Airbus A320-232

Service difficulty reports · 32,653

Newest first. General aviation reporting is voluntary.

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 CALA2018102902226Frame · not reportedREMOVED AND REPLACED LT FWD EMERGENCY EXIT 833 LT VERTICAL FRAME IAW SRM 51-42-11-001 PARA 2E INSTALLED LT VERTICAL FRAME ON LT FWD EMERGENCY HATCH IAW SRM 51-42-11-001 ON N/R S/N 9811397 FOR SDR REPORTING.Oct 29, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018102902225Stop Fitting · damagedL2 DOOR FR68 NO.1 DOOR STOP LOWER I/B HOLE HAS A REJECTABLE INDI CATION AD RELATED TASK NO. 2018-03-12 SUPPORT TASK GENERATED ON NR 9296748 REAMED I/B HOLE TO .391 PER SRM 53-41-12-300-008 STEP 2A(F). HFEC ROTORY SCAN COMPLETED WITH NO RELEVANT INDICATIONS. COOct 29, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018102902223Door Sill · corrodedL1 DOORSILL CORRODED AROUND AFT GIRTBAR FITTING AFT OUTBOARD HOLE. CORROSION REMOVED, NDT''D, AND REPAIR WASHER INSTALLED PER SRM 53-11-14-283-005 FIG 10108 SHEETS 1-5. PER STEP 1F OF SAME SRM NEED TO ACCOMPLISH INSPECTIONS PER SRI 53-11-14-205-001. PER TABLE Oct 29, 2018 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018102902222Pressure Switch · faultyG ENG 1 PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. - HYD HYD PUMP 31-2914-9-9003, AMM 29-11-51. FURTHER TSM REF 29-11-00- 810-804. BERG TOMC FAILING. NEEDS NEW SWITCH REF TSM TASK 29-11-00-810-804. FOUND PRESSURE SWITCH1074GK REMOVED AND REPLACED NR 1 ENG PUOct 29, 2018 · N469UA · Airbus A320232 · Hydraulic Pressure SensorSDR YENA2018110280722Relay · unknownELECTRICAL BURNING ODOR IN THE COCKPIT & CABIN. PERFORMED AMM 05-50-00-810-831-A AND ODOR DETERMINED TO BE TYPE 9. TSM INSPECTION 24-00-00-810-823-A PERFORMED. INSPECTION OF COCKPIT, CABIN, GALLEYS, LAVS AND AVIONICS BAYS AND NO ODORS FOUND. DURING ENGINE ROct 28, 2018 · N655JB · Airbus A320232 · Electrical Power SystemSDR AALA201810319023Lamp · burned outL1 AND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-11. OPS CHECKED GOOD.Oct 28, 2018 · N655AW · Airbus A320232 · Emergency LightingSDR AALA2018103109029Lamp · burned outL1 AND R1 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-11. OPS CHECKED GOOD.Oct 28, 2018 · N655AW · Airbus A320232 · Emergency LightingSDR AALA201810299045A/C Pack · odorAIRCRAFT WAS GROUNDED: FUMES AND ODOR IN CABIN. DISSIPATED WITH CABIN FANS AND PACK NR 1 TURNED OFF. MAINTENANCE ACCOMPLISHED JOBCARD AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Oct 28, 2018 · N647AW · Airbus A320232 · Cabin Cooling SystemSDR AALA201810299048Seal · obstructedL2 DOOR HAD A LOUD HISS THROUGHOUT FLIGHT. MAINTENANCE CHECKED AND CLEARED DEBRIS FROM DOOR CUTOUT AREA. MAINTENANCE ALSO PRESSURIZED AIRCRAFT TO TRY AND DUPLICATE HISS, NO SOUNDS NOTED.Oct 28, 2018 · N604AW · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018102902212Fastener · corrodedFWD CARGO BAY FASTENERS CORRODED @ FR 32 AND STR 39R-40R. REMOVED AND REPLACED CORRODED FASTENERS AT CLEAT AT FR 32 BTWN S TR 39R AND 40R AND RESTORED SURFACE PROTECTION IAW SRM 51-7 2-11-911-001, ER 5100R01017 REV E. AAR N/R 9019696.Oct 28, 2018 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018102902926Assist System · low pressureL1 DOOR ASSIST REQ SVC-SVCD L1 DOOR ASSIST WITH NITROGEN IN REF AMM 52-10-00. LEAK CK GOOD.Oct 28, 2018 · N634NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2018102902211Door Sill · corrodedSPEC NR A3NB-53-3-6299 DOT NR A3-007 CORROSION AROUND BLANKING PLATE FASTENER HOLE AT L2 DOOR FR 68 OUTBOARD AFT REMOVED DOOR SILL FOR L2 