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 DALA13039813217Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM Y254 IN FWD PAX CABIN . REPLACED FLOORBEAM IAW SRM A320 51-72-11 AND DWG D53112816 , D513110984 AND D53110900.Aug 17, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13039803217Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y465. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472000.Aug 16, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13039793217Clamp · corrodedDURING INSPECTION, FOUND CORROSION ON CLAMP RING OF THE ACCESS PANEL 540DB LT WING FUEL TANK SSI 572040. L=0.05", W=0.03", D=0.001 APPROX. REPLACED CLAMP RING THE ACCESS PANEL 540DB LT WING FUEL TANK IAW AMM 57-27-11-000-001-A. THE INSTALLATION IS DOCUMENTEDAug 16, 2013 · N317US · Airbus A320211 · Wing Miscellaneous StructureSDR DALA13039783217Clamp · corrodedDURING INSPECTION, FOUND CORROSION ON CLAMP RING THE ACCESS PANEL 540CB LT WING FUEL TANK SSI 572040. L=0.05" W=0.03" D=0.001" APPROX. REPLACED CLAMP RING THE ACCESS PANEL 540CB LT WING FUEL TANK IAW AMM 57-27-11-000-001-A. THE INSTALLATION IS DOCUMENTED IN Aug 16, 2013 · N317US · Airbus A320211 · Wing Miscellaneous StructureSDR DALA13039773217Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 BETWEEN FR 66+5" AND FR 70. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472000.Aug 15, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13039763217Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM Y765 IN AFT CABIN BETWEEN FR 66+5" AND FR 70. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472000.Aug 15, 2013 · N317US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13039413217Rail · corrodedDURING INSPECTION, FOUND CORROSION ON RAIL DUMMY Y503.2 LOCATED AT LEVEL OF FR 16 FWD PAX CABIN, FLOOR STRUCTURE LT SIDE L=1" W=0.5" AND D=0.002" APPROX. REPLACED RAIL DUMMY Y503.2 LOCATED AT LEVEL OF FR 16 FWD PAX CABIN FLOOR STRUCTURE LT SIDE IAW SRM 51-72-Aug 14, 2013 · N317US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13038903216Light · damagedDURING NON ROUTINE CHECK, FOUND EMERGENCY SEAT MOUNTED LIGHT DAMAGED AND INOPERATIVE. MX REPLACED LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL.Aug 11, 2013 · N316US · Airbus A320211 · Emergency LightingSDR CA130808006Check Valve · cracked(CAN) DURING ROUTINE "C" CHECK MAINTENANCE, THE APU BLEED CHECK VALVE WAS FOUND TO HAVE A 1" CRACK IN THE FLAPPER NEAR THE HINGE LINE. THE CRACK WAS VERIFIED BY DYE PENETRANT INSPECTION. THE CHECK VALVE WAS REPLACED.Aug 7, 2013 · Airbus A320211 · Pneumatic Distribution SystemSDR CA130802002Pulley · sheared(CAN) DURING ROUTINE C-CHECK MAINTENANCE, THE RT MLG FREE FALL CABLE PULLEY WAS FOUND WITH THE SHEAR PIN SHEARED. REF IPC 32-33-03-32, ITEM 40. THE PIN WAS REPLACED IAW AMM 32-33-17-350-001A.Jul 31, 2013 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA130731003Line · failed(CAN) CREW REPORTED A BLUE HYDRAULIC SYSTEM LOSS, FLIGHT CONTINUED TO DESTINATION. FLEX LINE, PN AE2464051J0225. REPLACED IAW AMM 20-23-00 AND 29-00-00-870-009-A.Jul 30, 2013 · Airbus A320211 · Hydraulic System, MainSDR CA130723005Uplock · overserviced(CAN) FLIGHT DEPARTED AND WAS UNABLE TO STOW AND LOCK LT MAIN GEAR. CYCLED GEAR A COUPLE OF TIMES TO NO AVAIL. DIVERTED BACK, HAD OVERWEIGHT LANDING ROUGHLY 69.1 BOTH RT AND LT MLG UPLOCKS CLEANED OF COAGULATED GREASE. GEAR SWINGS CARRIED OUT NO FURTHER FAJul 23, 2013 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA130722005Line · failed(CAN) WHEN THE CREW EXTENDED THE LANDING GEAR THE REPORTED A GREEN HYDRAULIC SYS LOW PRESSURE CONDITION. CHECK LIST FOLLOWED AND LANDING CARRIED OUT. EMERGENCY