N820AW

Service difficulty reports · 347

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 = 'N820AW' 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 USAA2012090400008Floor Support · corrodedSY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR16, -Y254. REPLACED FLOOR SUPPORT AT FR16, -Y254 IAW A319 SRM 53-11-14, 51-42-11 & AMM 27-41-44-0401.Sep 1, 2012 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012090400007Floor Support · corrodedSY6 CHECK - CORROSION ON FLOOR SUPPORT AT FR70, -Y160. REPLACED FLOOR SUPPORT AT FR70, -Y160 IAW A319 SRM 51-74-00, 51-10-04, 51-42-11, DRAWING 18.Sep 1, 2012 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012070600006Eec · surgesPRIOR TO 1,000 AGL ENGINE 1 SHUT DOWN - ECAM ACTIONS COMPLETED DURING DOWN WIND - POPPING SOUND COMPRESSOR STALL. COMPLIED WITH TROUBLESHOOTING AND ENGINEERING REQUEST. REMOVED AND REPLACED FMU, FUEL PUMP, AND EEC. COMPLIED WITH FUNCTIONAL CHECK OF BLEED VAJul 4, 2012 · N820AW · Airbus A319132 · Fuel Control/Turbine EnginesSDR USAA2012070500023Fmu · surgesPRIOR TO 1,000 AGL ENGINE 1 SHUT DOWN - ECAM ACTIONS COMPLETED DURING DOWN WIND - POPPING SOUND COMPRESSOR STALL. COMPLIED WITH TROUBLESHOOTING AND ENGINEERING REQUEST. REMOVED AND REPLACED FMU, FUEL PUMP, AND EEC. COMPLIED WITH FUNCTIONAL CHECK OF BLEED VAJul 4, 2012 · N820AW · Airbus A319132 · Fuel Controlling SystemSDR USAA2012060400001Cylinder · damagedR2 DOOR CYLINDER DAMPER SHEER PIN STUCK IN HOUSING. REMOVED AND REPLACED R2 DOOR DAMPER CYLINDER IAW AMM 52-13-14-0401. OPS CHECKED GOOD.May 30, 2012 · N820AW · Airbus A319132 · Service DoorsSDR USAA2012042300019Windshield · crackedAT FL 360 FIRST OFFICER FORWARD WINDSHIELD CRACKED. COMPLIED WITH QRH DESCENT TO FL200. DECLARED EMERGENCY. REMOVED AND REPLACED FIRST OFFICER FORWARD WINDSHIELD IAW JOB CARD 26L21056001. OPS CHECKED GOOD.Apr 22, 2012 · N820AW · Airbus A319132 · Flight Compartment WindowsSDR USAA2012021700005Lens · missingR1 DOOR MISSING EMERGENCY EXIT LIGHT LENS COVER. REPLACED R1 DOOR EMERGENCY EXIT LIGHT LENS COVER.Feb 14, 2012 · N820AW · Airbus A319132 · Emergency LightingSDR USAA2011071900012Slide · unsecureSLIDE R1 NOT ARMING PROPERLY. RESECURED AND STOWED SLIDE AT BOTTOM. OPERATIONAL CHECK GOOD.Jul 17, 2011 · N820AW · Airbus A319132 · Escape SlideSDR USAA2011062800032Coffeemaker · malfunctionedDFW-PHX - ELECTRICAL SMELL - NR 1 FORWARD COFFEEMAKER HAS ELECTRICAL SMELL, ALL LIGHTS ON. REMOVED AND REPLACED FORWARD NR 1 COFFEEMAKER. PERFORMED OPERATIONAL CHECK PER AMM 25-35-15. OPERATIONAL CHECK GOOD.Jun 26, 2011 · N820AW · Airbus A319132 · Buffet/GalleysSDR USAA2010112292626Lens · brokenFLT 185 - FLL - EEL - EMERGENCY EXIT SIGN COVER IS BROKEN AT ROW 9 LEFT FORWARD BOTTOM SIDE OF EMERGENCY DOOR. MAINTENANCE REPLACED EMERGENCY EXIT SIGN COVER AT ROW 9 LEFT.Nov 20, 2010 · N820AW · Airbus A319132 · Emergency LightingSDR USAA2010111592604Flashlight · inoperativeFLT 396 - DFW-LAS - EMERGENCY LIGHTS - L2 EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED L2 EMERGENCY FLASHLIGHT.Nov 14, 2010 · N820AW · Airbus A319132 · Emergency EquipmentSDR USAA2009111093081Lens · brokenSAL - BC6 - EEL - BROKEN UPPER "EXIT" LIGHT LENS ON LEFT & RIGHT EMERGENCY EXIT DOORS. REPLACED UPPER "EXIT" LIGHT LENS ON LEFT & RIGHT EMERGENCY EXIT DOORS IAW A319 AMM 33-57-16.Nov 9, 2009 · N820AW · Airbus A319132 · Emergency LightingSDR USAA2009111293088Damper · low pressureSAL - BC6 - EES - LOW PRESSURE DAMPER AT R-1 