Airbus A320-232

Service difficulty reports · 32,652

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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"

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 CALA2025040703574Slide · not disengagedFA OPENED L2 DOOR BEFORE DISARMING AT GATE. SLIDE DID NOT DEPLOY NOT ABLE TO CLOSE DOOR, DEACTIVATED ESCAPE SLIDE SYSTEM TO PERFORM DOOR DAMPER DIAPHRAM REPLACEMENT. REF AMM 25-62-44. VERYFIED SLIDE DEACTIVATION IAW REF.AMM 25-62-44-000-002-A VERYFIED SLIDE DApr 1, 2025 · N425UA · Airbus A320232 · Escape SlideSDR CALA2025040403533Stop Fitting · crackedCRACK INDICATION AT RH FR68 DOOR STOP #1 AT 6 OCLOCK HRS POSITIO N LOWER I/B HOLE. ESFR COMPLETEDApr 1, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2025040300364Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43 LOC BTW FR57 TO FR59 IN AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1381650 TASKCARD: NR-00003) REFERENCE AEROMAN NR 2025-221681. REMOVED AND REPLACED PERMANENT REPAIR LOC ON STRINGER 43L LOC BTW FR 57 TO FR 59 IN AApr 1, 2025 · N554JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025040300363Structure · within limitsDURING HEAVY MAINTENANCE: CORROSION T/E OVERHANG BTW RIB 8 AND RIB 9 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1381650 TASKCARD: NR-00004) REFERENCE AEROMAN NR 2025-221712.PERFORMED REWORK ON RIB 7A (WX 4013) PLUS 7.800 IN ON LH WING AND FOUND WITHIN THE ALApr 1, 2025 · N554JB · Airbus A320232 · Wing Main, Frame StructureSDR YENA2025040200356None · noneFLT#2637, JFK-STI. 'WE ENCOUNTERED SEVERE TURBULENCE ON DEPARTURE LASTING 2 - 3 MINUTES CLEAN CONFIGURATION AND BETWEEN 5000-9000 FEET NO ADVERSER EFFECTED NOTED AFTER. AIRSPEED WAS 250-260 KTS INDICATED; PERFORMED AMM 05-51-17 INSPECTION AFTER FLIGHT EXCESSIVApr 1, 2025 · N607JB · Airbus A320232 · Standard Practices/StructuresSDR CALA2025040203448Stringer Splice · corrodedAFT WET AREA STRG 24RH ANGLE SPLICE CORRODED @ FRM 70. GENERATED BY V937268 ON HAECO LCQ NR 9292694/34694 SFR COMPLETED FOR LP 4361893 REMOVED SPLICE ON AFT AREA STGR 24RH FR 70 IAW A320 SRM 51-42-11 /001 REV 152 REPLACED SPLICE ON AFT AREA STGR 24RH FRM 70 IAApr 1, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2025040103373Gauge · cloudySLIDE PRESSURE GAUGE - VISIBILITY POOR AT DOOR 2L REMOVED L2 DOOR SLIDE. REF AMM 25-62-44 REPLACED L2 DOOR SLIDE. REF AMM 25-62-44. VEREFIED DOOR 2L SLIDE PART NUMBER IS CORRECT REF IPC 25-62-04-02W. VEREFIED PROPER INSTALLATION REF MM 25-62-44-400-006. VEApr 1, 2025 · N463UA · Airbus A320232 · Escape SlideSDR CALA2025040303483Cover · detachedDOOR L AFT EMER EXIT ECAM DUE TO COVER FALLING OFF PRESSURIZATIO N NORM VERIFIED ECAM MESSAGE DISPLAYS WHEN LEFT HAMD AFT EMERGENCY EXIT COVER IS REMOVED AND DISAPPEARS WHEN COVER IS INSTALLED. RE-INSTALLED COVER AND SECURED. NO FAULTS NOTED AT THIS TIME.Mar 31, 2025 · N1902U · Airbus A320232 · Emergency ExitsSDR YENA2025040200353Filter · contaminatedFLT#1519, BOS-MIA. 