N669AW

Service difficulty reports · 185

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 = 'N669AW' 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 USAA2014072800013Cylinder · low pressureR2 DOOR ASSIST LOW PRESS INDICATION. SERVICED R2 DOOR ASSIST TO PROPER PRESS.Jul 25, 2014 · N669AW · Airbus A320232 · Service DoorsSDR USAA2014051900022Wire Harness · damagedSEAT MOUNTED EMERGENCY EXIT LIGHT AT 24C HAS DAMAGED WIRE HARNESS. REPLACED EMERGENCY EXIT LIGHT WIRE HARNESS AT SEAT 24C.May 18, 2014 · N669AW · Airbus A320232 · Light System WiringSDR USAA2014051900021Wire Harness · unsecureLIGHTING HARNESS WIRING NEEDS TO BE SECURED TO SEAT RAIL AT 26C. REPLACED SEAT PORTION OF EMERGENCY EXIT LIGHT WIRING HARNESS SEAT 26C.May 17, 2014 · N669AW · Airbus A320232 · Light System WiringSDR USAA2014032500008Bottle · low pressureDOOR R2 ASSIST BOTTLE PRESS IS LOW. SERVICED DOOR R2 ASSIST BOTTLE IAW AMM 52-10-00-0301.Mar 24, 2014 · N669AW · Airbus A320232 · Service DoorsSDR USAA2014012900005Seat Track · corrodedC11 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON RT SEAT TRACK BETWEEN FRAME 57 TO FRAME 64, SRM 53-41-15-201, FIG 202.Jan 28, 2014 · N669AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2014012800010Floor Panel · delaminatedC11 SYS 6 CHECK DELAMINATION ON FLOOR PANEL 221PF BETWEEN FRAME 12 TO FRAME 24, Z 500 & BETWEEN Y 520 TO Y 765. REPLACED FLOOR PANEL 221PF IAW IRM 9701, REV G.Jan 28, 2014 · N669AW · Airbus A320232 · Fuselage Floor PanelSDR USAA2014012700036Shear Web · crackedC11 SYS 6 CHECK CRACK ON AFT CABIN FLOOR STRUCTURE SHEAR WEB BETWEEN FRAME 68 TO FRAME 69, Z 500 & Y 1300. REPLACED AFT CABIN FLOOR STRUCTURE SHEAR WEB BETWEEN FRAME 68 TO FRAME 69, Z 500 & Y 1300 IAW SRM 51-42-11.Jan 26, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700030Plate · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR CTR SHAPE SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589. REPLACED L2 DOOR CTR SHAPE SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589 IAW SRM 51-44-11 & DWG D53480505.Jan 26, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700028Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500 & Y 1292. REPLACED FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500 & Y 1292 IAW SRM 51-42-11.Jan 25, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012700023Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FRAME 16, Z 500, Y 503. REPLACED FLOOR BEAM AT FRAME 16, Z 500, Y 503 IAW A320 SRM 51-72-11.Jan 19, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014020700017Fitting · corrodedC1 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR LOWER FWD CORNER SILL PLATE SHAPE FITTING AT FRAME 66, Z 500, Y 1589. REPLACED R2 DOOR LOWER FWD CORNER SILL PLATE SHAPE FITTING AT FRAME 66, Z 500, Y 1589 IAW SRM 51-72-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014013000004Floorbeam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FRAME 66, Z 500 & Y 1292. REPLACED FLOOR BEAM AT FRAME 66, Z 500 & Y 1292 IAW SRM 51-72-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014013000003Seat Track · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FRAME 63, Z 500 & Y 765. REPAIRED SEAT TRACK AT FRAME 63, Z 500 & Y 765 IAW SRM 53-00-15 & EA 206739.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2014012900008Floorbeam · corrodedC11 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON Z FLOOR BEAM BETWEEN FRAME 66 TO FRAME 68, Z 500 & BETWEEN Y 1292 TO Y 1162.5. REPLACED Z FLOOR BEAM BETWEEN FRAME 66 TO FRAME 68, Z 500 & BETWEEN Y 1292 TO Y 1162.5 IAW SRM 51-72-11 & 51-42-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012900007Floorbeam · corrodedC11 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FRAME 68, Z 500 & Y 1162. REPLACED FLOOR BEAM AT FRAME 68, Z 500 & Y 1162 IAW SRM 51-21-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012900006Seat Track · corrodedC11 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FRAME 63, Z 500 & Y 1292. REPLACED SEAT TRACK AT FRAME 63, Z 500 & Y 1292 IAW SRM 53-41-15.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2014012900004Shear Web · corrodedC11 SYS 6 LEVEL 2 EXFOLIATION CORROSION ON RT AFT SHEAR WEB BETWEEN FRAME 69 TO FRAME 70, Z 500, & Y 1160. REPLACED RT AFT SHEAR WEB BETWEEN FRAME 69 TO FRAME 70, Z 500 & Y 1160 IAW EA 206715.