Airbus A320-232

Service difficulty reports · 32,652

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 YENA2025061700627Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 AND 12 O'CLOCK, CRACK DEPTH IS 0.110 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKJun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061700626Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ON RH WING IAW (CPCP FINDING); REF AEROMAN WO 2025-180/1 WCC#2025-298913 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ONJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700625Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TIP SKIN LOWER SURFACE BETWEEN RIB 21 TO RIB 22 ON RH WING (CPCP FINDINGS); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00042) AEROMAN WO# 2025 180/1 WCC 2025-2984859 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700624Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10") TO RIB 19 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00044) AEROMAN WO 2025-180/1 NR 2025-298902 FOR WORK PERFORMED; PERFORMED BLEND OUT Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700623Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 TO RIB 17 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00053) AEROMAN WO 180/1 NR# 2025-298901 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR LOCATED Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700622Skin · corrodedDURING HEAVY MAINTENANCE: AEROMAN WO# 180/1 NR# 2025-298911 FOR WORK PERFORMED: PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVERHANG AREA, BTW RIB 14 (PLUS 17 INCHES) TO RIB 15, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITSJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700621Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 15 (PLUS 16") TO RIB 16 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00055) REF TASK CARD 72179-01-1-575 JB WO# 1389906 PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SUJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700620Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10 INCHES) TO RIB 19 ON LH WING; TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCAION TRAILING EDGE TOP SKIN LOWER SURFACE RIB 18 PLUS 10 INCHES TO RIBJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700619Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 (PLUS 15 INCHES) TO RIB 17 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00057) TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCATED TRAILING EDGE TOP SKJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700618Skin · damagedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TEOH BTWN RIB 15 - 19 / LOWER SURFACE / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0046-25 REV 0 (COVER AND PARTS 1 - 4) /2/ AIRBUS RDAF 81592930/005/2025#A /3/ AIRBUS DOSSIER 8159Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061600610Duct · detachedFLT#1058,AUA-JFK. (AIRCRAFT DIVERTED TO SJU) .'ECAM:EXCESSIVE CABIN ALTITUDE MAX CABIN ALT REACHED WAS 11,900; PERFORMED PACK # AND #2 FOUND PACK #1 AIR DUCT HOSE OUT OFF POSITION ALSO VERIFY ALL CLAMPS, HOSE AND SENSOR TEMP, PRESS AND FLOW FOUND LOOSE ADJUSTEJun 13, 2025 · N615JB · Airbus A320232 · Cabin Cooling SystemSDR CALA2025062605895Seat Track · corrodedMAIN CABIN L/H O/B SEAT TRACK Y1292 HAS PITTING AND GOUGES ALONG TRACK FROM FR 46+14" TO FR64. EVALUATED CORROSION ON Y1292 LH, FOUND TO BE OUT OF LIMITS IAW A 320 SRM 53-41-15-283-001. REMOVED Y1292 L/H SEAT TRACK FROM FR47 TO FR64 TO FOAM IAW A320 SRM 51-42Jun 12, 2025 · N465UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA2025061238955Relay · faulty#2 CENTER TANK PUMP INOP-PERFORMED TSM 28-21-00-810-818-A AND FOUND GFI 70QA TRIPPED. RESET AND OPS CHECKED CTR TANK PUMP IAW AMM 28-18-00-710-8010-A. REPLACED RELAY 52QA FOR PRECAUTIONARY IAW ESPM 20-46-50. ALL OPS CHECKS GOOD. NO FAULTS NOTED AT THIS TIME . Jun 12, 2025 · N698NK · Airbus A320232 · Fuel Boost PumpSDR AALA202506164121Elec Connector · looseAIRCRAFT WAS NOT GROUNDED: 11C EMERGENCY MOUNTED SEAT LIGHT INOP. MAINTENANCE RECONNECTED LOOSE CONNECTOR AT WALL DISCONNECT. OPS CK GOOD IAWAMM 33-51-00-710-007-A.Jun 11, 2025 · N601AW · Airbus A320232 · Light System WiringSDR YENA2025061100584Outflow Valve · failedFLT#195, HPN-MCO (AIRCRAFT DIVERTED TO JFK). 