DOOR IAW SRM 51-42-11-001. NO CORROSION PERMITED IN AREA PER SRM 53-41-14-238-002. LOCATED, DRILLED NEW DOOR SILL FOR L2 IOct 27, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018102902210Door Sill · corrodedSPEC NR A3NB-53-3-6299 DOT NO. A3-009 CORROSION ON R2 DOOR SILL REMOVED R2 DOOR SILL IAW SRM 51-42-11-001. ORIGINAL THICKNESS .098. MATERAIL LOSS .036 MAX ALLOWED .024 OUT OF LIMITS IAW SRM 53-41-14-283-002. LOCATED DRILLED AND INSTALLED NEW SILL IAW SRM AND 5Oct 27, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018102902925A/C Pack · odorSTRONG ODOR OF FUEL IN AFT GALLEY, F/A HAD TO USE O2, EMS CALLED.-ACCOMPLISHED TSM 05-50-00-810-831-A. ACCOMPLISHED EXTERNAL INSPECTION OF ENGS, APU AND WING ROOT AREA, NO LEAKS NOTED. RAN ENGS 1 AND 2 WITH FLT CREW. PACK2 CONFIRMED AT FAULT. SEE LOGPAGE 23925Oct 27, 2018 · N648NK · Airbus A320232 · Cabin Cooling SystemSDR GTIA2018102902924Oil System · overserviced"CABIN ODOR/FUME DURING DECENT, LAST 10 MIN-ACCOMPLISHED TSM 05-50-00-810-831-A. FOUND APU OIL OVER SERVICED, FOUND OIL ON APU COMPARTMENT. PERFORMED PACK BURN OUT PROCEDURES IAW AMM 21-00-00. ALL OPS CHECK GOOD, A/C OKAY FOR CONTINUED SVC. NO EVIDENCE OF ODOROct 27, 2018 · N650NK · Airbus A320232 · APU Oil SystemSDR YENA201810260707Epsu · failedFT 2044, PBI-EWR. RT AND LT EMERG BATT POWER SUPPLY UNIT FAIL DURING TEST AT PTP. R&R RT AND LT EPSU IAW AMM 33-51-38 OPS CHECK SAT.Oct 26, 2018 · N648JB · Airbus A320232 · Emergency LightingSDR CALA2018102702200Light · brokenOVERHEAD BIN EMERGENCY LIGHT 22WL AT ROW 11DEF HAS BROKEN ATTACH LEGS. REMOVED AND REPLACED OVERHEAD BIN EMERGENCY LIGHT 22WL (P/N: 10- 1266-1) AT ROW 11 DEF IAW AMM 33-51-11-000-001-A AND AMM 33 -51-11-400-001-A. OPERATIONAL CHECK ACCOMPLISHED ON TASK CARD 1Oct 26, 2018 · N420UA · Airbus A320232 · Emergency LightingSDR CALA2018102702196Stop Fitting · damagedR2 DOOR NR 4 STOP FITTING OTBD UPPER HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP AT LCQ PER REF NR 9296646. REPLACED DOOR R2 NR 4 STOP FITTING P/N D5348017920000. REAMED HOLE IN STOP FITTING TO 2ND OVER TO .2825 PER SRM 51-44-11-00Oct 26, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018102702194Stop Fitting · damagedR2 DOOR NR 5 STOP FITTING OTBD UPPER HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSPECTION AD 2018-03-1 2. REPLACED STOP FITTING P/N D5348017920000. REAMED HOLE IN STOP FITTING TO .2825 PER SRM 51-44-11-001 TABLE 00112 & SRM 53-41-12-3Oct 26, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018102702195Stop Fitting · damagedR2 DOOR NR 1 STOP FITTING INBD LWR HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP. REPLACED DOOR R2 NR 1 STOP FITTING P/N D5348017920000. REAMED INBD LOWER HOLE TO 2ND OVER .2821 PER SRM 51-44-11-001 TABLE 00112 A ND SRM 53-41-12-300-Oct 26, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018102702186Stop Fitting · damagedR2 DOOR NR 6 STOP FITTING INBD LWR HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP PER REF NR 9296644. REPLACED R2 NR 6 DOOR STOP FITTING P/N D5348017920000. REAMED I/B LWR HOLE TO 2ND O/S .2825 PER SRM 51-44-11-001 TABLE 00112 AND 5 3Oct 25, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2018113024786Actuator · failedFT # 714, DFW-BOS. EMERGENCY DECLARED. THE FLIGHT CREW REPORTED THAT AT FL 370 THEY HAD A F/CTL ALT LAW, F/CTL STAB TRIM, AND F/CTL ELAC 1 PITCH FAULT ECAM MESSAGE. THEY COMPLIED WITH F/CTL STABILIZER JAM QRH PROCEDURE 7-44. THE CREW REPORTED THAT MANUAL PITCOct 24, 2018 · N568JB · Airbus A320232 · Stabilizer Control SystemSDR YENA2018102940706Light · malfunctionedFLT 993, BOS-DEN. UPON PREFLIGHT EXIT ROW LIGHT 10DEF REMAINS ON - END; RESET AND OPS CHECK OF EMER LIGHT SYS OK IAW AMM 33-50-00.Oct 24, 2018 · N608JB · Airbus A320232 · Emergency LightingSDR CALA2018102702179Stringer · corrodedFWD CARGO FR 28-34 STR 41R HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED STR IAW SRM 51-72-11 FROM FR24-35 STR 41R.Oct 23, 2018 · N422UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018102702177Stringer · corrodedLT FR61 TO FR63 STR42 HAS EVIDENCE OF CORROSION (A3NB-53-4-6179). REMOVED AND REPLACED STRINGER 42L AT FR60 TO FR64 IAW SRM 51-72-11-911-001.Oct 22, 2018 · N422UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA201810220705Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR STRUCTURE, SEAT TRACK Y765, FR 62 +8.00", STR 23L. CORROSION MEAS. 3.90"L X .772"W X .063" D. MATERIAL LOSS = 29%; CORROSION THAT IS BEYOND ALLOWABLE LIMITS, PER SRM 53-41-15-283-001 ON SEAT TRACK Y76Oct 22, 2018 · N621JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201810239014Lens · detachedEXIT LIGHT LENS FELL OFF THE R2 DOOR, RETAINED IN COCKPIT. REPLACED THE LENS.Oct 22, 2018 · N665AW · Airbus A320232 · Emergency LightingSDR CALA2018102202171Unknown · malfunctionedBOTH TRANSFER VALVES STUCK IN CLOSED POSITION REPORTED BY CREW. TOMC BROADSTONE. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN VERIFY TRANSFER VALVES OPEN REF MEL 2815R. CONTACT TOMC 847-700- 9980. ACCOMPLISHED CHECK OF REFUEL POWER SWITCH UPON LANDING, SWITCH Oct 22, 2018 · N414UA · Airbus A320232 · Fuel Transfer ValveSDR AALA2018102429036Detector · out of adjustLEFT AFT OVERWING EMERGENCY EXIT INDICATOR INOPERATIVE. ADJUSTED THE ACCESS PANEL TARGET IAW 52-71-00-710-001. OPERATIONS NORMAL.Oct 21, 2018 · N653AW · Airbus A320232 · Door Warning SystemSDR YENA201810200703Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL AT FR 61 +1 REF NR 40196. REMOVED CORROSION AND INSTALLED DOUBLER AS PER SRM REF 53-41-49-300-03 FIG 1 SHEET 001 A.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201810200702Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FR60+11 REF NR 40195. CORROSION REMOVED AND INSTALLED REPAIR AS PER SRM REF 53-41-40.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201810200701Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FR61 +9 REF NR 40198. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW SRM REF 53-41-48-300-063 FIG 001.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201810200700Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16. FLOORBEAM Y765 CORRODED REF NR 40126. REMOVED AND REPLACED FLOORBEAM Y765 IAW SRM 51-72-11.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201810200699Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16, DUMMY FLOORBEAM Y 254. REMOVED AND REPLACED FLOORBEAM Y254 IAW SRM 51-72-11 STEP C & 51-42-11.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201810200698Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 Y1292. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR 16 IAW SRM 51-42-11.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201810200697Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 DUMMY FLOORBEAM Y 940. REMOVED AND REPLACED DUMMY FLOORBEAM Y940 IAW SRM 51-42-11 PAR F.