N162UW

Service difficulty reports · 338

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 = 'N162UW' 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 AALA201904129027Floor Panel · damagedAIRCRAFT WAS GROUNDED: FORWARD CARGO FLOOR PANEL 131EF SPONGY. REPLACED FLOOR PANEL PER AMM 53-22-14.Apr 11, 2019 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201812119018Bottle · low pressureR1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.Dec 9, 2018 · N162UW · Airbus A321211 · Emergency EquipmentSDR AALA201810239015Bottle · low pressureR3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. CHARGED THE BOTTLE IAW AMM 52-22-00 AND PERFORMED LEAK CHECK. CHECK IS OK, NO LEAK FOUND.Oct 22, 2018 · N162UW · Airbus A321211 · Emergency EquipmentSDR AALA201810199028Hinge Fitting · wornNOSE LANDING GEAR RIGHT AFT DOOR AFT HINGE HAS EXCESSIVE PLAY. REPLACED THE DOOR HINGE IAW CMM 52-82-32-400-802, AND 52-82-32-400-805-A001.Oct 18, 2018 · N162UW · Airbus A321211 · Landing Gear DoorsSDR AALA201810199027Hinge Fitting · wornNOSE LANDING GEAR RIGHT AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED THE DOOR HINGE IAW CMM 52-82-32-400-802, AND 52-82-32-400-805-A001.Oct 18, 2018 · N162UW · Airbus A321211 · Landing Gear DoorsSDR AALA201810049024Bearing · migratedRIGHT PYLON OUTBOARD THRUST REVERSER AFT ATTACHMENT POINT HINGE FITTING BEARING HAD MIGRATED. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.Oct 3, 2018 · N162UW · Airbus A321211 · Engine Thrust ReverserSDR AALA201810049023Bearing · migratedRIGHT PYLON, INBOARD THRUST REVERSER MIDDLE ATTACHMENT POINT HINGE FITTING BEARING HAS MIGRATED. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.Oct 3, 2018 · N162UW · Airbus A321211 · Engine Thrust ReverserSDR AALA201810039021Rub Strip · deterioratedAIRCRAFT IN BASE MAINTENANCE. DETERIORATED RUBBER STRIP PASSENGER CREW DOOR 831 AND 841 IN PASSENGER CABIN. REPLACED RUBBER STRIP PER AMM 52-11-18-300-002-A.Oct 2, 2018 · N162UW · Airbus A321211 · Passenger/Crew DoorsSDR AALA201810039005Hinge Fitting · excess playLEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING HAD EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW CMM 52-81-18.Oct 2, 2018 · N162UW · Airbus A321211 · Landing Gear DoorsSDR AALA201810059012Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 67 + 15 INCHES, -Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.Sep 27, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201809259002Floor Panel · perforatedPERFORATION ON FLOOR PANEL 131XF IN FWD CARGO BAY. REPAIRED FLOOR PANEL IAW SRM 53-02-00-300-004, PARA2A (1) (2) (7) TO (9).Sep 24, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810059017Hinge Arm · excess playRIGHT ELEVATOR NR 4 HINGE ARM HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-001-A.Sep 20, 2018 · N162UW · Airbus A321211 · Elevator StructureSDR AALA201810059016Hinge Arm · excess playRIGHT ELEVATOR NR 5 HINGE ARM HAD EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-16-42-400-001-A.Sep 20, 2018 · N162UW · Airbus A321211 · Elevator StructureSDR AALA201810059013Hinge Arm · excess playRIGHT ELEVATOR NR 6 HINGE ARM HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-11-42-400-001-A.Sep 20, 2018 · N162UW · Airbus A321211 · Elevator StructureSDR AALA201810229002Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR, LEFT HAND AFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-ASep 18, 2018 · N162UW · Airbus A321211 · Landing Gear DoorsSDR AALA201810229001Hinge Fitting · wornNOSE LANDING GEAR, LEFT HAND AFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-ASep 18, 2018 · N162UW · Airbus A321211 · Landing Gear DoorsSDR AALA201810159002Angle · crackedCRACKED VERTICAL ANGLE AT FRAME 42 IN THE RIGHT HYDRAULIC COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810109004Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IN THE FORWARD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53112812, AND D53110984.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810099005Floor Support · corrodedCORROSION FOUND ON THE FORWARD GALLEY FLOOR SUPPORT BETWEEN FRAMES 12 AND 24, -Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810089044Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON L2 DOOR CUT OUT LOWER SILL CENTER SILL SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL CENTER SILL SHAPE FITTING PER SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810089040Coupling · damagedAIRCRAFT IN BASE MAINTENANCE. L2 DOOR CUTOUT LOWER SILL INBOARD COUPLING AT FR 66 AND S23L HAS ELONGATED HOLE. REPLACED COUPLING PER SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810089039Coupling · damagedAIRCRAFT IN BASE MAINTENANCE. L2 DOOR CUTOUT LOWER SILL OUTBOARD COUPLING AT FR 66 AND S23L HAS ELONGATED HOLE. REPLACED COUPLING PER SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810089038Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON L2 DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PER SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059011Cover · corrodedCORROSION ON JOINT COVER IN THE FORWARD GALLEY AREA LOCATED BETWEEN FRAMES 12 TO 16, -Y81. REPLACED THE JOINT COVER IAW SRM 51-72-11, DWG D53112829, AND D53110984.