Airbus A320-211

Service difficulty reports · 5,271

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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 DALA14033133221Shear Tie · corrodedCORROSION ON FWD CARGO COMPARTMENT SHEAR TIE FRAME 31 BETWEEN S40-41R. REPLACED SHEAR TIE IAW SRM A320 51-72-11 AND DWG D53231582.May 30, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14033123221Shear Tie · corrodedCORROSION ON FWD CARGO COMPARTMENT SHEAR TIE OF FR33 BETWEEN S41-42R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231582.May 30, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14032543221Floor Support · brokenDURING INSPECTION, FOUND BROKEN FLOOR SUPPORT Y254 BETWEEN FRAMES 24 - 28. PERFORMED PERMANENT REPAIR IAW SRM 53-00-14, PARA 4.G FIG 207 SHEET 1 AND DWG D53231346, D53110876.May 29, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14032533221Floor Support · brokenDURING INSPECTION, FOUND BROKEN FLOOR SUPPORT -Y254 BETWEEN FRAMES 24-28. PERFORMED PERMANENT REPAIR IAW SRM 53-00-14, PARA 4.G, FIGURE 207, SHEET 1 AND DWGS D53231346.May 29, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14032483221Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO BAY SHEAR TIE OF FRAME 26 BETWEEN S41-42L. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231712.May 28, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14032473221Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE OF FRAME 27 BETWEEN S43-44R, , REPLACED SHEAR TIE LOCATED FR.27 BETWEEN STR 43R TO STR 43L IAW SRM A320 51-72-11 AND DWG D53231712.May 28, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14032463221Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE OF FR28 BETWEEN STR41R TO STR42R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.May 28, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14032443221Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 - 23 Y-189. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.May 27, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14032103221Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED FWD PAX CABIN AT FRAME 20, Y-1732. REPLACED THE WEB BETWEEN FRAMES 20-24 IAW SRM 51-72-11 AND DWG D53114392.May 26, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140523001Line · leaking(CAN) ON GEAR RETRACTION AFTER DEPARTURE, CREW ADVISED THAT THE YELLOW HYDRAULIC SYSTEM RESERVOIR LEVEL WAS INDICATING LOW. FLIGHT RETURNED TO DEPARTURE, DECLARED AN EMERGENCY WITH ATC. FOUND YELLOW SYSTEM EDP PRESSURE LINE LEAKING. YELLOW SYSTEM EDP PRESSURMay 22, 2014 · Airbus A320211 · Hydraulic System, MainSDR DALA14032113217Light · damagedF/A FOUND EMERGENCY FLOOR LIGHTING DAMAGED AND INOPERATIVE AT SEAT 17C. MANTENANCE REPLACED EMERGENCY FLOOR LIGHTNING AT 17C AND FUNCTIONAL CHECKED NORMAL.May 22, 2014 · N317US · Airbus A320211 · Emergency LightingSDR DALA14032013212Battery Pack · no testDURING SERVICE CHECK, EMERGENCY LIGHTS TEST FAILED. R & R BATTERY PACK AT LT OVERWING EXIT AND TESTED IAW AMM 33-51.May 22, 2014 · N312US · Airbus A320211 · Emergency LightingSDR CA140520003B-Nut · loose(CAN) THE ACFT ENCOUNTERED A YELLOW HYDRAULIC SYS PRESSURE MESSAGE DURING CRUISE AFTER DEPARTURE. AS A PRECAUTION, THE FLIGHT CREW DECLARED A PAN PAN FOR PRIORITY WITH ATC. ONCE STABILIZED, THE FLIGHT CREW IN CONJUNCTION WITH MAINTENENCE AND FLIGHT DISPATCH,May 16, 