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 AWXA200601258Floor Panel · corrodedSAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945413. CORROSION ON FLOOR PANEL NR 262 FF BETWEEN FRAME 66 TO FRAME 68 RIGHT SIDE PASSENGER CABIN. MAINTENANCE REMOVED AND REPAIRED FLOOR PANEL 262 F BETWEEN FR 66 TO FR 68 AND INSTALLED WITH AWA CARD CID 25318 SEQ 97.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601257Floorbeam · corrodedSAL - MAJOR REPAIR - CHECK NR BC - 4. NR 5945287. CORROSION LOCATED ON FLOORBEAM Y 1292 PASSENGER CABIN FR 68. (1 POINT). MAINTENANCE REWORKED AREA AND FOUND OUT OF LIMITS IAW SRM A 319 53 - 00 - 14 FIG 102 PAG 106 AND FLOORBEAM Y 1292 BETWEEN FR 68 TO FR 69 WJul 4, 2006 · N820AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601256Floor Panel · corrodedSAL - MAJOR REPAIR - CHECK NR BC - 4. NR NO. 5945214. CORROSION ON FLOOR PANEL OF FWD PASSENGER CABIN ON LOWER RIGHT CREW DOOR. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 222 FF BETWEEN FR 16 TO FR 20 AND WAS INSTALLED WITH AWA CARD CID25306. JOG 89.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601255Floor Panel · perforatedSAL - MAJOR REPAIR - NR NR 5944810. DURING B - 04 CHECK THE FLOOR PANEL NR 131 CF OF FWD. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 131 CF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601254Floor Panel · perforatedSAL - MAJOR REPAIR - CHECK NR B - 04. NR 5944858. FLOOR PANEL NR 151 TG OF THE AFT. CARGO COMPARTMENT WAS FOUND WITH PERFORATION. FLOOR PANEL NO. 151 TG WAS REPLACED IAW IRM 9701 REV. I AND SRM 53 - 02 - 00 PAR 8H - 8G.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601204Floorbeam · corrodedSAL - MAJOR REPAIR - CHECK NO. BC-4. NR NR 5945290. CORROSION LOCATED ON FLOORBEAM Y 1292 PASSENGER CABIN FR 67, FR 67 + 4", FR 67 + 8" (3 POINT). REWORKED AREA FOUND OUT OF LIMITS IAW SRM A319 53 - 00 - 14 FIG 102 PAG 106 AND FLOOR BEAM Y 1292 BETWEEM FR 66 TJul 4, 2006 · N820AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AWXA200601203Seat Track · corrodedSAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5944998. CORROSION LOCATED ON SEAT TRACK FRAME 43 + 3" AND FRAME 46-4" (2 POINT). SEAT TRACK LOCATED BTW FR 41 TO FR 47 OUTBOARD Y 1292 WAS REPLACED IAW SRM A379 51 - 72 - 11 PAG 42 AND IAW SRM A319 53 - 31 - 75 FIG Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601183Seat Track · corrodedCORROSION LOCATED ON SEAT TRACK - Y 765 FROM FS 41 + 5" FS 45 + 16". REPLACED SEAT TRACK ON - Y 765 FROM FS 41 FS 47 IAW SRM A319 51 - 72 - 11 AND SRM A319 51 - 42 - 11 PAR 7 EVALUATED AND WAS FOUND OUT OF LIMITS IAW SRM A319 53 - 31 - 75 PAGE 107 FIG 103.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601182Plate · corrodedFOUND CORROSION LOCATED ON SHEAR PLATE PASSENGER CABIN BETWEEN FS 69 TO FS 70 STRINGER 23 L. CORROSION LOCATED ON SHEAR PLATE PASSENGER CABIN BETWEEN FS 69 TO FS 70 STRINGER 23 L WAS REPLACED AND INSTALLED IAW SRM A319 51-72-11, PAGE 1 - 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601181Seat Track · corrodedFOUND CORROSION ON FLOORBEAM Y 765 FS 16 PAX CABIN. SEATTRACK LDC ON PAX CABIN Y 765 FROM FS 12 TO FS 24 WAS REMOVED AND REPLACED IAW SRM A319 51-42-11 AND SRM A319 51-72-11. BECAUSE AFTER IT HAD BEEN REWORKED AND WAS FOUND OUT OF LIMITS IAW SRM A319 53-11-1Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601180Floor Panel · perforatedFLOOR PANEL NR 151 DE WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 DE WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601179Floor Panel · perforatedFLOOR PANEL NR 161 CF WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 161 CF WAS REPAIRED IAW SRM 53-02-00.