'ODOR/FUMES TRANSIENT IN CLIMB. DISSIPATED PACK 1 SELECTOR OFF RETURNED WITH DELECTION OF PACK 1 IN DECENT BECAME LEVEL 2-3 WITH APU AND PACKS; C/W INFO NOTICE 2017-T015, SECTION B2 IDENTIFIED ODOR REPLACE RECIRCULATION FILTERS DECONTAMINATIMar 31, 2025 · N665JB · Airbus A320232 · Air Distribution SystemSDR YENA2025040200352Windshield · crackedFLT#1454, SJU-FLL. (AIRCRAFT DECLARED AN EMERGENCY INTO FLL) 'ANTI ICE LEFT WINDSHIELD OUTER PANE CRACKED. EMERGENCY, LANDED UNEVENTFUL.' (SUPPLEMENTAL INFORMATION TO FOLLOW)Mar 31, 2025 · N804JB · Airbus A320232 · Flight Compartment WindowsSDR YENA2025040200351Wire · burnedFLT#765, JFK-GCM. 'IN-FLT REPORTED AN ELECTRICAL BURNING SMELL BETWEEN ROWS 9-10 DEF. SMELL DISSIPATED ONCE IFE SYSTEM WAS TURNED OFF ( THALES AVANT IFE (ENTIRE SYSTEM) ); REACTIVATED AVANT SYS AND PERFORMED AIRCRAFT WIRING INSPECTION AND COMPONENT INSPECTION Mar 31, 2025 · N766JB · Airbus A320232 · Air Conditioning System WiringSDR CALA2025040303469Target · out of adjustDOOR L FWD EMER EXIT ECAM IN FLT DURING DESC ENT. FOUND FLAP COVER TARGET ON L FWD EMERGENCY EXIT DOOR OUT OF RANGE, ADJUSTED TARGET ON FLAP COVER REF AMM 52-71-13-400-001-A. ECAM MESSAGE NO LONGER PRESENT AND SYSTEM OPERATES NORMALLY REF TSM 52-21-00-810-80Mar 30, 2025 · N457UA · Airbus A320232 · Accessory CompartmentSDR YENA2025040200354Microphone · failedFLT#2476, SJU-BDL. (AIRCRAFT PERFORMED AN AIRTURN BACK TO SJU) ACP ONE WENT INTO TRANSMIT CAP SIDE SPEAKER WOULD HAVE TRANSMIT TONER P.A. BUTTON INOP ON ACP ALONG W/ 02 MASK MICROPHONE. COULD NOT TRANSMIT AT ALL FROM ACP 1.' ; C/W TSM 23-12-00-810-828-A AND FOMar 29, 2025 · N708JB · Airbus A320232 · Communications SystemSDR CALA2025040203443Slide · unknownFORWARD DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0020} - L1 DOOR SLIDE REQS REPLACEMENT R/R L1 DOOR ESCAPE SLIDE IAW AMM 25-62-44. CIDS TEST GOOD.Mar 29, 2025 · N444UA · Airbus A320232 · Escape SlideSDR YENA2025033100343Slat · damagedFLT#891, BOS-TPA.' BIRD STRIKE R WING LEADING EDGE OUTBOARD OF ENGINE; REMOVED AND REPLACED RH SLAT #2 REFERENCE AMM 27-84-64. OPS CHECK GOOD AT THIS TIME REFERENCE AMM 27-84-00.Mar 29, 2025 · N509JB · Airbus A320232 · Leading Edge DevicesSDR CALA2025040103387Cleat · corrodedFWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-F3R. FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-43R ESFR COMPLETED REMOVED AND REPLACED FWD CARGO CLEAT AT FR31 STR 42R-43R IAW A32 0 SRM 51-72-11-911-001.Mar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025040103384Fitting · corrodedR2 PAX DOOR LOWER FWD CORNER ANGLE FITTING CORRODED. GENERATED B Y V937268 PER HAECO LCQ NR 9292674/34674. REMOVED AND REPLACED CORNER FITTING AT R-2 PAX DOOR LOWER FWD IAW A320 SRM 51-42-11, SRM 51-72-11 REMOVED AND REPLACED CORNER FITTING AT R2 PAX DOOR LOWEMar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025040103383Door Sill · corrodedL2 DOOR SHAPE SILL HAS CORROSION. REMOVED AND REPLACED L2 DOOR SHAPE SILL IAW SRM A320-51-72-11-911-001. REMOVED AND REPLACED L2 DOOR SHAPE SILL IAW SRM A320 51-72-11-91 1-001.Mar 28, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025040103381Cleat · corrodedFWD CARGO CLEAT HAS CORROSION FR 31 STR 43R-43L. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R-43R IAW A320 SRM 51-72-11-911-001 WPB V061616. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R- 43A IAW A320 SRM 51-72-11-911-00Mar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025033100344Unknown · odorFLT#1453, FLL-SJU. 