DECLARED WITH ATC, DID NOT DECLARE MAYDAY OR PANPAN. LT MLG ACTUATOR AFT HYDRAULIC LINE REPLACED IJul 20, 2013 · Airbus A320211 · Hydraulic System, MainSDR CA130719002Uplock · overserviced(CAN) OVERWEIGHT LANDING DUE TO AIRBORNE RETURN DUE TO GEAR UP LOCK INDICATION. UPON RAISING GEAR AFTER T/O, L/G GEAR NOT UPLOCKED ON ECAM. R/H MAIN AND GEAR DOORS INDICATED NOT UPLOCKED. SUBSEQUENT CYCLING OF GEAR AS PER ECAM WITH SAME RESULT FOUND R/H MLG UJul 18, 2013 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR DALA13035493226Battery Pack · no testON SERVICE CHECK, FOUND RT EMERGENCY BATTERY PACK FAIL ON LIGHT TEST. REPLACED 12WL EMERGENCY BATTERY AMM 33-51-38. OK FOR SERVICE.Jul 18, 2013 · N326US · Airbus A320211 · Emergency LightingSDR DALA13035083213Battery Pack · failedDURING CRUISE EMERGENCY EXIT LIGHTS AND THE EMERGENCY AISLE LIGHTING WERE FLASHING ERRATICALLY ON AND OFF WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. MX REPLACED FWD LT EPSU AND BATTERY. FUNCTIONAL CHECKED NORMAL.Jul 12, 2013 · N313US · Airbus A320211 · Emergency LightingSDR CA130711003Motor · shorted(CAN) AIR RETURN DUE TO SMOKE IN THE COCKPIT, PAN PAN DECLARED. SKIN AIR INLET REMOVED IAW AMM 21-26-52, FOUND AIR INLET VALVE MOTOR SHORTED. AIR INLET ACTUATOR REPLACED IAW CMM 21-26-52.Jul 11, 2013 · Airbus A320211 · Air Distribution SystemSDR DALA13034043213Epsu · failedDURING NON ROUTINE CHECK, FOUND EPSU INTERNAL LOAD EMERGENCY LIGHT FAILED. MX REPLACED EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.Jul 8, 2013 · N313US · Airbus A320211 · Emergency LightingSDR CA130704001Connector · arced(CAN) DURING C-13 CHECK WHILE PERFORMING ROUTINE MAINTENANCE, NR 2 CENTER FUEL TANK CANISTER PUMP WAS FOUND TO HAVE BURNED/ARCING PIN AND SOCKET IN CONNECTORS 38QA AND 38QA-1. THE FUEL PUMP AND CONNECTOR ON ACFT SIDE WERE REPLACED.Jul 2, 2013 · Airbus A320211 · Fuel System WiringSDR DALA13033183227Power Supply · inoperativeDURING SERVICE CHECK, FOUND CIDS FAULT AT AFT LT UNIT, MANY ESCAPE PASSNGER LIGHTS INOPERATIVE. MX REPLACED 13WL EPSU AND OPS CHECKED NORMAL.Jul 1, 2013 · N327NW · Airbus A320211 · Emergency LightingSDR DALA13032713219Battery Pack · inoperativeDURING INSPECTION, FOUND EXT LOADS EMERGENCY RT MESSAGE ON SERVICE CHECK FOR EMERGENCY LIGHT TEST. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL. .Jun 30, 2013 · N319US · Airbus A320211 · Emergency LightingSDR DALA13032633218Profile · crackedDURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS CRACK. HFEC IAW NTM 51-10-08 PT6, CONFIRMED CRACK BY FASTENER HOLE. REPLACED PROFILE, PN D5227902620200, BATCH NR 0002155894 IAW SRM 51-42-11 & DWG NR D52279010.Jun 28, 2013 · N318US · Airbus A320211 · Emergency ExitsSDR DALA13032703226Wire · damagedDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 2AB. MX INSTALLED NEW SPLICE CONNECTOR AND OPS CHECK WAS NORMAL.Jun 28, 2013 · N326US · Airbus A320211 · Light System WiringSDR DALA13032693218Profile · crackedDURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER HOLES. HFEC IAW NTM 51-10-08, PT6, CONFIRMED CRACK AROUND FASTENERS. REPLACED PROFILE IAW SRM 51-42-11 & DWG D52279010.Jun 28, 2013 · N318US · Airbus A320211 · Emergency ExitsSDR DALA13032683218Attach Fitting · corrodedDURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LWR AFT LATCH HOOK ATTACH FITTING HAS CORROSION. REMOVED OLD FITTING IAW SRM 51-42-11. LOCATED AND DRILLED NEW LATCH HOOK FITTING, IAW SRM 51-44-11. INSTALLED NEW FITTING IAW SRM 51-42-11 AND DWG D5227904Jun 28, 2013 · N318US · Airbus A320211 · Emergency ExitsSDR DALA13032673218Plate · chafedDURING INSPECTION, FOUND LT NR 3 SLAT TRACK COVER PLATE CHAFING W/ SLAT T/E LWR