Airbus A321-211

Service difficulty reports · 12,330

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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 aircraft_model_key = 'A321211'
  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 AALA201908169067Shear Plate · crackedAIRCRAFT IN BASE VISIT: CRACK SHEAR PLATE STR 23 L BTW FR 69 TO FR 70 AT AFT GALLEY AREA (1EA), (L=0.792"). REPLACED SHEAR PLATE STR 23L BTW FR69 TO FR70 AT AFT GALLEY AREA IAW SRM A321 51-42-11, SRM A321 51-72-11 AND DRAWING #D53474180.Jul 10, 2019 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA2019081589053Bolt · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING #2 SPOILER ACTUATOR STOP BOLT WORN. REPLACED STOP BOLT PER SRM 57-70-00.Jul 10, 2019 · N180US · Airbus A321211 · SpoilersSDR AALA2019081589051Bolt · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #3 SPOILER ACTUATOR STOP BOLT WORN. REPLACED STOP BOLT PER SRM 57-70-00.Jul 10, 2019 · N180US · Airbus A321211 · SpoilersSDR AALA2019081589050Bolt · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING #4 SPOILER ACTUATOR STOP BOLT WORN. REPLACED STOP BOLT PER SRM 57-70-00.Jul 10, 2019 · N180US · Airbus A321211 · SpoilersSDR AALA2019081589046Bolt · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING #3 SPOILER ACTUATOR STOP BOLT WORN. REPLACED STOP BOLT PER SRM 57-70-00.Jul 10, 2019 · N180US · Airbus A321211 · SpoilersSDR AALA20190815047Bolt · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #2 SPOILER ACTUATOR STOP BOLT WORN. REPLACED STOP BOLT PER SRM 57-70-00.Jul 10, 2019 · N180US · Airbus A321211 · SpoilersSDR AALA201907259010Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.Jul 10, 2019 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201907229017Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD RIGHT HAND LOWER CONTINUITY FITTING CRACKED, REPLACED CONTINUITY FITTING PER EA 296093.Jul 10, 2019 · N192UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201907229016Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD LEFT HAND LOWER CONTINUITY FITTING CRACKED, REPLACED CONTINUITY FITTING PER EA 296093.Jul 10, 2019 · N192UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR DALA2019071004164Door · damagedRAMP AGENT REPORTS 4L DOOR DAMAGE ON THE BOTTOM OF DOOR, REPAIR COMPLETE PER A321 SRM 52-10-00-300-005.Jul 10, 2019 · N344DN · Airbus A321211 · Passenger/Crew DoorsSDR AALA201907119022Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR SHEAR PLATE CRACKED BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.Jul 10, 2019 · N157UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA2019081489063Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT FR 35.2 AND S41R. REPAIRED STRINGER PER EA 296153.Jul 9, 2019 · N180US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA2019081489057Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT FR 35.3 AND S40R. REPAIRED STRINGER PER EA 296152.Jul 9, 2019 · N180US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA20190815064Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT FR 53.3 AND S41R. REPAIRED STRINGER PER EA 296153.Jul 9, 2019 · N180US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA2019081489066Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT FR 35.5 AND S41R. REPAIRED STRINGER PER EA 296153.Jul 9, 2019 · N180US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR AALA201909049018Frame · crackedAIRCRAFT IN BASE MAINTNENANCE:CRACKED LEFT HAND FRAME AT FR 66 AND DOOR STOP 1. REPAIRED FRAME PER EA 296132.Jul 8, 2019 · N182UW · Airbus A321211 · Fuselage Main, FrameSDR AALA201908169074Intercostal · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON INTERCOSTAL FRAME 16 LH UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP FITTING 7 AT FWD GALLEY AREA (2 EA), (D:0.310"). REPLACED INTERCOSTAL FRAME 16 LH AT LEVEL OF DOOR STOP FITTING #7 IAW A321 SRM 51-72-11 AND DWJul 8, 2019 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201908169075Intercostal · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON INTERCOSTAL FRAME 16 RH UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP FITTING 7 AT FWD GALLEY AREA (2 EA), (CRACK D=0.330). REPLACED INTERCOSTAL FRAME 16 RH AT LEVEL OF DOOR STOP FITTING #7 IAW A321 SRM 51-72-11 AJul 8, 2019 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201908169076Intercostal · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON INTERCOSTAL FRAME 16 RH LOWER INBOARD HOLE AT LEVEL DOOR STOP 1 AT FWD GALLEY AREA (1 EA), (D=0.265"). REPLACED INTERCOSTAL FRAME 16 RH AT LEVEL DOOR STEP 1 AT FWD GALLEY AREA IAW A321 SRM 51-72-11 AND DWG# D53112300Jul 8, 2019 · N182UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201907099003Wire Harness · damagedAIRCRAFT WAS GROUNDED: EMERENCY EXIT LIGHT AT SEAT ROW 1 A AND C INOPERABLE, WIRING HARNESS DAMAGED. MAINTENANCE REPLACED WIRE HARNESS PER AMM 33-51-00.Jul 8, 2019 · N193UW · Airbus A321211 · Light System WiringSDR CA190708009Sensor · false indication(CAN) PILOTS HAD A WARNING FOR HOT BRAKES AND NOTICED THE BRAKE TEMPERATURE OF 995C ON BRAKE #3 IN FLIGHT. PILOTS FOLLOWED THE QRH WHICH WAS FOR `WHEEL TIRE DAMAGE SUSPECTED`. AIRCRAFT HAD TO DECLARE AN EMERGENCY FOR THE LANDING JUST IN CASE. LANDING WAS NORMAJul 7, 2019 · Airbus A321211 · Landing Gear Brake SystemSDR AALA201909069019Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE SKIN LOWER SURFACE BETWEEN RIB 7 AND RIB 9. REPAIRED SKIN PER EA 296664.Jul 7, 2019 · N182UW · Airbus A321211 · Wing, Plate/SkinSDR AALA201909049019Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE SKIN PANEL TRAILING EDGE AREA AT WS 5512 AND RIB 10. REPAIRED SKIN PANEL PER EA 296662.Jul 7, 2019 · N182UW · Airbus A321211 · Wing, Plate/SkinSDR AALA2019082989054Skin · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR LOWER SURFACE SKIN HAS TRAPPED WATER INDICATION BETWEEN RIB 6 AND RIB 7, 88" FROM INBOARD END AND 4.5" FROM THE TRAILING EDGE. REPAIRED ELEVATOR SKIN PER SRM 55-21-11-300-005.Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA2019082989053Skin · damagedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR LOWER SURFACE SKIN HAS TRAPPED WATER INDICATION BETWEEN RIB 6 AND RIB 7, 94" FROM INBOARD END AND 5" FROM THE TRAILING EDGE. REPAIRED ELEVATOR SKIN PER SRM 55-21-11-300-005.Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908239021Skin · damagedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED 77.5 INCH OUTBD FROM ELEVATOR RIB 5 AND 5.5 INCH FROM T/E. SIZE L=2.5 INCH X W=2.0 INCH APPROX. ON RH HORIZONTAL STABILIZER (1 EA), (L=2.32", W=1.93"Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908239023Skin · damagedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED 48.5 INCH OUTBD FROM ELEVATOR RIB 5 AND 3.0 INCH FROM T/E. SIZE IS L=3.0 INCH X W=2.5 INCH APPROX. ON LH HORIZONTAL STABILIZER (1 EA), (L=2.95", W=2.Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908239024Skin · damagedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED AT 20.5 INCH OUTBD FROM ELEVATOR RIB 5 AND 3.5 INCH FROM T/E. SIZE IS L=3.0 INCH X W=2.5 INCH APPROX. ON LH HORIZONTAL STABILIZER (1 EA), (L=2.75" W=Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908239025Skin · damagedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED 1.5 INCH INBD FROM ELEVATOR RIB 4 AND 4 INCH FROM T/E . SIZE IS L=3.0 INCH X W=2.0 INCH APPROX. ON RH HORIZONTAL STABILIZER (1 EA), (L=3.08" W=2.53" Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908169078Skin · debondedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED 41.0 INCH OUTBD FROM ELEVATOR RIB 5 AND 3.0 INCH FROM T/E. SIZE IS L=2.5 INCH X W=2.0 INCH APPROX ON LH HORIZONTAL STABILIZER (1 EA), (L=2.52", W=2.1Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA201908169079Skin · debondedAIRCRAFT IN BASE VISIT: TRAPPED WATER INDICATION ON ELEVATOR HONEYCOMB CORE STRUCTURE LOWER SKIN PANEL LOCATED 86.0 INCH OUTBD FROM ELEVATOR RIB 5 AND 4 INCH FROM T/E. SIZE IS L=3 INCH X W=1.5 INCH APPROX. ON RH HORIZONTAL STABILIZER (1 EA), (L=3.52", W=1.56" Jul 7, 2019 · N182UW · Airbus A321211 · Elevator, Plate/SkinSDR AALA20190815037Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #8 LOWER MIDDLE BOLT. REPLACED BOLT PER AMM 27-84-65.Jul 7, 2019 · N180US · Airbus A321211 · Leading Edge DevicesSDR AALA201907079018Connector · looseAIRCRAFT WAS GROUNDED: PILOT REPORTS SHORTLY AFTER 80K ON TAKE OFF, ECAM MSG ENG1 COMPRESSOR VANE ILLUMINATED. ECAM PROCEDURE AND FOLLOW UP ACTIONS COMPLETED. REST OF FLIGHT FLOWN WITH AUTO-THROTTLES OFF. MAINTENANCE ADJUSTED BLEED VALVE STOP MECHANISM IAW AMMJul 7, 2019 · N171US · Airbus A321211 · Engine Bleed Air System WiringSDR AALA201907089005Control Lever · stiffAIRCRAFT WAS GROUNDED: PILOT REPORTS FLAP HANDLE IS DIFFICULT TO MOVE BETWEEN SETTINGS, ESPECIALLY BETWEEN 1 AND 2. MAINTENANCE REMOVED AND REPLACED FLAP HANDLE LEVER CONTROL IAW AMM 27-51-43. NO FURTHER DEFECTS NOTED. OPS CHECK GOOD.Jul 7, 2019 · N186US · Airbus A321211 · Trailing Edge Flap Control SystemSDR AALA201907089016Unknown · malfunctionedAIRCRAFT WAS GROUNDED: PILOT DIVERTED TO MCI ON ACCOUNT OF #2 ENGINE NOT MAKING POWER. EMERGENCY WAS NOT DECLARED. MAINTENANCE REPORTS IAW TSM 77-00-00-810-861-A WITHIN LIMITS (1.6%0) WITH AN ENGINE MISMATCH WHICH IS TRUE FOR THIS AIRCRAFT.Jul 7, 2019 · N187US · Airbus A321211 · Engine (Turbine/Turboprop)SDR AALA201907159032Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY AT VERTICAL STABILIZER RIB 11. REPLACED HINGE FITTING PER AMM 55-36-41-400-001-A.Jul 6, 2019 · N181UW · Airbus A321211 · Rudder StructureSDR DALA2019070704163Cover · missingPDA PART DEPARTING AIRCRAFT 3067 LOG 5428765, DURING SERVICE CHECK FOUND 532CB INBOARD FLAP TRACK MOVABLE FAIRING PIVOT COVER MISSING, INSTALLED 532CB INBOARD FLAP FAIRING PIVOT COVER.Jul 6, 2019 · N367DN · Airbus A321211 · Trailing Edge FlapsSDR AALA201907089013Pressure Switch · failedAIRCRAFT WAS GROUNDED: PILOT DIVERTED TO CLT ON ACCOUNT OF ELECTRICAL ISSUE/LOSS OF APU. EMERGENCY WAS DECLARED. APU AUTO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED LOW OIL PRESSURE SWITCH, AND DE-OIL SOLENOID VALVE IAW AMM 49-91-49 , OPS CHECK GOOD. (SEE SDR Jul 6, 2019 · N183UW · Airbus A321211 · APU Oil SystemSDR AALA201907099020Solenoid Valve · unreliableAIRCRAFT WAS GROUNDED: PILOT DIVERTED TO CLT ON ACCOUNT OF ELECTRICAL ISSUE/LOSS OF APU. EMERGENCY WAS DECLARED. APU AUTO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED LOW OIL PRESSURE SWITCH, AND DE-OIL SOLENOID VALVE IAW AMM 49-91-49, OPS CHECK GOOD. (SEE SDR #Jul 6, 2019 · N183UW · Airbus A321211 · APU Oil SystemSDR AALA201907229020Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANEL 232DF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.Jul 5, 2019 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR AALA201907059002Light · inoperativeAIRCRAFT NOT GROUNDED: CABIN CEILING EMERGENCY LIGHT AT ROW 34 INOPERATIVE. REMOVED AND REPLACED CABIN CEILING EMERGENCY LIGHT ASSY IAW AMM33-51-11. OPS CHECK GOOD.Jul 5, 2019 · N152UW · Airbus A321211 · Emergency LightingSDR AALA201907059003Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.Jul 4, 2019 · N181UW · Airbus A321211 · Fuselage Floor PanelSDR AALA2019081589040Bolt · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #4 HINGE FITTING STOP BOLT WORN. REPLACED STOP BOLT PER SRM 55-26-41.Jul 3, 2019 · N180US · Airbus A321211 · Elevator StructureSDR AALA20190815036Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT DOOR CUT OUT CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-72-11.Jul 3, 2019 · N180US · Airbus A321211 · Fuselage Main, StructureSDR AALA201907119015Battery · dischargedAIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CONDITION LED DID NOT ILLUMINATE DURING PERIODIC SERVICE CHECK, BATTERY DISCHARGED. REPLACED FLASHLIGHT BATTERY PER CMM 25-60-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Jul 3, 2019 · N155UW · Airbus A321211 · Emergency EquipmentSDR AALA201907049004Bleed Valve · malfunctionedAIRCRAFT WAS GROUNDED: REJECT TAKE OFF. REMOVED AND REPLACED E1 TRANS BLEED VALVE IAW AMM 75-26-10 OPS AND LK CHK.Jul 3, 2019 · N199UW · Airbus A321211 · Compressor Bleed ValveSDR AALA201907119021Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR SHEAR PLATE CRACKED AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.Jul 2, 2019 · N157UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201907089021Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.Jul 2, 2019 · N157UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA201907039008Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR 2R DOOR ASSIST BOTTLE PRESSURE WAS LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-22-00.Jul 2, 2019 · N187US · Airbus A321211 · Emergency ExitsSDR CA190703010Engine · malfunctioned(CAN) CREW REPORTED A LOW-SPEED REJECTED TAKE OFF. APPROX 60 KTS DURING POWER UP ON RWY 23. NUMBER 1 ENGINE.TWO LOUD BANGS HEARD.ECAM MSG NB 1 ENG STALL. RETURN TO GATE. (TC# 20190703010)Jul 1, 2019 · Airbus A321211 · Engine (Turbine/Turboprop)
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