'VOMIT / RANCID SMELL ON TAKE OFF ROLL; PERFORMED DECONTAMINATION BOTH PACKS AND REPLACEMENT BOTH EPA FILTER ALSO PACK BURN ALSO OPEN APU CLEAN WITH ALCOHOL RUN INSPECTED NO LEAK AT THIS TIME CLOSED AND SECURED BOTH DOORS AS PER INFO.NOTICE Mar 28, 2025 · N623JB · Airbus A320232 · Air Distribution SystemSDR AALA202503316751Circuit Breaker · trippedAIRCRAFT WAS GROUNDED: "C/B TRIPPED REAR PANEL J-M" (SEE CURRENT BRAKE FAN MEL) DISPLAYED ON UPPER ECAM WITH SIMULTANEOUS DISCONNECT OF AUTO PILOT ANDAUTO THRUST. A/P RECONNECTED BUT AUTO THRUST WOULD NOT INITIALLYRECONNECT. WHEN AUTO THRUST DID LATER REENGAGEMar 28, 2025 · N651AW · Airbus A320232 · Landing Gear Brake SystemSDR CALA2025040103380Floor Support · corrodedL2 DOOR FWD AND AFT GIRT BAR FITTING MAIN STRUCTURE HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-911-001.Mar 27, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025033100341Servo · faultedFLT#21, BOS-PBI. (AIRCRAFT DIVERTED TO JFK). 'ELAC #1 AND #2 FAULT CLIMB AND CRUISE ELEVATOR PITCH OSCILLATIONS; REF LP 4239540 (ELAC # 2 REINSTALLED AFTER MX PER AMM 27-93-33. OPS CHECK OK. CATIII TEST REQ), 4239545 (REMOVED AND REPLACED LH ELEVATOR SERVO 34 Mar 27, 2025 · N651JB · Airbus A320232 · Stabilizer Control SystemSDR CALA2025032803281Stringer Splice · corrodedFWD CARGO STRINGER SPLICE HAS CORROSION FR 31 STR 41L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR41L I/A/W A320 SRM 51--42-11-001. W/P/B V075620 REMOVED AND REPLACED FISHPLATE(SPLICE) @ FWD CARGO FR31 STR 41L IAW A320 SRM 51-42-11/001.Mar 27, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2025040103379Bracket · crackedOB CROSSBEAM TO FRAME CONNECTING BRACKET AT FR 68 LEFT HAND IS C RACKED AT FASTENER HOLE. REMOVED AND REPLACED O/B CROSSBEAM TO FRAME CONNECTING BRACKET A T FR 68 IAW SRM A320 51-72-11-911-001.Mar 26, 2025 · N460UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025040103370Linkage · out of adjustTHIS IS THE 3RD LEVEL 2 CHRONIC FWD CARGO DOOR ECAM, WORK WITH MEL 4280311. REF TSM 52-31-00-810-801-A FOR TROUBLESHOOTING. REF LOG PG 3814370 THERE WAS ISSUE WITH HANDLE TARGET, THAT PROX SW (28WV) WAS REPLACED BUT WAS A TARGET ALIGNMENT ISSUE, ENSURE THAT TAMar 25, 2025 · N424UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2025032703247Stringer Splice · corrodedFWD CARGO STRINGER SPLICE HAS CORROSION FR 31 SRT 43L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR43L IAW 51-72-11. REMOVED AND REPLACED FISHPLATE SPLICE @ FWD CARGO FR 31 STR 43L IAW A320 SRM 51-72-11-911-00.Mar 25, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025032600335A/C Pack · fumesFLT#1588, SXM-JFK. 'LEVEL 1 FUMES EVENT FROM PACK 1 IN THE DESCENT AT 11000FT DID ISOLATION PROCEDURE AND AFTER 3-5 MIN THE SMELL BACK SO LEFT PACK 1 OFF AND BLEED SHUT FOR THE REST OF THE FLIGHT . FA DID NOT SMELL ANYTHING ; ACCOMPLISHED LEVEL C DECONTAMINATMar 25, 2025 · N715JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2025032600332Unknown · odorFLT#1483, JFK-MCO. 