N825AW

Service difficulty reports · 224

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 = 'N825AW' 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 USAA2014041400024Lens · missing10C EXIT LIGHT RED BEZEL MISSING. REPLACED EMERGENCY EXIT LIGHT LENS AT SEAT ROW 10C.Apr 13, 2014 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2014030300018Mechanism · obstructedCANNOT ARM L1 DOOR. HANDLE SEEMS JAMMED. REMOVED DEBRIS FROM ARMING MECHANISM, OPERATIONS GOOD.Feb 28, 2014 · N825AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2013100300002Angle · cracked2S CHECK, CRACK IN SEGMENT ANGLE OF LT OVERWING EMERGENCY EXIT DOOR NR 834 BETWEEN FRAMES 40 TO 41, S17L. REPLACED SEGMENT ANGLE OF LT OVERWING EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41, S17L IAW EO 5210Y228.Oct 2, 2013 · N825AW · Airbus A319132 · Emergency ExitsSDR USAA2013093000035Floor Panel · delaminated2S CHECK, DELAMINATION TO FLOOR PANEL 231CF BETWEEN FRAMES 20 TO 24, Z-500 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000033Floor Panel · delaminated2S CHECK, UPPER SURFACE DELAMINATION TO FLOOR PANEL 221DF BETWEEN FRAMES 16 TO 20, Z-500 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000032Floor Panel · delaminated2S CHECK, UPPER SURFACE DELAMINATION TO FLOOR PANEL 221EF BETWEEN FRAMES 16 TO 20, Z-500 & BETWEEN Y765 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000031Floor Panel · delaminated2S CHECK, UPPER SURFACE DELAMINATION TO FLOOR PANEL 232DF BETWEEN FRAMES 20 TO 24, Z-500 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000030Floor Panel · delaminated2S CHECK, UPPER SURFACE DELAMINATION TO FLOOR PANEL 222CF BETWEEN FRAMES 12 TO 16, Z-500 & BETWEEN -Y1584 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000029Floor Panel · damaged2S CHECK, SURFACE DAMAGE TO FLOOR PANEL 222EF BETWEEN FRAMES 18 TO 20, Z-500 & BETWEEN -Y1292 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 27, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013093000034Floor Panel · delaminated2S CHECK, DELAMINATION TO FLOOR PANEL 231BF BETWEEN FRAMES 23 TO 24, Z-500 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Sep 19, 2013 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013080700007Lens · wrong partSEAT ROW 8ABC EMERGENCY EXIT LIGHT LENS COVER CLEAR AS OPPOSED TO RED & CLEAR. REPLACED EMERGENCY FLOOR LIGHT LENS COVER AT ROW 10 RT.Aug 6, 2013 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2013070200007Reservoir · low pressureMX FOUND PRESSURE LOW ON RT OVERWING EMERGENCY EXIT HATCH INFLATION RESERVOIR. MX R & R RT OVERWING ESCAPE SLIDE INFLATION RESERVOIR IAW AMM 25-62-46. OPS CHECK NORMAL.Jul 1, 2013 · N825AW · Airbus A319132 · Emergency ExitsSDR USAA2013061300014Lens · missingCREW REPORTED THE LENS MISSING FROM EMERGENCY EXIT LIGHT ON LOWER WALL PANEL OF LEFT AFT LAV. MX INSTALLED LENS. EMERGENCY LIGHTS CHECK NORMAL IAW AMM 33-51-00-701-001-A. NO DEFECTS NOTED AT THIS TIME.Jun 12, 2013 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2013061000004Apu · contaminatedF/A'S REPORTED A "DIRTY SOCK" SMELL DURING DESCENT AND ON GROUND WITH APU AND PACKS RUNNING. ALSO REPORTED HEADACHES AND TIGHTNESS OF CHEST. STARTED AT TOP OF DESCENT AFTER POWER RETARDED WHILE IN MANAGED MODE. MX ACCOMPLISHED JOB CARDS 26L00021001 AND 26L00Jun 7, 2013 · N825AW · Airbus A319132 · APU Core EngineSDR USAA2013060600004Cylinder · low pressureMX REPORTED THE L1 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. MX SERVICED L1 DOOR EMERGENCY ACCUMULATOR TO 1,850 PSI AT 37 DEG. C. REF AMM 52-10-00-614-001.Jun 6, 2013 · N825AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2013030700020Cover · missingMAINTENANCE REPORTED THE EMERGENCY LIGHT LENS COVER MISSING AT 3L. MAINTENANCE REPLACED EMERGENCY LIGHT LENS COVER AT 3L.Mar 6, 2013 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2013021300002Oven · malfunctionedCREW REPORTS NR 1 OVEN UNUSABLE. SMOKE DURING WARM-UP. MISSING INSERT. MAINTENANCE REMOVED AND REPLACED NR 1 OVEN.Feb 12, 2013 · N825AW · Airbus A319132 · Buffet/GalleysSDR USAA2013012200023Lens · missingCREW REPORTED THE CLEAR LENS FROM EMERGENCY EXIT LIGHTS MISSING AT SEAT 6C. MAINTENANCE INSTALLED CLEAR LENS ON EMERGENCY EXIT LIGHT AT SEAT 6C.Jan 21, 2013 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2012121200004Slide · low pressureMAINTENANCE REPORTED THE L2 DOOR SLIDE HAS LOW PRESSURE. MAINTENANCE REPLACED L2 DOOR SLIDE PER J/C 26L00025010.Dec 11, 2012 · N825AW · Airbus A319132 · Escape SlideSDR USAA2012121200003Fitting · out of adjustCREW REPORTED THE 2L DOOR DOES NOT SHOW SLIDE ARMED IN FLIGHT. CABIN PRESSURE INDICATION ON 2L DOOR BLINKING RED CONTINUIOUSLY. THE "B" F/A REPORTS THAT ARMED LEVER WAS OUT OF ARMED POSITION APPROXIMATELY 3/4 - 1 INCH AND CANNOT BE RE-ENGAGED. MAINTENANCE ADec 10, 2012 · N825AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2012121000001Cover Plate · missingSY6 CHECK - AFT CABIN FLOOR PANEL COVER PLATE IS MISSING BETWEEN FR66 TO FR68 & BETWEEN Y765 TO Y1292. INSTALLED COVER PLATE ON FLOOR PANEL IAW EA 504541.Dec 8, 2012 · N825AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012121000004Skin · saturatedSY6 CHECK - TRAPPED WATER INDICATION ON RIGHT ELEVATOR UPPER SURFACE AT RIB 3, 7 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE AT RIB 3 IAW A319 SRM 55-21-11, PAR. 5-E & AMM 51-75-12.Dec 7, 2012 · N825AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012121000003Skin · saturatedSY6 CHECK - TRAPPED WATER INDICATION ON RIGHT ELEVATOR UPPER SURFACE AT RIB 9, 5 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE AT RIB 9 IAW A319 SRM 55-21-11, PAR. 5-E & AMM 51-75-12.Dec 7, 2012 · N825AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012121000002Skin · saturatedSY6 CHECK - TRAPPED WATER INDICATION ON RIGHT ELEVATOR UPPER SURFACE AT RIB 7, 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE AT RIB 7 IAW A319 SRM 55-21-11 PAR 5-E & AMM 51-75-12.Dec 7, 2012 · N825AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2012120700008Sill · corrodedSY6 CHECK - DOOR SILL CORRODED BETWEEN FR 66 AND FR 68 AT Y -1732. REMOVED AND REPLACED SILL IAW A319 SRM 51-42-11 AND EA 504538.Dec 6, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120600015Attach Fitting · wornSY6 CHECK - NOSE LANDING GEAR WHEEL WELL LT SIDE SUPPORT ROD ATTACHMENT FITTING WORN. REMOVED AND REPLACED FITTING IAW A319 SRM 51-42-11.Dec 4, 2012 · N825AW · Airbus A319132 · Nose/Tail Landing GearSDR USAA2012120600014Floorbeam · corrodedSY6 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 67 & FR 68 AT Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.Dec 3, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120600013Floorbeam · corrodedSY6 CHECK - LONGITUDINAL FLOORBEAM CORRODED BETWEEN FR 68 & FR 69 AT Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIGURE 102 & 51-42-11.Dec 3, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120600012Floorbeam · corrodedSY6 CHECK - LONGITUDINAL FLOORBEAM CORRODED AT FR 66 AND Y -1292. REMOVED AND REPLACED BEAM IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.Dec 3, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120300041Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR16, -Y1379.5. REPLACED LONGITUDINAL BEAM AT FR16, -Y1379.5 IAW A319 SRM 53-11-14, FIG 102 & 51-42-11.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120300040Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR68, -Y765. REPLACED LONGITUDINAL BEAM AT FR68, -Y765 IAW A319 SRM 53-00-14, FIG 102 & 51-42-11.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120300039Floorbeam · corrodedSY6 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.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120300038Floorbeam · corrodedSY6 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.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2012120300036Seat Track · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR20, -Y1292. REPLACED SEAT TRACK BETWEEN FR16 TO FR20, -Y1292 IAW A319 SRM 51-42-11 & 51-75-12.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012120300035Shear Plate · corrodedSY6 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 & 51-75-12.