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601178Floor Panel · perforatedTHE FLOOR PANEL NR 161 EF OF AFT CC WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 161 EF OF AFT CC WAS FOUND WITH PERFORATION, WAS REPAIRED.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601177Floor Panel · damagedFLOOR PANEL NR 151 Z6 WAS FOUND WITH MISSING MATERIAL. FLOOR PANEL NR 151, Z6 WAS REPLACED IAW IRM 9701 REV F AND SRM 53-02-00 PAR 86, 8H.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601175Floor Panel · perforatedFOUND FLOOR PANEL NR 131 DF WAS FOUND WITH PERFORATION IN FWD CC. FLOOR PANEL NR 131 WAS REPAIRED IAW SRM 53-02-00 PARA 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601174Floor Panel · perforatedTHE FLOOR PANEL NR 161 BF OF AFT CC WAS FOUND WITH PERFORATION. THE PANEL NR 161 BF IN 2FT CC WAS REPAIRED IAW SRM 53-02-00 PARA 8C 2 FIG 204.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601173Floor Panel · perforatedTHE FLOOR PANEL NR 162 FF OF AFT CARGO COMPARTMENT WAS FOUND WITH PERFORATION. THE FLOOR PANEL NR 162 FF WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2 FIG 204.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601172Floor Support · corrodedFOUND CORROSION LOCATED ON FLOORBEAM - Y 1292 PAX CABIN FRAME 66 + 13 " AND FRAME 67 + 11 ". CORROSION LOCATED ON FLOORBEAM - Y 1292 PAX CABIN FRAME 66 + 13 " AND FRAME 67 + 11 " WAS REPLACED IAW SRM A379 51-72-11.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601171Floor Support · corrodedFOUND CORROSION LOCATED ON FLOORBEAM - Y 1292 PASSENGER CABIN FRAME 66. REWORKED AREA FOUND OUT OF LIMITS IAW SRM A319 53-00-14 FIG 102 PAGE 106 AND FLOORBEAM - Y 1292 BETWEEN FS 64 TO FS 66 WS REPLACED IAW SRM A319 51-72-11 PAGE 1 AND PAGE 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AWXA200601170Floor Panel · perforatedFLOOR PANEL NR 151 FE WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 FE WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601169Skin Panel · lightning strikeFOUND LIGHTNING STRIKE, FLOOR PANEL ON RIVET EXTERNAL FUSELAGE AT FRAME 2L 2171 CM APPROX. PERFORMED PERMANENT REPAIRS ON EXTERNAL FUSELAGE FRAME 2L Z + 71 CM APPROX IAW SRM A319 53-00-11 PAGE 353 TO 362 FIG 223 SHEET 2.Jul 4, 2006 · N820AW · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR AWXA200601168Floor Panel · perforatedSAL - FLOOR PANEL NR 151 UG WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 151 UG WAS REPAIRED IAW SRM 53-02 -00 PAR 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601167Plate · lightning strikeSAL - MAJOR REPAIR - CHECK NR BC - 4. RN NR 5945019. LIGHTNING STRIKE ON BLANKING PLATE ON STATIC PORT EXTERNAL FUSELAGE AT FRAME 4 - 0.5 Z + 62 CM. REVLORED AREA ON BLANKING PLATE OF STATIC PORT FRAME 4 - 0.5 + Z + 62 CM. APPROXIMATELY SIDE LH ER NO. 25 - 531Jul 4, 2006 · N820AW · Airbus A319132 · Nacelle/Pylon Miscellaneous StructureSDR AWXA200601166Floor Panel · perforatedFLOOR PANEL NR 152 WAS FOUND WITH PERFORATION IN AFT CC. FLOOR PANEL NR 152 WAS REPAIRED IAW SRM 53-02-00 PAR 8C 2.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601165Panel · lightning strikeFOUND LIGHTNING STRIKE ON RIVER EXTERNAL FUSELAGE AT FRAME 5L Z55 CM APPROX. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE FRAME 5L Z55 CM APPROX IAW SRM A319 53-00-11 PNG 353 TO 362 FIG 223 SHEET 2 AND FASTENER REPLACED IAW SRM A319 51-42-11.Jul 4, 2006 · N820AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AWXA200601270Floor Panel · delaminatedSAL - MAJOR REPAIR - CHECK NR BC-4. NR 5945415. DELAMINATION LOCATED FLOOR PANEL NR 251 SF BETWEEN FRAME 58 TO FRAME 62 PASSENGER CABIN. FLOOR PANEL NR 251 SF WAS REPAIRED IAW SRM 53 - 02 - 00 PAR 3.Jul 3, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601176Floor Panel · delaminatedDELAMINATION LOCATED FLOOR PANEL NR 251 SF BETWEEN FRAME 58 TO FRAME 62 PASSENGER CABIN. FLOOR PANEL NR 251 SF WAS REPAIRED IAW SRM 53-02-00.Jul 3, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601259Floor Panel · delaminatedSAL - MAJOR REPAIR - CHECK NO. BC-4. NR NO. 5945414. DELAMINATION LOCATED ON FLOOR PANEL LOWER SILL DOOR L2 FR 68 LEFT SIDE. REMOVED AND REPLACED FLOOR PANEL LOWER SILL DOOR FR 68 LEFT SIDE.Jul 2, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200601274Seat Track · corrodedSAL - MAJOR REPAIR - CHECK NR BC-4. NR 5944992. CORROSION LOCATED ON SEAT TRACK - Y 1292 (3 POINT) FRAME 42 + 8" - FR 42 + 16.5" - FR 44 + 8". SEAT TRACK - Y 1292 BETWEEN FR 41 TO FR 51 REPLACED IAW SRM A319 51 - 72 - 11 PAG 1 AND PAG 2, SEAT TRACK EVALUATED AJun 29, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601164Seat Track · corrodedFOUND CORROSION LOCATED ON SEAT TRACK - Y 1292 (3 POINT) FRAME 42 + 8 IN - FS 42 + 16.5 IN - FS 44 + 8 INCH SEAT TRACK - Y 1292 BETWEEN FS 41 TO FS 51 REPLACED IAW SRM A319 51 - 72 - 11 PAGE 1 AND SRM 53 - 31 - 15 PAGE 107 FIG 103.Jun 29, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601163Seat Track · corrodedFOUND CORROSION LOCATED ON SEAT TRACK Y - 1292 FS 39 - 2 INS SEAT TRACK Y - 1292 BETWEEN FS 36 TO FS 41 REPLACED IAW SRM A319 51-72-11 PAX 1, 2, SEAT TRACK EVALUATED AND IS OUT LIMIT IAW SRM A319 53 - 31 - 15 PAX 102 FIG 101.Jun 29, 2006 · N820AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200601205Floor Panel · corrodedSAL - MAJOR REPAIR - CHECK NR BC -4. NR 5945416. CORROSION LOCATED ON FLOOR PANEL LOWER SILL DOOR R2 FRAME 68 RIGHT SIDE PASSENGER CABIN. REMOVED AND REPLACED FLOOR PANEL LOWER SILL R2 DOOR FR 68 RIGHT SIDE PASSENGER CABIN IAW SRM 5/ 7211.Jun 28, 2006 · N820AW · Airbus A319132 · Fuselage Floor PanelSDR AWXA200600836Power Supply · failedATL - EEL - MAINTENANCE REPORTED THAT THE FORWARD GALLEY EMERGENCY LIGHT, POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY LIGHT EMERG LIGHT POWER SUPPLY IAW AWA TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD.May 20, 2006 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200500020Fmu · malfunctionedBOS - ABORTED TAKEOFF - FLT 0068 - ON TAKEOFF AT BOS EN ROUTE FOR PHX RECEIVED ECAM INDICATIONS, ENG 1 FADEC, ENG 1 COMPRESSOR, ENG 1 FAIL, ENG 1 FUEL CTRL FAULT. REJECTED TAKEOFF AT LOW SPEED. MAINTENANCE TROUBLESHOT AND REPLACED NR 1 ENGINE FUEL METERING UJan 8, 2005 · N820AW · Airbus A319132 · Fuel Controlling SystemSDR AWXA200401176Actuator · failedON TAKEOFF AT EWR EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "ENG 1 COMPRESSOR VANE FAILURE", REJECTED TAKEOFF AT 68 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED HIGH POWER ASSURANCE TEST, NOct 28, 2004 · N820AW · Airbus A319132 · Compressor Bleed ControlSDR AWXA200400238Selector Valve · failedPHX - AIR