'FUME EVENT ON DESC. OLD SOCK SMELL LEVEL 2 PASSING 6000 FT, STRONG ODOR CONTINUED AFTER LANDING. ( APU SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)Mar 25, 2025 · N552JB · Airbus A320232 · Air Distribution SystemSDR YENA2025032600331Oil System · leakingFLT#65, BOS-RSW. ' DURING DESCENT BELOW FL10 WITH HP VLVS OPEN - CP CREW EXPERIENCED AN ODOR EVENT THAT LASTED UNTIL TOUCHDOWN (PACKS); COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. IDENTIFIED ODOR (LEAKS FOUND IN THE APU AFT DRAIN) DECONTAMINATION LEMar 25, 2025 · N597JB · Airbus A320232 · APU Oil SystemSDR YENA2025032600330Unknown · odorFLT#808, STT-SJU. ' DESCENDING THRU 6000 I GOT A CALL REAR REPORTING STRONG BURNT RUBBER / ELECTRICAL / CHEMICAL SMELL THIS ODOR WAS PRESENT FROM AFT GALLEY TO ROW THE TWO AFT FA STATED THEY FELT DIZY AND NAUSEOUS BOTH BLEED AND PACKS WERE ON APU THE ODOR DISAMar 25, 2025 · N703JB · Airbus A320232 · Air Distribution SystemSDR YENA2025032600329Controller · malfunctionedFLT#1510, SDQ-JFK. 'ON DESCENT -CAB PR EXCESS CAB ALT -DOOR L AFT CABIN -DOOR R AFT CABIN; REF SUBSEQUENT L/P'S 9217, 9218 FOR T/S & R&R OF COMPONENTS, AFTER T/S AND PRECAUTIONARY R&R OF CPC1 SDAC 1 DIFFERENTIAL PRESS SQ. PERFORMED CABIN PRESSURIZATION TEST PEMar 25, 2025 · N603JB · Airbus A320232 · Cabin Pressure ControllerSDR YENA2025032600328Unknown · odorFLT#221, BOS-PBI. 'INFLIGHT REPORTED DIRTY SOCK / CHEMICAL SMELL THROUGHOUT CABIN LAST 5 MINS OF FLIGHT INCREASING INTENSITY; INSPECTED APU - NO EVIDENCE OF OIL LEAKS COMPLIED WITH INFONOTICE 2017-T015 SEC B2 ACCOMPLISHED DECONTAMINATION PER AMM 05-50-00 WITH Mar 25, 2025 · N629JB · Airbus A320232 · Air Distribution SystemSDR AALA202504071775Duct · blownAIRCRAFT WAS GROUNDED: AFTER TAKEOFF NAC TEMP FLASHING ON RIGHT ENG. TEMP UP TO 380.EGT RIGHT ENGINE 630. NAC TEMP REMAINS FLASHING AT 320 IN SLOWCRUISE. RT ENG MADE SURGING SOUND AT THRUST SET AT TAKEOFF. NO ASYMMETRIC THRUST FELT. AIRCRAFT DIVERTED TO TUMar 24, 2025 · N650AW · Airbus A320232 · Engine Temperature Indicating SystemSDR AALA202503271775Duct · blownAIRCRAFT WAS GROUNDED: AFTER TAKEOFF NAC TEMP FLASHING ON RIGHT ENG. TEMP UP TO 380.EGT RIGHT ENGINE 630. NAC TEMP REMAINS FLASHING AT 320 IN SLOWCRUISE. RT ENG MADE SURGING SOUND AT THRUST SET AT TAKEOFF. NO ASYMMETRIC THRUST FELT. AIRCRAFT DIVERTED TO TUMar 24, 2025 · N650AW · Airbus A320232 · Pneumatic SystemSDR YENA2025032600326Unknown · odorFLT#251, HPN-RSW. 'INFLIGHT ADVISES CABIN ODOR DURING DESCENT. ODOR IMPROVED UPON DEPLANNING; PERFORMED PACK BURN IAW AMM 21-00-00 PACK OPERATES NORMAL NO ODOR MX 4 UPDATED PLACARD REMOVED,'Mar 24, 2025 · N517JB · Airbus A320232 · Air Distribution SystemSDR CALA2025032603211Cleat · corrodedFWD CARGO CLEAT HAS CORROSION FR 31 STR 41R-42R. INSTALLED CLEAT @ FWD CARGO FR 31 STR 41R-42R I/A/W A320 SRM 51-72-11. W/P/B V075620 REMOVED AND REPLACED CLEAT FWD CARGO FR31 STR 41R-42R IAW A320 S RM 51-42-11-001 P6.Mar 24, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025032503186Lamp · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - CIDS EMERG LIGHT TEST FAILS: EPSU INT LOAD FWD LH, ATA 33-51-38 RPLCD LAMPS AT LH LWR EXIT SIGN, CIDS EMERG LTS PASS REF AMM 33-51-38Mar 24, 2025 · N445UA · Airbus A320232 · Emergency LightingSDR GTIA2025032438819Fan · failedON DESCENT LOUD HUMMING SOUND LIKE A FAN GOING BAD FOLLOWED WITH AN ELECTRICAL ODOR IN FLIGHT DECK-PERFORMED OPS CHECK OF EXTRACT AND BLOWER FANS IAW AMM 21-26-51 OPS CHECK GOOD WITH NO ODOR NOTICHED AC OK FOR SERVICEMar 24, 2025 · N619NK · Airbus A320232 · Air Distribution FanSDR CALA2025032703252Skin · corrodedAFT CARGO LH FR58, STRG 43L HAS CORROSION. BLENDED CORROSION