Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  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 CALA2017082102842Stringer · corrodedFWD CARGO COMPARTMENT INNER BOTTOM STRINGER 43R BETWEEN FRAMES 31 - 32 HAS CORROSION, REMOVED & REPLACED THE STRINGER IAW SRM 5 1-42-11, REV 119.Aug 21, 2017 · N411UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2017082102841Slide · no testR2 DOOR SLIDE FAILED EMERGENCY LIGHT TESTS. REPLACED THE R2 DOOR SLIDE IAW AMM 25-62-44-400.Aug 21, 2017 · N433UA · Airbus A320232 · Escape SlideSDR CALA2017082102840Slide · no testL2 DOOR SLIDE FAILED EMERGENCY LIGHT TESTS. REPLACED THE SLIDE ASSY IAW AMM 25-62-44.Aug 21, 2017 · N433UA · Airbus A320232 · Escape SlideSDR CALA2017082102839Battery Pack · inoperativeDURING SERVICE CHECK FOUND BOTH LT AND RT OVER WING BATTERY PACK INOPERATIVE. REPLACED BOTH BATTERY PACKS. OPS CHECKED NORMAL.Aug 21, 2017 · N433UA · Airbus A320232 · Emergency LightingSDR CALA2017082102838Hinge Bracket · detachedONE OF THE HINGES BRACKETS AT TOP OF SLIDE MECHANISM AT THE L2 DOOR NOT CONNECTED. THE BRACKET WAS REINSTALLEDAug 21, 2017 · N427UA · Airbus A320232 · Escape SlideSDR CALA2017082102837Slide · no testCABIN EMERGENCY LIGHT SYS TEST ON CIDS DISPLAYS MESSAGE, EPSU EXT LOAD FWD L. DURING 2 SERVICE OPS CHECKS IAW AMM 33-51-00-710-001-A. REPLACED THE NR 1 LEFT DOOR SLIDE ASSEMBLY IAW AMM 25-62-4 4-400-006-A.Aug 21, 2017 · N497UA · Airbus A320232 · Escape SlideSDR CALA2017082102816Door Sill · corrodedAFT CABIN R2 DOOR SILL HAS CORROSION. REMOVED AND REPLACED THE R2 DOOR SILL IAW SRM 51-42- 11, PARA 2E.Aug 21, 2017 · N411UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017082102814Door Sill · corrodedL2 DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.Aug 21, 2017 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2017082002146Bottle · low pressureL2 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.Aug 20, 2017 · N612NK · Airbus A320232 · Passenger/Crew DoorsSDR YENA201708200688Fan · failedDIRTY SOCK ODOR THROUGHOUT AIRCRAFT. ODOR ISOLATED TO APU. PEFORMED DECONTAMINATION OF THE (ECS) IAW AMM 21-00-00-615-004-A. R & R DEOILER CASING SEAL ASSY AT ENG #1 IAW AMM 72-60-31. NO LEAKS. REMOVED & REPLACED APU COOLING FAN IAW AMM 49-52-51 & APU OIL CAug 20, 2017 · N517JB · Airbus A320232 · APU Oil SystemSDR YENA201708200687Oil Cooler · failedDIRTY SOCK ODOR THROUGHOUT AIRCRAFT, DETECTED BY ALL FLIGHT CREW MEMBERS. ODOR ISOLATED TO APU. PEFORMED DECONTAMINATION OF THE (ECS) IAW AMM 21-00-00-615-004-A. R & R THE DEOILER CASING SEAL ASSY AT THE NR 1 ENGINE IAW AMM 72-60-31. NO LEAKS. REMOVED & REAug 20, 2017 · N517JB · Airbus A320232 · APU Oil SystemSDR YENA201708200685Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON TOP FACE MAIN CABIN RT SEAT TRACK -Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-11-15.Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201708200684Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN LT SEAT TRACK Y1292 AT FRAME 16; REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-11-15, AND 51-42-11.Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201708200683Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOORBEAM -Y765; REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-41-14 FIG 001.Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201708200678Condenser · crackedRETURN TO FIELD DUE TO THE COCKPIT TEMP WAS UNCONTROLLABLE, OUTPUT REACHED 118 DEGREES AND COCKPIT TEMP REACHED 94 DEGREES. TURNED OFF THE NR 2 PACK, THE TEMPS CONTINUED TO CLIMB. TROUBLESHOT AND FOUND LOW REGULATING PRESSURE IN THE NR 1 PACK, R & R THE FLOW Aug 20, 2017 · N659JB · Airbus A320232 · Cabin Temperature Control SystemSDR YENA201708200677Solenoid Valve · failedRETURN TO FIELD DUE TO THE COCKPIT TEMP WAS UNCONTROLLABLE, OUTPUT REACHED 118 DEGREES AND COCKPIT TEMP REACHED 94 DEGREES. TURNED OFF THE NR 2 PACK. THE TEMPS CONTINUED TO CLIMB. TROUBLESHOT AND FOUND LOW REGULATING PRESSURE IN THE NR 1 PACK, R & R THE FLOAug 20, 2017 · N659JB · Airbus A320232 · Cabin Temperature Control SystemSDR YENA201708200676Control Valve · failedRETURN TO FIELD DUE TO THE COCKPIT TEMP WAS UNCONTROLLABLE, OUTPUT