SRM 53-41-04. (M)Nov 16, 2002 · N704US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA020461Floorbeam · corrodedTPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOORBEAM Y1292 AT FRAME 16. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-11-15. (M)Nov 16, 2002 · N704US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA020460Floor Support · corrodedFOUND BEAM CORRODED .5 INCH AREA AROUND ATTACH HOLE, UPPER SURFACE FLOOR SUPPORT BEAM Y1292 AT FRAME 66. BLENDED CORRODED AREA AND RESTORED FINISH PER EA 94374. (M)Nov 16, 2002 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA020459Floor Support · corrodedPIT - FOUND BEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT 71292 AT FRAME 68. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR TRIPLER AT EXISTING SPLICE PER EA 94375. (M)Nov 16, 2002 · N704US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA020458Floorbeam · corrodedTPA - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, UPPER SURFACE FLOOR SUPPORT BEAM Y1732 FRAME 66. CLEANED CORRODED AREA, INSTALLED REPAIR ANGLES PER SRM 53-41-14 FIG 201. (M)Nov 16, 2002 · N704US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAASA02023Proximity Sensor · faultyPIT - FLT 1686 - EN ROUTE DFW-PIT, ON APPROACH TO PIT, WHEN THE LANDING GEAR WAS EXTENDED, RECEIVED 'L/G DOORS NOT CLOSED' AND 'L/G SYSTEM DISAGREE' MESSAGES. THE NOSE GEAR DID NOT INDICATE GREEN. THE LANDING GEAR WAS RECYCLED AND THE GEAR EXTENDED ON THE SEFeb 17, 2002 · N704US · Airbus A319112 · Landing Gear Position and WarningSDR USAASA02021Landing Gear · malfunctionedPIT - FLT 2153 - EN ROUTE PIT-MSP, THE NOSE LANDING GEAR FAILED TO EXTEND ON APPROACH TO MSP. THE LANDING GEAR WAS CYCLED AND WAS EXTENDED ONCE MORE. THE LANDING GEAR EXTENDED OK ON THE SECOND ATTEMPT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TEFeb 15, 2002 · N704US · Airbus A319112 · Landing Gear Retraction/Extension SystemSDR USAASA01018Wire · brokenSFO - ROWS SIX AND THIRTEEN SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE WITH BROKEN WIRES AT THE SEAT CONNECTORS. MAINTENANCE REPLACED THE WIRES. OPERATIONALLY CHECKED OK. (M)May 11, 2001 · N704US · Airbus A319112 · Light System WiringSDR USAASA00007Power Supply · dischargedTPA - THE RIGHT OVERWING EXIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRES FOUND UNDER THE SEAT AND REPLACED THE POWER SUPPLY. OPS CHECKED OK. (M)Feb 13, 2000 · N704US · Airbus A319114 · Emergency Lighting
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