ON FR58, STRG 43L. DETERMINED TO BE OUT OF LIM ITS IAW SRM 53-41-13-283-002, FIG 1, SHEET 1. MAX REWORK DEPTH B EYOND 10 PERCENT OF NOMINAL THICKNESS. FLOW CHART TAKES YOU TO S RM 53-41-13 BUT FR58 NMar 23, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025032600325Power Supply · failedFLT#714, FLL-HPN.' WITH NO POWER ON AIRCRAFT GPU AND APU OFF, AND EMER LIGHT SWITCH IN THE ON OR AM POSITION, CABIN EMER. LIGHTS DOES NOT COME ON; REMOVED AND REPLACED 10WL EPSU AND BATT PACK IAW AMM 33-51-38 REF LP 4245975-2 (REMOVED AND REPLACED 11WL EPSU & Mar 23, 2025 · N655JB · Airbus A320232 · Emergency LightingSDR YENA2025032600324Battery · failedFLT#714, FLL-HPN.' WITH NO POWER ON AIRCRAFT GPU AND APU OFF, AND EMER LIGHT SWITCH IN THE ON OR AM POSITION, CABIN EMER. LIGHTS DOES NOT COME ON; REMOVED AND REPLACED 10WL EPSU AND BATT PACK IAW AMM 33-51-38 REF LP 4245975-2 (REMOVED AND REPLACED 11WL EPSU & Mar 23, 2025 · N655JB · Airbus A320232 · Emergency LightingSDR YENA2025032600323Battery · failedFLT#714, FLL-HPN.' WITH NO POWER ON AIRCRAFT GPU AND APU OFF, AND EMER LIGHT SWITCH IN THE ON OR AM POSITION, CABIN EMER. LIGHTS DOES NOT COME ON; REMOVED AND REPLACED 10WL EPSU AND BATT PACK IAW AMM 33-51-38 REF LP 4245975-2 (REMOVED AND REPLACED 11WL EPSU & Mar 23, 2025 · N655JB · Airbus A320232 · Emergency LightingSDR YENA2025032600322Battery · failedFLT#714, FLL-HPN.' WITH NO POWER ON AIRCRAFT GPU AND APU OFF, AND EMER LIGHT SWITCH IN THE ON OR AM POSITION, CABIN EMER. LIGHTS DOES NOT COME ON; REMOVED AND REPLACED 10WL EPSU AND BATT PACK IAW AMM 33-51-38 REF LP 4245975-2 (REMOVED AND REPLACED 11WL EPSU & Mar 23, 2025 · N655JB · Airbus A320232 · Emergency LightingSDR CALA2025032603220Sensor · faultedECAM FUEL IDG 1 COOL FAULT ON PARKING/ENGINESHUTDOWN AT GATE REMOVED AND REPLACED FLSCU1, THE FAULT CONTINUED, MORE TROUBLESHOOTING NEEDED. R&R FLSCU1 REF AMM 28-46-34 PERFORMED ENGINE RUN #1, MESSAGE CLEARED AFTER START, MESSAGE RETURNED AT SHUTDOWN. CORROMar 23, 2025 · N431UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2025032603205Door Frame · crackedR/H AFT EMERGENCY EXIT DOOR FWD VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR FWD VERTICAL SEGMENT REMOVED AND REPL ACED IAW A320 SRM 51-42-11/001 51-72-11-911-002.Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025032603204Door Frame · crackedL/H FWD EMERGENCY EXIT HATCH FWD. VERTICAL FRAME IS CRACKED. COMPLETED L/H FWD EMERGENCY EXIT FWD VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-72-11-911-002.Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025032603203Door Frame · crackedR/H AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME SEGMENT REMOVED AN D REPLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002.Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025032603202Door Frame · crackedL/H AFT EMERGENCY EXIT HATCH AFT. VERTICAL FRAME IS CRACKED. COMPLETED L/H AFT EMERGENCY EXIT AFT VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025032503170Bleed Air Sys · fluctuatesDURING CLIMB AND CRUISE, LT BLEED CYCLING 8-48 PSI AT LVL FLT CABIN RATE CYCLING +/-500FPM. SEE LOG PAGE 4268613 FOR FIX. BLEED AND CABIN ALT CHECKS GOOD.Mar 23, 2025 · N444UA · Airbus A320232 · Engine Bleed Air System
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