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"

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SDR DALA2016092706957Floorbeam · corrodedCORROSION ON FLOORBEAM +Y1225 TO +Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA. REPLACED FLOORBEAM +1165 BETWEEN FRAME 66 + 5" TO FRAME 67 + 18" AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D5317200.Sep 25, 2016 · N332NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2016091506696Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y160, FRAME 69+18 AT AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT FRAMES 68 TO 70 IAW SRM 51-72-11 AND DWG D53472780.Sep 14, 2016 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016091406672Skin · dentedDENT ON EXTERNAL SKIN FRAME 27 + 12.5" AND BETWEEN STRINGERS 42 & 43R, PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN ON FRAME 27 + 12.5" AND BETWEEN STRINGER 42R TO STRINGER 43R AT LOWER FUSELAGE ASPER ERA 547954-14 REV.ORIGINAL AND PRI 547954-14 REV. 0Sep 13, 2016 · N324US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016090906502Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED ON LEFT SIDE AFT EMERGENCY EXIT. REPLACED THE POWER SUPPLY.Sep 8, 2016 · N330NW · Airbus A320211 · Emergency LightingSDR DALA2016090406501Trunnion · crackedCRACK INDICATION FOUND ON FWD HINGE FITTING AND FLANGE ON RT MAIN LANDING GEAR, REPLACED FWD HINGE FITTING IAW DRAWING D53370600 AND SRM 51-72-11.Sep 4, 2016 · N324US · Airbus A320211 · Fuselage, Landing Gear Attach FittingsSDR DALA2016081706315Box Beam · crackedRIGHT SIDE BOX BEAM FR43 AND Y1650 CRACK INDICATION. REPAIR IAW PRI 549564-14AD REV.0, REV.1, REV.2, REV.3Aug 16, 2016 · N320US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016081706045Fastener · crackedCRACK INDICATIONS, 4 EA ON 2 LOWER FASTENERS LOCATED ON DOOR STOP FITTING 1 AND 3 OF FRAME 68, RT SIDE IN AFT GALLEY AREA. PERMANENT REPAIR ON 2 LOWER FASTENERS LOCATED ON DOOR STOP FITTING AND 3 OF FRAME 68. RT SIDE IN AFT GALLEY AREA IAW PRI 547942-14, REVAug 16, 2016 · N323US · Airbus A320211 · Fuselage Main, StructureSDR DALA2020020500896Stringer · damagedEVALUATION FOR POSSIBLE FCS REPAIR ON STRINGER 33L ON UNDER FLOOR STRUCTURE AT AFT GALLEY AREA BETWEEN FRAME 66 TO FRAME 68, REPAIR LOC ON STRINGER 33LH BETWEEN FRAME 66 TO FRAME 68 AS PER ER/A 549159-14 REV.A AND A320 SRM 53-00-13. FIG 201Aug 15, 2016 · N323US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2020020500898Skin · damagedEVALUATION FOR POSSIBLE FCS REPAIR ON UPPER SKIN ON TAIL ON FRAME 83 BETWEEN STRINGER 4L TO STRINGER 5L, REMOVED AND REINSTALLED EXISTING REPAIR LOCATED ON TAIL ON FRAME 82 AND BTW STR 4L TO STR 5L AS PER ER/A 549159-14 REV. A AND A320 SRM 53-51-11 FIGURE 203.Aug 14, 2016 · N323US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016080905920Battery Pack · no testDURING EMERGENCY LIGHT TEST, BATTERY PACK FAILED. REMOVED & REPLACED THE BATTERY PACK IAW AMM 33-51. CHECKED GOOD.Aug 8, 2016 · N325US · Airbus A320211 · Emergency LightingSDR DALA2020020500897Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 21 TO FRAME 22 BETWEEN STRINGER 22L TO STRINGER 23L, REMOVED AND REINSTALLED EXISTING REPAIR LOC. ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 21 TO FRAME 22 BETWEEN SAug 6, 2016 · N323US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016072805619Fitting · damagedDAMAGE ON RIGHT CRUCIFORM, REPAIRED IAW ER/A 548323-14AD REV A FOR WING CENTER CRUCIFORM FITTING.Jul 27, 2016 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016072105469Frame · damagedDAMAGE ON FRAME 24, STRINGER 6R ON THE AFT SIDE OF THE FRAME. CUTOUT DAMAGE AND REPAIRED IAW ERA 548700-14.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016072105468Frame · crackedCRACK INDICATIONS AT FRAME 16. COMPLIED WITH FINAL ERA 548219-14AD REV ORIGINAL.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016072105467Box Beam · not reportedCENTER FUSELAGE RT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548164-14AD.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016072105466Box Beam · not reportedCENTER FUSELAGE LT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548129-14AD.