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 GTIA201804232596Megaphone · damagedFA MEGAPHONE VOLUME KNOB MISSING. REPLACED THE MEGAPHONE IAW AMM 25-65-51-920-001-A, OPS CHECKED GOOD. ACFT OK FOR SERVICE.Apr 22, 2018 · N636NK · Airbus A320232 · Emergency EquipmentSDR GTIA201804232595Bottle · low pressureL1 & L2 DOOR ASSIST BOTTLES HAD LOW PRESURE. SERVICED THE BOTTLES IAW AMM 52-10-00.Apr 22, 2018 · N620NK · Airbus A320232 · Passenger/Crew DoorsSDR AALA201804239009Bulb · inoperativeSEVERAL BULBS INOPERATIVE IN ALL EMERGENCY EXIT SIGNS. REPLACED THE BULBS IAW AMM 33-50-00.Apr 20, 2018 · N652AW · Airbus A320232 · Emergency LightingSDR GTIA2018041902592Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. R & R THE AFT MEGAPHONE IAW DRAWINGS NK 320-232-EQ.Apr 19, 2018 · N620NK · Airbus A320232 · Emergency EquipmentSDR YENA201804180914Skin · gougedDURING B6 CHECK AT (SAL), A GOUGE AND DENT DAMAGE WERE FOUND ON THE CENTER FUSELAGE SKIN (PN: 170-92554-005) AT FR24 AND ABOVE STGR 16L. SEE REF /1/ EA FOR MORE DETAILS. THE DAMAGE DIMENSIONS ARE AS FOLLOWS: (1) DENT: L=0.997 IN, W=1.109 IN, DEPTH=0.045 IN (2)Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA201804180913Bushing · migratedDURING C9 CHECK AT SAL, FOUND WITH THE RT WING SIDE STAY FITTING OUTBOARD BUSH MIGRATED VIA REF /4/ MPD TASK. CANNOT ACCOMPLISH REF /3/ SRM TASK BECAUSE IT’S NO LONGER APPLICABLE AND CANNOT ACCOMPLISH REF /2/ SB DUE TO LACK OF TOOLING. CONTACTED VIA REF /5/ DApr 18, 2018 · N565JB · Airbus A320232 · Wing Miscellaneous StructureSDR YENA201804180912Crossbeam · crackedDURING THE CURRENT XC9 HMV CHECK, REPORTED THAT ONE HOLE (J) WAS FOUND WITH CRACK FR20 LT CROSSBEAM SPLICING AS PER REF/5/ MPD ALI INSPECTION AND REF/6/ SB. WAS CONTACTED BY AND ASSESSMENT WAS PROVIDED BY MEANS OF REF/1/ DOSSIER TO ACCOMPLISH REF/6/WITHOUT DEApr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804100911Crossbeam · crackedDURING THE CURRENT XC9 HMV CHECK, REPORTED THAT ONE HOLE (J) WAS FOUND WITH CRACK FR20 LT CROSSBEAM SPLICING AS PER REF/5/ MPD ALI INSPECTION AND REF/6/ SB. ASSESSMENT WAS PROVIDED BY MEANS OF REF/1/ DOSSIER TO ACCOMPLISH REF/6/WITHOUT DEVIATION AND REPAIR BAApr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804180910Crossbeam · crackedDURING THE CURRENT (04/2018) XC9 HMV CHECK, REPORTED THAT ONE HOLE (J) WAS FOUND WITH CRACK FR20 LT CROSSBEAM SPLICING AS PER REF/5/ MPD ALI INSPECTION AND REF/6/ SB. CONTACTED AND ASSESSMENT WAS PROVIDED BY MEANS OF REF/1/ DOSSIER TO ACCOMPLISH REF/6/WITHOUTApr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804180186Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + 765, FRAME 66 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 IAW SRM 51-72-11, AND DWG D53472815.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018042000185Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + Y 503.2, FRAME 16 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 16 IAW SRM 51-72-11, AND DWG D53112825.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804180184Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + Y 1292, FRAMES 16 TO 20 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804180183Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y 1292, FRAME 68 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 68 TO 69 IAW SRM 51-72-11, DRAWINGS D5347280, AND D57472816.