N165US

Service difficulty reports · 389

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 = 'N165US' 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 AALA202012149015Battery · faultedAIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING JOB CARD 26L00025012 FOR DOOR L2 SLIDE REINSTALLATION, OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNIT FAILED BUILT IN TEST EQUIPMENT CHECK WITH FOLLOWING FAILURES, ATA 33-51-38. EMERGENCY POWER SUPPLY UNIT BATTERYDec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR AALA202012149014Battery · faultedAIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING JOB CARD 26L00025012 FOR DOOR L2 SLIDE RE INSTALLATION, OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNIT FAILED BUILT IN TEST EQUIPMENT CHECK WITH FOLLOWING FAILURES, ATA 33-51-38. EMERGENCY POWER SUPPLY UNIT BATTERDec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR AALA202012149013Bulb · inoperativeAIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING JOB CARD 26L00025012 FOR DOOR L2 SLIDE REINSTALLATION, OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNIT FAILED BUILT IN TEST EQUIPMENT CHECK WITH FOLLOWING FAILURES, ATA 33-51-38. EMERGENCY POWER SUPPLY UNIT BATTERYDec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR AALA202012139002Bulb · inoperativeAIRCRAFT WAS GROUNDED. WHILE ACCOMPLISHING JOB CARD 26L00025012 FOR DOOR L2 SLIDE RE-INSTALLATION, OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNIT FAILED BUILT IN TEST EQUIPMENT CHECK WITH FOLLOWING FAILURES. ATA 33-51-38 EMERGENCY POWER SUPPLY UNIT BATTERYDec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR 2020FA0000532Battery Pack · no testDURING MAINTENANCE IT WAS FOUND THAT EPSU BATTERY FAILED OPERATIONAL TESTING. BATTERY WAS REMOVED FROM SERVICE.Dec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR 2020FA0000531Battery Pack · no testDURING MAINTENANCE IT WAS FOUND THAT EPSU BATTERY FAILED OPERATIONAL TESTING. BATTERY WAS REMOVED FROM SERVICE.Dec 12, 2020 · N165US · Airbus A321211 · Emergency LightingSDR AALA202011089004Slide · faultyAIRCRAFT WAS NOT GROUNDED. L2 DOOR SLIDE DUE TO BE CHANGED ON BOW. UPON COMPLETION OF REMOVAL AND REPLACEMENT OF THE L2 SLIDE, FOUND THE NEW PART TO BE BAD FROM STOCK. RE-INSTALLED OLD PART BACK ON A/C, IAW J/C 26L00025012.Nov 7, 2020 · N165US · Airbus A321211 · Escape SlideSDR AALA202006159022Structure · delaminatedAIRCRAFT IN RON VISIT: L/H FWD NLG DOOR UPPER FWD CORNER HAS EXPOSED COMPODSITE/SLIGHT DELAMINATION. ACCOMPLISHED REPAIR INSTRUCTION IAW EA 306599.Jun 13, 2020 · N165US · Airbus A321211 · Landing Gear DoorsSDR AALA2020010639003Smoke Detector · false activationAIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE ECAM CAME ON FOR 5 SECONDS THEN EXTINGUISHED. LAVATORIES CHECKED WITH NO EVIDENCE OF SMOKE. ***SUPPLEMENTAL TO UPDATE SECTION 4 AND SECTION 5. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK.*** (CLOSED)Jan 2, 2020 · N165US · Airbus A321211 · Smoke DetectionSDR AALA201909199016Lubrication Unit · low pressureAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO DEN ON ACCOUNT OF APU SHUTDOWN WITH 1 GENERATOR ON PLACARD. EMERGENCY WAS DECLARED. MAINTENANCE REPLACED OIL LUBE MODULE IAW AMM 49-91-45, LEAK CHECK AND OPS CHECK NORMAL.Sep 18, 2019 · N165US · Airbus A321211 · APU Oil SystemSDR AALA201909179006Gcu · failedAIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO BNA ON ACCOUNT OF APU SHUT DOWN AND NUMBER TWO GENERATOR ON PLACARD. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE GCU IAW AMM 24-22-34. OPS CHECK OK. REMOVED AND REPLACED LOW OIL PRESSURE SSep 16, 2019 · N165US · Airbus A321211 · AC RegulatorSDR AALA201909189019Pressure Switch · unreliableAIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO BNA ON ACCOUNT OF APU SHUT DOWN AND NUMBER TWO GENERATOR ON PLACARD. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE GCU IAW AMM 24-22-34. OPS CHECK OK. REMOVED AND REPLACED LOW OIL PRESSURE SSep 16, 2019 · N165US · Airbus A321211 · APU Oil SystemSDR AALA201903049026Battery · failedJUMPSEAT AT THE R4 DOOR, FLASHLIGHT LED STOPPED FLASHING. MAINTENANCE REPLACED BATTERY, PERFORMED SATISFACTORY OPERATIONAL CHECK.Mar 1, 2019 · N165US · Airbus A321211 · Emergency EquipmentSDR AALA2019020439009Windshield · crackedCRACKED FIRST OFFICERS WINDSHIELD. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDSHIELD IAW AMM 56-11-11-400-001-A.Feb 2, 2019 · N165US · Airbus A321211 · Flight Compartment WindowsSDR AALA2018122769023Handle · crackedFOUND THE HANDLE FOR THE SLIDING WINDOW CAPTAIN SIDE IN THE COCKPIT CRACKED. REPLACED THE HANDLE IAW AMM 56-12-12-400-003-A, AND AMM 56-12-11-400-001-A. PERFORMED AN OPERATIONAL CHECK.Dec 21, 2018 · N165US · Airbus A321211 · Flight Compartment WindowsSDR AALA201812269001Shear Plate · crackedCRACKED SHEAR PLATE, STRINGER 23R BETWEEN FRAMES 69 TO 70 IN THE AFT GALLEY. REPLACED THE SHEAR PLATE IAW SRM 51-42-11, DRAWINGS D53471124, AND 517211.Dec 20, 2018 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201812209004Shear Plate · crackedA CRACK WAS FOUND ON THE SHEAR PLATE BETWEEN FRAMES 69 TO 70, STRINGER 23L IN THE AFT GALLEY. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DRAWING D53471124.Dec 19, 2018 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201812199027Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD THRUST REVERSER, AFT ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 2. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 18, 2018 · N165US · Airbus A321211 · Nacelle/Pylon Miscellaneous StructureSDR AALA201812199026Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUT BOARD THRUST REVERSER, CENTER ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 2. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 18, 2018 · N165US · Airbus A321211 · Nacelle/Pylon Miscellaneous StructureSDR AALA201812199025Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON OUT BOARD THRUST REVERSER, AFT ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 2. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 18, 2018 · N165US · Airbus A321211 · Nacelle/Pylon Miscellaneous StructureSDR AALA2018121890005Handle · crackedTHE THE FIRST OFFICER`S SLIDING WINDOW HANDLE WAS CRACKED. REPLACED THE HANDLE IAW AMM 56-12-12-400-003-A, AND AMM 56-12-11-400-001-A.Dec 16, 2018 · N165US · Airbus A321211 · Flight Compartment WindowsSDR AALA201812129026Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD THRUST REVERSER, AFT ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 2. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 11, 2018 · N165US · Airbus A321211 · Engine Thrust ReverserSDR AALA201812129025Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON OUT BOARD THRUST REVERSER, AFT ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 2. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 11, 2018 · N165US · Airbus A321211 · Engine Thrust ReverserSDR AALA201812129008Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON OUT BOARD THRUST REVERSER, FORWARD ATTACHMENT POINT HINGE FITTING BEARING BORE WORN AT PYLON RIB 1. REPLACED HINGE FITTING PER AMM 54-57-17-400-000-003-A.Dec 11, 2018 · N165US · Airbus A321211 · Engine Thrust ReverserSDR AALA201812129016Hose · tornAIRCRAFT WAS IN BASE MAINTENANCE. TORN PASSENGER CREW DOOR 831 FLEXIBLE CONTROL HOSE AT FWD GALLEY AREA. REPLACED FLEXIBLE CONTROL HOSE PER AMM 52-11-22-400-001-A STEP 4B THRU 4C.Dec 11, 2018 · N165US · Airbus A321211 · Passenger/Crew DoorsSDR AALA201812129010Floor Panel · delaminatedFORWARD GALLEY FLOOR PANEL 232DF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW TC 26C22053014.Dec 11, 2018 · N165US · Airbus A321211 · Fuselage Floor PanelSDR AALA201812129009Floor Panel · corrodedCORROSION FOUND ON THE AFT GALLEY FLOOR PANEL 261AG. REPLACED THE FLOOR PANEL IAW TC 26C2605309.Dec 11, 2018 · N165US · Airbus A321211 · Fuselage Floor PanelSDR AALA201812129024Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT PRESSURE BULKHEAD AFT FACE HAS SUPPORT ANGLE CRACKED AT FR 46 AND S38L. REPLACED SUPPORT ANGLE PER SRM 51-72-11.Dec 8, 2018 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201812269004Skin · corrodedCORROSION FOUND ON THE SKIN BETWEEN RIBS 5 - 6 ON THE LEFT WING. REPAIRED THE SKIN IAW EA 105103A.Dec 4, 2018 · N165US · Airbus A321211 · Wing, Plate/SkinSDR AALA201812109047Hinge Arm · wornRIGHT ELEVATOR NR 3 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209046Hinge Arm · wornRIGHT ELEVATOR NR 4 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209045Hinge Arm · wornRIGHT ELEVATOR NR 6 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209044Hinge