DOOR. CHARGED DAMPER AT R-1 DOOR & PERFORMED LEAK TEST IAW A319 AMM 52-10-00.Nov 7, 2009 · N820AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2009112393187Support · wornSAL - BC6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY AT INBOARD END OF LEFT INBOARD FLAP AT RIB 1. REPLACED TORSION SUPPORT ASSEMBLY AT INBOARD END OF LEFT INBOARD FLAP AT RIB 1 IAW CMM 57-52-21.Nov 6, 2009 · N820AW · Airbus A319132 · Trailing Edge FlapsSDR USAA2009111293087Damper · low pressureSAL - BC6 - EES - LOW PRESSURE DAMPER AT DOOR 842. CHARGED DAMPER AT DOOR 842 & PERFORMED LEAK TEST IAW A319 AMM 52-10-00.Nov 6, 2009 · N820AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2009112393188Support · wornSAL - BC6 - MAJOR REPAIR - WEAR ON TORSION SUPPORT ASSEMBLY AT INBOARD END OF RIGHT INBOARD FLAP AT RIB 1. REPLACED TORSION SUPPORT ASSEMBLY AT INBOARD END OF RIGHT INBOARD FLAP AT RIB 1 IAW CMM 57-52-21.Oct 21, 2009 · N820AW · Airbus A319132 · Trailing Edge FlapsSDR USAA2009062991622Power Supply · inoperativeFLT 679 - PHX-BOI - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT ON SEAT 1C IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) IN FORWARD GALLEY PER MAINTENANCE MANUAL 33-51-38-401. OPERATIONAL CHECK WAS GOOD.Jun 27, 2009 · N820AW · Airbus A319132 · Emergency LightingSDR USAA2009052991352Connector · brokenLOGPAGE:4501176 - FLT 321 - LAS-ORD - EMERGENCY LIGHTS - FLOOR LEVEL LIGHT AT 20ABC FOR EMERGENCY LIGHT IS INOPERATIVE. FOUND ONE WIRE PULLED FROM WALL CONNECTOR AT SEAT 20ABC. REMOVED AND REPLACED CONNECTOR. OPERATIONAL CHECK WAS GOOD.May 28, 2009 · N820AW · Airbus A319132 · Light System WiringSDR USAA2009051891197Lens · missingLOGPGE:8444354 - FLT 486 - PHX-DEN - EMERGENCY LIGHTS - EMERGENCY EXIT SIGN LENS MISSING OVERHEAD CENTER AISLE ROW 9. REPLACED LENS COVER EMERGENCY EXIT SIGN OVERHEAD CENTER AISLE, ROW 9. OPERATIONAL CHECK WAS GOOD.May 15, 2009 · N820AW · Airbus A319132 · Emergency LightingSDR USAA920081945Connector · disconnectedLOG PAGE 4329007 FLT NR 536 SEA-PHX EMERGENCY LIGHTS AT 18L ARE INOPERATIVE. FOUND BULKHEAD CONNECTOR DISCONNECTED. RECONNECTED CANNON PLUG. OPS CHECK WAS GOOD.Oct 22, 2008 · N820AW · Airbus A319132 · Light System WiringSDR USAA920081394Coffeemaker · defectiveFLT 350 PHX-LAX - BURNING SMELL - COFFEEMAKER WILL NOT BREW. COFFEEMAKER WENT OFF AND THERE WAS A SMELL OF WIRE BURNING. NO SMOKE WAS DETECTED. MAINTENANCE REMOVED AND REPLACED THE COFFEEMAKER. OPERATIONAL CHECK WAS GOOD. (A)Jul 21, 2008 · N820AW · Airbus A319132 · Buffet/GalleysSDR SA08007Epsu · faultedPHX - THE LEFT, MID-CABIN, EMERGENCY POWER SUPPLY UNIT FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED THE LEFT, MID-CABIN, EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK.Mar 6, 2008 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200701051Control Unit · failedPHX - OTH - LOG NR 7809886 - MX REPORTED SMOKE LAV AND CARGO DET FAULT ON ECAM. MX REPLACED THE SDCU, OPERATIONAL CHECK WAS GOOD.Aug 31, 2007 · N820AW · Airbus A319132 · Smoke DetectionSDR AWXA200700279Power Supply · failedATL - EEL - FOUND EMERGENCY POWER SUPPLY UNIT FWD LEFT INOP. MX REMOVED AND REPLACED EPSU AND BATTERY IAW REF AMM 33-51-38-000-001, 33-51-38-400-001 AND 33-51-38-400-2, OPERATIONAL CHECK WAS NORMAL.Feb 25, 2007 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200601719Wire · looseLAX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE AFT ESCAPE PATH LIGHT WAS INOP. MX RESECURED THE WIRE FOR