N815AW

Service difficulty reports · 211

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 = 'N815AW' 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 USAA2012120400010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 132DG BETWEEN FR28 TO FR34 & BETWEEN -Y765 TO -Y1042.1. REPLACED FLOOR PANEL 132DG IAW A319 SRM 53-02-00, PAR 8H, FIG 209 & IRM 9701 REV G.Nov 18, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 132EG BETWEEN FR28 TO FR34 & BETWEEN -Y1042.1 TO -Y1328. REPLACED FLOOR PANEL 132EG IAW A319 SRM 53-02-00 FIG 209 & IRM 9701 REV G.Nov 18, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012111900008Slide · out of alignment2S CHECK - DURING DVI OF RIGHT OFF WING ESCAPE SLIDE THE ENCLOSURE DOOR (194AT) AND BALL LOCK MECHANISM WAS FOUND NOT FLUSH WITH OUTER SURFACE. REPACKED SLIDE IAW CMM 25-60-58 AND FOLDING PROCEDURE P-11907 REV R. CHECK THAT ENCLOSURE DOOR & BALL LOCK MECHANINov 18, 2012 · N815AW · Airbus A319132 · Escape SlideSDR USAA2012121000006Web · cracked2S CHECK - CRACK FLOOR STRUCTURE WEB BETWEEN FR8 TO FR11, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53113378, D53113386.Nov 16, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000024Web · cracked2S CHECK - CRACK ON WEB BETWEEN FR8 TO FR11, Y765. REPLACED WEB BETWEEN FR8 TO FR11, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53113377.Nov 16, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120500009Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR27, -Y1292. REPAIRED SEAT TRACK AT FR27, -Y1292 IAW A319 SRM 53-21-15, PARA 5.D FIGURE 204 PAGE 239/240.Nov 15, 2012 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012113000015Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR26, Y1765. REPAIRED SEAT TRACK BETWEEN FR24 TO FR26, Y1765 IAW A319 SRM 53-21-15 FIG 204 PAGE 239/240.Nov 15, 2012 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012113000020Sill · cracked2S CHECK - CRACK ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 151BE BETWEEN FR53 TO FR55A & BETWEEN Y1043.1 TO Y1328. REPLACED FLOOR PANEL 151BE IAW A319 SRM 53-02-00 FIG 209 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000013Floor 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 FIG 209 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO -Y254. REPLACED FLOOR PANEL 231BF IAW A319 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000009Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231EF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 231EF IAW A319 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000008Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 22EF BETWEEN FR16 TO FR20 & BETWEEN -Y254 TO -Y1292. REPLACED FLOOR PANEL 222EF IAW A319 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012113000007Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL 221EF IAW A319 SRM 53-12-00 FIG 206 & IRM 9701 REV G.Nov 14, 2012 · N815AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012121200002Shear 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 51-72-11, TYPICAL REPAIR TR320-2528-10-0011E & AIRBUS DRAWING D53474180.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012121200001Shear Plate · corroded2S CHECK - LEVEL 2 INTERGRANULAR 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.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120600011Hinge · excess playQ3 CHECK - EXCESSIVE PLAY ON RUDDER HINGE NR 5. REMOVED AND REPLACED RUDDER HINGE NR 5 IAW A319 SRM 51-72-11.Nov 13, 2012 · N815AW · Airbus A319132 · Rudder StructureSDR USAA2012120500008Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR16, Y765. REPLACED SEAT TRACK AT FR16, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812 & D53110920.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012113000023Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT R2 DOOR ENTRYWAY BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SILL AT R2 DOOR ENTRYWAY BETWEEN FR66 TO FR68, S23R IAW A319 SRM 51-72-11 & EA 503575.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000022Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT L1 DOOR ENTRYWAY BETWEEN FR16 TO FR20, S23L. REPLACED LOWER SILL AT L1 DOOR ENTRYWAY BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53110339.