2014 · Airbus A320211 · Hydraulic System, MainSDR CA140515001Brake · overheated(CAN) CREW REPORTED THEY RETRACTED LANDING GEAR AT 20 KTS ABOVE NORMAL. THEY REPORTED A DEPARTURE PROBLEM WITH HOT BRAKES. IN CONTINUING ACTIONS STARTED IN THE TROUBLESHOOTING SECTION, "TO BE C/OUT: REF J/C 05-51-12-200-001A. NOSE GEAR DOOR, WHEEL WELL, FLAMay 14, 2014 · Airbus A320211 · Landing Gear Brake SystemSDR DALA14030483226Connector · unsecureEMERGENCY LIGHTS INOPERATIVE ROWS 5, 6, & 7ABC. SEATED CONNECTOR. EMERGENCY LIGHTS CHECKED OK IAW AMM 33-50.May 14, 2014 · N326US · Airbus A320211 · Light System WiringSDR DALA14029573209Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT SIGN MID CABIN AND EXIT SIGN OVER WING INOPERATIVE. MAINTENANCE REPLACED EPSU 11WL AND BATTERY. FUNCTONAL CHECK WAS NORMAL.May 12, 2014 · N309US · Airbus A320211 · Emergency LightingSDR DALA14029563209Battery Pack · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS ON SEATS INOPERATIVE. MAINTENANCE REPLACED BATTERY AND FUNCTIONAL CHECKED NORMAL.May 12, 2014 · N309US · Airbus A320211 · Emergency LightingSDR DALA14029133216Wire · unsecureDURING NON-ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 4C. MAINTENANCE SECURED WIRE AND FUNCTIONAL CHECKED NORMAL.May 10, 2014 · N316US · Airbus A320211 · Light System WiringSDR DALA14028663211Battery Pack · inoperativeRT EMERGENCY LIGHT PACK BATTERY FAULTED. R & R BATTERY PACK IAW AMM 33-51. CHECKED NORMAL.May 5, 2014 · N311US · Airbus A320211 · Emergency LightingSDR CA140501002Autopilot Sys · failed(CAN) AFTER TAKEOFF, AUTO FLT YAW DAMPER 2 ECAM. ALSO, LOST FD2 AND HAVE NO AUTOPILOT 1 OR AUTOPILOT 2. CONVERSED WITH MOC FOR POSSIBLE RESETS. UNABLE RESET. ELECTED TO DIVERT AND WILL LAND APPROXIMATELY 5.0 TONES OVERWEIGHT. PERFORMED RESET OF FAC 1 AND 2Apr 30, 2014 · Airbus A320211 · Autopilot SystemSDR DALA14026203221Power Supply · faultedDURING NON ROUTINE CHECK, FOUND HARD FAULT AGAINST RT EMERGENCY EXIT EPSU 12WL. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECK WAS NORMAL.Apr 27, 2014 · N321US · Airbus A320211 · Emergency LightingSDR CA140414007Transmitter · malfunctioned(CAN) APPROXIMATELY .5 MILE BACK ON APPROACH, HAD A RED CAUTION ON THE ENGINE PAGE FOR LOW PRESSURE SHOWING 6 PSI AND HAD TO BRING ENGINE BACK TO IDLE. NO ECAM MESSAGE WAS DISPLAYED FOR THE CONDITION. ON TAXI-IN, AS A PRECAUTIONARY MEASURE, ENGINE WAS SHUTDOWApr 13, 2014 · Airbus A320211 · Engine Oil Indicating SystemSDR DALA14021943211Light · damagedDURING NON-ROUTINE CHECK, FOUND 16 ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT AND LAMP HOLDER AT SEAT 16 ABC AND FUNCTIONAL CHECKED NORMAL.Apr 9, 2014 · N311US · Airbus A320211 · Emergency LightingSDR CA140407006Headphones · shorted(CAN) TWO HEADSETS SHORTED OUT. VIDEO SYS AT 12AB "SURGED" AND CAUSED STATIC BLAST IN PASSENGER`S HEADPHONES, FRYING THEM BOTH . THE CREW DEFINITELY SMELLED A FAINT BURNING ODOR BUT SYS SEEMED TO WORK JUST FINE AND DID NOT REQUIRE A SHUTDOWN. CHECKED BOTHApr 5, 2014 · Airbus A320211 · Passenger Compartment EquipmentSDR DALA14021433231Light · inoperativeDURING A NON ROUTINE CHECK, FOUND AISLE EMERGENCY LIGHTS AT 13 AND 15 ABC INOPERATIVE. MAINTENANCE INSTALLED LIGHT ASSEMBLY AND FUNCTIONAL CHECKED NORMAL.Apr 5, 2014 · N331NW · Airbus A320211 · Emergency LightingSDR DALA14020703209Strap · crackedDURING INSPECTION, FOUND