THE AFT EMERGENCY ESCAPE PATH LIGHTS. OPS CHECK WAS GOOD.Oct 7, 2006 · N820AW · Airbus A319132 · Light System WiringSDR AWXA200601262Floor Panel · delaminatedSAL - MAJOR REPAIR - CHECK NR B - 04. NR 5944831. FLOOR PANEL NR 162 EF AFT. CARGO COMPARTMENT WAS FOUND WITH DELAMINATION. FLOOR PANEL NR 162 EF WAS REPLACED IAW IRM 9701 REV 8 SRM 53 - 02 - 00 PAR 8 G,H.Jul 6, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601268Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NR B-04. NR 5944856. THE FLOOR PANEL NR 151 BE ON THE AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 BE IN AFT. CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601260Floorbeam · corrodedSAL - MAJOR REPAIR - CHECK NR BC-4 NO NR. 5945288. CORROSION LOCATED ON FLOORBEAM - Y 765 PASSENGER CABIN FRAME 64 + 10". FLOORBEAM WAS REPLACED IAW SRM A319 51 - 42 - 11 AND 51 - 72 - 11 LOCATED BETWEEN FR 64 TO FR 66 - Y 765 PASSENGER CABIN FLOOR STRUCTURE.Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601198Skin Panel · dentedDENT IN A/C LEFT BEHIND BOARDING DOOR. PERFORMED PERMANENT REPAIR LOCATED FS 23 + 2.5 ", STRINGER 23L IAW SRM A319 53-00-11 PAGE 219 - 220 FIG 204, MEASURED OF DOUBLER L = 9.5 " W = 8. 25 ".Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AWXA200601197Floor Panel · damagedTEMPORARY REPAIR ON FWD CC FLOOR PANEL NR 131 CG. FLOOR PANEL NR 131 CG WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601196Floor Panel · perforatedFLOOR PANEL NR 151 PE WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 PE WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601195Floor Panel · perforatedFLOOR PANEL NR 151 GE OF THE AFT CC WAS FOUND WITH PERFORATION. FLOOR PANEL NR 151 GE OF THE AFT CC WAS REPAIRED IAW SRM 53-02-00 PAR 8C.Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601194Floor Panel · perforatedTHE FLOOR PANEL NR 132 EG OF FWD CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 132 EG OF FWD CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601193Floor Panel · perforatedTHE FLOOR PANEL NR 132 DG IN FWD CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 132 DG IN FWD CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-02-00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601192Floor Panel · perforatedTHE FLOOR PANEL NR 131 BF OF FWD CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 BF OF FWD CC WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601191Floor Panel · debondedTHE FLOOR PANEL NR 151 VG IN AFT CARGO COMPARTMENT WAS FOUND WITH DISBONDED DOUBLER. THE FLOOR PANEL NR 151 VG WAS REPLACED IAW SRM 53 - 02 - 00 PAR 8G, 8H, AND IRM 9701 REV F PROTECTIVE DOUBLER WAS BONDED IAW ER NS 26 - 5326 - 05209 - RC1C PAR 1G AND AWA CARJul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601190Floor Panel · perforatedTHE FLOOR PANEL NR 152 XE IN AFT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 152 XE IN AFT WAS REPAIRED IAW SRM 53-02-00 PAR 8C C21.Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601185Floor Panel · perforatedTHE FLOOR PANEL NR 151 HE OF THE AFT CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 151 WAS REPAIRED IAW SRM 53 - 02 - 00.Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601184Floor Panel · perforatedTHE FLOOR PANEL NR 131 EG IN FWD CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 EG WAS REPAIRED IAW SRM 53 - 02 - 00 PARA 8 C. (2).Jul 5, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601296Floor Panel · corrodedSAL - FOUND CORROSION LOCATED ON FLOOR PANEL NR 261 FF BETWEEN FRAME 66 TO FRAME 68 LEFT SIDE PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261 FF BETWEEN FS 66 TO FS 68 AND INSTALLED WITH AWA CARD CID25318 SEQ 97.