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012800009Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 68 TO FRAME 70, Z 500 & Y 160.5. REPLACED FLOOR BEAM BETWEEN FRAME 68 TO FRAME 70, Z 500 & Y 160.5 IAW SRM 51-72-11 & DWG D53472780.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012800008Floorbeam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 68 TO FRAME 70, Z 500 & Y 160.5. REPLACED FLOOR BEAM BETWEEN FRAME 68 TO FRAME 70, Z 500 & Y 160.5 IAW SRM 51-72-11 & DWG D53472780.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012800007Sill · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589. REPLACED R2 DOOR SILL BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589 IAW SRM 51-72-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700040Beam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOOR STRUCTURE Z BEAM FWD SECTION BETWEEN FRAME 66 TO FRAME 69, Z 500 & Y 1162.5. REPLACED AFT CABIN FLOOR STRUCTURE Z BEAM FWD SECTION BETWEEN FRAME 66 TO FRAME 69, Z-500 & Y 1162.5 IAW SRM 51-40-00 Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700039Beam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOOR STRUCTURE Z BEAM CTR SECTION BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1292. REPLACED AFT CABIN FLOOR STRUCTURE Z BEAM CTR SECTION BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1292 IAW SRM 51-72-11, 51Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700038Beam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOOR STRUCTURE Z BEAM BETWEEN FRAME 64 TO FRAME 66, Z 500 & Y 1292. REPLACED AFT CABIN FLOOR STRUCTURE Z BEAM BETWEEN FRAME 64 TO FRAME 66, Z 500 & Y 1292 IAW SRM 53-11-14, 51-42-11 & 51-72-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700037Shear Web · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON AFT CABIN FLOOR STRUCTURE SHEAR WEB BETWEEN FRAME 69 TO FRAME 70, Z 500 & Y 1350. REPLACED AFT CABIN FLOOR STRUCTURE SHEAR WEB BETWEEN FRAME 69 TO FRAME 70, Z 500 & Y 1350 IAW SRM 51-42-00.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700031Plate · corrodedC11 SYA6 CHECK LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589. REPLACED L2 DOOR SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z 500 & Y 1589 IAW SRM 51-72-11, DWG D53480505 & D53474250.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700029Fitting · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR LOWER AFT CORNER SHAPE FITTING AT FRAME 68, Z 500. REPLACED L2 DOOR LOWER AFT CORNER SHAPE FITTING AT FRAME 68, Z 500 IAW A320 SRM 51-74-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012700027Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500 & Y 765. REPLACED FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500 & Y 765 IAW SRM 51-42-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012700026Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500, & Y 254. REPLACED FLOOR BEAM BETWEEN FRAME 16 TO FRAME 20, Z 500 & Y 254 IAW SRM 53-11-14.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012700025Floorbeam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 66 TO FRAME 70, Z 500, Y 765. REPLACED FLOOR BEAM BETWEEN FRAME 66 TO FRAME 70, Z 500, Y 765 IAW SRM 53-11-14.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012700024Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FRAME 24, Z 500, Y 1584. REPLACED FLOOR BEAM AT FRAME 24, Z 500, Y 1584 IAW A320 SRM 53-11-14.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012700018Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FWD SECTION OF FLOOR BEAM AT FRAME 66, Z 500, Y 765. REPLACED SECTION OF FLOOR BEAM AT FRAME 66, Z 500, Y 765 IAW A320 SRM 51-42-11 & DWG D53472816.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012400013Fitting · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR WAY LOWER FWD SHAPE FITTING AT FRAME 68, Z 500. REPLACED L2 DOOR WAY LOWER FWD SHAPE FITTING AT FRAME 68, Z 500 IAW SRM 51-74-00.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012400007Floorbeam · corrodedC11 SYS6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FRAME 12 TO FRAME 24, Z 500, Y 254. REPLACED FLOOR BEAM BETWEEN FRAME 12 TO FRAME 24, Z 500, Y 254 IAW SRM 51-42-11 & DWG D53110920.