CRACK ON BUTT STRAP LOCATED IN T/E BETWEEN RIB 10 TO RIB 11 RT WING. REPLACED BUTT STRAP, LOCATED ON T/E BETWEEN RIB 10 TO RIB 11 RT WING IAW SRM 51-72-11 AND DWG D57541686.Apr 5, 2014 · N309US · Airbus A320211 · Wing Miscellaneous StructureSDR DALA14020693209Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED FR 79 AND BETWEEN STR 1-STR 2R UPPER FUSELAGE TAIL CONE AREA. PERFORMED PERMANENT REPAIR, FR 79 AND BETWEEN STR 1-STR 2R ON UPPER FUSELAGE TAIL CONE AREA IAW SRM 53-51-11, PAR 5B, FIG 203, SHEET 2.Apr 5, 2014 · N309US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14022713209Skin · scratchedDURING INSPECTION, FOUND SCRATCH ON EXTERNAL SKIN BETWEEN FRAMES 57A AND 4" ABOVE OF BEAM, 3 INCHES AFT CARGO DOOR. REPAIRED IAW SRM 52-32-00, PARA 4E, FIG 205, PAGES 229-234.Apr 4, 2014 · N309US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14019843217Terminal · looseDURING NON ROUTINE CHECK, FOUND IN-SEAT EMERGENCY LIGHT INOPERATIVE AT SEAT 17 ABC. MAINTENANCE SECURED LOOSE TERMINAL UNDER SEAT AND FUNCTIONAL CHECKED NORMAL.Mar 29, 2014 · N317US · Airbus A320211 · Light System WiringSDR DALA2016103108035Doubler · corrodedCORROSION WAS FOUND ON SKIN REINFORCEMENT DOUBLER AT RT NLG BAY ASSEMBLY. REPAIR ON INTERNAL FUSELAGE SKIN LOCATED BTW FR 17 TO FR 18 AND AT LEVEL STR 39R IN RT LATERAL AVIONIC COMPARTMENT AS PER ER/A N 524162-14 REV 0 REV A.Mar 22, 2014 · N319US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016041502928Panel · corrodedFOUND SEVERAL CORROSION SPOTS, 5 E/A ON DIFFERENT PARTS OF THE NLG BAY, SIDE PANEL. THE CORROSION REMOVED IAW SRM AND REPAIR ACCOMPLISHED IAW 522877-14, SECTION I.Mar 22, 2014 · N319US · Airbus A320211 · Fuselage Main, StructureSDR DALA14017853219Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 31R BETWEEN FRAMES 65-66 IN AFT BULKHEAD AREA. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.Mar 22, 2014 · N319US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14017863219Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND INOPERATIVE EPSU. MAINTENANCE REPLACED EPSU AFT LEFT EPSU AND FUNCTIONAL CHECKED NORMAL.Mar 21, 2014 · N319US · Airbus A320211 · Emergency LightingSDR DALA14017833220Web · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN WEB -Y1732 BETWEEN FRAMES 15 - 16. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.Mar 20, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14017823220Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE BETWEEN FRAMES 69-70, STRINGER 23R. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53470100, 1358880.Mar 20, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14017743220Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FRAMES 48 AND 49, S38R. REPLACED WEB IAW SRM 51-72-11 AND ER/A 523821-14.Mar 20, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA140320002Pump · leaking(CAN) DURING CRUISE THE CREW RECEIVED AN INDICATION THAT THE GREEN HYD SYS WAS LOSING FLUID & EVENTUALLY SHOWED A QTY OF ZERO. THE CREW PREPARED FOR A LANDING AS IF THE GREEN SYS WAS UNAVAILABLE. UPON EXTENDING THE LG THERE WAS AN INCREASE IN GREEN SYS FLUIDMar 19, 2014 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR CA140320001Transmitter · faulty(CAN) NUMBER 2 ENG OIL PRESS, FLUCTUATING 10 - 20 PSI, ENG NOT SHUT DOWN. EMER VEHICLES NOT REQUESTED. ENG 2 OIL PRESS TRANSMITTER REPLACED IAW