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018042000182Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y 1292, FRAME 66 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 IAW SRM 51-71-11, AND DRAWING D53472832.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804200181Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM, + Y 919, FRAME 66 IN THE AFT GALLEY. REPLACED THE FLOORBEAM IAW SRM 51-72, AND DWGS D53472812.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804200180Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + Y 254, FRAME 16 IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53110920, D53110984, AND D53112816.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018042000179Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y254, FRAME 16 IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 24 IAW SRM 51-72-11, DRAWINGS D53110920, D5311098, AND D53112816.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018042000178Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, +Y765, FRAME 68 IN THE AFT GALLEY. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 70 IAW SRM 51-72-11, AND DRAWING D53472816.Apr 18, 2018 · N565JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA201804192591Unknown · odorCLASS 2 MAINTENANCE MESSAGE ON STATUS PAGE, E/A REPORTED A BURNING ODOR IN THE FORWARD GALLEY. RESET THE SYSTEM IAW AMM 23-73-00. FAULT CLEARED , NO DEFECTS NOTED OR ODOR OF BURNING NOTED.Apr 18, 2018 · N634NK · Airbus A320232 · Air Distribution SystemSDR GTIA201804192590Filter · dirtyFLIGHT ATTENDANT REPORTED A DIRTY SOCK ODOR AFTER APU BLEED TRANSFER. PERFORMED A DECONTAMINATION OF THE ECS IAW AMM 21-00-00. FOUND NO TRACES OF OIL LEAKAGE IN APU, PACK DUCKS ,OR ENGINE DEOILER. FOUND RECIRCULATION FILTERS IN UNSATISFACTORY CONDITION. R &Apr 18, 2018 · N614NK · Airbus A320232 · Air Distribution SystemSDR GTIA201804192589Seal · leakingAFT FLIGHT ATTENDANTS REPORTED DIRTY SOCK FUMES ON FINAL APPROACH. R & R THE NR 1 ENGINE DEOILER SEAL ASSY IAW AMM 72-60-31 AND PERFORMED A PACK BURN OUT IAW AMM 21-00-00. NO FUMES NOTED. ACFT OK FOR SERVICE.Apr 17, 2018 · N628NK · Airbus A320232 · Turbine Engine Oil SystemSDR GTIA2018041702588Seal · leakingDECENDING THROUGH 4000 AFT, CABIN PAX SMELLED INTENSE DIRTY SOCK ODOR, SEEMED TO DISSIPATE AROUND 8 MINUTES LATER ON SHORT FINAL APPROACH. ACCOMPLISHED TSM 05-50-00-810-831-A FOUND THE NR 1 ENGINE DEOILER SEAL LEAKING. R & R THE DEOILER SEAL IAW AMM 72-60Apr 17, 2018 · N624NK · Airbus A320232 · Turbine Engine Oil SystemSDR GTIA2018041902587Unknown · odorFA REPORTED FUMES IN REAR CABIN. FUMES WERE NOTICED JUST PRIOR TO LANDING. A SNIFF CHECK IN THE REAR CABIN BOTH PACKS TURNED OFF AND CHECKED ENGINES, NO LEAKS NOTED IAW TSM 05-50-00-810-831-A, ACFT OK FOR SERVICE.Apr 17, 2018 · N605NK · Airbus A320232 · Air Distribution SystemSDR CALA2018041801179Bulb · inoperativeFWD LT WINDSCREEN EMERGENCY LIGHT NOT FUNCTIONAL. REPLACED THE BULBS IN THE EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-51-20-400-001C3.Apr 17, 2018 · N495UA · Airbus A320232 · Emergency LightingSDR CALA2018041801185Stringer · damagedFWD CARGO STRINGER 42R, FRAME 32 HOLE REQUIRES OVERSIZE FASTENER. REPAIRED THE STRINGER IAW SRM 53-00-11-300-022, FIG 21026.Apr 16, 2018 · N447UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018041801183Cover · crackedAFT CARGO DOOR INNER STRUCTURE AT FRAME 61, STRINGERS 34 - 35L CRACKED. REMOVED AND REPLACED THE AFT CARGO