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000021Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT L2 DOOR ENTRYWAY AT FR66+5 INCHES, S23L. REPLACED LOWER SILL AT L2 DOOR ENTRYWAY AT FR66+5 INCHES, S23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503581.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000019Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT L2 DOOR ENTRYWAY AT FR68, S23L. REPLACED CORNER FITTING AT L2 DOOR ENTRYWAY AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012113000018Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT R2 DOOR ENTRYWAY AT FR68, S23R. REPLACED CORNER FITTING AT R2 DOOR ENTRYWAY AT FR68, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Nov 13, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012121000007Floorbeam · cracked2S CHECK - CRACK FLOORBEAM AT FR8 BETWEEN -Y254 & -Y765. REPLACED FLOORBEAM AT FR8 BETWEEN -Y254 & -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53113223.Nov 12, 2012 · N815AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012050700003Apu · malfunctionedACRID CABIN ODOR THROUGHOUT AIRCRAFT MOST NOTICABLE DURING APPROACH. REMOVED AND REPLACED APU. COMPLIED WITH ENVIRONMENTAL CONTROL SYSTEM PER 26L00021004. NO ODORS NOTED. SUP WILL SUBMIT ROOT CAUSE INFORMATION UPON RECEIPT OF TEAR DOWN REPORT FROM HONEYWELMay 4, 2012 · N815AW · Airbus A319132 · APU Core EngineSDR USAA2012022700026Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y1160. REPLACED FLOORBEAM AT FR68, Y1160 IAW A319 SRM 51-42-11.Feb 25, 2012 · N815AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012022700025Floorbeam · corrodedC11 CHECK - CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-42-11 & 51-42-00.Feb 23, 2012 · N815AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012022700024Floor Support · corrodedC11 CHECK - CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR16, Z-500, Y503.2. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR16, Z-500, Y503.2 IAW A319 SRM 51-42-11 & 51-42-00.Feb 23, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012022700023Floor Support · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR65 TO FR69, Y1252. REPLACED FLOOR SUPPORT BETWEEN FR65 TO FR69, Y1252 IAW A319 SRM 51-42-11.Feb 23, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012022700022Sill · corrodedC11 CHECK - LEVEL 2 CORROSION ON AFT RIGHT DOOR SILL BETWEEN FR67 TO FR68, S23R, -Y1732. REPAIRED AFT RIGHT DOOR SILL BETWEEN FR67 TO FR68, S23R, -Y1732 IAW SRM 53-41-14 FIG 201 LETTER "K" PAGE 213-24.Feb 23, 2012 · N815AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2011102800020Power Supply · inoperativeEMERGENCY POWER SUPPLY UNIT 11WL FAULT FAILURE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 11WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-002 AND 33-51-38-400-002. OPS CHECKED GOOD.Oct 27, 2011 · N815AW · Airbus A319132 · Emergency LightingSDR USAA2011083000005Brake Assy · overtempJUST PRIOR TO ROTATION, THE AIRCRAFT VEERED LEFT. AIRCRAFT RETURNED TO FIELD. AFTER LANDING BRAKE NR 1 REACHED 390 DEGREES WHILE BRAKE NR 2 ONLY REACHED 190 DEGREES. REMOVED AND REPLACED NR 1 MAIN LANDING GEAR BRAKE PER AIRBUS MAINTENANCE MANUAL 32-42-27-00Aug 28, 2011 · N815AW · Airbus A319132 · BrakeSDR USAA2011081500015Seat Belt · out of positionL2 EMERGENCY SLIDE ARM STICKS HALFWAY RESULTING IN DOOR NOT ARMED. FOUND FLIGHT ATTEDANT SEAT BELT INTERFERRING WITH GIRT BAR. STOWED BELT. L2 DOOR SLIDE ARM/DISARM CHECKS GOOD.Aug 12, 2011 · N815AW · Airbus A319132 · Passenger Compartment EquipmentSDR USAA2011020490519Lens · missingFLT 395 - LAS-DFW - EMERGENCY LIGHTS - EMERGENCY EXIT ROW LENS COVER MISSING 8C. REPLACED EMERGENCY EXIT LENS COVER AT SEAT 8C.Jan 31, 2011 · N815AW · Airbus A319132 · Emergency LightingSDR USAA2010052591032Pin · wornMCN - TRIPLE GEAR CHANGE - MAJOR REPAIR - RIGHT MAIN LANDING GEAR AFT PINTLE PIN WORN. REPLACED RIGHT MAIN LANDING GEAR AFT PINTLE PIN.May 20, 2010 · N815AW · Airbus A319132 · Main Landing Gear Attach SectionSDR USAA2010031990613Oven · dirtyFLT 526 - PHX - SMOKE - NR 1 OVEN CAUSED SMOKE FROM BURNT DEBRIS IN BOTTOM OF OVEN AND CAUSED FORWARD LAV SMOKE DETECTOR EMERGENCY ECAM DURING CRUISE. FOUND BURNT DEBRIS ON NR 1 OVEN INSERT. REMOVED INSERT AND RAN THROUGH HEATING CYCLE. NO SMOKE NOTED.Mar 18, 2010 · N815AW · Airbus A319132 · Buffet/GalleysSDR USAA2009100792729Lens · missingFLT 456 - PHX-SLC - EMERGENCY