'CAB PR EXCESS CAB ALT ECAM AT FL 320 TO 10500 FT. AS WE INITIATED EMG DESCENT CABIN ALT REMAINED OVER 10000 FT AS WE MADE OUR RAPID DESCENT TO 10K; REMOVED AND REPLACED OUTFLOW VALVE IAW AMM 21-31-51. OPS CHECK GOOJun 11, 2025 · N506JB · Airbus A320232 · Pressure Regulator/Outflow ValveSDR YENA2025061300602Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.085 INCH, AT AFT GALLEY AREA (1 EA); AEROMAN PERFORMED REPAIR. PER SRM 53-41-12Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300601Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC. BTW FR59 TO FR60 AND BTW STR29 TO STR30 LH SID E AT LOWER USELAGE; (RESOLVED ON W/O: 1354689 TASKCARD: NR-00023) PERFORMED DETAIL VISUAL INSPECTION AND NOT FOUND DENT ONLY SCRATCH IAW NTM 51-90-00 THEN PERFORMEJun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025061300600Splice · corrodedDURING HEAVY MAINTENANCE: CORROSION SPLICE LOCATED BTW FR30 TO FR31 AND STR41L IN FWD CARGO COMPARTMENT (CPCP FINDING ); (RESOLVED ON W/O: 1354689 TASKCARD: NR-00027) REMOVED AND REPLACED SPLICE LOCATED BTW FR30 TO FR31 AND STR41L IN FWD CARGO COMPARTMENT I.A.Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300599Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON FRAME SEGMENT (1) BOTH SIDES LOCATED ON EME RGENCY EXIT DOOR (834), TOTAL CRACK LENGTH: 3.4 INCH APPROX MUST BE AC COMPLISHED SERVICE BULLETIN A320-52-1144 FOR THE NEXT FURTHER FLIGHT; (RESOLVED ON W/O: 1354Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300598Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON FRAME SEGMENT (1) BOTH SIDES LOCATED ON EMERGENCY EXIT DOOR (843), TOTAL CRACK LENGTH: 3.10 INCH APPROX MUST BE A CCOMPLISHED SERVICE BULLETIN A320-52-1144 FOR THE NEXT FURTHER FLIGHT. REMOVED AND REPLACED Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300597Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATIONS FOUND ON FRAME SEGMENT (1) BOTH SIDES LOCATED ON EME RGENCY EXIT DOOR (833), TOTAL CRACK LENGTH: 3.15 INCH APPROX MUST BE A CCOMPLISHED SERVICE BULLETIN A320-52-1144 FOR THE NEXT FURTHER FLIGHT; (RESOLVED ON W/O: 135Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300596Door Frame · crackedDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATIONS FOUND ON FRAME SEGMENT (1), BOTH SIDES LOCATED ON EME RGENCY EXIT DOOR (844), TOTAL CRACKLENGTH: 3.50 INCH APPROX MUST BE ACCOMPLISHED SERVICE BULLETIN A320-52-1144 FOR THE NEXT FURTHER FLIGHJun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300595Crossbeam · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON NOSE FWD FUSELAGE/CROSSBEAM SPLICING FR16 LH HOLE 2, CRACK DIRECTION 2 O'CLOCK, CRACK LENGTH 0.105 INCHES; (RESOLVED ON W/O: 1354689 TASKCARD: NR-00032) PERFORMED REPAIR LOCATED FR 16 LH FRAME LAYER ONLY TO HOLE 2 Jun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300594Skin · damagedDURINH HEAVY MAINTENANCE: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 69 BTW STR17L TO STR19L UPPER FUSELAGE(FOR A320 AGING AIRCRAFT PROGRAM ); (RESOLVED ON W/O: 1354689 TASKCARD: NR-00033) PERFORMED PERMANENT REPAIR LOCATED FR69 BTWJun 10, 2025 · N760JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025061300593Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. AT LEVEL OF FRAME 66 LH SIDE AT AFT GALLEY AREA (CPCP FINDING ); (RESOLVED ON W/O: 1354689 TASKCARD: NR-00035) REFERENCE AEROMAN