DOOR INNER COVER PLATE IAW SRM 51-42-11-001, PARA E .Apr 16, 2018 · N4901U · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2018041801182Fitting · corrodedL2 DOOR SILL AFT CORNER UNDER GIRT BAR FITTING HAS CORROSION. REMOVED AND REPLACED THE DOOR SILL FITTING IAW SRM 51-42-11-001, PARA E.Apr 16, 2018 · N4901U · Airbus A320232 · Fuselage Main, Attach FittingsSDR AALA201804179030Connector · damagedEMERGENCY LIGHT AT ROW 15ABC INOPERATIVE. MAINTENANCE PINNED THE CONNECTOR PLUG IAW AMM 33-51-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Apr 16, 2018 · N661AW · Airbus A320232 · Light System WiringSDR AALA201804179035Floor Support · brokenFLOOR SUPPORT, FRAME 18, Y1006 BROKEN. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11. THE AIRCRAFT WAS GROUNDED.Apr 16, 2018 · N660AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201804179034Floor Support · brokenFLOOR SUPPORT BROKEN ON FRAME 27. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11. THE AIRCRAFT WAS GROUNDED.Apr 16, 2018 · N660AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201804179033Floorbeam · brokenFLOORBEAM, FRAME 18, Y254 IS BROKEN. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11. THE AIRCRAFT WAS GROUNDED.Apr 16, 2018 · N660AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA201804179032Web · corrodedLEFT OTBD FLOOR WEB DAMAGED AND CORRODED AT FRAME 16. REMOVED AND REPLACED THE FLOOR WEB IAW SRM 51-42-11. THE AIRCRAFT WAS GROUNDED.Apr 16, 2018 · N660AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018041601166Connector · disconnectedSEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 12 - 22, FOUND THE CONNECTOR DISCONNECTED UNDER SEAT 21A, CONNECTED THE CONNECTOR AND PREFORMED AN OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-001A, AND 33-51-00-710-009A. OPS CHECKED GOOD, NO FAULTS NOTEApr 16, 2018 · N490UA · Airbus A320232 · Light System WiringSDR CALA2018041601165Battery · no testEMERGENCY LIGHTS TEST FAILED. EPSU COMM AFT L FAULT. REPLACED AFT LEFT EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.Apr 16, 2018 · N425UA · Airbus A320232 · Emergency LightingSDR GTIA2018041602586Unknown · odorDURING DESCENT, AROUND 20K FT, FLT ATTENDANT IN THE AFT CABIN, REPORTED AN ODOR OF DIRTY SOCKS. IDENTIFICATION OF CAUSE OF CABIN ODORS WAS PERFORMED IAW TSM 05-50-00-810-831. NO EVIDENCE OF LEAKAGE AROUND ACFT IR EVIDENCE OF BIRDSTRIKE ENGINE RUN-UP WAS PERApr 16, 2018 · N904NK · Airbus A320232 · Air Distribution SystemSDR GTIA2018041602585Ecs · contaminatedPOSSIBLE FUMES IN CABIN, FLT ATTENDANTS REPORTED A DIRTY SOCK ODOR AROUND ROW 3. AFTER TURNING OFF THE NR 2 PACK, THE ODOR DISSAPATED. PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00. NO FURTHER ODOR DETECTED. AIRCRAFT OK FOR CONTINApr 16, 2018 · N621NK · Airbus A320232 · Air Distribution SystemSDR YENA201804150177Oil System · leakingODOR IN CABIN AND THROUGH OUT THE ACFT. INSPECTED THE NR 1 & 2 ENGINES FOR OIL QTY & LEAKS, NO LEAKS NOTED, OIL QTY OK. INSPECTED THE APU AND FOUND APU TO HAVE AN ACTIVE OIL LEAK FROM AFT DRAIN MAST TUBE. APU OIL LEVEL APPROXIMATELY 1/2 QT LOW. PULLEDApr 15, 2018 · N519JB · Airbus A320232 · APU Oil SystemSDR YENA201804140962Spar · gougedDURING C6 CHECK (LCQ), A GOUGE WAS FOUND ON THE LOWER SPAR WEB (PN: D54610003206) AT RIB 5 ON THE RT PYLON. SEE REF /1/ REO FOR MORE DETAILS. THE GOUGE DAMAGE WAS BLENDED PER SRM AND THE REMAINING THICKNESSES WERE