SKIN. ACCOMPLISHED REPAIR IAW ER/A 494603-14MA, SECTION 1, PERMANENT REPAIR IDENTIFIED REPAIR AS PERMANENT & ENGINEERING APPROVED IAW PS 900-5-1, NR 4.Jun 28, 2013 · N318US · Airbus A320211 · Leading Edge DevicesSDR DALA13032653218Floor Support · crackedDURING INSPECTION, FOUND COCKPIT FLOOR SUPPORT RT SIDE FWD FR8 Y-1292, AROUND NUTPLATE SHEETMETAL CRACKED. ACCOMPLISHED REPAIR IAW ER/A 515379-14, REV ORIGINAL SECTION I PERMANENT REPAIR. IDENTIFIED REPAIR AS ENGINEERING APPROVED & PERMANENT IAW PS 900-5-1, Jun 27, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13031563217Wire · brokenDURING NON ROUTINE CHECK, FOUND ROW 10 EMERGENCY PATH LIGHTING OUT. FOUND WIRE BROKEN AT SPLICE. REPAIRED AND FUNCTIONAL CHECK WAS NORMALJun 25, 2013 · N317US · Airbus A320211 · Light System WiringSDR DALA13031543216Profile · crackedDURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITING PROFILE LOCATED AT INTERNAL STRUCTURE OF RT FWD EMERGENCY EXIT. REPLACED LT AND RT LOAD TRANSMITTING PROFILE INTERNAL STRUCTURE OF RT FWD EMERGENCY EXIT IAW SRM 51-72-11.Jun 25, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13031533218Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO BETWEEN FR 58-59, STR 44, FLOOR SUPPORT HAS SURFACE CORROSION. BLENDED CORROSION. BLENDED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS IAW SRM 53-41-14, REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13031523218Floor Panel · damagedMID CABIN, FLOOR PANEL 241AF FOUND ONE ELONGATED HOLE AND CRACKED. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A.Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13031513218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162CF DELAMINATED 21" X 15". AFT CARGO COMPARTMENT SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209.Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13031503218Floorbeam · corrodedDURING INSPECTION, FOUND AFT CARGO FLOORBEAM AT FR58, LT SIDE, FWD FACE HAS 2EA AREAS OF CORROSION. REMOVED FLOORBEAM AT FR 58 IAW SRM 51-42-11. NO ALLOWABLE LIMITS IN SRM. INSTALLED NEW FLOORBEAM IAW SRM 51-42-11.Jun 24, 2013 · N318US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13033173218Skin · damagedDURING INSPECTION, FOUND AFT LT PASSENGER DOOR EXTERNAL FROM LOWER EDGE TO ABOVE 16 INCHES SKIN HAS DENT. FOUND OUT OF LIMITS IAW SRM 52-10-00, DIAGRAM 103. CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-42-11 & SRM 52-10-00, FIG 2Jun 23, 2013 · N318US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13031493216Profile · crackedDURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITTING PROFILE LOCATED INTERNAL STRUCTURE OF RT AFT EMERGENCY EXIT 844 MEASURES ARE LT L=1" RT L=3" APPROX. REPLACED LT AND RT LOAD TRANSMITTING PROFILE LOC. INTERNAL STRUCTURE OF RT AFT EMERGENCY EXIT 84Jun 23, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13030913218Stringer · corrodedDURING INSPECTION, FOUND AFT CARGO COMPARTMENT BETWEEN FR56-FR57, STR 43L CORRODED. CLEANED AREA IAW AMM 12-21-12. CORROSION FOUND. NO LIMITS ESTABLISHED IAW SRM 53-41-13, FIG 101. REPAIRED DAMAGE STRINGER IAW SRM 53-00-13, FIG 201, STRINGER FABRICATED ON Jun 22, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13030893216Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 44 IN BULK CARGO COMPARTMENT BETWEEN FR 66 AND FR 67. REPAIRED IAW SRM 53-00-13.Jun 22, 2013 · N316US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13030883216Seal Bracket · corrodedDURING INSPECTION, FOUND CORROSION ON SEAL LOCATED UNDER INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA FWD CARGO. REPLACED SEAL LOCATED UNDER INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA FWD CARGO IAW SRM 51-72-11 AND DWG D53231668.Jun 22, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13032663218Stringer · damagedDURING INSPECTION, FOUND AFT CARGO AT FR 65, STR 43L HAS CORROSION. REMOVED CORROSION IAW SRM A320 51-74-00. NO ALLOWABLE DAMAGE FOUND ON SRM. PERFORMED STRINGER REPAIR IAW SRM 53-00-13, FIG 201, SHEET 2.Jun 21, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13030903218Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT BILGE AREA AT FR 28 STGR 41R -42R CLIP HAS CORROSION. REMOVED SHEAR CLIP IAW SRM 51-42-11. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. FABRICATED, LOCATED & DRILLED, TREATED AND PRIMED, APPLIED TOPCOAT, AND INSTALLED NEJun 21, 2013 · N318US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13030873216Crossbeam · bentDURING INSPECTION, FOUND BEND ON CROSSBEAM LOCATED IN FWD CARGO BAY FR 32 BETWEEN STR 37L TO STR 37R. REPLACED CROSSBEAM IAW SRM 51-72-11 AND DWG.Jun 21, 2013 · N316US · Airbus A320211 · Fuselage Main, StructureSDR DALA13030863216Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 40-41R AT FR 31. REPLACED CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STR 40R AND STR 41R AT FR 31 IAW SRM 51-72-11 AND DWG D53232747.Jun 21, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029963216Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 43L AND STGR 44 AT FR 32. REPLACED CLEAT IAW 51-72-11.Jun 19, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13030153218Stringer · corrodedDURING INSPECTION, FOUND FWD CARGO BAY, FR 33-34, S41L CORRODED. BLENDED CORROSION IAW SRM 51-74-00 CHECKED LIMITS, WITH NO ALLOWABLE DAMAGE FOUND ON SRM. CUT OUT DAMAGED STRINGER IAW SRM 53-00-13, FIG 201. LOCATED AND DRILLED NEW STRINGER IAW SRM 51-44-11.Jun 19, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13030143218Stringer · corrodedDURING INSPECTION, FOUND AFT CARGO BAY FR58 - 59 S42L CORRODED. CLEANED AREA IAW AMM 12-21-12. NO LIMITS ON CORROSION ESTABLISHED IAW SRM 53-41-13, FIG 101. REMOVED DAMAGED STRINGER IAW SRM 53-00-13, FIG 201, SHT. 2. REPAIRED STRINGER IAW SRM 53-00-13, FIG Jun 19, 2013 · N318US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13030133216Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT STR 41-42R FR 32 FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DRAWING D53231582.Jun 19, 2013 · N316US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13030123216Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY BETWEEN STRINGER 43 - 44L FR 32. REPLACED CLEAT AND FASTENER FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231212.Jun 19, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13029953216Cleat · corrodedDURING INSPECTION FOUND CORROSION ON CLEAT LOCATED BETWEEN STR 41R AND STR 42R AT LEVEL FR 31 FWD CARGO COMP. L=0.50", W=0.20", D=0.001" APROX. REPLACED CLEAT LOCATED BETWEEN STR 41R AND STR 42R AT LEVEL FR 31 FWD CARGO COMPARTMENT, IAW SRM 51-72-11 AND DWG DJun 18, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13029943216Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STGR 40L AND STGR 41LIN FWD CARGO COMPARTMENT L=0.800", W=0.500", D=0.001" APPROX. REPLACED CLEAT LOCATED FR 32 BETWEEN STR 40L AND STR 41L IN FWD CARGO COMPARTMENT, IAW SRM 51-72-11 AND DWGJun 18, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13029923216Floorbeam · brokenDURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR.32+13" AND -Y254 FWD PAX CABIN. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14. FIG 204 (SHEET 1) PARA 4D, PAGES 225-226.Jun 18, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor Beam
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