Airbus A320-211

Service difficulty reports · 5,271

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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 = 'A320211'
  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 DALA2014071104059Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1379.5 BETWEEN FRAMES 12 - 16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112825.Jul 10, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014071104057Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732 FRAME 20. REPLACED WEB FRAMES 20 - 24 IAW SRM 51-72-11 AND DWG D53114392 AND D53110920.Jul 10, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014071004013Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472040.Jul 9, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016081605986Skin · dentedDENT AFT OF GALLEY DOOR STRINGER 24 AFT OF FRAME 69. DENTJul 8, 2014 · N323US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2014070903986Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB -Y1732, FRAME 16. REPLACED WEB FRAMES 12 - 16 IAW 51-72-11 AND DWG D53114392.Jul 8, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070803941Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON DUMMY RAIL Y503.2 FRAMES 12 TO 16. REPLACED DUMMY RAIL IAW SRM 51-72-11, DRAWING D53112825 & D53110984.Jul 7, 2014 · N323US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014070803940Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON AFT CORNER FITTING AT FRAME 20 LOWER AREA THE L1 DOOR CUT OUT. REPLACED AFT CORNER FITTING IAW SRM 51-72-11 AND DRAWING D53112109.Jul 7, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070703899Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN FLOOR SUPPORT Y1292 BETWEEN FRAMES 16 - 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.Jul 7, 2014 · N336NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070703898Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472832.Jul 6, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070703897Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472040.Jul 6, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140714016Actuator · leaking(CAN) AIRCRAFT HAD A NR 2 ENGINE FUEL LEAK AT GATE WHILE BOARDING. PAX/CREW DEPLANED AND CRF CALLED TO THE GATE. APPROXIMATE SIZE OF THE LEAK WAS 8FT X 4 FT. RT ENG LT VSV ACTUATOR REPLACED IAW AMM 75-32-10-000-001-A AND AMM 75-32-10-400-001-A. CS FOR CORRECJul 5, 2014 · Airbus A320211 · Compressor Bleed ControlSDR DALA2014070603896Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D534-72040.Jul 5, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070603895Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y465 BETWEEN FRAMES 67+15 - 70. REPLACED FLOOR SUPPORT IAW SRM A-320 51-72-11 AND DWG D534-72040.Jul 5, 2014 · N323US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070703901Wire · pulledDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEATS 08C-23C INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM SPLICE AT EACH LOCATION. SPLICED WIRES BACK TOGETHER AND FUNCTIONAL CHECK WAS NORMAL.Jul 4, 2014 · N313US · Airbus A320211 · Light System WiringSDR CA140704005Seal · failed(CAN) DURING DESCENT, ACFT LOST IT`S YELLOW HYD SYSTEM AND DECLARED A PAN PAN. HYD PTU CHECK VALVE 3094GM FOUND LEAKING. SEAL REPLACED IAW AMM 29-13-15-560-050A.Jul 3, 2014 · Airbus A320211 · Hydraulic System, MainSDR CA140702002Line · failed(CAN) FLIGHT EXPERIENCED A GREEN HYDRAULIC FAILURE. CREW CONTINUED ON, WHILE SPEAKING TO DISPATCH AND MOC . TOW CREW WAS SET UP TO ASSIST GETTING ACFT OFF RWY. FLIGHT DECLARED A PAN PAN WITH ATC AND EMERGENCY EQUIPMENT WAS CALLED OUT. FLIGHT LANDED ON RWY 2Jul 1, 2014 · Airbus A320211 · Hydraulic System, MainSDR CA140702003Accumulator · defective(CAN) AIRCRAFT HAD A BLUE HYDRAULIC RESERVOIR SYS LOW PRESSURE INDICATION. FLIGHT CREW DECLARED "PAN PAN" FOR ARRIVAL. ACFT LANDED WITHOUT ISSUE, AND TAXIED TO THE GATE. BLUE SYSTEM HYD ACCUMULATOR REPLACED IAW AMM 29-12-42 PB401.Jun 30, 2014 · Airbus A320211 · Hydraulic Power Accumulator, MainSDR