REACHED 118 DEGREES AND COCKPIT TEMP REACHED 94 DEGREES. TURNED OFF THE NR 2 PACK THE TEMPS CONTINUED TO CLIMB; TROUBLESHOT AND FOUND LOW REGULATING PRESSURE IN THE NR 1 PACK, R & R FLOW CONTRAug 20, 2017 · N659JB · Airbus A320232 · Cabin Temperature Control SystemSDR AALA201708219023Bulb · burned outSERVERAL EMERGENCY EXIT SIGN LIGHT BULB INOPERATIVE. REPLACED THE BULB IAW AMM.Aug 20, 2017 · N650AW · Airbus A320232 · Emergency LightingSDR YENA201708190680Actuator · leakingA MUSTY ODOR DURING DESCENT. AN APU TEST DUPLICATED FAULT. ACCOMP TSM 49-00-81-810. FOUND APU OIL LEVEL OVERSERVICED. REPLENISH LEVEL IAW AMM 49-00-00. ALSO ALSO FOUND IGV ACTUATOR LEAKING. ACTUATOR REPLACED IAW AMM 49-23-51. LEAK CHECKED GOOD. ECS DECONTAAug 19, 2017 · N827JB · Airbus A320232 · APU Oil SystemSDR CALA2017082102813Seat Track · damagedDAMAGED INBD SEAT TRACK +Y254 FR28, FOUND TO BE OUT OF LIMITS 100% MATERIAL LOSS IAW SRM 53-00-15-283-001, PAGE 3. CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED A REPAIR. LOCATED, AND DRILLED THE REPAIR. TREATED, PRIMED AND CUTOUT. INSTALLED THE REPAIR IAAug 19, 2017 · N452UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2017082102812Door Sill · corrodedL1 DOOR SILL WAS CORRODED AROUND FWD AND AFT GIRT BAR ATTACH FITTING HOLES. CORROSION REMOVED, AREA NDT AND REPAIR WASHERS INSTALLED IAW SRM 53-11-14-283-005, PG 5.Aug 19, 2017 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017082102811Support · corrodedLEFT SUPPORT FOR SHEAR PLATE AT FRAMES 69 TO 70 IS CORRODED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-72-11-911, AND DRAWING 18D53471173.Aug 19, 2017 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017082102810Shear Plate · corrodedFRAME 70 OTBD SHEAR PLATE CORRODED. THREE PLACES. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-72-11Aug 19, 2017 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017082102809Shear Tie · corrodedSHEAR TIE CORRODED BEYOND LIMITS 50% MATERIAL LOSS AT FRAME 30, STRINGER 41-42R. REMOVED AND REPLACED THE SHEAR TIE IAW 51-42-11-001, REV 119, AND SRM 51-44-11-001.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802793Battery · dischargedEMERGENCY LIGHTS TEST FAULT AFT L BATTERY. REPLACED AFT L BATTERY PER MM 33-51-38. EMERGENCY LIGHTS TEST OK.Aug 18, 2017 · N410UA · Airbus A320232 · Emergency LightingSDR CALA2017081802751Shear Tie · corrodedFWD CARGO SKIN AT FRAME 31, BETWEEN STRINGERS 41- 42R, SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, AND SRM 51-44-11-001.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802750Shear Tie · corrodedFWD CARGO, SHEAR TIE, FRAME 32 BETWEEN STRINGERS 42 - 43L HAS A SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, REV 119, AND SRM 51-44-11-001, REV 119.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802749Door Sill · corrodedAFT CORNER FITTING OF L2 DOOR CORROSION IS PRESENT IN AREA OF FRAME 68. REMOVED AND REPLACED DOOR SILL IAW SRM 53-41-14-001, ITEM 18, AND 51-72-11-911-00Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017081802748Fitting · corrodedAFT CABIN L2 DOOR SILL AFT CORNER FITTING HAS CORROSION FRAME 69. REMOVED AND REPLACED THE FITTING IAW SRM 53-41-79-001, ITEM 355, AND 51-77-11-911-001.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2017081802747Shear Tie · corrodedFWD CARGO, SHEAR TIE FRAME 27 BETWEEN STRINGERS 42 - 43R HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW 320 SRM 51-42-11-001, REV 119.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802746Shear Tie · corrodedFORWARD CARGO COMPARTMENT INNER SKIN FRAME 26 BETWEEN STRINGERS 41 TO 42R. SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11-001.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802745Shear Tie · corrodedFWD CARGO BAY INNER BOTTOM SHEAR TIE CORRODED AT FRAME 32 BETWEEN STRINGERS 41 - 42R. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001, AND SRM 51-44-11-001, REV 119.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802744Shear Tie · corrodedFWD CARGO BAY INNER BOTTOM SKIN AT FRAME 31 AND BETWEEN STRINGERS 40 - 41R, SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001-A, AND SRM 51-44-11-001, REV 119.