TURNBACK - FLT 0251 - AFTER TAKEOFF FROM PHX EN ROUTE TO MSP RECEIVED ECAM MESSAGE LG LGCIU 2 FAULT, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL AND INTERFACE FACE UNIT (LGCIU) NR 2 (5GAMar 3, 2004 · N820AW · Airbus A319132 · Landing Gear Retraction/Extension SystemSDR AWXA200400160Flashlight · inoperativePHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Feb 7, 2004 · N820AW · Airbus A319132 · Emergency EquipmentSDR AWXA200400157Odor · detectedAN ELECTRICAL BURNING ODOR OBSERVED IN THE COCKPIT & CABIN NEAR SEAT ROW 4, DECLARED EMERGENCY, LANDED WITHOUT FURTHER DIFFICULTIES. MX REMOVED AFT WALL OF FWD BAG PIT & INSPECTED RECIRCULATION FANS & DUCTING FOR EVIDENCE OF OVERHEATING & ODOR, NO DEFECTS NOTFeb 7, 2004 · N820AW · Airbus A319132 · Air Distribution SystemSDR AWXA200300845Ballast · overheatedON CLIMBOUT FROM SAN EN ROUTE FOR LAS AT 20,000 FT, FLT ATTENDANT REPORTED A STRONG ELECTRICAL BURNING ODOR IN MID TO AFT CABIN, DIVERTED TO LAX. MAINTENANCE FOUND CABIN LIGHTING BALLAST AT SEAT ROW 16 LT EXTREMELY HOT. REMOVED AND REPLACED BALLAST, PERFORMEJul 26, 2003 · N820AW · Airbus A319132 · Passenger Compartment LightingSDR AWXA200300744Housing · defectiveEMERGENCY LIGHT FLASHING ON AND OFF AT RT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT HOUSING AT THE RT OVERWING EXIT, OPERATIONAL CHECK WAS GOOD.Jun 27, 2003 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200300742Skin · corrodedMCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054;Jun 21, 2003 · N820AW · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR AWXA200300741Skin · corrodedMCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054;Jun 21, 2003 · N820AW · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR AWXA200300416Thermocouple · defectiveON DESCENT WITH AUTO THROTTLE ON 11,000 FT, NR 2 ENGINE SPOOLED NORMALLY TO MAINTAIN MANAGED SPEED, NR 1 ENGINE DID NOT SPOOL FOR 3 TO 4 SECONDS. NR 1 ENGINE WENT TO CLIMB THRUST RESULTING IN SUBSTANTIAL YAW (3 TO 5 DEG) ROLL OF 2 TO 3. ON IDLE DESCENT 6000 Apr 14, 2003 · N820AW · Airbus A319132 · Engine Fuel and ControlSDR AWXA200300271Battery · dischargedMAINTENANCE FOUND EMERGENCY LIGHTS LEFT ON 2 HOURS AFTER CREW LEFT. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS, ZONES 221, 241, 242, AND 263. FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM WAS GOOD.Mar 15, 2003 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200200645Power Supply · dischargedPHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 14, 17, AND 20 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-04, OPERATIONAL CHECK WAS GOOD.Jul 22, 2002 · N820AW · Airbus A319132 · Emergency LightingSDR AWXA200100603Valve · failedDEN - AIR TURNBACK -C - WHILE EN ROUTE ACFT RECEIVED ECAM MESSAGE FOR VENT SKIN FAULT. DURING TURN AT DEN DEACTIVATION OF THE VENT SKIN AIR VALVE WAS ACCOMPLISHED. UPON TAKEOFF FROM DEN TO LAS ECAM MESSAGE REAPPEARED AND ACFT WOULD NOT PRESSURIZE, ACFT TURNENov 27, 2001 · N820AW · Airbus A319132 · Cabin Pressure Control SystemSDR AWXA0001372Relief Valve · rupturedCMH - DIVERTED FLIGHT - 2/14/01 - EN ROUTE FROM PHL TO PHX THE CREW GOT AN ECAM AUTO FUEL FAULT. SELECTED MANUAL AND NOTICED FLASHING QUANTITY NR 2 MAIN AND OUTBOARD RESERVE AND DECREASING FUEL QUANTITY IN NR 1 MAIN; TRIED NR 1 FUEL PUMPS OFF, DECREASE CONTINFeb 19, 2001 · N820AW · Airbus A319132 · Fuel Storage
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