MAPPED. LCQ CONCLUDED THAT THE REMAINING THICKApr 14, 2018 · N652JB · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR YENA201804140436Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT PASSENGER DOOR RT FR 66 LOWER CORNER STRUCTURE FWD IB BOLT HOLES. REMOVED AND REPLACED AFT PASSENGER DOOR RT SILL AT FR 66 IAW SRM 51-42-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804140435Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN R2 DOOR SILL AT FR 66 STR 23R. REMOVED CORROSION VERIFIED BEYOND 25% ALLOWABLE LOSS LIMITS IAW SRM 53-41-14-283-002 REMOVED AND REPLACED AFT RT SILL AT FRAME 66 IAW SRM 51-42-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804140434Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN LEFT SIDE OF CABIN Y1292 STR23L FRAME 68. REMOVED AND REPLACED LEFT SIDE OF CABIN FLOORBEAM Y1292 AT STR 23 LT IAW SRM 51-42-11 AND 51-72-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804140433Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN LEFT OF CABIN Y765 STR 23 LT FRAME 68. REMOVED AND REPLACED FLOORBEAM Y765 P/N D53476219220000 IAW SRM 51-72-11-911-001.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804140432Shear Plate · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN RT SHEAR WEB FRAME 69+16" STR 23R. REMOVED CORROSION ON RT SHEAR PLATE AT FRAME 69+16" STR23 RT FOUND TO BE OUT OF LIMITS AND REPLACED NEW SHEAR PLATE IAW SRM 51-42-11 PG 6 PARA 2A.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804140431Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN LEFT SIDE BEAM Y1292 AT THE FOLLOWING LOCATIONS FRAME 16 & FRAME 18 23L. REMOVED AND REPLACED FLOORBEAM INSIDE CABIN LEFT SIDE BEAM Y1292 IAW SRM 51-41-11, 5-72-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804140430Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON INSIDE CABIN LEFT SIDE BEAM Y1292 AT THE FOLLOWING LOCATIONS FRAME 16 & FRAME 18 23L. REMOVED AND REPLACED FLOORBEAM INSIDE CABIN LEFT SIDE BEAM Y1292 IAW SRM 51-41-11, 5-72-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804140173Skin · chafedDURING HEAVY MAINTENANCE, THE NR 2 PYLON LOWER SKIN SURFACE FOUND CHAFED, INCLUDING THE HORIZONTAL DOUBLER AT RIB 5. REPAIRED THE NR 2 PYLON LOWER SKIN RIB 5 IAW SRM 54-51-12-283-003, 54-51-12-300-003, REO L21289, EC A18-277-01, AND RDAS 80441834-003-2018. CLApr 14, 2018 · N652JB · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR YENA201804140172Battery Pack · no testDURING HEAVY MAINTENANCE, EPSU BATTERY 11WL FAILED AN EMERGENCY LIGHT TEST. R & R THE EPSU BATTERY 11WL IAW AMM 33-51-38, EMERGENCY LIGHT SYSTEM CHECKED OK.Apr 14, 2018 · N652JB · Airbus A320232 · Emergency LightingSDR YENA201804140171Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION DISCOVERED INSIDE CABIN, LEFT SIDE Y1292, FRAME 68. REMOVED AND REPLACED THE CABIN FLOORBEAM IAW SRM 51-42-11, AND 51-72-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201804140170Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION DISCOVERED INSIDE CABIN AT THE R2 DOOR SILL, FRAME 66, STRINGER 23R. REMOVED AND REPLACED AFT PAX DOOR SILL IAW SRM 51-42-11, AND 51-72-11.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201804140169Floorbeam · corrodedCORROSION DISCOVERED ON THE FLOORBEAM, FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.Apr 14, 2018 · N652JB · Airbus A320232 · Fuselage Main, Floor Beam
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