N828AW

Service difficulty reports · 294

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 = 'N828AW' 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 USAA2011111400008Cylinder · low pressureDOOR EMERGENCY CYLINDER / ACCUMULATOR PRESSURE LOW R1 DOOR, APPROXIMATELY 1495 PSI. CHARGED TO PROPER LEVEL IAW AMM 52-10-00.Nov 12, 2011 · N828AW · Airbus A319132 · Service DoorsSDR USAA2011111400007Cylinder · low pressureDOOR EMERGENCY CYCLINDER /ACCUMULATOR PRESSURES LOW L1 DOOR, APPROX 1640 PSI. CHARGED TO PROPER LEVEL IAW AMM 52-10-00.Nov 12, 2011 · N828AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2011072500005Battery · dischargedAFT EMERGENCY FLASHLIGHT STUCK IN 'ON' POSITION. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY AND HOLD DOWN STRAP.Jul 24, 2011 · N828AW · Airbus A319132 · Emergency EquipmentSDR USAA2011070600024Dampener · leakingTGC - L-2 DOOR EMERGENCY ASSIST BOTTLE HAS LOW PRESSURE. REMOVED AND REPLACED DIAPHRAGM ON L-2 EMERGENCY ASSIST BOTTLE AND SERVICED, LEAK CHECKS GOOD IAW A319 AMM 52-10-00-610-001.Jul 2, 2011 · N828AW · Airbus A319132 · Escape SlideSDR USAA2010092792097Eec · defectiveFLT 85 SJC-PHX - RTO - ENGINE NR 1 SURGED DURING TAKEOFF. VISIBLE INDICATIONS ON EPR GAUGE; NOTICEABLE AUDIBLE AND YAW FLUCTUATIONS. TAKEOFF WAS REJECTED AT 128 KTS. MAINTENANCE FOUND BURNER PRESSURE SENSOR TUBE CONTAMINATED WITH WATER. CLEARED WITH NITROGSep 23, 2010 · N828AW · Airbus A319132 · Fuel Control/Turbine EnginesSDR USAA2010061791154Lens · missingFLT 49 - LAS-DCA - EMERGENCY LIGHTS - L2 DOOR EMERGENCY EXIT LENS MISSING. REPLACED MISSING EMERGENCY EXIT LENS AT L2 DOOR.Jun 15, 2010 · N828AW · Airbus A319132 · Emergency LightingSDR USAA2010052691033Epsu · faultyFLT 34 - PHX - LAX - EMERGENCY LIGHTS - AFT EMERGENCY POWER SUPPLY UNIT (EPSU) FAULTING. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT (EPSU). OPERATIONAL CHECK WAS GOOD AS PER AMM 33-33-51-38 PB 401.May 25, 2010 · N828AW · Airbus A319132 · Emergency LightingSDR USAA2010050390880Bolt · disconnectedFLT 400 BOS-PHX - EMERGENCY LANDING - ON DESCENT INTO PHX GOT ENGINE 1 STALL ECAM THEN SELF CLEARED - PARAMETERS LOOKED NORMAL. AT 12000 FEET GOT THIRD STALL MESSAGE FOLLOWED BY ENGINE 1 FAIL ECAM. THIS TIME EGT WAS ABOUT 549 DEGREES WITH LEVERS AT IDLE. SHApr 30, 2010 · N828AW · Airbus A319132 · Compressor Bleed ValveSDR USAA2010040890743Damper · low pressureSAL - C6 - EES - LOW PRESSURE AT L-2 EMERGENCY DOOR DAMPER CYLINDER. PERFORMED CHARGING OF THE DAMPER & EMERGENCY OPERATION CYLINDER AT L-2 DOOR IAW A319 AMM 52-10-00-614-051.Apr 5, 2010 · N828AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010040890744Damper · low pressureSAL - C6 - EES - LOW PRESSURE AT R-1 EMERGENCY DOOR DAMPER CYLINDER. PERFORMED CHARGING OF THE DAMPER & EMERGENCY OPERATION CYLINDER AT R-1 DOOR IAW A319 AMM 52-10-00-614-051.Apr 1, 2010 · N828AW · Airbus A319132 · Service DoorsSDR USAA2010040690723Striker · out of adjustSAL - C6 - EES - DIMENSION "B" IS OUT OF ADJUSTMENT BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT SERVICE DOOR. PERFORMED ADJUSTMENT CLEARANCE BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT SERVICE DOOR IAW A319 AMM 52-13-Apr 1, 2010 · N828AW · Airbus A319132 · Service DoorsSDR USAA2010040690722Rod · out of adjustSAL - C6 - EES - DIMENSION "A" IS OUT OF ADJUSTMENT BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT ENTRY DOOR. PERFORMED ADJUSTMENT CLEARANCE BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT ENTRY DOOR IAW A319 AMM 52-13-14-8Apr 1, 2010 · N828AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010041290765Skin · saturatedSAL - C6 - MAJOR REPAIR - 2 INCHES OF TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010041290764Skin · saturatedSAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 12 TO RIB 13. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 12 TO RIB 13 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010041290763Skin · saturatedSAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 6 TO RIB 7. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 6 TO RIB 7 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010041290762Skin · saturatedSAL - C6 - MAJOR REPAIR - 1.5 INCHES OF TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010041290761Skin · saturatedSAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 5 TO RIB 6. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 5 TO RIB 6 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010041290760Skin · saturatedSAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF RIGHT ELEVATOR UPPER SKIN BETWEEN RIB 9 TO RIB 10. REPAIRED RIGHT ELEVATOR UPPER SKIN BETWEEN RIB 9 TO RIB 10 IAW A319 SRM 55-21-11 & 55-77-13.Mar 31, 2010 · N828AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010021090329Battery · dischargedFLT 467 - SFO-LAS - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST FAILED LEFT FORWARD EPSU BATTERY. REMOVED AND REPLACED LEFT FORWARD EPSU BATTERY PER AMM 33-51-00, PB 501. OPERATIONAL CHECK WAS GOOD.Feb 9, 2010 · N828AW · Airbus A319132 · Emergency LightingSDR USAA2010020190241Battery · dischargedFLT 221 - SJC-PHX - EMERGENCY LIGHTS - FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT HAS NO RED INDICATOR LIGHT ILLUMINATED. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.Jan 31, 2010 · N828AW · Airbus A319132 · Emergency EquipmentSDR USAA2009042090930Wire · damagedFLT 77 - DCA-PHX - EMERGENCY LIGHTS - EMERGENCY LIGHT INOPERATIVE AT ROW 12 LEFT. WIRES RE-TERMINATED AT CONNECTOR. OPERATIONAL CHECK WAS GOOD.Apr 18, 2009 · N828AW · Airbus A319132 · Light System WiringSDR USAA2008112492108Power Supply · malfunctionedFLT 341 - MZT-PHX - EEL - CIDS EMERGENCY LIGHT OPERATIONAL TEST FAILS EMERGENCY POWER SUPPLY UNIT INITIAL LOAD ON FORWARD LEFT. RESET EMERGENCY POWER SUPPLY UNIT FORWARD LEFT AND RIGHT. OPERATIONAL CHECK WAS GOOD.Nov 23, 2008 · N828AW · Airbus A319132 · Emergency LightingSDR USAA920082019Battery · dischargedLOGPAGE 8342494 FLT NR 464 PIT-SFO FLIGHT ATTENDANT FLASHLIGHT UNDER FORWARD JUMP SEAT NOT CHARGING. R&R FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.Nov 7, 2008 · N828AW · Airbus A319132 · Emergency EquipmentSDR USAA920081658Power Supply · dischargedLOGPAGES 4436783, 4436784 & 4436787 FLT NR 0272 PHX-MSP EMERGENCY EQUIPMENT. EMERGENCY PATH LIGHTS AT SEAT 8C AND 10C AND EMERGENCY OVERWING LIGHTS DO NOT WORK RT SIDE. RESET RT OVERWING EMERGENCY POWER SUPPLY UNIT 12WL. OPS CHECK WAS GOOD.Sep 9, 2008 · N828AW · Airbus A319132 · Emergency LightingSDR SA07081Interface Unit · failedPHX FLT 0132 EN ROUTE LAS TO PHX. ON TAKEOFF, WITH THE GEAR HANDLE SELECTED UP, A RED ECAM MESSAGE FOR GEAR UNSAFE, GEAR NOT DOWN WAS GENERATED. THE GEAR WAS RECYCLED AND THE MESSAGE CLEARED. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPDec 11, 2007 · N828AW · Airbus A319132 · Landing Gear Position and WarningSDR AWXA200602104Stringer · crackedSAL - CRACK FOUND ON STRINGER 33R, FS 72+10" - FS 74+4". REPAIRED STRINGER 33R, FS 72+10" - FS 74+4" IAW A319 SRM 53-00-13 FIG 201.Dec 21, 2006 · N828AW · Airbus A319132 · Fuselage Main, Longeron/StringerSDR AWXA200602099Power Supply · inoperativeSAL - EEL - BC-4 CHECK - CABIN PASSENGER LEFT EMERGENCY EXIT EPSU (11WL) INOPERATIVE. REMOVED AND REPLACED CABIN PASSENGER LEFT EMERGENCY EXIT EPSU PER AMM 33-51-38.Dec 19, 2006 · N828AW · Airbus A319132 · Emergency LightingSDR AWXA200602097Floor Panel · corrodedSAL - CORROSION ON FLOOR PANEL NR 222FF, FS 16 - FS 20, FROM Y-1292 TO Y-1348. REPLACED FLOOR PANEL NR 222FF, FS 16 - FS 20, FROM Y-1292 TO Y-1348 IAW A319 SRM 51-42-11 AND AWA TASK CARD C1C53302.Dec 19, 2006 · N828AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200602087Fitting · wornSAL - R2 DOOR CUT OUT LOWER SILL FWD CORNER FITTING WORN, FS 66, -Y1620. REPLACED R2 DOOR CUT OUT LOWER SILL FWD CORNER FITTING, FS 66, -Y1620 IAW A319 SRM 51-72-11 AND 51-42-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200602078Floor Support · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 68, -Y1162. REPLACED MAIN ABIN FLOORBEAM, FS 67 - FS 69, -Y1162 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200602077Shear Plate · corrodedSAL - CORROSION ON MAIN CABIN SHEAR PLATE, FS 69 - FS 70, +Y1732. REPLACED MAIN CABIN SHEAR PLATE, FS 69 - FS 70, +Y1732 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200602076Floorbeam · corrodedSAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 67+18", +Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 68 - FS 69, +Y1162 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200602075Fitting · corrodedSAL - CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, -Y1730. REPLACED R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, -Y1730 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200602074Fitting · corrodedSAL - CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, +Y1730. REPLACED L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, +Y1730 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AWXA200602073Seat Track · corrodedSAL - CORROSION ON MAIN CABIN DUMMY RAIL/TRACK, FS 20, -Y190. REPLACED MAIN CABIN DUMMY RAIL/TRACK, FS 20 - FS 24, -Y190 IAW A319 SRM 51-72-11.Dec 10, 2006 · N828AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200602096Seat Track · corrodedSAL - CORROSION ON PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y-1292. REPLACED PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y-1292 IAW A319 SRM 51-72-11.Dec 9, 2006 · N828AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200602095Seat Track · corrodedSAL - CORROSION ON PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y1292. REPLACED PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y1292 IAW A319 SRM 51-72-11.Dec 9, 2006 · N828AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601557Relay · shortedJFK - THE CREW ALSO RECEIVED AN ECAM MSG FOR: CB TRIPPED REAR PNL N-R. CB R7 POPPED (ELECTRONIC INSTRUMENT SYSTEM RELY BOX FO). MAINTENANCE REPLACED RELAY 20WT2 IAW ESPM CHAPTER 20. OPS CHECK GOOD.Aug 25, 2006 · N828AW · Airbus A319132 · Instrument PanelSDR AWXA200501386Diaphragm · leakingPHX - EES - DURING OVERNIGHT INSPECTION, DISCOVERED THE L-1 DOOR ASSIST BOTTLE PRESSURE LOW, AT 300 PSI. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE BUT FAILED LEAK CHECKS. REMOVED AND REPLACED THE L1 DOOR ASSIST BOTTLE DIAPHRAGM IAW AIRBUS 319 AMM 52-10-Nov 12, 2005 · N828AW · Airbus A319132 · Passenger/Crew DoorsSDR AWXA200301428Power Supply · faultySEA - EEL - DURING 4-DAY CHECK THE LT MID CABIN EMERGENCY POWER SUPPLY UNIT FAULTED DURING EMERGENCY PATHWAY LIGHT OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED LT MID CABIN EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.Nov 14, 2003 · N828AW · Airbus A319132 · Emergency LightingSDR AWXA200300967Control Unit · failedDURING CRUISE SELECTIVE CALLING SYSTEM TONE SOUNDED CONTINUOUSLY WITH NOBODY CALLING, UNABLE TO RESET. PULLED SEVERAL CIRCUIT BREAKERS & TONE STOPPED. TONE SOUNDED AGAIN, UNABLE TO RESET. SELCAL TONE COULD NOT RECEIVE OVER CAPTS HEADSET THRU ACP NR 1. USEDAug 21, 2003 · N828AW · Airbus A319132 · VHF Communications SystemSDR AWXA200300437Engine · failedEN ROUTE FROM PHX TO DCA AT FL 370 A LOUD BANG WAS HEARD COMING FROM NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A CLOGGED OIL MESSAGE, ALL OTHER PARAMETERS NORMAL. CREW CONTACTED MOC AND WERE TOLD TO MONITOR ENGINE. APPROXIMATELY 15 MINUTES LATER TWO MORE BANGS WEREApr 27, 2003 · N828AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AWXA200300393Tire · damagedSNA - ABORTED TAKEOFF - FLT 0250 - EN ROUTE FROM SNA TO PHX - AS AIRCRAFT STARTED TAKEOFF ROLL AT FROM EPR OF 1.05 THE THRUST CAME UPSLIGHTLY STAGGERED, AIRCRAFT STARTED TO DEVIATE FROM CENTER LINE, CAPTAIN TOOK CONTROL AND REJECTED TAKEOFF. NOSE TIRES WERE DApr 19, 2003 · N828AW · Airbus A319132 · TireSDR AWXA0002211Computer · failedPHX - ABORTED TAKEOFF - FLT 79 - ON TAKE ROLL ECAM MESSAGE FOR AVIONICS VENT SKIN FAULT APPEARED AND THE TAKEOFF WAS ABORTED UNDER 80 KTS. MAINTENANCE TROUBLESHOT AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC), FUNCTIONAL CHECKS WERE GOOD. NSep 1, 2001 · N828AW · Airbus A319132 · Cabin Pressure Control System
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