N756US

Service difficulty reports · 219

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 = 'N756US' 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 USAA2014043000007Floor Panel · delaminatedWEEKLY CHECK DELAMINATION ON AFT CARGO FLOOR PANEL 151VG BETWEEN FRAME 53 TO FRAME 56 & BETWEEN STRINGER 35L TO STRINGER 35R, Z 150. REPLACED AFT CARGO FLOOR PANEL 151VG IAW AMM 53-42-14.Apr 30, 2014 · N756US · Airbus A319112 · Fuselage Floor PanelSDR USAA2014042400005Slide · dischargedGDAFR VISIT LT OFF WING SLIDE INFLATION RESERVOIR DISCHARGED. REPLACED LT OFF WING SLIDE INFLATION RESERVOIR IAW AMM 25-62-46-400-001-A.Apr 23, 2014 · N756US · Airbus A319112 · Escape SlideSDR USAA2014042200001Fitting · dirtyCREW REPORTED DOOR 1L ARMING HANDLE HARD TO MOVE. CLEANED GIRT BAR FLOOR FITTINGS & SPRING PAWLS. ARMING MECHANISM CHECKED GOOD IAW AMM 25-62-44-400-006.Apr 21, 2014 · N756US · Airbus A319112 · Emergency EquipmentSDR USAA2014011300002Engine · bird ingestionJUST AFTER LIFTOFF, MULTIPLE BIRD STRIKES ON RT SIDE OF ACFT, MULTIPLE COMPRESSOR STALLS. RETARDED NR 2 ENG TO CLIMB, STALLS STOPPED. FLIGHT ATTENDANT REPORTED ODOR FROM AIR CONDITIONING. SELECTED NR 2 BLEED & NR 2 PACK OFF. FLIGHT RETURNED TO DCA, LANDED Jan 11, 2014 · N756US · Airbus A319112 · Engine (Turbine/Turboprop)SDR USAA2013092600008Proximity Switch · faultyCREW REPORTED THE R2 DOOR SHOWS OPEN WHEN CLOSED. MX REPLACED R2 DOOR SWITCH IAW AMM 52-71-11-000-001. OPS CHECKED OK.Sep 25, 2013 · N756US · Airbus A319112 · Door Warning SystemSDR USAA2013092300026Light · inoperativeMX REPORTED THE FLOOR EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. R & R LIGHT. OPS CHECKED GOOD, IAW 33-51-12.Sep 23, 2013 · N756US · Airbus A319112 · Emergency LightingSDR USAA2013091000008Cover · brokenCREW REPORTED THE EMERGENCY LIGHT COVER ABOVE 2R DOOR BROKEN. MX REPLACED MISSING LENS ABOVE 2R DOOR. CHECKS GOOD.Sep 9, 2013 · N756US · Airbus A319112 · Emergency LightingSDR USAA2013050700009Cover · missingCREW REPORTED THE EMERGENCY EXIT LIGHT COVER MISSING FROM LOWER 2L SERVICE DOOR. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT COVER.May 7, 2013 · N756US · Airbus A319112 · Emergency LightingSDR USAA2013041800012Bottle · low pressureMAINTENANCE FOUND THE L1 SLIDE PRESSURE LOW (OUT OF GREEN BAND). MAINTENANCE REMOVED AND REPLACED L1 SLIDE ASSEMBLY PER JOB CARD 6L00025010.Apr 17, 2013 · N756US · Airbus A319112 · Escape SlideSDR USAA2013041700012Unknown · malfunctionedFLIGHT DEPARTED MCI WITH MEL 21-26-04A APPLIED, SKIN AIR OUTLET VALVE INOP. AFTER TAKEOFF, CREW RECEIVED AN ECAM MESSAGE: VENT SKIN VALVE FAULT. PERFORMED ECAM PROCEDURE PER OPS PROCEDURE FOUND IN MEL 21-26-04 (WHICH THE AIRPLANE IS CORRECTLY UNDER). ECAM PApr 16, 2013 · N756US · Airbus A319112 · Cabin Cooling SystemSDR USAA2012122000012Cover · missingCREW REPORTED THE EMERGENCY EXIT LIGHT COVER AT ROW 1 NEEDS REPLACED. MAINTENANCE REPLACED EXIT LIGHT COVER AT ROW 1.Dec 18, 2012 · N756US · Airbus A319112 · Emergency LightingSDR USAA2012062900003Power Supply · failed2S CHECK - CABIN AFT EPSU 13WL FAILED ON TEST. REPLACED EPSU 13WL IAW A319 AMM 33-51-38-000-001A, OPS CHECKED GOOD IAW A319 AMM 33-51-00-710-009A.Jun 28, 2012 · N756US · Airbus A319112 · Emergency LightingSDR USAA2012062900002Wire Harness · broken2S CHECK - CABIN EMERGENCY ESCAPE PATH LIGHTING HARNESS BROKEN ON LEFT SEATS AT ROWS 14, 18 & 20. REPLACED HARNESS LEFT SEATS AT ROWS 14, 18 & 20 IAW A319 AMM 33-51-18-400-001-A, OPS CHECKED GOOD IAW AMM 33-51-00-710-009A.Jun 28, 2012 · N756US · Airbus A319112 · Light System WiringSDR USAA2012062800011Epsu · failed2S CHECK - CABIN MID LEFT EPSU 11WL FAILED ON TEST. REPLACED CABIN MID LEFT EPSU 11WL IAW A319 AMM 33-51-38, OPS CHECKED GOOD IAW A319 AMM 33-51-38.Jun 27, 2012 · N756US · Airbus A319112 · Emergency LightingSDR USAA2012062700018Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL ACCESS PANEL 540HB BETWEEN RIB 13 & RIB 14 & BETWEEN S8L & S11L. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540HB IAW A319 SRM-51-74-00 & 51-42-11.Jun 23, 2012 · N756US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012062700017Skin · corroded2S CHECK - CORROSION ON FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41R & S42R. REPAIRED FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41R & S42R IAW EA 134670.Jun 23, 2012 · N756US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012062700016Skin · corroded2S CHECK - CORROSION ON FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L & S42L. REPAIRED FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L & S42L IAW EA 134669.Jun 23, 2012 · N756US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012062500005Slide · low2S CHECK - L2 DOOR SLIDE INFLATION BOTTLE PRESSURE READS ZERO. REPLACED L2 DOOR SLIDE IAW A319 AMM 25-62-44-400-006-A. PERFOMRED OPS TEST IAW A319 AMM 25-62-44-400-006A STEP C1 TO 4 CHECK GOOD.Jun 23, 2012 · N756US · Airbus A319112 · Escape SlideSDR USAA2012062000025Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FUEL ACCESS PANEL 340HB BETWEEN S8R & S9R ALSO BETWEEN RIB 13 & RIB 14. REPLACED FUEL ACCESS PANEL 340HB IAW A319 AMM 20-21-00.Jun 18, 2012 · N756US · Airbus A319112 · Wing, Plate/SkinSDR USAA2012062000015Seat Track · cracked2S CHECK - CRACK ON SEAT TRACK BETWEEN FR47 TO FR51, -Y765. REPLACED SEAT TRACK BETWEEN FR47 TO FR51, -Y765 IAW A319 SRM 51-42-11.Jun 17, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000014Shear Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-42-11.Jun 3, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000013Shear 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 51-42-11.Jun 3, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062700020Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON R2 DOOR SILL BEAM BETWEEN FR66 TO FR68, -Y1782. REPLACED R2 DOOR SILL BEAM BETWEEN FR66 TO FR68, -Y1782 IAW A319 SRM 53-41-14 FIG 101 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062700019Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR16 TO FR18, Y254. REPLACED DUMMY RAIL BETWEEN FR16 TO FR18, Y254 IAW A319 SRM 53-11-14 FIG 107 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012060800013Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR20, Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR20, Y1292 IAW A319 SRM 53-11-15 FIG 104 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000024Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL AT FR16, -Y81. REPLACED DUMMY RAIL AT FR16, -Y81 IAW A319 SRM 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000023Beam · corroded2S CHECK - LEVEL 2 FILIFORM CORROSION ON L2 DOOR SILL BEAM BETWEEN FR66 TO FR68, Y1732. REPLACED L2 DOOR SILL BEAM BETWEEN FR66 TO FR68, Y1732 IAW A319 SRM 53-41-14 FIG 101, 51-42-11 & EA 134663.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000022Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR67 TO FR68, Y765. REPLACED LONGITUDINAL BEAM BETWEEN FR67 TO FR68, Y765 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000021Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR66, Y765. REPLACED LONGITUDINAL BEAM AT FR66, Y765 IAW A319 SRM 53-41-15 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000020Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON L2 DOOR SHAPE SILL BETWEEN FR66 TO FR68, Y1782. REPLACED L2 DOOR SHAPE SILL BETWEEN FR66 TO FR68, Y1782 IAW A319 SRM 53-41-14 FIG 101 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000019Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON R2 DOOR SHAPE SILL AT FR66, -Y1782. REPLACED R2 DOOR SHAPE SILL AT FR66, -Y1782 IAW A319 SRM 53-41-79 FIG 101 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062000018Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR64 TO FR65, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR65, -Y765 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR23, -Y1292. REPLACED SEAT TRACK BETWEEN FR20 TO FR23, -Y1292 IAW A319 SRM 53-11-15, 51-42-11 & 51-75-12.