N432UA

Service difficulty reports · 176

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N432UA' AND registry_match = 'registration'
  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 CALA2026102120485Fuel Cap · missingCA REPORTED FUEL CAP MISSING. OK TO APPLY CDL 28A. CREW INSTALLED PLACARD. REPLACED THE FUEL CAP IAW AMM 28-25-41.Oct 19, 2026 · N432UA · Airbus A320232 · Fuel StorageSDR CALA2026092919980Wire · damagedEMERGENCY LIGHT SEAT AT 34C INOPERATIVE. RESTORED WIRING TO ORIGINAL CONDITION IAW AMM 33-51-00- 2-C. EMERGENCY ESCAPE PATH LIGHT WORKS AT SEAT ROW 34 C. NO DEFECTS NOTED, ALL EMERGENCY LIGHTS OPE CHECKED GOOD.Sep 27, 2026 · N432UA · Airbus A320232 · Light System WiringSDR CALA2026070917625Unknown · odorFA SMELLED BURNED TOAST ODOR IN AFT GALLEY. INSPECTED AFT GALLEY AND CABIN FOR FUMES AND SIGNS OF SMOKE IAW AMM 05-51-10. NO SIGNS OF ODOR. RAN THE APU AND PACKS AND COULD NOT REPLICATE ODOR. INSPECTED THE 2001VU PANEL REF AMM 24-92-00. NO DAMAGE OR ODOR FOUJul 6, 2026 · N432UA · Airbus A320232 · Air Distribution SystemSDR CALA2026052016418Uplock · faultedMLG NOT UPLOCKED AFTER TAKEOFF, ECAM NO HELP PERFORMED BITE TEST OF LGCIU 1 AND 2. LGCIU 1 REPORTED FAULT "N LG UPLOCK (2530GM)/(2527GM)". PILOTS REPORTED CYCLING GEAR IN FLIGHT, NO HELP. FOUND BACKSHELL ON CONNECTOR IAW AMM 32-31-21/401 CONFIG 00 SHEET 2. May 15, 2026 · N432UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR CALA2025110610935Liner · unsecureL1 DOOR ESCAPE SLIDE LOOSE LINING WAS CAUGHT BETWEEN DOOR. SECURED ESCAPE SLIDE LINING AT THE L1 DOOR IAW AMM 25-62-44.Nov 4, 2025 · N432UA · Airbus A320232 · Escape SlideSDR CALA2025070806318Battery · faultedEMER LIGHT TEST FAILED. ESPU BATTERY EMER L AND EPSU BATTERY AFT L MESSAGES DISPLAYED. REPLACED EPSU BATTERIES AT 11WL AND 13WL. EMERGENCY LIGHTS OPS CHECK GOOD, NO FAULTS ON CIDS.Jul 7, 2025 · N432UA · Airbus A320232 · Emergency LightingSDR CALA2025062705985Cids · faultedALL INTERCOM FUNCTIONS INOP INCLUDING EMERGENCY. REPLACED DEU B 300RH05. SYS CHECKS NORMAL REF AMM 23-73-47PARTS USED: 31-2300-9-0005, QTY :1 ROTABLE PARTS CHG:TT # 1761896 SN OFF 9762 PN OFF 31-2300-9-0005. UNIT, CIDS DECO OFF 31-2300-9-0005 9762 ON 31-2300-Jun 24, 2025 · N432UA · Airbus A320232 · Communications SystemSDR CALA2024101700852Computer · faultedIN FLIGHT LOST MOSTNAV AND ATTITUDE INFOON CA PFD AND ND ANDENG 1 EPR/EGT/N1/N2/FF TECH SUPPORT UPDATE: DMC 1 FAULTS NOTED IN AVIATAR, ADDING DMC-1 (1WT1) TO PARTS FOR REPLACEMENT REF AMM. 31-63-34. REF 31-63-81-810-867-A REMOVED AND REPLACED #1 DMC 1WT1 REF MOct 15, 2024 · N432UA · Airbus A320232 · Central DisplaySDR CALA2024053001639Compressor · stalledESDR EVENTNO 1 COMP STALL ON FLXABORT AT 20KTSNO FIRE ALARM OBSERVERED METAL SHAVINGS IN THE TAIL PIPE. ESDR EVENTNO 1 COMP STALL ON FLXABORT AT 20KTSNO FIRE ALARM OBSERVERED METAL SHAVINGS IN THE TAIL PIPE.SDR# 1036353 GENERATED AND ENGINE CHANGE RECORDED ON May 27, 2024 · N432UA · Airbus A320232 · Turbine Engine Compressor SectionSDR CALA2024031500744Oven · odorCREW REPORTS DURING CLIMBOUT THE AFT GALLEY HAD A ELECTRICAL ODOR NOTICED BY THE FLT ATTENDANTS. LASTED A SHORT TIME AND DISIPATED. NO EQUIPMENT WAS NOTICED TO BE INOPERATIVE AND PASSENGERS DID NOT NOTICE DURING THIS INCIDENT, COMPLIED WITH TASK 05-51-10-200-8Mar 14, 2024 · N432UA · Airbus A320232 · Buffet/GalleysSDR CALA2023120103516Fuel Cap · missingPDA 2 FUEL CAP FOUND MISSING