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201810200696Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 DUMMY FLOORBEAM Y503.2. REMOVED AND REPLACED FLOORBEAM 503.2 IAW SRM 51-72-11.Oct 20, 2018 · N503JB · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA2018102329035Container · crackedRIGHT OVERWING SLIDE ENCLOSURE HAS A CRACK AT THE LOWER CORNER EDGE. REPLACED THE SLIDE ENCLOSURE IAW JC 26L20025014.Oct 20, 2018 · N654AW · Airbus A320232 · Escape SlideSDR GTIA2018102202907Accumulator · low pressureL1 DOOR ASSIST ACCULULATOR REQUIRE SERVICE. -SERVICED L1 DOOR ASSIST ACCUMULATOR TO PROPER PRESSURE IAW AMM 52-10-00.Oct 20, 2018 · N617NK · Airbus A320232 · Passenger/Crew DoorsSDR AALA2018102329028Cover · leakingTHE AIRCRAFT WAS GROUNDED. DIRTY SOCK ODOR DURING CLIMB, DISSIPATED AFTER ENGINE NR 2 BLEED AND PACK 2 OFF. APU OIL HEATER COVER LEAKING OIL. SEALED THE APU OIL HEATER COVER IAW AMM 4-96-51. LEAK CHECKED GOOD.Oct 19, 2018 · N679AW · Airbus A320232 · APU Oil SystemSDR AALA201810229050Lamp · dimAFT MOST FORWARD FACING EMERGENCY EXIT SIGN VERY DIM. REPLACED THE LAMPS IAW AMM 33-51-17-400-001A. OPS TESTED GOOD.Oct 19, 2018 · N660AW · Airbus A320232 · Emergency LightingSDR CALA2018101902147Spring · brokenCABIN FLOOR GIRT BAR. L1 AFT GIRT BAR FITTING SPRING BROKEN. REMOVED AND REPLACED L1 DOOR AFT GIRT FITTING SPRING IAW AMM 52-13-31-400-003.Oct 19, 2018 · N457UA · Airbus A320232 · Emergency EquipmentSDR CALA2018102002148Pin · corrodedCABIN FLOOR GIRT BAR L2 AFT SPRING RETAINING PIN CORRODED. REMOVED AND REPLACED L2 DOOR AFT GIRT FITTING SPRING PIN IAW AMM 52-13-31-400-003.Oct 19, 2018 · N457UA · Airbus A320232 · Emergency EquipmentSDR CALA2018101902145Screw · wornREMOVED AND REPLACED LOWER AFT STOP SCREW ON R2 DOOR IAW AMM 52-13-31-400-002-A SUBTASK 52-13-31-420-056-A. N LMR AFT STOP SCREW WORN BEYOND LIMITS ON R2 DOOR.Oct 19, 2018 · N420UA · Airbus A320232 · Passenger/Crew DoorsSDR AALA2018102499021Apu · odorDESCENDING OUT OF 20,000 FT, RECEIVED STRONG DIRTY SOCK ODOR IN THE COCKPIT, LASTING THOUGH SHUTDOWN AT GATE. ACCOMPLISHED JC 26L00021001, AND 26L00021002. FOUND THE SOURCE OF THE ODOR TO BE THE APU. REPLACED THE APU IAW CARD 26L31049005. OPS CHECKED GOOOct 18, 2018 · N663AW · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR AALA2018101989019Smoke Detector · false activationLAVATORY SMOKE ECAM MESSAGE APPEARED AND CLEARED ITSELF WITHIN SECONDS. LAVATORY A CHECKED AND APPEARED CLEAR. MAINTENANCE TESTED THE SMOKE DETECTOR IAW 26-17-15 AND TESTED GOOD. THE AIRCRAFT WAS GROUNDED.Oct 17, 2018 · N647AW · Airbus A320232 · Smoke DetectionSDR AALA2018102329027Cooling Fan · leakingCABIN ODOR REPORT RECEIVED. THE AIRCRAFT WAS GROUNDED. FOUND SOURCE OF ODOR TO COME FROM THE APU COMPARTMENT, APU COOLING FAN LEAKING OIL. REPLACED THE APU COOLING FAN IAW AMM 49-52-51. LEAK AND OPS CHECKED GOOD.Oct 16, 2018 · N679AW · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2018101902134Seal · damagedHUMMING NOISE AND VIBRATION IN CABIN AT ROW 21. NO SPECIFIC LOCATION NOTED. REPLACED WING TO BODY FAIRING SEALS PANEL 192DT REF AMM 53-35-11. VERIFIED SAFETY AND SECURITY OF PANEL INSTALLATION. OP CK OF EEL LIGHTING NORMAL. WING ROOT PANEL HAS EMERGENCY LIGHTIOct 16, 2018 · N409UA · Airbus A320232 · Aerodynamic FairingsSDR YENA2018101960694Battery · dischargedFLT 2074, TPA-EWR. EMERGENCY LIGHT BATTERY BY FWD L1 DOOR OVERHEAD GALLEY AREA INOP. FIN 10 WL; R & R EMERGENCY LIGHT BATTERY PER AMM 31-51-38, OPS CHECK GOOD.Oct 16, 2018 · N521JB · Airbus A320232 · Emergency LightingSDR YENA2018101960693Light · inoperativeFLT 2074, TPA-EWR. 41WL EXIT MARKING SIGN AND 100 WL 1 BLOWN DURING TROUBLESHOOTING; FIN : 41 WL ( EXIT MARKING SIGN) + FIN 100 WL (LIGHT) RELAMPED PER AMM 33-51-00. FUNCTIONS NORMALLY AFTER TESTING.Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
Back to Airbus A320-232