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802743Shear Tie · corrodedFWD CARGO UNDER FLOOR AREA, SHEAR TIE, FRAME 32 BETWEEN STRINGERS 40 - 41L HAS A SURFACE CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11-001 AND SRM 5 1-44-11-001, REV 119.Aug 18, 2017 · N411UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2017081802718Door Sill · corrodedR1 DOOR SILL WAS CORRODED AROUND FWD AND AFT GIRT BAR ATTACH FITTING HOLES. CORROSION REMOVED, AREA NDT AND REPAIR WASHERS INSTALLED IAW SRM 53-11-14-283-005, PG 5.Aug 18, 2017 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708170666Unknown · odorAT FL 350, DURING CRUISE, APPROXIMATELY 42 MIN INTO FLIGHT, A DISTINCT ODOR PERSISTED WHILE IN CRUISE, SMELLED LIKE DIRTY LAUNDRY. STRONG IN COCKPIT. CABIN REPORTED NO ODOR. ACCOMPLISHED TSM 05-50-00-810-831-A. RAN APU AND ENGINES AND PACKS. ENGINES AT HIAug 18, 2017 · N589JB · Airbus A320232 · Air Distribution SystemSDR YENA201708180665Lens · brokenEMERGENCY EXIT LIGHT LENS AT SEAT 11C IS BROKEN. REPLACED THE LENS, OK FOR SERVICE.Aug 18, 2017 · N562JB · Airbus A320232 · Emergency LightingSDR YENA201708170674Proximity Switch · out of adjustR2 DOOR SLIDE DOES NOT INDICATE ARMED WHEN PRESSURIZED. PERFORMED TSM 52-13-00-810-805-A AND ADJUST PROXIMITY SWITCH 7WN2 IAW AMM 52-71-00-820-002-A , OK. PERFORMED OPERATIONAL TEST TO MEASURE STRUCTURE LEAKAGE IAW AMM 05-53-00-780-003-A01. R2 DOOR SLIDE SHOWAug 17, 2017 · N639JB · Airbus A320232 · Escape SlideSDR YENA201708170673Floor Support · corrodedCORROSION WAS DISCOVERED ON THE FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND SRM 51-42-11.Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708170672Floor Support · corrodedCORROSION WAS DISCOVERED ON FLOOR SUPPORT + Y1292 BETWEEN FRAMES 66 AND 68. R & R THE FLOOR SUPORT IAW SRM 51-72-11.Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708170671Splice · corrodedCORROSION WAS DISCOVERED ON THE SPLICE LOCATED BETWEEN FRAMES 68 - 69, -Y 1162.5. R & R THE SPLICE IAW SRM 51-42-11.Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708170670Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT +Y 1292 AT FWD GALLEY AREA BETWEEN FRAMES 12 - 24. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708170669Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL Y 503.2, AT FWD GALLEY AREA BETWEEN FRAMES 12 - 16. R & R THE DUMMY RAIL IAW SRM 51-42-11, AND 51-72-11.Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201708170663Battery Pack · no testEMERGENCY BATTERY 11WL FAILED EMERGENCY LIGHT SYSTEM TEST. R & R THE BATTERY PACK IAW AMM 33-51-38. SYSTEM OPS CHECKED GOOD.Aug 17, 2017 · N558JB · Airbus A320232 · Emergency LightingSDR YENA201708160668Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.Aug 16, 2017 · N534JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708160667Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT -Y254 BETWEEN FRAMES 12 TO 24 FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.Aug 16, 2017 · N534JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201708160664Wire Harness · damagedEMERGENCY EXIT LIGHT INOPERATIVE AT ROW 11DEF. FOUND THE WIRE HARNESS DAMAGED. THE WIRE HARNESS WAS REPLACED IAW AWM 94-40-01. EMERGENCY LIGHTS OPS CHECKED SATISFACTORY IAW AMM 33-51-00.Aug 16, 2017 · N607JB · Airbus A320232 · Light System WiringSDR AALA201708179018Service Door · departedDURING POST FLIGHT, OBSERVED THE NR 1 ENGINE OIL SERVICE DOOR MISSING FROM AIRCRAFT. AIRCRAFT WAS GROUNDED.Aug 16, 2017 · N659AW · Airbus A320232 · Fluid Service DoorsSDR YENA201708140661Oil System · leakingDURING DESCENT WITHOUT APU RUNNING, PASSING 18K, HAD A COCKPIT ODOR. ODOR GOT STRONGER PASSING 5K, PERFORMED INFO NOTICE AND TASK 05-50-00-810-831-A. INSPECTED THE APU IAW AMM 49-00-81-810-874-A. FOUND DRAIN LEAKING OIL FROM AFT DRAIN TUBE. PERFORMED TAug 14, 2017 · N662JB · Airbus A320232 · APU Oil SystemSDR CALA2017081802716Stringer · corrodedFWD CARGO BAY RIGHT AT FRAMES 30 - 31, STRINGER 41R CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11, P1.Aug 14, 2017 · N412UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
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