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000016Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y765 IAW A319 SRM 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012060800019Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR68, -Y1292. REPLACED LONGITUDINAL BEAM AT FR68, -Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060800015Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060700005Beam · corrodedS2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGITUDINAL BEAM BETWEEN FR68 TO FR69, Y160. REPLACED LONGITUDINAL BEAM BETWEEN FR68 TO FR69, Y160 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061200022Profile · corroded2S CHECK - LEVEL 2 CORROSION ON PROFILE AT FR66, Y1732. REPLACED PROFILE AT FR66, Y1732 IAW A319 SRM 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061200021Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR18 TO FR20, -Y254. REPLACED SEAT TRACK BETWEEN FR18 TO FR20, -Y254 IAW A319 SRM 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012060800018Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR66, -Y1292. REPLACED LONGITUDINAL BEAM AT FR66, -Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060800017Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR66, Y1292. REPLACED LONGITUDINAL BEAM AT FR66, Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060800016Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR68 TO FR69, Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR68 TO FR69, Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060800014Beam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060700006Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR70, -Y160. REPLACED FLOORBEAM AT FR70, -Y160 IAW A319 SRM 51-74-14 FIG 102, 51-42-11, 51-75-12.Jun 2, 2012 · N756US · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012050400007Lens · missingC11 CHECK - MISSING EMERGENCY EXIT SIGN COVER RIGHT BETWEEN OVERWING EMERGENCY EXIT DOOR SIDEWALL. INSTALLED EMERGENCY EXIT SIGN COVER RIGHT BETWEEN OVERWING EMERGENCY EXIT DOOR SIDEWALL IAW A319 AMM 35-51-16.May 3, 2012 · N756US · Airbus A319112 · Emergency LightingSDR USAA2012042300020Lens · missingAFT RIGHT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED NEW LENS AT AFT RIGHT EMERGENCY EXIT PER AMM 33-51-13-401.Apr 21, 2012 · N756US · Airbus A319112 · Emergency LightingSDR USAA2012040200008Attach Fitting · brokenMECHANIC REPORT - LEFT ELEVATOR OUTBOARD SERVO ACTUATOR ROD END ATTACH FITTING HAS THE ANTI-ROTATION TAB FOR MOUNTING BOLT HEAD MISSING. REPAIRED LEFT ELEVATOR OUTBOARD SERVO ACTUATOR ROD END ATTACH FITTING IAW A319 SRM 55-26-47 PAGE BLOCK 202. 5.A. REPAIR.Mar 31, 2012 · N756US · Airbus A319112 · Elevator Miscellaneous StructureSDR USAA2011111100001Lens · missingLEFT OVERWING WALL MOUNTED EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER AMM 33-51-13. OPS CHECKED GOOD.Nov 9, 2011 · N756US · Airbus A319112 · Emergency LightingSDR USAA2009100192680Disk · wornPIT - EES - L-1 DOOR ASSIST BOTTLE EMPTY. REPLACED DISK IAW A319 AMM 52-10-00-610-001.Oct 1, 2009 · N756US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2009091792562Flashlight · inoperativeFLT 1724 - TPA - DCA - EMERGENCY LIGHTS - EMERGENCY FLASHLIGHT INOPERATIVE UNDER FLIGHT ATTENDANT SEAT FORWARD FACING AFT GALLEY. REMOVED AND REPLACED FLASHLIGHT.Sep 16, 2009 · N756US · Airbus A319112 · Emergency Equipment
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