N816AW

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 = 'N816AW' 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 USAA2012050800009Hinge Fitting · excess play2S CHECK - EXCESS PLAY ON RUDDER HINGE POINT NR 2 AT VERTICLE STAB STA 193, RIB 4. REPLACED HINGE FITTING NR 2 AND FASTENERS AT VERTICLE STAB STA 193, RIB 4 IAW A319 SRM 51-72-11 AND AMM 55-36-41-400-001.Apr 15, 2012 · N816AW · Airbus A319132 · Rudder StructureSDR USAA2012050800008Hinge Fitting · excess play2S CHECK - EXCESS PLAY ON RUDDER HINGE POINT NR 4 AT VERTICLE STAB STA 263, RIB 6. REPLACED HINGE FITTING NR 4 AND FASTENERS AT VERTICLE STAB STA 263, RIB 6 IAW A319 SRM 51-72-11 AND AMM 55-36-41-400-001.Apr 15, 2012 · N816AW · Airbus A319132 · Rudder StructureSDR USAA2012050400004Seat Track · corroded2S CHECK - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46, Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR46, Y765 IAW A319 SRM 51-72-11 AND DRAWING D53371000.Apr 15, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050300007Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.Apr 15, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050300006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57130300.Apr 15, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050100012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Apr 15, 2012 · N816AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012050100009Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 TO FR20, S23R AT R1 DOOR ENTRYWAY. REPLACED CENTER FITTING BETWEEN FR16 TO FR20, S23R IAW A319 SRM 51-72-11.Apr 14, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050100008Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 TO FR20, S23L AT L1 DOOR ENTRYWAY. REPLACED CENTER FITTING BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11.Apr 14, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012051600012Floorbeam · 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.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012051400007Shear Plate · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R, -Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012051400006Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53472815 & EA 500684.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012051400005Coupling · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SPLICE (COUPLING) AT FR66+5 INCHES INBOARD SIDE, Y1292. REPLACED SPLICE (COUPLING) AT FR66+5 INCHES INBOARD SIDE, Y1292 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012051400004Coupling · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON SPLICE (COUPLING) AT FR66+5 INCHES OUTBOARD SIDE, Y1292. REPLACED SPLICE (COUPLING) AT FR66+5 INCHES OUTBOARD SIDE, Y1292 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050900008Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050800016Shear 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 D53474180.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050800015Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23R, -Y1732. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23R, -Y1732 IAW A319 SRM 51-72-11, EA 500647 & AIRBUS DRAWING D53480505.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050800014Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23L. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11 & EA 500648.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050800013Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL COUPLING AT FR66, S23L. REPLACED LOWER SILL COUPLING AT FR66, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474250.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050200012Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050200011Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050200010Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050200009Coupling · damaged2S CHECK - ELONGATED HOLE ON COUPLING AT FR67+16 INCHES, -Y1162. REPLACED COUPLING AT FR67+16 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050200008Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, -Y1162 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100030Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, Y1162. REPLACED COUPLING AT FR67+16 INCHES, Y1162 IAW A319 SRM 53-41-14.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050100029Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, Y1162. REPLACED COUPLING AT FR67+16 INCHES, Y1162 IAW A319 SRM 53-41-14.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050100025Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, Y1162. REPLACED LONGITUDINAL BEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, Y1162 IAW A319 SRM 51-72-11, 53-41-14 & AIRBUS DRAWING D53472780.