LIGHTS - LAV D EMERGENCY LIGHT LENS MISSING. INSTALLED NEW EMERGENCY LIGHT LENS AT LAV D.Oct 5, 2009 · N815AW · Airbus A319132 · Emergency LightingSDR USAA2009071391802Safety Wire · brokenPIT - BC6 - EES - REMOVED SLIDE AND FOUND COVER RELEASE SAFETY WIRE BROKEN, REPLACE SLIDE. REPLACED SLIDE IAW US AIRWAYS TASK CARD 26C83252002.Jun 30, 2009 · N815AW · Airbus A319132 · Escape SlideSDR USAA2009042891005Lens · missingFLT 537 - BWI-LAS - EMERGENCY LIGHTS - EMERGENCY PATH LIGHT AT SEAT 3C HAS LENS COVER MISSING. REPLACED MISSING LENS COVER.Apr 27, 2009 · N815AW · Airbus A319132 · Emergency LightingSDR USAA2009011490073Wire Harness · shortedLOGPAGE:8317680 - FLT NR 34 - LAX-PHX - EMERGENCY LIGHTS AT SEATS ROW 14,18,22, DO NOT WORK. ALSO EMERGENCY EXIT LIGHTS AT DOORS 2R, 2L. FOUND WIRES UNDER SEAT ROWS 18 AND 22 SHORTED. R&R EMERGENCY POWER SUPPLY UNIT 13WL AND HARNESSES AT ROWS 18 + 22 - REF Jan 13, 2009 · N815AW · Airbus A319132 · Light System WiringSDR USAA2009011490071Power Supply · dischargedLOGPAGE:8317680 - FLT NR 34 - LAX-PHX - EMERGENCY LIGHTS AT SEATS ROW 14,18,22, DO NOT WORK. ALSO EMERGENCY EXIT LIGHTS AT DOORS 2R, 2L. FOUND WIRES UNDER SEAT ROWS 18 AND 22 SHORTED. R&R EMERGENCY POWER SUPPLY UNIT 13WL AND HARNESSES AT ROWS 18 + 22 - REF Jan 13, 2009 · N815AW · Airbus A319132 · Emergency LightingSDR USAA2009010690038Power Supply · faultyLOGPAGE 4301273 P09 CHK EMERGENCY LIGHT AFT CABIN EMERGENCY POWER SUPPLY KEEPS GIVING UNIT FAULT. R&R AFT CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECK WAS GOOD.Jan 5, 2009 · N815AW · Airbus A319132 · Emergency LightingSDR AWXA200700020Eec · out of toleranceFLIGHT 237: DTW - PHX - THE A/C HAD JUST REACHED CRUISE ALTITUDE WHEN THE CREW NOTICED THE NR 1 ENGINE HAD RETARDED TO FLIGHT IDLE FOLLOWED BY AN ENGINE FLAMEOUT/SHUT DOWN. THE CREW ATTEMPTED AN IN-FLIGHT RESTART, THE IN-FLIGHT RESTART WAS NOT SUCCESSFUL. THJan 1, 2007 · N815AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200601696Power Supply · inoperativePHX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE CABIN EMERGENCY LIGHTS TEST FAILED SYSTEM TEST. EPSU 10WL FAILED TEST. MAINTENANCE REPLACED EPSU IAW AMM 33-51-38-000. OPS CHECK WAS GOOD.Oct 2, 2006 · N815AW · Airbus A319132 · Emergency LightingSDR AWXA200601141Indicator · inoperativeAIR TURNBACK - FLT 454 - CREW REPORTED LEFT FUEL QUANTITY INNER AND OUTER WENT TO DEGRADED MODE, THEN QUANTITY DROPPED APPROX 3000 LBS UNDER INNER FROM 7500 TO 4800. DROPPED 800 LBS ON OUTER FROM 1500 TO 700. INDICATIONS LATER RETURNED TO NORMAL. FUEL QUANTJul 4, 2006 · N815AW · Airbus A319132 · Fuel Quantity IndicatorSDR AWXA200600587Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION, LEVEL 2 GALVANIC, ON SEAT TRACK, 3 POINT, LOCATED AT BS 43 +13, 44 +7, 46 +13 LT INBD Y765L. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15. REMOVED AND INSTALLED NEW SEAT TRACK FROMar 28, 2006 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600541Seat Track · corrodedDURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE R/H OUTBOARD SEAT TRACK, 5 POINTS, AT FR 41+10", FR 42+16", FR 44+7", FR 45+4" AND FR 45+16" AT Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 PAGE 107 FIG 103. MAINTEMar 26, 2006 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600539Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK AT 3 POINTS LOCATED AT FS 38+1"; FS 38+4" AND FS 40+1" AT Y1292. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS IAW AIRBUS 319 SRM 53-31-15 PAGE 107 FIGURE 103. MAINTENANCE REMOVED AND REMar 25, 2006 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600538Seat Track · corrodedSAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK AT 6 POINTS LOCATED AT FS 41+10"; FS 42+17"; FS 43+15"; FS 44+7"; FS 45+17"; AND FS 46+14" AT Y1292. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS IAW AIRBUS 319 SRM 53-31-15 PAGE 107 FIGMar 25, 2006 · N815AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600535Floorbeam · corrodedSAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION AROUND TWO FASTENERS HOLES LOCATED AT Y-1292 FR67+17"AND FR68. CORROSION WAS FOUND OUT OF LIMITS AND BEAM WAS REPLACED FROM FR 67+15" TO FR 69+4" IAW AIRBUS 319 SRM 51-72-11 AND 51Mar 24, 2006 · N815AW · Airbus A319132 · Fuselage Main, Floor Beam
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