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120300034Shear Plate · corrodedSY6 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.Nov 30, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120300037Floor Support · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR66+3 INCHES, Y765. REPLACED FLOOR SUPPORT BEAM AT FR66+3 INCHES, Y765 IAW A319 SRM 51-42-11, 51-74-00 & 53-00-14.Nov 29, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120300033Tray · crackedSY6 CHECK - CRACK IN SHEAR PLATE TRAY BETWEEN FR68 TO FR69, -Y1732. REPLACED SHEAR PLATE TRAY BETWEEN FR68 TO FR69, -Y1732 IAW A319 SRM 51-42-11, 53-41-14, FIG 18 & 51-31-00, TABLE 4.Nov 29, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120300032Seat Track · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, Y503.2 INCHES. REPLACED DUMMY RAIL BETWEEN FR12 TO FR16, Y503.2 INCHES IAW A319 SRM 53-11-14, FIG 102 & 51-42-11.Nov 29, 2012 · N825AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012120300031Floor Support · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R. REPLACED FLOOR SUPPORT BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-42-11, 51-44-11 & 51-75-12.Nov 29, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012120300030Sill · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SILL PLATE BETWEEN FR67 TO FR68, Y1732. REPAIRED SILL PLATE BETWEEN FR67 TO FR68, Y1732 IAW A319 SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 5.Nov 29, 2012 · N825AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012052200018Megaphone · inoperativeAFT MEGAPHONE FAILED PRE-FLIGHT READINESS CHECK. REMOVED AND REPLACED MEGAPHONE IN AFT CABIN, OPS CHECKED GOOD.May 21, 2012 · N825AW · Airbus A319132 · Emergency EquipmentSDR USAA2012022400021Epsu · faultyPERFORMED EMERGENCY POWER SUPPLY UNIT (EPSU) TEST. UNIT "FAULT" WAS DISPLAYED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) PER JOBCARD 26C00033004. OPS CHECKED GOOD.Feb 21, 2012 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2010102992452Wire Harness · faultyFLT 527 - RNO-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT AT ROW 8 RIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT SEAT HARNESS AT ROW 8 RIGHT FROM QUICK DISCONNECT TO LIGHT ASSEMBLY. SYSTEM OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-00-710-001.Oct 28, 2010 · N825AW · Airbus A319132 · Light System WiringSDR USAA2010060491060Battery · dischargedFLT 506 - PHX-YVR - EMERGENCY LIGHTS - FLASHLIGHT UNDER FORWARD FLIGHT ATTENDANT JUMP SEAT DEAD AND SEAL BROKEN. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.Jun 3, 2010 · N825AW · Airbus A319132 · Emergency EquipmentSDR USAA2010032990673Attach Fitting · corrodedSAL - C6 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF RIGHT FITTING BASE PLATE ATTACH ENGINE PYLON. REPAIRED LOWER SURFACE OF RIGHT FITTING BASE PLATE ATTACH ENGINE PYLON IAW EA 132934.Mar 19, 2010 · N825AW · Airbus A319132 · Nacelle/Pylon, Attach FittingsSDR USAA2010032990672Attach Fitting · corrodedSAL - C6 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF LEFT FITTING BASE PLATE ATTACH ENGINE PYLON. REPAIRED LOWER SURFACE OF LEFT FITTING BASE PLATE ATTACH ENGINE PYLON IAW EA 132924.Mar 19, 2010 · N825AW · Airbus A319132 · Nacelle/Pylon, Attach FittingsSDR USAA2009101992797Power Supply · dischargedFLT 210 - SMF-PHX - EMERGENCY LIGHTS - CIDS LIGHT CYCLING ON AND OFF. REMOVED AND REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.Oct 16, 2009 · N825AW · Airbus A319132 · Emergency LightingSDR USAA2009051991228Lanyard · unsecureLOGPAGE:8558477 - FLT 49 - LAS-DCA - EMERGENCY EQUIPMENT - AIRCRAFT AFT DOOR RIGHT LANYARD HANGING DOWN FROM SLIDE. CORRECTLY SECURED LANYARD ON RIGHT AFT SLIDE PER MAINTENANCE MANUAL 25-61-00.May 18, 2009 · N825AW · Airbus A319132 · Escape SlideSDR USAA2009040790814Flashlight · inoperativeFLT 468 - CMH-PHX - EMERGENCY LIGHTS - FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT. OPERATIONAL CHECK WAS GOOD.Apr 6, 2009 · N825AW · Airbus A319132 · Emergency Equipment
Back to N825AW