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016111808959Stringer · corrodedCORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016111808958Stringer · corrodedCORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016071405308Battery Pack · inoperativeLEFT EMERGENCY LIGHT BATTERY FAILED. REPLACED THE BATTERY.Jul 13, 2016 · N314US · Airbus A320211 · Emergency LightingSDR DALA2016071205309Skin · damagedSKIN MISDRILLED THRU STRINGER FRAME 64 STRINGER 10L. REPAIRED THE SKIN IAW SRM 53-00-11 FIG. 239, PARA 4.W. AND REPAIRED STRINGER IAW SRM 53-00-13 FIG 203 PAR 4.AJul 10, 2016 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016070605180Light · inoperativeEMERGENCY EXIT PATH LIGHT AT SEAT ROW 23 ABC INOPERATIVE, INSTALLED NEW LIGHT ASSY.Jul 2, 2016 · N316US · Airbus A320211 · Emergency LightingSDR DALA2016063005103Light · brokenROW 7ABC EMERGENCY SEAT LIGHT INOPERATIVE, REPAIRED BROKEN .Jun 28, 2016 · N310NW · Airbus A320211 · Emergency LightingSDR DALA2016062304895Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 AND XP297 TO XP453 AT FORWARD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 ANDJun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304894Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN, LOCATED 6" ABOVE RT SIDE STR AT FRAME 9 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE OF LOWER STR RT AND FRAME 9 IAW ER/A 547910-14AD, REV ORIGINAL AND PRI 5479Jun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304893Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE RT SIDE STR AT FR 11 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED "6" ABOVE OF LOWER STR RT SIDE AND FRAME 11 IAW ER/A N547910-14 AD REV ORIGINAL AND PRIJun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304892Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 1L. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 2LT TO 2RT IAW ER/A 546749-14, REV ORIGINJun 22, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304891Skin · dentedDENT ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65 IAW ER/A 546748-14.Jun 22, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062004848Frame · crackedCRACK INDICATION FOUND IN OPEN HOLE ON CROSSBEAM SPLICING ON FRAME 16 FIRST HOLE FROM OTBD EDGE IN LATERAL AVIONIC COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATION ON CROSSBEAM SPLICING ON FRAME 16 FIRST HOLE FROM OTBD EDGE IN LATERAL AVIONINC COMPARTMENT LJun 17, 2016 · N330NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2016120709700Skin · gougedSLAT GOUGED AT 2 LOCATIONS ON LWER SKIN TRAILING EDGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN ON SLAT 3 BTW RIB 7 TO RIB 8 ON RH WING IAW PRELIMINARY REPAIR INSTRUCTION ER/A 547917-14 REVISION 0 AND ER/A 545659-14 REVISION A, TABLE 1, ITEM 28 PAGE 17 AND Jun 16, 2016 · N330NW · Airbus A320211 · Leading Edge DevicesSDR DALA2020011500311Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOC BTW FR72 TO FR73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FR 72 TO FR 73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE AS PER SRM 53-Jun 13, 2016 · N330NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016053104254Floor Support · corrodedCORROSION ON LOWER SILL AT AFT GALLEY AREA ON STR 23R BETWEEN FRAME 66 TO FRAME 68, REPLACED LOWER SILL AT AFT GALLEY AREA LEVEL OF STR 23R BETWEEN FRAME 66 TO FRAME 68 IAW SRM 51-72-11 AND DWG D53480019.May 30, 2016 · N370NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2016053004253Receptacle · missingBOTH RT OVERWING EXIT DOOR HANDLE EMERGENCY LIGHT RECEPTICLES MISSING, UNDER COVER, BOTH LT OVERWING EXIT DOOR HANDLE EMERGENCY LIGHTS INOPERATIVE. RELAMPED LT OVERWING EXIT DOOR HANDLE LIGHTS. REPLACED RT FWD OVERWING EXIT DOOR HANDLE LIGHT.May 27, 2016 · N325US · Airbus A320211 · Emergency LightingSDR DALA2016052004091Power Supply · faultedAFT LT EPSU FAULT, REPLACED AFT LT EPSU W/O BATTERY, 13WL.May 19, 2016 · N324US · Airbus A320211 · Emergency LightingSDR DALA2016052004086Structure · puncturedPERFORATION ON TIP ON LT HORIZONTAL STABILIZER, PERFORMED REPAIR BY WELDING ON TIP LT HORIZONTAL STABILIZER IAW SRM 55-14-11.May 19, 2016 · N337NW · Airbus A320211 · Horizontal Stabilizer StructureSDR DALA2016051904085Wire · damagedSEAT 11 EMERGENCY ESCAPE LIGHT INOPERATIVE, REPAIRED WIRE CONNECTION IAW