Arm · wornLEFT ELEVATOR NR 6 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209043Hinge Arm · wornLEFT ELEVATOR NR 1 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209042Hinge Arm · wornLEFT ELEVATOR NR 5 HINGE ARM WAS WORN AND HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018121209041Hinge Arm · wornLEFT ELEVATOR NR 4 HINGE ARM WAS WORN AND HAS EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-002-A.Nov 30, 2018 · N165US · Airbus A321211 · Elevator StructureSDR AALA2018122769002Skin · damagedDURING CURRENT 3S CHECK, WEAR DAMAGE WAS FOUND ON THE TOP SKIN OF THE LT SLAT NR 2. REPAIRED THE SLAT AREA TRACK #6 ON LEFT HAND WING, TOP SKIN LOWER SURFACE PER EA #287661.Nov 26, 2018 · N165US · Airbus A321211 · Leading Edge DevicesSDR AALA2018121219001Bolt · wornRIGHT WING NR 5 SLAT, NR 11 SLAT TRACK ATTACHMENT BOLT HAD WORN THREADS. REPLACED THE BOLT IAW AMM 27-84-67-400-002-A.Nov 22, 2018 · N165US · Airbus A321211 · Leading Edge DevicesSDR AALA2018121209039Bolt · corrodedCORROSION ON THE RIGHT WING NR 9 SLAT TRACK FORWARD LOWER ATTACHMENT BOLT. REPLACED THE BOLT IAW AMM 27-84-66.Nov 22, 2018 · N165US · Airbus A321211 · Leading Edge DevicesSDR AALA201812109034Bolt · corrodedCORROSION ON THE RT WING NR 11 SLAT TRACK UPPER ATTACHMENT BOLT. REPLACED THE BOLT IAW AMM 27-84-67.Nov 22, 2018 · N165US · Airbus A321211 · Leading Edge DevicesSDR AALA2018121989054Stringer · corrodedSTRINGER 41R HAD CORROSION BETWEEN FRAMES 60 & 64, IN THE BULK CARGO BAY. REPLACED THE STRINGER IAW SRM 51-72-11, AND DRAWING D53474324.Nov 19, 2018 · N165US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA201812199006Skin · damagedTRAPPED WATER INDICATION FOUND ON THE LEFT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL. 7.75 INCHES INBD FROM LIGHTNING STRIP 3, AND 4.15 INCHES FROM THE TRAILING EDGE. REPAIRED THE ELEVATOR SKIN IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812199005Skin · damagedTRAPPED WATER INDICATION FOUND ON THE LEFT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL. 10 INCHES OTBD FROM RIB 1, AND 4.5 INCHES FROM TRAILING EDGE. REPAIRED THE ELEVATOR SKIN IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2018121989057Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR, HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL. 1.5 INCH OTBD, RIB 1, AND 4 INCH FROM TRAILING EDGE. REPAIRED THE SKIN PANEL IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA2018121989055Skin · damagedTRAPPED WATER INDICATION ON THE LT ELEVATOR, HONEYCOMB CORE STRUCTURE SKIN. 16 INCH OTBD FROM LIGHTNING STRIP 1, AND 4 INCHES FROM TRAILING EDGE. REPAIRED THE ELEVATOR SKIN IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812199009Skin · damagedTRAPPED WATER INDICATION FOUND ON THE LEFT ELEVATOR, HONEYCOMB CORE STRUCTURE, UPPER SKIN PANEL. 1.5 INCHES FROM ELEVATOR RIB 3, AND 4 INCHES FROM TRAILING EDGE. REPAIRED THE LEFT ELEVATOR IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812199008Skin · damagedTRAPPED WATER INDICATION FOUND ON THE RIGHT ELEVATOR HONEYCOMB CORE STRUCTURE, UPPER SKIN PANEL. 21 INCHES INBOARD FROM RIB 4, AND 15 INCHES FROM THE TRAILING EDGE. REPAIRED THE ELEVATOR IAW SRM 55-21-11-300-005.Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812199007Skin · damagedTRAPPED WATER INDICATION FOUND ON THE RIGHT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL. 20.5 INCHES INBOARD FROM RIB 4 AND 12 INCHES FROM LEADING EDGE. REPAIRED THE RT ELEVATOR IAW SRM 55-21-11-300-005Nov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812179020Skin · saturatedAIRCRAFT WAS IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR AT HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL LOCATED 4.0 INCH OUTBOARD FROM ELEVATOR RIB 4 AND 4.250 IN FROM TRAILING EDGE ON LEFT HAND HORIZONTAL STABILIZER. REPAIRED ELEVATOR UPPER SKIN PNov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/SkinSDR AALA201812179019Elevator · saturatedAIRCRAFT WAS IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR AT HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL LOCATED 5.500 INCH OUTBOARD FROM ELEVATOR RIB 5 AND 4.0 INCH FROM TRAILING EDGE ON LEFT HAND HORIZONTAL STABILIZER. REPAIRED ELEVATOR UPPER SKINNov 14, 2018 · N165US · Airbus A321211 · Elevator, Plate/Skin
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