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100011Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 TO FR66+5 INCHES, Y765. REPLACED SEAT BEAM RAIL BETWEEN FR64 TO FR66+5 INCHES, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050100010Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23L. REPLACED SHAPE SILL BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012050100007Seat 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 & AIRBUS DRAWING D53112812.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050100006Seat Track · worn2S CHECK - SEAT TRACK WORN BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110984.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050100005Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100004Coupling · elongated2S CHECK - ELONGATED HOLE ON FLOORBEAM COUPLING (SPLICE) AT FR64, -Y1292. REPLACED FLOORBEAM COUPLING (SPLICE) AT FR64, -Y1292 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100003Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100002Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050100001Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN -Y1292 TO -Y1162. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN -Y1292 TO -Y1162 IAW A319 SRM 51-72-11.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012042500008Dummy Rail · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY FR12 TO FR16, Y503.2. REPLACED RAIL DUMMY FR12 TO FR16, Y503.2 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112825.Apr 13, 2012 · N816AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012050200004Skin · saturated2S CHECK - 3.07 AREA OF WATER INGRESS SUSPECT ON UPPER SURFACE OF LEFT ELEVATOR AT STA 404, THS RIB 10 APPROX 3.2 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012050100028Skin · saturated2S CHECK - 3.84 AREA OF WATER INGRESS SUSPECT ON UPPER SURFACE OF LEFT ELEVATOR BETWEEN STA 227 TO STA 271 & BETWEEN THS RIB 6 & RIB 7 APPROX 3.2 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012050100027Elevator · saturated2S CHECK - .078 AREA OF WATER INGRESS SUSPECT ON UPPER SURFACE OF LEFT ELEVATOR BETWEEN STA 227 TO STA 271 & BETWEEN THS RIB 6 & RIB 7 APPROX 3.2 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012050100026Skin · saturated2S CHECK - .078 AREA OF WATER INGRESS SUSPECT ON UPPER SURFACE OF LEFT ELEVATOR BETWEEN STA 342 TO STA 404 & BETWEEN THS RIB 9 & RIB 10 APPROX 3.5 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012050100018Skin · saturated2S CHECK - WATER INGRESS SUSPECT ON UPPER SURFACE OF RIGHT ELEVATOR BETWEEN STA 181 TO STA 227 & BETWEEN THS RIB 5 & RIB 6 APPROX 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012050100017Skin · saturated2S CHECK - 3.82 AREA OF WATER INGRESS SUSPECT ON LOWER SURFACE OF LEFT ELEVATOR AT STA 404, THS RIB 10 APPROX 3 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR LOWER SURFACE IAW A319 SRM 55-21-11.Apr 12, 2012 · N816AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2011100700034Battery · dischargedAFT FLIGHT ATTENDANT FLASHLIGHT WILL NOT CHARGE (FLASHING RED LIGHT INDICATOR). REMOVED AND REPLACED AFT FLASHLIGHT BATTERY.Oct 6, 2011 · N816AW · Airbus A319132 · Emergency EquipmentSDR USAA2011060700009Pin · missingFLT 98 - PIT-PHL - EMERGENCY EGRESS SYSTEM - COCKPIT DOOR EMERGENCY EXIT PIT PINS MISSING RINGS. INSTALLED NEW PIT PINS.Jun 6, 2011 · N816AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2011050991809Battery · dischargedFLT 632 - PHX-PIT - EMERGENCY LIGHTS - FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT NOT BLINKING. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.May 8, 2011 · N816AW · Airbus A319132 · Emergency EquipmentSDR USAA2010112292627Battery · dischargedFLT 471 - LAS - EEL - NR 2 FORWARD FLIGHT ATTENDANT FLASHLIGHT INSTALLED IMPROPERLY - BATTERY IS DEAD. MAINTENANCE REPLACED NR 2 FORWARD FLASHLIGHT BATTERY.Nov 20, 2010 · N816AW · Airbus A319132 · Emergency EquipmentSDR USAA2010101192247Battery · dischargedFLT 472 - YEG-PHX - EMERGENCY LIGHTS - FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE IN AFT GALLEY. REMOVED AND REPLACED FLASHLIGHT BATTERY UNDER AFT DIRECT VIEW OF FLIGHT ATTENDANT JUMPSEAT.Oct 10, 2010 · N816AW · Airbus A319132 · Emergency EquipmentSDR USAA2010100492189Power Supply · inoperativeFLT 627 - CMH-PHX - EMERGENCY LIGHTS - EMERGENCY PATH LIGHT ROW 14 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY 13WL & BATTERY - REF AMM CH 33-51-38-400-001. OPERATIONAL CHECK WAS GOOD.Oct 1, 2010 · N816AW · Airbus A319132 · Emergency LightingSDR USAA2010082591780Battery · dischargedFLT 9206 - ABQ-PHX - EMERGENCY LIGHTS - EMERGENCY LIGHT EPSU BATTERY AFT LEFT FAIL. REMOVED AND REPLACED BATTERY FOR AFT EMERGENCY POWER SUPPLY UNIT. PASSED TEST PER AMM 33-51-38 PB401.Aug 24, 2010 · N816AW · Airbus A319132 · Emergency LightingSDR USAA2010080691607Power Supply · inoperativeFLT 34 - PHX-LAX - EMERGENCY LIGHTS - AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT (ESPU) IAW AMM 33-51-38. OPERATIONAL CHECK WAS GOOD.Aug 5, 2010 · N816AW · Airbus A319132 · Emergency Lighting
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