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601273Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NO. B-04. NR NO. 5944842. FLOOR PANEL NO. 151 CE WAS FOUND WITH PERFORATION IN AFT. CARGO COMPARTMENT. FLOOR PANEL NO. 151 CE WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601272Plate · lightning strikeSAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5945020. LIGHTNING STRIKE ON BLANKING PLATE OF STATIC PORT EXTERNAL FUSELAGE AT FRAME 4 - 0.5" , Z + 67CM. REWORKED AREA ON BLANKING PLATE OF STATIC PORT, FRAME 4 - 0.5" L/H SIDE IAW ER NO. 25 - 5311 - 06184 - 553 (ZJul 4, 2006 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601271Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NR B-04. NR 5945421. FLOOR PANEL NR 131 DG WAS FOUND WITH PERFORATION IN FWD. CARGO COMPARTMENT. FLOOR PANEL NR 131 WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601269Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NR B-04. NR 5944836. FLOOR PANEL NR 161 CF WAS FOUND WITH PERFORATION IN AFT. CARGO COMPARTMENT. FLOOR PANEL NR 161 CF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601267Floorbeam · corrodedSAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945286. CORROSION LOCATED ON FLOORBEAM - Y 1292 PASSENGER CABIN FR 67 + 17" FRAME 68" , AND FRAME 68 + 2" (3 POINT). REWORKED AREAS FOUND OUT OF LIMITS IAW SRM A319 53 - 00 - 14 FIG 102 PAG 106 AND FLOORBEAM - Y 1292 BETJul 4, 2006 · N820AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601266Floor Panel · delaminatedSAL - MAJOR REPAIR - CHECK NR B-04. NR 5944859. THE FLOOR PANEL NR 152 TG OF THE AFT. CARGO COMPARTMENT WAS FOUND WITH DELAMINATION. THE FLOOR PANEL NR 152 TG WAS REPLACED IAW IRM 9701 REV. F AND SRM 53 - 02 - 00 PAR 8G, 8H.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601265Seat Track · corrodedSAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945123. CORROSION ON FLOORBEAM Y - 1292 FR 20 PASSENGER CABIN. SEAT TRACK LOCATED Y - 1292 BETWEEN FR 12 TO FR 24 REPLACED IAW SRM A319 51 - 72 - 11 SEAT TRACK CORRODED WAS EVALUATED AND FOUND OUT OF LIMITS IAW SRM A319 Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601264Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NR B-04. NR 5944833. THE FLOOR PANEL NR. 161 FF OF AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NR 161 FF AFT. CARGO COMPARTMENT WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C (2).Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601263Floor Panel · corrodedSAL - MAJOR REPAIR- CHECK NR BC-4. NR 5945412. CORROSION LOCATED ON FLOOR PANEL NR 261 FF BETWEEN FRAME 66 TO FRAME 68 LEFT SIDE PASSENGER CABIN. REMOVED AND REPLACED FLOOR PANEL 261 FF BETWEEN FR 66 TO FR 68 AND WAS INSTALLED WITH AWA CARD CID 255318. SEQ 97.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601261Shear Plate · corrodedSAL - MAJOR REPAIR - CHECK NR BC - 4. NR 5945409. CORROSION LOCATED ON PLATE SHEAR PASSENGER CABIN BETWEEN FRAME 69 TO FR 70 STRINGER 23R. SHEAR PLATE LOCATED ON PASSENGER CABIN BETWEEN FR 69 TO FR 70 STRINGER 23R WAS REPLACED AND INSTALLED IAW SRM A 319 51 - Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Internal Mounting Structure
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