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012300006Sill · corrodedSYS6 C11 CHECK LEVEL 2 EXFOLIATION CORROSION IN GIRT BAR SILL PLATE FASTENER HOLES BETWEEN FRAME 16 TO FRAME 20, Z 500, Y 1584. REPAIRED GIRT BAR SILL PLATE FASTENER HOLES BETWEEN FRAME 16 TO FRAME 20, Z 500, Y 1584 IAW SRM 53-11-14.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR USAA2014012300005Floorbeam · corrodedSYS6 C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FRAME 66, Z 500, Y 512.5. REPLACED FLOOR BEAM AT FRAME 66, Z 500, Y512.5 IAW SRM 51-42-11.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2014012200010Floorbeam · corrodedC11 SYS 6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT Z 500, Y 765. REPLACED FLOOR BEAM AT Z500, Y 765 IAW SRM 51-74-00.Jan 17, 2014 · N669AW · Airbus A320232 · Fuselage Main, Floor BeamSDR USAA2013091600014Skin · chafedRIGHT WING FIXED LEADING EDGE SKIN CHAFED AT NR 1 SLAT TRACK CUTOUT. REPAIRED SKIN IAW US AIRWAYS EA 205674.Sep 13, 2013 · N669AW · Airbus A320232 · Wing, Plate/SkinSDR USAA2013080800017Computer · malfunctionedDURING CRUISE, RECEIVED AN ECAM MESSAGE FROM SMOKE IN LAVATORY AND ASSOC CONTINUOUS REPETATIVE CHIME. F/A NOTED THE SOURCE WAS LAV E AND DID A VISUAL INSPECTION. NOTHING WAS NOTED. MESSAGE LASTED ONLY A FEW SECONDS AND RETURNED TO NORMAL. REPLACED SMOKE DEAug 7, 2013 · N669AW · Airbus A320232 · Smoke DetectionSDR USAA2013050200014Lens · missingLENS MISSING ON SEAT 9LT EMERGENCY LIGHT. EMERGENCY LIGHT LENS INSTALLED ON SEAT 9LT.May 1, 2013 · N669AW · Airbus A320232 · Emergency LightingSDR USAA2013021900005Fire Bottle · low pressureAFT HALON FIRE EXTINGUISHER IS IN THE RED MARKS. REPLACED AFT HALON FIRE EXTINGUISHER.Feb 18, 2013 · N669AW · Airbus A320232 · Fire Bottle, PortableSDR USAA2013020100013Coffeemaker · defectiveCOFFEEMAKER MADE AN ARCING SOUND WITH A BURNT ELECTRICAL SMELL. SMELL DISSIPATED AFTER TURNING OFF COFFEEMAKER. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD GALLEY COFFEEMAKERS.Jan 31, 2013 · N669AW · Airbus A320232 · Buffet/GalleysSDR USAA2013010300002Seat Track · corrodedMECHANIC REPORT - CORROSION ON SEAT TRACK AT FR58, S23R, -Y1292. REPAIRED SEAT TRACK AT FR58, S23R, -Y1292 IAW A320 SRM 53-00-15 FIG 201.Jan 2, 2013 · N669AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013010300001Seat Track · corrodedMECHANIC REPORT - CORROSION ON SEAT TRACK AT FR57, S23L, Y1292. REPAIRED SEAT TRACK AT FR57, S23L, Y1292 IAW A320 SRM 53-00-15 FIG 201.Dec 31, 2012 · N669AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012111300013Fire Bottle · low pressureFLIGHT ATTENDANT REPORTED THE AFT HALON FIRE EXTINGUISHER PRESSURE IS IN THE RED. REPLACED AFT HALON FIRE EXTINGUISHER.Nov 11, 2012 · N669AW · Airbus A320232 · Fire Bottle, PortableSDR USAA2012103000012Cylinder · low pressureR2 DOOR EMERGENCY CYLINDER ACCUMULATOR IS LOW. SERVICED R2 DOOR EMERGENCY ACCUMULATOR PER AMM 52-10-00-614-001.Oct 27, 2012 · N669AW · Airbus A320232 · Service DoorsSDR USAA2012081600015Fire Bottle · low pressureFORWARD LAV FIRE EXTINGUISHER NOT IN GREEN BAND. REMOVED AND REPLACED FORWARD LAV FIRE EXTINGUISHER IAW AIRBUS MAINTENANCE MANUAL 26-25-41.Aug 15, 2012 · N669AW · Airbus A320232 · Fire Bottle, FixedSDR USAA2012073000043Battery · dischargedAFT LEFT FLASHLIGHT DOES NOT WORK. REPLACED BATTERY IN AFT LEFT FLASHLIGHT.Jul 27, 2012 · N669AW · Airbus A320232 · Emergency EquipmentSDR USAA2012052400016Power Supply · inoperativeEMERGENCY LIGHTS ON AISLE SIDE OF SEATS 22A & 26A INOPERATIVE. REMOVED AND REPLACED LEFT AFT EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-400-001.May 23, 2012 · N669AW · Airbus A320232 · Emergency LightingSDR USAA2012041700009Wire · strippedFOUND EMERGENCY LIGHT MOUNTED ON SEAT 9ABC WIRE STRIPPED. RE-TERMINATED EMERGENCY LIGHTS AT SEAT 9ABC.Apr 16, 2012 · N669AW · Airbus A320232 · Light System WiringSDR USAA2012041300006Proximity Sensor · faultyCREW REPORTED ENGINE 2 REVERSER FAULT ON LANDING WHEN THRUST REVERSERS WERE SELECTED ON. DEACTIVATED NR 2 THRUST REVERSER AND PLACED ON MEL. REPEATED FAULTS2. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE EEC (ELECTRONIC ENGINE CONTROL) AND NR 2 T/R LOCK PROXApr 9, 2012 · N669AW · Airbus A320232 · Engine Thrust Reverser
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