SWPM CH 20. OPS CK OK, SEAT 11.May 18, 2016 · N377NW · Airbus A320211 · Light System WiringSDR DALA2016051203921Light · smokeDIVERTED DUE TO SMOKE IN THE COCKPIT. F/O LEFT FLOOD LIGHT ASSY WAS FOUND TO BE CAUSE OF THE SMOKE.May 11, 2016 · N377NW · Airbus A320211 · Flight Compartment LightingSDR DALA2016050203594Wire · damaged12A EMERGENCY LIGHTS ON SEAT INOPERATIVE, REPLACED SPLICE ON SEAT ASSY.Apr 29, 2016 · N320US · Airbus A320211 · Light System WiringSDR DALA2016033002627Stop Fitting · crackedCRACK INDICATION ON FRAME 68 COMMON TO STOP DOOR FITTING AT STR 22R LOWER INBD HOLE AT AFT GALLEY AREA . PERFORMED PERMANENT REPAIR ON FRAME 68 AT STR 22 LOWER INBD HOLE IAW SRM 53-41-12, PARA 5E, PAGE 220.Mar 29, 2016 · N319US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016032302318Power Supply · faultedLT EMERGENCY POWER SUPPLY UNIT FAULT LIGHT. R & R LT EMERGENCY POWER SUPPLY IAW AMM 33-51.Mar 22, 2016 · N331NW · Airbus A320211 · Emergency LightingSDR DALA2016031201924Stringer · corrodedCORROSION ON STRINGER 43L BETWEEN FRAMES 56 & 57. PERFORMED NDT NO CRACKS NOTED. FABRICATED A REPAIR AND INSTALLED IAW SRM 53-00-13. MAJOR REPAIR.Mar 11, 2016 · N371NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016031301925Skin · dentedDENT ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 69 BETWEEN STR 28 RT TO STR 29 RT. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATION ON FRAME 69, STR 27 RT TO STR 32 RT IAW ERA 544182-14AD REV A AND PRI 524182-14.Mar 10, 2016 · N309US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016031001917Skin · corrodedCORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R TO STR 30R. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R, STR 30R IAW SRM 53-41-11 PARA 5.D FIG 205 PAGES 256/262Mar 9, 2016 · N309US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016031401926Stringer · corrodedCORROSION ON STRINGER 44 BETWEEN FRAMES 33 TO 34 IN FWD CARGO COMPARTMENT. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231544, D53370500.Mar 4, 2016 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA160223004Brake · worn(CAN) FLIGHT-CREW REPORTED BAD VIBRATIONS ON T/O, SUSPECT RT MLG. DURING INVESTIGATION FOUND NR 4 MAIN WHEEL WORN TO LIMITS. NR 4 MAIN WHEEL REPLACED IAW AMM 32-41-11 AND NR 4 MAIN BRAKE WAS REPLACED DUE TO SEIZED DISCS IAW AMM 32-42-27.Feb 23, 2016 · Airbus A320211 · BrakeSDR DALA2016030301619Bushing · corrodedCORROSION FWD BUSHING OF PINTLE PIN AT RIB 5 ON RETRACTION ACTUATOR ON LT MLG REPLACED BUSHING, 1 EA OF FWD POSITION ON RETRACTION ACTUATOR ON LT MLG IAW CMM 32-11-33.Feb 23, 2016 · N309US · Airbus A320211 · Main Landing Gear Strut/Axle/TruckSDR CA160215019Outflow Valve · failed(CAN) UNABLE TO PRESSURIZE CABIN. AIRBORNE RETURN. RESOLUTION - SKIN AIR OUTLET VALVE REPLACED IAW AMM 21-26-53-PB401. AVEC COMPUTER REPLACED IAW AMM 21-26-34 PB401, AND NEW DUCTS INSTALLED IAW AMM 21-26-42-401. CARRY OUT OPS TEST OF THE VENTILATION SYS OF TFeb 15, 2016 · Airbus A320211 · Pressure Regulator/Outflow ValveSDR CA160215006Valve · failed(CAN) SMOKE AVIONICS ECAM MESSAGE APPEARED DURING POWER TRANSFER FROM GROUND POWER UNIT TO ACFT WHILE AT THE GATE. NO ASSOCIATED SMOKE OR FUMES PRESENT. PASSENGERS DEPLANED. DISPATCH AND MAINTENANCE NOTIFIED. INLET SKIN AIR VALVE R & R IAW AMM 21-26-52, PB4Feb 12, 2016 · Airbus A320211 · Air Distribution SystemSDR CA160215003Actuator · failed(CAN) LOST GREEN HYDRAULIC FLUID ON ARRIVAL FLL R10R, TOW IN REQUIRED. RESOLUTION R & R LT MLG DOOR ACTUATOR IAW AMM 32-31-35 LEAK AND OPS CK NO LEAKS. SERVICED GREEN HYD RESERVIOR TO PROPER LMTS, RAN NR 1 ENGINE DAS OIL.Feb 12, 2016 · Airbus A320211 · Landing Gear Door ActuatorSDR DALA2016021101057Skin · corrodedCORROSION DAMAGE, 2 AREAS, TO THE INTERNAL SIDE OF THE SKIN, JUST OTBD OF S-43L, BETWEEN FRAME 56 TO FRAME 57. REPAIR IAW ERA 543887-14, REV O.Feb 11, 2016 · N330NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016021101056Stringer · corrodedEVIDENCE OF CORROSION ON STR S43L BETWEEN FRAMES 56-57. REMOVED STR 43L MIDDLE OF FRAME 55 TO MIDDLE OF FRAME 58, SRM 53-00-13, FIG 201 IAW ERA 543887-14, REV O.Feb 11, 2016 · N330NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
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