DALA2014070103843Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66 +5 - 70. REPLACED FLOOR SUPPORT IAW DWG D53472000 AND SRM 51-72-11.Jun 30, 2014 · N336NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140702008Control Unit · leaking(CAN) CREW RECEIVED A HYD Y RESERVIR LOW LEVEL, ECAM DURING CRUISE. THE ECAM AND QRH WERE ACTIONED. ATC ADVISED, NO EMERGENCY DECLARED. TSM 29-13-00-810-A CARRIED OUT. FOUND NR 2 ENG THRUST REVERSER HYD CONT UNIT LEAKING. AMM 29-00-00-280-006-A01 CAVITATIOJun 28, 2014 · Airbus A320211 · Engine Thrust ReverserSDR DALA2014062703811Window Frame · crackedDURING M-CHECK, A CRACK FOUND ON THE UPPER ATTACHMENT OF THE RT SLIDING WINDOW FRAME, IN HOLE NR 3 IAW ALI 53-11-35-PB6.Jun 26, 2014 · N330NW · Airbus A320211 · Flight Compartment WindowsSDR DALA2014062603783Stringer · corrodedDURING INSPECTION, FOUND CORRODED STRINGER 31R BETWEEN FRAMES 64 - 65 IN AFT CARGO BAY. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480505.Jun 25, 2014 · N330NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014062403721Floor Panel · corrodedDURING INSPECTION, FOUND CORROSION LOCATED AROUND OF FLOOR PANEL 231AF AT FWD GALLEY AREA. REPLACED FLOOR PANEL.Jun 23, 2014 · N330NW · Airbus A320211 · Fuselage Floor PanelSDR CA140702015Unknown · odor(CAN) APPROXIMATELY 2 HRS FROM DESTINATION A NOTICEABLE ELECTRICAL ODOR WAS DETECTED IN THE CABIN. MOC WAS NOTIFIED AND THEY ADVISED THAT THE IFE SYSTEM BE SHUTDOWN. CREW COMPLIED AND THE ODOR DISSIPATED. RAN RANDOM STATIC TEST 45 MINS AND PHYSICAL CHECK OF Jun 22, 2014 · Airbus A320211 · Air Distribution SystemSDR CA140623017Control Servo · failedCREW REPORTED UNUSUAL VIBRATION IN CLIMB AT FL190. THEY BACKED OFF ON SPEED AND PROBLEM DISAPPEARED. WHEN SPEED WAS INCREASED THE SAME PROBLEM RE-OCCURRED. CREW SUSPECTED FLIGHT CONTROL PROBLEMS AND ELECTED TO RETURN. CREW DECLARED A PAN PAN WITH ATC. ACFT LAJun 22, 2014 · Airbus A320211 · Rudder ActuatorSDR DALA2014062303683Connector · unsecureDURING NON ROUTINE CHECK, FOUND SEAT 16C WHITE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED LOOSE CONNECTION AT SEAT 16 AND FUNCTIONAL CHECK WAS NORMAL.Jun 22, 2014 · N326US · Airbus A320211 · Light System WiringSDR DALA2014062003657Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT IAW SRM 51-72-11, DWGS D53231568, AND D53230811.Jun 19, 2014 · N330NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014062003656Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT FR 33 BETWEEN S41-42R IAW SRM 51-72-11 AND DWG D53230514.Jun 19, 2014 · N330NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA14036503230Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 AND 21, Y-1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.Jun 18, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140618006Control Valve · failed(CAN) ON ARRIVAL FUELER NOTICED A TRAIL OF FUEL FROM THE NUMBER 1 ENGINE ALL THE WAY TO THE GATE. THE LEAK WAS CLEANED UP WITH ABSORBALL AND NO CFR WERE CALLED OUT...THE CREW DID AN ENGINE RUN TO HAVE THE FUEL LEAK FROM ENGINE AGAIN. ONCE AGAIN CLEANED BY FUEJun 17, 2014 · Airbus A320211 · Fuel Control/Turbine EnginesSDR DALA14036263230Profile · crackedDURING INSPECTION, FOUND CRACK ON LOAD TRASMITING PROFILE, RT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834. REPLACED TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036253230Profile · crackedDURING INSPECTION, FOUND CRACK ON LT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 844. REPLACED LT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036243230Profile · crackedDURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 844. REPLACED RT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036233230Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 AND 21 Y-765 . REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53112812.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036223230Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40R BETWEEN FRAMES 30 - 31 FWD CARGO BAY.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14036213230Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 40R BETWEEN FRAMES 32 TO 33 IN FWD CARGO BAY. REPLACED STRINGER 40R IAW SRM 51-72-11 AND DWG D53231568.