AMM 79-33-15 PB 401. CHECKS SERVICE.Mar 19, 2014 · Airbus A320211 · Engine Oil PressureSDR DALA14017733220Support Rib · corrodedDURING INSPECTION, FOUND CORROSION ON OTBD FACE OF THE OUTER WING GEAR SUPPORT RIB 5. PERFORMED TYPICAL REPAIR ON SUPPORT RIB IAW SRM 57-26-13.Mar 19, 2014 · N320US · Airbus A320211 · Fuselage, Landing Gear Attach FittingsSDR DALA14017723220Stringer · corrodedAFTER REMOVED REFORCING PLATE IN BULK CARGO AREA PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND FOUND STRINGER 43L CORRODED FRAMES 64-65. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480030.Mar 19, 2014 · N320US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14017483220Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FRAMES 56 AND 57 STRINGER 38R. REPAIRED IAW ER/A N523815-14, REV.Mar 19, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14017473220Channel · corrodedDURING INSPECTION, FOUND CORROSION ALONG T/E CHANNEL UPPER AND LOWER SURFACE OF THE RIGHT AILERON. REPLACED T/E CHANNEL OF THE RT AILERON IAW SRM 51-72-11 AND DWG D57640033.Mar 19, 2014 · N320US · Airbus A320211 · AileronsSDR DALA14017463220Structure · crackedDURING INSPECTION, FOUND E/E HATCH DOOR 843 MULTIPLE CRACK INDICATIONS WERE FOUND IN BOTH INNER FRSEGMENTS. REPLACED BOTH SEGMENTS ANGLES, LOC ON E/E HATCH DOOR NR 843 IAW SRM 51-72-11 AND DWG D52279040.Mar 18, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14017453220Skin · corrodedDURING INSPECTION, FOUND CORROSION ON SKIN AT FRAME 70 AND BETWEEN STRINGERS 31 AND 32 RT. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FUSELAGE LOCATED AT FR 70 AND BETWEEN STRG 29R-STRG 32R REAR FUSELAGE IAW ENGINEERING REPAIR, EA 522873-14, REV, ORIGINAL.Mar 18, 2014 · N320US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14017273220Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN FLOOR SUPPORT -Y254 BETWEEN FRAMES 18-20. REPAIRED IAW ERA 523465-14 AND SRM 51-72-11, ERA REV ORIGINAL.Mar 18, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14017263220Angle · crackedDURING INSPECTION, SEVERAL CRACKS WERE FOUND IN BOTH SEGMENT ANGLES LOCATED BETWEEN BEAM 1&3. INTERNAL STRUCTURE E/E BAY DOOR. REPLACED ANGLES IAW SRM 51-72-11 AND DWG D52279010.Mar 18, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14017253220Angle · crackedDURING INSPECTION, FOUND SEVERAL CRACKS ON BOTH SEGMENT ANGLES LOCATION BETWEEN BEAM 1 & 3 OF INTERNAL STRUCTURE E/E HATCH DOOR 834. REPLACED BOTH SEGMENT ANGLES IAW SRM 51-72-11 AND DWG D52279010.Mar 18, 2014 · N320US · Airbus A320211 · Electrical/Electronic Compartment DoorsSDR DALA14017243220Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE BETWEEN FRAMES 69-70 AT S23L. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D534-74180.Mar 18, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14017233220Skin · gougedDURING INSPECTION, FOUND A GOUGE ON EXTERNAL SKIN AT FRAME 18+1 S23R UNDER SCUFF PLATE AREA. REPAIRED IAW EA 523473-14, REV ORIGINAL.Mar 18, 2014 · N320US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA14017223220Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE BETWEEN FRAMES 69 - 70 AT STRINGER 23L IN AFT PAX CABIN. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D534-74180.Mar 18, 2014 · N320US · Airbus A320211 · Fuselage Miscellaneous Structure
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