Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  ORDER BY difficulty_date DESC"

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SDR AALA202110117933Light · inoperativeAIRCRAFT WAS GROUNDED: SEAT 4C FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 4C EMERGENCY LIGHT HARNESS PER A320 ESPM 20-33-11-0201-1.Oct 8, 2021 · N665AW · Airbus A320232 · Emergency LightingSDR GTIA2021101136034None · noneR1 DOOR ASSIST BOTTLE LOW-SERVICED R1 DOOR ASSIST BOTTLE TOO PROPER LEVEL IAW AMM 52-10-00. LEAK CHECK GOODOct 8, 2021 · N647NK · Airbus A320232 · Passenger/Crew DoorsSDR AALA202110131724Actuator · defectiveAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATOct 7, 2021 · N660AW · Airbus A320232 · Turbine Engine Compressor SectionSDR AALA202110131345Pump · defectiveAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATOct 7, 2021 · N660AW · Airbus A320232 · Engine Fuel PumpSDR YENA2021101100673Slide Raft · failedFLT #1134, SJU-MCO. DURING EMER LT TEST REQUIRED BY R1 SLIDE R&R TEST FAILED W/ FWD ESPU L FAIL T/S IAW TSM 33-51-00-810-808-A FOUND L1 DOOR SLIDE LIGHTS CAUSING FAULT; R&R FWD LH DOOR SLIDE REFERENCE AMM 25-62-44-400-007-A OPS CHKS GOOD REFERENCE AMM 25-62-44Oct 7, 2021 · N665JB · Airbus A320232 · Emergency EquipmentSDR AALA202110081724Engine · overtempAIRCRAFT WAS GROUNDED: ENGINE # 1 ECAM MESSAGES FOR COMPRESSOR VANE FAULT, ENGINE 1 FAIL AND EGT EXCEEDED ENGINE SHUTDOWN IN FLIGHT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT PHX SAFELY WITHOUT FURTHER INCIDENT. A REVIEW OF THE DFDR DATA NOTED THATOct 7, 2021 · N660AW · Airbus A320232 · Engine Temperature Indicating SystemSDR YENA2021100700661Unknown · odorFLT 2593, JFK-MIA. F/A REPORTED ON ELECTRICAL BURNING SMELL FROM THE AFT GALLEY DURING APPROACH ; PERFORMED TSM 05-50-00-810-831-A AND 24-00-00-810-823-A. NO DEFECTS NOTED. NO BURNING ODOR NOTED. ALL CHECKS GOOD.Oct 6, 2021 · N809JB · Airbus A320232 · Air Distribution SystemSDR CALA2021100601803None · noneREFERENCE LP7161768 PLANNING TO CONTACT ENGINEERING AFTER 29-JAN -22, BUT BEFORE 28-FEB-22 FOR ECRA 5341-01271 PART 3 PERMANENT REPAIR ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5341-01271. PLANNING TO CONTACT ENGINEERING AFTER 29-JAN-Oct 6, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021100601797None · noneON HAECO LCQ REF NR 9294610 JUST FWD OF FR64 @ STRINGER 41R- STR INGER IS CORRODED GENERATED BY V899260 REMOVED AND REPLACED STRINGER 41R IN AFT CARGO IAW A320 SRM 51-7 2-11-911-001 WORK ACCOMPLISHED BY MECH V052030 AND INSP BY V0613 34Oct 6, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021100601806Engine · none4285-2 ESN V10979 DUE TO IFSD ACCOMPLISH WINDMILL INSPECTION PER AMM 72-00-00-200-021 4.A.(2)(B). REPORT FINDINGS TO TOMC EMC. FLAGGING SDR FOR FLT 2369-01 PERFORMED WINDMILL INSPECTION PER AMM 72-00-00-200-0214. A (2) (B), REPLACED MAIN PUMP OIL FILTER AND SCOct 6, 2021 · N485UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA2021100700663Brake Sys · reads lowFLT # 394, DEN-BOS. LEFT SIDE ALT BRAKE ONLY SHOWS 1000 PSI ; RIGHT BRAKE PEDAL BOTH SIDES HAS NO FEEL AND WHEN DEPRESSED ONLY INDICATES 100PSI ON TRIPLE INDICATOR (ALTINATE SYS), REF ABOVE ITEM. SVCD ALTERNATE BRAKE RESERVOIR PER AMM 12-12-32 & BOTH BRAKE PEDOct 5, 2021 · N633JB · Airbus A320232 · BrakeSDR CALA2021100601794Fitting · noneR2 DOOR LOWER SILL FWD CORNER FITTING HAS CORR - A3NB-53-3-6033 - NR 9294554 (28554) GENERATED BY V061334 AT HAECO LCQ. REMOVED & REPLACED WITH NEW R-2 DOOR LOWER SILL FWD CORNER FITTI N PER A320 UAL SRM 51-42-11/001. DOT REMOVED. ACCOMPLISHED BY V0 61737, INSOct 5, 2021 · N436UA · Airbus A320232 · Fuselage Main, FrameSDR YENA2021100500653Slat · dentedDURING HEAVY MAINTENACE, DENT ON LH SLAT 4 ; PERFORMED PERMANENT REPAIR TOP SKIN LEADING EDGE OUTBOARD LH WING SLAT 4 IAW A320 SRM 57-45-21-300-003. REPAIR IS CAT A.MDDR CLEARED ON WO 1118256 NR 00009.Oct 5, 2021 · N806JB · Airbus A320232 · Wing StructureSDR YENA2021100500652Mount Fitting · out of limitsDURING HMV, FUSELAGE (AVENT/ VIASAT2 MOD) FWD FUSELAGE/ FR33-34 & STGR 5R-6R/ SHORT EDGE DISTANCE- TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)Oct 5, 2021 · N806JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR GTIA2021100736032Seal · leakingDIRTY SOCK SMELL DURING DESCENT AND APP PROCEDUE APPLIED FOR PACK 1 ODER WENT AWAY ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )-UPON INSP. FOUNOct 4, 2021 · N634NK · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2021100601786None · noneREFERENCE VT MAE N/R #0013869 ROTO PROBE OF ADDITIONAL FASTENER HOLES PER STEP 3.2 OF EA 5330-05216 REV B OP002 FOUND SIX ADDITI ONAL FASTENER HOLES WITH CRACKS O/B OF Y+1292 24-MAR-2022 REF VT MAE N/R #0013869. REPAIRED LH PRESSURE PANEL IAW ECRA INTERIM REPAOct 4, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021100601784Bulkhead · cracked(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() COMPLIED WITH EC/RA 5321-02055 TO REPAIR FR35 STR 30 HOLE #1 RH WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT MOBILE AEROSPACOct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100601783Bulkhead · damaged(AD 2016-14-03) DURING ROTO PROBE INSPECTION OF LH FR35 BTW STGR 28 AND STG31. REJECTABLE DAMAGE INDICATIONS WAS NOTED IN 8 HOLES CIRCLED IN RED. REPAIR BEFORE FURTHER FLIGHT.() REPAIRED LH FR35 HOLES BETWEEN STGR28-31 BY COMPLYING WITH EC/RA 5321-02055 WITH NOct 4, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021100601782Bulkhead · damaged(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT LH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() REPAIR FR35 STGR30 HOLE #1 L/H BY COMPLY WITH EC/RA 5321-02055 W ITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AEROSPA CE MOBIOct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100601781Bulkhead · crackedDURING ROTO PROBE OF FASTENER HOLES AT LH FR35 STR30, A CRACK IN DICATION WAS NOTED IN THE BOTTOM AFT HOLE.() REPAIRED LH FR35 STR 30 HOLE #2 BY COMPLYING WITH EC/RA 5321-020 55 WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AER OSPACE MOBILE. NR#00Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100601780Bulkhead · none(SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, A DAMAGE INDICATION WAS NOTED AT THE BOTTOM AFT HOLE.() REPAIRED R/H FR35 STR30 HOLE #2 BY C/W EC/RA 5321-02055 WITH NO DEVIATIONS. EMP#V933440 AT BFM VT AEROSPACE MOBILE. NR#0013369Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100601779Fitting · corrodedR2 DOOR LOWER SILL AFT CORNER FITTING HAS CORR - A3NB-53-3-6033 - NR 9294552 (28552) GENERATED BY V061334 AT HAECO LCQ. REMOVED AND REPLACED R2 DOOR LOWER AFT CORNER FITTING IAW A320 S RM 51-72-11-911-001 PAR. 2D REMOVED DOT. ACCOMPLISHED BY V074845 , INSP BY Oct 4, 2021 · N436UA · Airbus A320232 · Fuselage Main, FrameSDR AALA202110050822Mechanism · lack of lubeAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR 1L DIFFICULT TO CLOSE. LUBRICATED PUSH BUTTON SWITCH AND DOOR STAY MECHANISM PER AMM 52-10-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.Oct 4, 2021 · N664AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA202110054569Light · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT ON FORWARD ENTRY PARTITION INOPERATIVE. BROKEN