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14036203230Profile · crackedDURING INSPECTION, FOUND CRACK ON LOAD TRANSMITTING PROFILE RT OF EMERGENCY EXIT HATCH 843. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, RT SIDE OF EMERGENCY HATCH 843 IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036193230Profile · crackedDURING INSPECTION, FOUND CRACK ON LOAD TRANSMITTING PROFILE LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 834 IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036183230Profile · crackedDURING INSPECTION, FOUND CRACK ON LT LOAD TRANSMITTING PROFILE OF EMERGENCY EXIT HATCH 843. REPLACED TRANSMITTING PROFILE, SEGMENT ANGLE, LT SIDE OF EMERGENCY EXIT HATCH 843 IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036173230Profile · crackedDURING INSPECTION, FOUND CRACK ON LOAD TRANSMITING PROFILE LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED TRANSMITING PROFILE, SEGMENT, LT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833 IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036163230Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER FITTING AFT POSITION LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED LOWER FITTING, TEE SECTION, LOCATED AT AFT POSITION ON EMERGENCY EXIT HATCHES NR 833 IAW SRM 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Emergency ExitsSDR DALA14036153230Profile · crackedDURING INSPECTION, FOUND CRACK ON LOAD TRANSMITING PROFILE RT SIDE LOCATED ON EMERGENCY EXIT HATCHES 833. REPLACED TRANSMITING PROFILE, SEGMENT, RT SIDE LOCATED ON EMERGENCY EXIT HATCHES NR 833 IAW SRM A320 51-72-11 AND DWG D52279010.Jun 17, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14036143221Door Frame · crackedDURING INSPECTION, ONE CRACK WAS FOUND AT LT AFT PASSENGER DOOR CUT-OUT AT FRAME 68 AND AT STRINGER 8L. REPAIRED IAW ERA 526355-14, SECT I. ERA 526355-14 SECTION I.Jun 17, 2014 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2017112808356Frame · corrodedCORROSION WAS FOUND ON FRAME 16, STRINGER 23R, CORROSION WAS REMOVED IAW SRM 53-11-12 AND ERA 522853 SECT. I.Jun 16, 2014 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA14036133230Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 39R BETWEEN FRAMES 30 & 31 INE FWD CARGO BAY. REPLACED STRINGER 39R IAW SRM 51-72-11 AND DWG D53231568.Jun 16, 2014 · N330NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14036123230Plate · corrodedDURING INSPECTION, CORROSION ON PLATE LOCATED AT STRINGER 43L BETWEEN FRAMES 28- 29 IN FWD CARGO BAY. REPLACED PLATE IAW 51-72-11 AND DWG D53230861.Jun 16, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140618002Wire Harness · failed(CAN) OCCURRENCE DESCRIPTION: TAXIING OUT FOR DEPARTURE, BEGAN TO RECEIVE INTERMITTENT LEFT LANDING GEAR POSITION INDICATOR RED LIGHT AND LGCIU 1 RED INDICATION ON WHEEL PAGE. AT FIRST INDICATIONS WERE OF 1-2 SEC DURATION AND TRANSIENT. ADVISED GROUND CONTROLJun 15, 2014 · Airbus A320211 · Landing Gear System WiringSDR DALA14035683230Skin · gougedDURING INSPECTION, FOUND GOUGE ON FUSELAGE EXTERNAL SKIN FRAME 25+3 BETWEEN S41-42L. REPAIRED SKIN IAW SRM 53-00-11 PARA 4.W, FIG 238.Jun 15, 2014 · N330NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14035673230Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FRAME 20. REPLACED AFT LOWER CORNER OF RT FWD PASSENGER/CREW DOOR CUT OUT IAW SRM 51-72-11 AND DWG D53112109.Jun 14, 2014 · N330NW · Airbus A320211 · Fuselage Main, StructureSDR DALA14035663230Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FRAMES 17 - 19. REPLACED CENTER FITTING OF FWD PAX CABIN ENTRY DOOR IAW SRM 51-72-11 AND DWG D53112198.Jun 14, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14035653230Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER R1 DOOR SILL. REPLACED DOOR SILL BETWEEN FRAMES 16 TO 20 IAW SRM 51-72-11 AND DWG D53110339.Jun 14, 2014 · N330NW · Airbus A320211 · Fuselage Miscellaneous Structure
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