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059010Seat Track · corrodedCORROSION ON THE SEAT TRACK BETWEEN FRAMES 12 TO 16, IN THE FORWARD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM A321 51-72-11, AND DRAWING D53112825.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201810049015Fitting · corrodedCORROSION ON THE L1 DOOR SILL CENTER FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23L. REPLACED CENTER FITTING IAW SRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Main, Attach FittingsSDR AALA201810039003Fitting · corrodedCORROSION ON FOUND ON THE R1 DOOR LOWER SILL CENTER FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23R. REPLACED CENTER FITTING IAW SWRM 51-72-11.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA2018100219003Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 211EF IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA2018100219002Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 212EF IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810019015Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221DF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810019014Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222EF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810019013Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231CF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810019012Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211FF, IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810019009Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 221EF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201809219034Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261PF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201809219033Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261BG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201809219032Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261AG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.Sep 14, 2018 · N162UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201810159001Buttstrap · corrodedCORROSION ON FORWARD CARGO DOOR CUTOUT LOWER BUTT STRAP BETWEEN FRAMES 26 AND 28, STRINGER 38R. REPLACED THE BUTT STRAP IAW SRM 51-72-11.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Main, Plate/SkinSDR AALA201810059028Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT, FRAME 67, +Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059019Tray · crackedCRACKED TRAY BETWEEN FRAMES 68 AND 69, STRINGER 23L. REPLACED THE TRAY IAW SRM 51-72-11.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059022Seat Track · corrodedCORROSION ON THE SEAT TRACK BETWEEN FRAMES 64 TO 66, -Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472816.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201810059020Floor Support · corrodedCORRODED FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 + 5, +Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472815.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059014Floor Support · corrodedCORRRODED FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472816.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059023Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 67 TO 69, -Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810059021Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 67 + 15 INCHES TO FRAME 69, +Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810029004Seat Track · corrodedCORRODED SEAT TRACK, BETWEEN FRAMES 64 TO 66 + 5 INCHES, LBL Y765. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472780.Sep 13, 2018 · N162UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201810099004Fitting · crackedCRACKED INTERCOSTAL FITTING AT THE R1 DOOR CUTOUT, AT FRAME 16, STRINGER 10R. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11.Sep 12, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810089047Fitting · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED INTERCOSTAL FITTING AT FR 16 AND S10L. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.Sep 12, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810019010Intercostal · crackedCRACK INDICATION FOUND ON THE INTERCOSTAL, FRAME 20, STRINGERS 10 - 11. REPLACED THE INTERCOSTAL IAW SRM A321 51-72-11, AND DRAWING D53112331.Sep 12, 2018 · N162UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201810099009Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRONT WINDSHIELD FRAME CONTINUITY FITTING AT FR 4 AND S20L. REPLACED FRONT WINDSHIELD FRAME CONTINUITY FITTING PER EA 284805.Sep 9, 2018 · N162UW · Airbus A321211 · Fuselage Main, Structure
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