WIRE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY FORWARD ENTRY WALL.Oct 4, 2021 · N652AW · Airbus A320232 · Emergency LightingSDR YENA2021100400649Brake · failedFLT # 608, LAS-FLL. CHAPTER 5 INSPECTION REQUIRED DUE TO #2 TIRE BURST ; ACCOMPLISHED CHAPTER 5 TIRE BURST INSPECTION REF AMM 05-51-15. NO DEFECTS WERE NOTED AT THIS TIME. A/C IS OKAY TO CONTINUE SVC. R/R THE #1 MLG BRAKE ASSY REF AMM 32-42-27. OPS AND LEAK COct 4, 2021 · N659JB · Airbus A320232 · Brake Anti-Skid SectionSDR YENA2021100400648Brake · failedFLT # 608, LAS-FLL. CHAPTER 5 INSPECTION REQUIRED DUE TO #2 TIRE BURST ; ACCOMPLISHED CHAPTER 5 TIRE BURST INSPECTION REF AMM 05-51-15. NO DEFECTS WERE NOTED AT THIS TIME. A/C IS OKAY TO CONTINUE SVC. R/R THE #2 MLG BRAKE ASSY REF AMM 32-42-27. OPS AND LEAK COct 4, 2021 · N659JB · Airbus A320232 · Landing Gear Brake SystemSDR YENA2021100400647Landing Gear · failedFLT # 608, LAS-FLL. CHAPTER 5 INSPECTION REQUIRED DUE TO #2 TIRE BURST ; ACCOMPLISHED CHAPTER 5 TIRE BURST INSPECTION REF AMM 05-51-15. NO DEFECTS WERE NOTED AT THIS TIME. A/C IS OKAY TO CONTINUE SVC. R/R THE #1 MLG TIRE ASSY REF. AMM 32-41-11.Oct 4, 2021 · N659JB · Airbus A320232 · Brake Anti-Skid SectionSDR YENA2021100400646Brake Assy · failedFLT # 608, LAS-FLL. CHAPTER 5 INSPECTION REQUIRED DUE TO #2 TIRE BURST ; ACCOMPLISHED CHAPTER 5 TIRE BURST INSPECTION REF AMM 05-51-15. NO DEFECTS WERE NOTED AT THIS TIME. A/C IS OKAY TO CONTINUE SVC. R/R THE #2 MLG BRAKE ASSY REF AMM 32-42-27. OPS AND LEAK CHOct 4, 2021 · N659JB · Airbus A320232 · Landing Gear Brake SystemSDR YENA2021100400644Manifold · disconnectedFLT # 608, LAS-FLL. BRAKES - AUTO BRK FAULT, BRAKES - SYS 2 FAULT ; INSPECTED THE LMLG AND FOUND THE SERVO VALVE MANIFOLD DISCONNECTED (15GG, 17GG, 11GG, AND 13GG). ALSO INSPECTED WHEEL TACHOMETERS AND DID NOT NOTICE ANY DEFECTS. RECONNECTED THE CONNECTORS AT Oct 4, 2021 · N659JB · Airbus A320232 · Landing Gear Brake SystemSDR GTIA2021100436029Blower · failedEXTRACT VENT FAULT FOLLWED BY ELECTRICAL SMELL IN COCKPIT ONLY -R&R EXTRACT AND BLOWER FANS FIN(18HQ) IAW AMM 21-26-51-400 PERFOMED OPERATIONAL TEST IAW AMM 21-26-00-710-001 TEST PASS A/C GOOD FOR SERVICE.Oct 4, 2021 · N697NK · Airbus A320232 · Air Distribution FanSDR GTIA2021100436028None · noneAFT FA FLASHLIGHT NOT CHARGING -R/R AFT FA FLASHLIGHT ASSY IAW AMM 25-60-13Oct 4, 2021 · N646NK · Airbus A320232 · Escape SlideSDR YENA2021100400650Light · looseFLT # 38, SJO-FLL. OVERHEAD EMERGENCY ISLE LIGHT ABOVE ROW 18 INOP ; FOUND GROUND WIRE LOOSE - SECURED + OPS CHECK GOOD REF 35-50-00 A/C OK FOR SVCOct 3, 2021 · N793JB · Airbus A320232 · Emergency LightingSDR CALA2021100401771None · crackedWHILE AT VT MAE BFM REF N/R #0013859 (EA 5341-01231 REV ORIG) DURING HFEC INSPECTION OF THE LH FR68WEB AT DOOR STOP FITTING #1 A CRACK INDICATION WAS NOTED AT STGR 22 WEB HORIZONTAL FLANGE UPPER & BOTTOM RADUIS, CRACK LENGHT APPROX 0.663IN BEFORE 29-MAR-2022. Oct 3, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)SDR YENA2021100400643Computer · failedFLT # 316, TPA-LGA (DIVERTED TO JFK). SEC 1 FAULT ; R&R SEC 1 PER AMM 27-94-34 OPS CHECK GOOD A/C RETURNED TO SVC MCC NOTIFIEDOct 2, 2021 · N630JB · Airbus A320232 · Flight Control SystemSDR YENA2021100400642Warning Message · false activationFLT # 108, MBJ-EWR. SEC 1 FAULT INFLIGHT ; RESET CB B8. MESSAGE CLEARED AC OK FOR SVC.Oct 2, 2021 · N630JB · Airbus A320232 · Central WarningSDR YENA2021100400641Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710 .Oct 2, 2021 · N613JB · Airbus A320232 · Emergency LightingSDR YENA2021100400640Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710 .Oct 2, 2021 · N613JB · Airbus A320232 · Emergency LightingSDR YENA2021100400639Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710 .Oct 2, 2021 · N613JB · Airbus A320232 · Emergency LightingSDR YENA2021100400638Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710 .Oct 2, 2021 · N613JB · Airbus A320232 · Emergency LightingSDR GTIA2021100436025None · noneR2 DOOR ASSIST PRE-CHARGE LOW.-SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.Oct 2, 2021 · N638NK · Airbus A320232 · Passenger/Crew DoorsSDR GTIA2021100436024None · noneL1 MEGAPHONE INOP.-R&R L1 MEGAPHONE. MEGAPHONE CHECKED OK AS PER AMM 25-65-51.Oct 2, 2021 · N618NK · Airbus A320232 · Escape SlideSDR AALA202110041852Light · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT ROW 17 EMERGENCY PATHWAY LIGHT INOPERATIVE. REPLACED LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-19.Oct 2, 2021 · N662AW · Airbus A320232 · Emergency LightingSDR CALA2021100401770Oil Cooler · leakingFUEL LEAK NUMBER 2ENGINE.ENGINE SHUTDOWNIAW CHECKLIST INSTALLED MISSING BOLTS ON FCOC BOTTOM LINE AND REPLACED ORING DAMAGED IAW AMM 73-11-49/201 CONF 00, RAN ENGINE FOR LEAK CHECK, NO LEAKS NOTED. OIL SERVICE ACCOMPLISHED AT MEX FOR FLT 2369 ON 01 OCT 12:49:Oct 2, 2021 · N485UA · Airbus A320232 · Engine Fuel/Oil CoolerSDR CALA2021100401769Beam · corrodedPER NR 9296437/30437. CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL IN SEVERAL PLACES. GENERATED BY V892443 REMOVED AND REPLACED AFT CABINR2 DOOR SILL BEAM FR66-68 STR23R I AW A320 SRM 51-72-11-911-001. MECH V061619 INSP BY V892443Oct 2, 2021 · N444UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2021100401768None · damaged(AD 2019-20-10) DURING ROTO PROBE INSPECTION OF THE RH DOOR STOP FITTING #1 AT FR16. REJECTABLE DAMAGE INDICATION WAS NOTED IN UP PER I/B AND O/B HOLES DUE TO THREAD DAMAGE. () REPAIRED RH #1 DOOR STOP FITTING HOLES/AREA IAW EC/RA 5311-02639 VT MAE FINAL EA 32Oct 2, 2021 · N482UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2021100401767Skin · corrodedREMOVED CORROSION IAW SRM 51-74-00 ORIGINAL SKIN THICKNESS .063" L=1.660" W=1.020" D=.060" FOUND OT BE OUT OF LIMITS IAW SRM 53-4 1-11-283 FIG. REPAIRED IAW FINAL EC/RA 5331-02766 REV "-" AND EA 320-5341-13-A2686 REV "-" REMOVED CORROSION IAW SRM 51-74-00 ORIGOct 2, 2021 · N482UA · Airbus A320232 · Fuselage Main, StructureSDR GTIA2021100436022None · noneR 1 DOOR ASSIST NEED SERVICE-SERVICE R 1 DOOR IAW AMM 52-22-00 OPS CHECKS GOOD PRESSURE IS CORRECT FOR CONTINUE SERVICE.Oct 1, 2021 · N624NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021100401766Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y512.5 AT FR68. (A3NB-53-3-622 2) CORROSION ON FLOOR BEAM Y512.5 FR68 BLENDED OUT IAW SRM 51-74-00 SFR# 1026596. MAINTENANCE ACCOMPLISHED BY V933868 ON WC 0014619 , BLENDED AREA MEASURES LENGTH 1.5" WIDTH 0.15" ORIGINAL THICKNOct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100401765Beam · corrodedCORROSIN ON AFT CABIN FLOOR BEAM Y-1292 AT FR66. (A3NB-53-3-6222 ) BLENDED OUT CORROSION ON AFT CABIN BEAM Y-1292 AT FR66 IAW SRM 5 ING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-0 0-15-283-002 L=4.0" W=2.0" D=.046". REMOVED AND REPLACEOct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021100401764Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 AND FR68 (A 3NB-53-3-6222) BLEND OUT CORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 A E ACCOMPLISHED BY V933486 ON WC 0014617 AT ST ENGINEERING BFM ND FR68IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SOct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
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