UPON ARRIVAL TO ORD. COMPLIED W CDL REQUIREMENTS. NO DAMAGE TO COUPLER, STICKER APPLIED. CDL 28A COMPLIED WITH. OK TO APPLY CDL 28A.TOMC SMITH FUEL CAP NIS DEN CAP, COUPLING R OFF 0000 ON 31-2825-9-0001 7103 INSTALLED MISSING FUEL Nov 27, 2023 · N432UA · Airbus A320232 · Fuel StorageSDR CALA2023010600034Door Latch · mislocatedFORWARD CARGO DOOR INDICATED OPEN ON TAKEOFF ROLL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V903723 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003064678 AND PRTR OWENS, KEVIN (V903Jan 6, 2023 · N432UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2022102702957Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE LH SIDE INTERNAL AREA INBOARD VERTICAL FLANGE FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGHT IS 0.140 INCH APPROX., CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHTOct 25, 2022 · N432UA · Airbus A320232 · Flight Compartment WindowsSDR CALA2022102702947Pressure Blkhd · crackedCRACK INDICATION ON FR36LH PRESSURE PANEL IN OPEN FASTENER HOLES A AND B COMMON TO LONGITUDINAL BEAM Y1292, CONTACT PLANNING TO ASSIGN AND ACCOMPLISH EA 5330-05216 OP2 BEFORE NEXT FLIGHT IN FWD CARGO COMPARTMENT (2 EA). ED PART 1 INTERIM REPAIR ON AEROMAN NR#2Oct 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022102702946Skin · crackedCRACK INDICATION ON FRAME 35 LOWER AND MOST AFT OPEN FASTENER HOLE AT ELEVEN OF STGR30LH, CRACK DIRECTIONS ARE 7 AND 11 OCLOCK IN FWD CARGO COMPARTMENT (1 EA). SEE AEROMAN NO ROUTINE 2022-393517. 4.750MM, HOLE DIAMETER WITH CRACK REMOVED 9.042MM AND FINAL FWDOct 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022102702940Fitting · elongatedELONGATED HOLES R2, R3, R7, R8, R10, R12, R13, R14, R15, R16, R17, R19,R21, R74, R76, R78, R81, R83 AND R85 LOCATED KEEL BEAM AREA AT FR42 RH SIDE, ENGINEERING MUST BE CONTACTED. SEE AEROMAN NON ROUTINE 2022-394203 ACCOMPLISHED REPAIR INSTRUCTION FOR HOLES R2,Oct 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022102402917None · crackedCRACK INDICATION FOUND AT FASTENER HOLE LOCATED AT FRAME 35 AND STR 30 RH SIDE AT FWD CARGO COMPARTMENT. CRACK DIRECTION IS 3 AND 9 OCLOCK APROX LOOKING AFT. CRACK DEPTH IS 0.055 INCHES APROX. REPAIR BEFORE FURTHER FLIGHT. SEE AEROMAN NON ROUTINE 2022-394074 BOct 22, 2022 · N432UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022102402920None · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022102402919None · noneELONGATED HOLES L1, L2, L3, L10, L12, L13, L14, L15, L18, L20, L75, L76,L77, L78, L82, L83, L84 AND L85 LOCATED ON KEEL BEAM AREA AT FR42 LH SIDE. ENGINEERING MUST BE CONTACTED. SEE AEROMAN NON ROUTINE 2022-394202 CATEGORY B. AND MUST BE ACCOMPLISH INSPECTION Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022102402922None · crackedCRACK INDICATION ON FRAME 35 LOWER AND MOST AFT OPEN FASTENER HOLE AT LEVEN OF STGR30RH, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (4 EA) SEE AEROMAN NON ROUTINE 2022-393519 ACCOMPLISHED INTERIM REPAIR PART 1 PER ECRA 5331-02971 ON HOLE # Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022102402921None · crackedREPAIR FOR CRACK INDICATION FR36LH PRESSURE PANEL TOMC-APPROVAL FROM SC1ELBYC COMMENT FASTENER HOLES (#2-4, 8, 9, 13-17, 19-23, 26 AND 27), REF ECRA 5311-02905 PLANNING TO CONTACT ENGINEERING AFTER FEBRUARY 10,2023 BUT BEFORE MARCH 10, 2023 FOR THE PERMANENT OOct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100602702Frame · crackedCRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPPOct 4, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100602693Frame · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTE NER HOLE BTW STGR21 AND STGR22, CRACK DIRECTIONS ARE 3 AND 9 OCL OCK IN PASSENGER CABIN (1 EA). SEE AEROMAN NON-ROUTINE 2022-393 695. REPLACED FRAME FOOT COUPLING LOCATED ON FR43 LH SIDE IAW EA Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100602691Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022100602692Stiffener · crackedCRACK INDICATION FOUND ON VERTICAL STIFFENER OF THE LATERAL WINDOW FRAME 4 RIGHT SIDE LENGTH APPROXIMATELY =0.278 INCHES SEE AEROMAN NON ROUTINE 2022-393434. INDICATION NOT FOUND IAW NTM 51-10-08. THIS REPAIR IS CATEGORY A AND RE-INSPECTION ARE NOT REQUIRED PEOct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100602690Floor Panel · corrodedCORROSION FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-00Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022100602689Floorbeam · corrodedCORROSION FLOOR BEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022100602688Floorbeam · elongatedELONGATED HOLE FLOOR BEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-393859 REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER IS:9289332 MEASURE OF IAW SRM A320 51-72-11-911Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022100602687Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV AOct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100302650Flange · crackedCRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPPOct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022100302617Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H3 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393809 PERFORMED SCEPTRE ENTRY LOG PAGE NUMBER 9334409. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H3 FWD GALLEY AREA I.A.W. EA 531Oct 2, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022100302616Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA, FR16 RH SIDE; HOLE H4 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393810 TRE ENTRY LOG PAGE NUMBER 9334428. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H4 FWD GALLEY AREA I.A.W. EA 5310-06784 REV Oct 2, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022100302615Floorbeam · elongatedELONGATED HOLE FLOORBEAM -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA.SEE AEROMAN NON ROUTINE 2022-393856. INSTALLED NEW FLOOR BEAM Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, DWG #D53472201 AND DWG #D534722 00. PERFOMED SCPETRE ENTRY LOct 2, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022090902315None · noneREMOVE AND REPLACE AIR RELEASE VALVE FLOAT RH WING (FIN 87QM) THIS NR FOR TRACKING PURPOSE ONLY. SEE AEROMAN NON ROUTINE 2022- 394222. REMOVED AIR RELEASE VALVE FLOAT RH WING (FIN 87QM) P/N: FRH2800 SEQ# 438. THIS NR FOR TRACKING PURPOSE ONLY 02 S/N:FRTR0421AMSep 9, 2022 · N432UA · Airbus A320232 · Aircraft Fuel Filter/StrainerSDR CALA2022082602178None · noneCRACK INDICATION FOUND ON VERTICAL STIFFENER OF THE LATERAL WINDOW FRAME 4 RIGHT SIDE LENGTH APPROXIMATELY =0.278 INCHES SEE AEROMAN NON ROUTINE 2022-393434. INDICATION NOT FOUND IAW NTM 51-10-08. THIS REPAIR IS CATEGORY A AND RE-INSPECTION ARE NOT REQUIRED PEAug 26, 2022 · N432UA · Airbus A300* · Fuselage Main, FrameSDR CALA2022082402160Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV AAug 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022082402159Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA, FR16 RH SIDE; HOLE H4 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393810 TRE ENTRY LOG PAGE NUMBER 9334428. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H4 FWD GALLEY AREA I.A.W. EA 5310-06784 REV Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022082402158Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H3 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393809 PERFORMED SCEPTRE ENTRY LOG PAGE NUMBER 9334409. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H3 FWD GALLEY AREA I.A.W. EA 531Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022082402157Floorbeam · elongatedELONGATED HOLE FLOOR BEAM -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA.SEE AEROMAN NON ROUTINE 2022-393856. INSTALLED NEW FLOOR BEAM Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, DWG #D53472201 AND DWG #D534722 00. PERFOMED SCPETRE ENTRY Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022081902119Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30Aug 19, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022081902118Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4Aug 19, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022081602073Floorbeam · elongatedELONGATED HOLE FLOORBEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA. REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA.Aug 16, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022081002032Dummy Rail · corrodedCORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA Aug 9, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022080501974Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001 Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022080501973Dummy Rail · corrodedCORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022080501972Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-001Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2019112542058Power Supply · failedCIDS TEST FAILED. MSGS "EPSU EXT LOAD FWD L" REPLACED EPSU P/N 3214-54-10 AND EPSU BATTERY P/N AD3214-31. ORIGINAL MESSAGE GONE. NEW MESSAGE EPSU EXT LOAD FWD L PRESENT. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1104555 SN OFF 8398 POWER SUPPLY, C OFF 31-335Nov 23, 2019 · N432UA · Airbus A320232 · Emergency LightingSDR CALA2018070301554Wire Harness · damagedEEPL HARNESS ROWS 29-31 DAMAGED. REMOVED AND REPLACED EEPL CABLE AT SEAT ROW 29-31 IAW AMM 33-51-22-400-802C1.Jun 30, 2018 · N432UA · Airbus A320232 · Light System WiringSDR CALA2018071001580Intercostal · crackedRT FWD PAX DOOR NR 1 DOOR STOP FITTING LOWER I/B FASTENER HOLE HAS CRACK INDICATION. REMOVED NR 1 DOOR STOP FITTING, REMOVED AND REPLACED DAMAGED INTERCOSTAL AT RT FWD PAX DOOR FR16 IAW ECRA 5311-01961, INSTALLED NR 1 DOOR STOP FITTING IAW AMM 52-11-31-000-002Jun 25, 2018 · N432UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018070301558Beam · corrodedLT AFT EMERGENCY EXIT DOOR CUTOUT. LOWER SURFACE BETWEEN THE LATCHES FOUND CORRODED AFTER CHECKING MATING SURFACE OF CORRODED HATCH. REMOVED CORRODED BEAM AT LT AFT EMERGENCY EXIT DOOR LOWER BEAM. MATCH DRILLED NEW BEAM AND INSTALLED NEW BEAM RESTORED SURFACE Jun 22, 2018 · N432UA · Airbus A320232 · Fuselage Main, Structure
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