W..O. 2025 133/1 NR 2025 - 282021 * PERFORMED REWORK AND EVALUATED REWORKED ARJun 10, 2025 · N760JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025061305530None · noneREMOVED FWD LH EXIT HATCH IAW AMM 52-21-11-000-001-A AND INSTALLED LOCKPIN ON LH INFLATION RESERVOIR IAW AMM 25-62-00-481-001-A INSTALLED FWD LH EXIT HATCH IAW AMM 52-21-11-400-001-A AND REMOVED LOCKPIN FROM LH INFLATION RESERVOIR IAW AMM 25-62-00-081-001-A INJun 10, 2025 · N437UA · Airbus A320232 · Standard Practices/StructuresSDR YENA2025061100583Lgciu · failedFLT#690, FLL-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) .'EIS DMC #3 INOP; REMOVED AND REPLACED #1LGCIU IAW AMM 32-31-71. OPS CHECK GOOD SEE ITEM#2 FOR DMC #1 RESOLUTION.'Jun 10, 2025 · N645JB · Airbus A320232 · Central DisplaySDR YENA2025061100581Unknown · odorFLT#1941, BOS-SRQ. 'STRONG MAGIC MARKER SMELL FROM T/O THROUGH FL 200 NOTICED BY FLIGHT CREW & CABIN CREW LEVEL 3 EVENT . O2 MASK USED BY CAPT & FO; C/W WITH INFORMATION NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TAPE 10 SUSPECT SMELL COMES FROM RESIDUAL SOLJun 10, 2025 · N763JB · Airbus A320232 · Air Distribution SystemSDR AALA202506101176Power Supply · no testAIRCRAFT WAS NOT GROUNDED: LEFT EMERGENCY EXIT EPSU FAILED TEST. MAINTENANCE REPLACED LEFT EMERGENCY EXIT EPSU BATTERY PER AMM 33-51-38.Jun 10, 2025 · N658AW · Airbus A320232 · Emergency LightingSDR GTIA2025061838961Hydraulic Line · leakingDURING DESCENT FROM APPX 260 HYD SYS G LO LVL, LOSS OF HYD SYS G.-PERF. LEAK CHECK OF #1 ENG HYD LINES FOUND PYLON GRN SYS PRESS PIPE (2) LEAKING, R/R IAW AMM 29-11-49. OPS & LEAK CK GOOD.Jun 9, 2025 · N643NK · Airbus A320232 · Hydraulic System, MainSDR YENA2025061100579Oil System · leakingFLT#1858, AUA-JFK. 'FUME IN COCKPIT DESCENDING BELOW 12K DIRTY SOCK SMELL. NO ODOR IN BACK, FA'S SAID NOTHING; PERFORMED DETAILED VISUAL INSPECTION OF APU, FOUND NO EVIDENCE OF OIL OR LEAKS. SERVICED 1QT OF OIL PER AMM 12-13-49. PACK BURN ACCOMPLISHED PER INFOJun 9, 2025 · N598JB · Airbus A320232 · APU Oil SystemSDR YENA2025061000577A/C Pack · odorFLT#1248, TPA-LGA. ' OIL SMELL 15 SECONDS AT 12000 FT. DID ODOR RECOGNITION CHECKLIST. ODOR WENT AWAY AFTER WE ISOLATED THE PACK; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A. ISOLATED FAULT TO TYPE 10 AMBIENT AIR PER TSM 05-50-00-810-831-A. A/C IS OKJun 9, 2025 · N657JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2025061000576Unknown · odorFLT#1084, MCO-JFK. 'FUME IN COCKPIT DESCENDING BELOW 12K DIRTY SOCK SMELL. NO ODOR IN BACK, FA'S SAID NOTHING; PERFORMED DETAILED VISUAL INSPECTION OF APU, FOUND NO EVIDENCE OF OIL OR LEAKS. SERVICED 1QT OF OIL PER AMM 12-13-49. PACK BURN ACCOMPLISHED PER INFOJun 9, 2025 · N630JB · Airbus A320232 · Air Distribution SystemSDR CALA2025061205488Proximity Sensor · dirtyDOOR 2L SHOWS ARMED ONECAM. BUT F/A SAYS DOORSHOWING DISARMED. CLEANED ARM/UNARMED PROX SENSOR, NO HELP REMOVED AND REPLACED ARMED/UNARMED PROX SENSOR DOOR 2L REF AMM 52-71-11, AJUSTED AND OPS CHECK GOOD PER AMM 52-71-00 VERIFIED REPLACEMENT OF #2 L DOOR PROX Jun 8, 2025 · N438UA · Airbus A320232 · Door Warning SystemSDR CALA2025061205487Warning Message · activatedCABIN PRESSURE - LO DIFF PRESSURE RECEIVED AT 2000 ON APPROACH. FOLLOW TSM 21-31-00-810-810-A TO ISOLATE. T/S REF TSM 21-31-00-810-810-A FOUND NO FAULTS STEP 3.B. NO M/X ACTION REQUIREDJun 8, 2025 · N452UA · Airbus A320232 · Cabin Pressure Control SystemSDR CALA2025061105460Beam · corrodedFLOOR TRIPPLE BEAM IN FRONT OF L1 DOOR BETWEEN FR16-20 HAS AREAS OF MINOR SURFACE CORROSION. REMOVED AND REPLACEDS SEAT TRACK FROM FR12-FR24 IAW A320 SRM 51- 72-11.Jun 8, 2025 · N465UA · Airbus A320232 · Fuselage Main, StructureSDR AALA202506095251Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY OPERATION ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED R1 DOOR ACCUMULATOR BOTTLE IAW AMM 52-10-00.Jun 8, 2025 · N657AW · Airbus A320232 · Passenger/Crew DoorsSDR GTIA2025060938949Megaphone · inoperativeR2 MEGA PHONE NOT WORKING -R+R R2 MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD. MOC # 69661Jun 8, 2025 · N605NK · Airbus A320232 · Emergency EquipmentSDR YENA2025061300592Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325635. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 1 & 3 );Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300591Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325666. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 2 ); (Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300590Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325667. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 4 ); (RESJun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300589Hinge Fitting · brokenDURING HEAVY MAINTENANCE: BROKEN HINGE FITTING HINGE 3 ELEVATOR LH; REF: ARM W/O 2025-181/1 N/R # 2025-325674. PERFORMED PERMANENT REPAIR ON HINGE FITTING HINGE 3 ELEVATOR LH IAW A320 SRM 55-26-41-300-001, REPAIR IS CATEGORY A.Jun 7, 2025 · N606JB · Airbus A320232 · Elevator StructureSDR CALA2025061205479None · none2L SLIDE PRESSURE IN THE RED ZONE INSPECTED SLIDE GAUGE AND FOUND IT TO BE WITHIN NORMAL LIMITS. OKAY FOR CONTINUED SERVICEJun 7, 2025 · N429UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2025061005416Filter · cloggedPLANE HAS STRONGODORTHANKSWITH PACKS ON THE AIR DISTRIBUTION SENDING A STRONG PUNGENT SMELL IN CABIN MORE CONCENTRATED AT LEFT AND RIGHT OVERWING SECTION, REF FIM05-50-00-810-831-A ALSO FIM 05-51-10-200-801-C-1. FOLLOWING DECISION TABLE IN TSM 05-50-00-810-Jun 7, 2025 · N434UA · Airbus A320232 · Air Distribution SystemSDR YENA2025060900575Rivet · leakingFLT#488, MCO-ORH. (AIRCRAFT DIVERTED TO BOS). 'EXTREMELY LOUD SQUEAL DEVELOPED OVERHEAD BY THE COCKPIT DOOR, AT FL 370, CABIN PRESS 7400 FT. DESCENDED TO FL 330, CABIN PRESS 6050 FT SQUEAL STOPPED AFTER 10-15 MIN; REF LPG 4324310 ITEM 2 AND LPG 4324311 ITEM 2 Jun 7, 2025 · N634JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025060900573Pressure Switch · leakingFLT#436, STI-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) HYD B RSVR LO LVL ECAM WHILE IN CRUISE; REF LP 427922, ITEM 1 (REMOVED AND REPLACED BLUE HYD PUMP DUE TO CAVITATION LEAKS CHECKS GOOD IAW AMM 29-12-51) AND 2 (REPLACED THE FILTERS FOR THE BLUE HYD ANDJun 7, 2025 · N537JT · Airbus A320232 · Hydraulic System, MainSDR YENA2025060900572Proximity Switch · looseFLT#530, MCO-BQN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO MCO) ON CLIMBOUT, FA CALLED AND INDICATED DOOR 1L PRESSURE LIGHT ILLUMINATED WE WERE AT 3500 AND LEVEL D OFF. DOOR PAGE SHOWED 1L DOOR UNARMED-RETURNED TO MCO AND LANDED AT 147,200 VAPP 135 LANDED AT 25Jun 6, 2025 · N519JB · Airbus A320232 · Service DoorsSDR CALA2025060905360Wire Harness · damagedSEAT 38C EMERGENCY LIGHT IS INOP REMOVED AND REPLACED SEAT 38C EMERGENCY LIGHT SEAT HARNESS. PEFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 33-50-00.Jun 6, 2025 · N470UA · Airbus A320232 · Light System WiringSDR CALA2025061105457Window Frame · crackedWINDSHIELD FRAME LH AND RH CONTINUITY FITTING HAS CRACK INDICATI ON ON UPPER LEG APPROX. .400 IN OB FROM CRT POST. PER HAECO LCQ NON ROUTINE 9298538/28538 GENERATED BY V892444 ESFR COMPLETE. REMOVED & REPLACED WINDSHIELD FRAME L/H & R/H CONTINUITY FITTING PER Jun 5, 2025 · N465UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2025060900574Controller · failedFLT#991, FLL-SJU. (AIRCRAFT DECLARED AN EMERGENCY INTO SJU) 'IN CRUISE AL FL 350- ECAM-CAB PR SYS 2 FAULT; REMOVED AND REPLACED CPC-2 REF AMM 21-31-34 OPS CHECK NORMAL.'Jun 5, 2025 · N649JB · Airbus A320232 · Cabin Pressure Controller
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