# Service difficulty reports: N431UA

A list on [N431UA](https://openairdocs.org/aircraft/N431UA.md).

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

Page 1 of 3 · 130 reports

- [SDR CALA2026101520399](https://openairdocs.org/sdr/CALA2026101520399.md): Cover · broken · Oct 14, 2026 · N431UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 20C BROKEN, IAW AMM 33-51-18 REPLACED THE COVER. LIGHT OPERATIONAL.
- [SDR CALA2026022313972](https://openairdocs.org/sdr/CALA2026022313972.md): Wire Harness · damaged · Feb 19, 2026 · N431UA · Airbus A320232 · Light System Wiring
  > CABIN EMERGENCY LIGHT TEST FAILED WITH MESSAGE "EPSU EXT LOAD FWD L" SUSPECT DOOR 1L SLIDE HAS INTERNAL LIGHT FAILURE REF AMM 33-51-00-710-001-A FOUND BROKEN WIRE BETWEEN CONNECTOR 2871VC AND 2819VC. BROKEN WIRE IS MID POINT WHERE DOOR HINGE. BROKEN WIRE WAS
- [SDR CALA2025122912490](https://openairdocs.org/sdr/CALA2025122912490.md): Fuel Cap · missing · Dec 26, 2025 · N431UA · Airbus A320232 · Fuel Storage
  > FUEL CAP FOUND MISSING UPON ARRIVAL. FUEL CAP INSTALLED SERVICABLE FUEL CAP IAW AMM 28-25-41/401 CONFIG 00.
- [SDR CALA2025101009910](https://openairdocs.org/sdr/CALA2025101009910.md): Fuel Cap · missing · Oct 7, 2025 · N431UA · Airbus A320232 · Fuel Storage
  > ACFT ARRIVED WITH REFUEL ADAPTER CAP COMPLETELY MISSING. FUELER REPORTS FUEL CAP LANYARD NOT ATTACHED AND FUEL CAP HINGE IS BROKEN. VERFIED NO LEAKS NOTED AT THIS TIME. COMPLIED WITH CDL 28A.
- [SDR CALA2025091608968](https://openairdocs.org/sdr/CALA2025091608968.md): Bleed Valve · faulted · Sep 12, 2025 · N431UA · Airbus A320232 · Compressor Bleed Valve
  > ABORTED TAKEOFF DUE TO ECAMS NOT APPROPRIATE WITH MEL. ACP'D ON L/P 6256763.ENG1 HP VALVE INDICATES OPEN ON BLEED PAGE. ALLOTHER INDICATIONS NORMAL SECURED THE ENGINE 1 HPV CLOSED AND INSTALLED DF STICKER REF MEL 3611S. DM SUGGEST TSM 36-11-00-810-835-A, R &
- [SDR CALA2025091108772](https://openairdocs.org/sdr/CALA2025091108772.md): Fitting · damaged · Sep 9, 2025 · N431UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > UPON REINSTALLATION OF RT MLG DOOR ACTUATOR, REQURIED GAP COULD NOT BE OBTAINED AFTER WASHER NAS1149C1016R INSTALLED. REPLACED RH MLG DOOR ACTUATOR FITTING FWD AND AFT AIRBUS DWG R83 370501 ISSUE F.
- [SDR CALA2025060205160](https://openairdocs.org/sdr/CALA2025060205160.md): Lamp · inoperative · Jun 1, 2025 · N431UA · Airbus A320232 · Emergency Lighting
  > EPSU EXT LOAD EMER L R&R 11WL EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-400-001-A, DID NOT HELP. INSTALLED BACK THE OLD EPSU AND BATTERY. FOUND ON EPSU EXTERIOR LIGHTS FAULT LIGHT ON SEE PIC. CHECKED OVERWING LIGHTS FOUND AFT LIGHT NOT WORKING P/N GE1810.
- [SDR CALA2025043004327](https://openairdocs.org/sdr/CALA2025043004327.md): Medical Kit · out of date · Apr 29, 2025 · N431UA · Airbus A320232 · Emergency Equipment
  > EMERGENCY MEDICAL KIT (EMK) INSPECT {A3NB-25-3-6326} - FLIGHTDECK EMK REQS CHANGE IAW 25-64-99/201 REPLACED IAW 25-64-99/201
- [SDR CALA2025042804279](https://openairdocs.org/sdr/CALA2025042804279.md): Bottle · none · Apr 25, 2025 · N431UA · Airbus A320232 · Passenger/Crew Doors
  > DISARMING OF THE STRIKER LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER TO FACILITATE SLIDE REMOVAL R1 PASSENGER DOOR REF. FIG 52-10-00-991-00300-B - REARMED STRIKER LEVER FOR THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. SAFETIED PER AMM MED DO
- [SDR CALA2025042804273](https://openairdocs.org/sdr/CALA2025042804273.md): Slide · faulted · Apr 24, 2025 · N431UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR 1L SLIDE NEEDS REMOVED FOR TROUBLESHOOTING. REMOVED DOOR 1L ESCAPE-SLIDE PACK-ASSEMBLY REFERENCE: TASK 25-62-44-000-002-A INSTALLED DOOR 1L ESCAPE-SLIDE PACK-ASSEMBLY REF. AMM 25-62-44-400-006-A. OPS CHECK GOOD. WITNESSED INSTALLATION OF DOOR 1L ESCAPE-
- [SDR CALA2025032603220](https://openairdocs.org/sdr/CALA2025032603220.md): Sensor · faulted · Mar 23, 2025 · N431UA · Airbus A320232 · Aircraft Fuel System
  > ECAM 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. CORRO
- [SDR CALA2025011001864](https://openairdocs.org/sdr/CALA2025011001864.md): Elec Connector · damaged · Jan 9, 2025 · N431UA · Airbus A320232 · Light System Wiring
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - SEAT MOUNTED EMERGENCY LIGHT AT 22C AND 28C INOP. AT SEATS 22C & 28C, REPLACED DAMAGED PINS & SOCKETS ON LIGHT ASSY CONNECTORS IAW SWPM 20-42-01. EMERGENCY SEAT TRACK LIGHTING OPS CK'D NORMAL.
- [SDR CALA2025011001852](https://openairdocs.org/sdr/CALA2025011001852.md): Battery · discharged · Jan 9, 2025 · N431UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - TEST FAIL SHOWED FWD LH EPSU BATTERY. REPLACED EPSU BATTERY REF AMM TASK 33-51-38-000-002-A AND TASK 33-51-38-400-002-A. ACP EPSU BITE, BITE CHECKS OKAY. ACP CIDS POWER ON TEST, TES
- [SDR CALA2024090302347](https://openairdocs.org/sdr/CALA2024090302347.md): Fitting · damaged · Aug 30, 2024 · N431UA · Airbus A320232 · Landing Gear Doors
  > LH MLG DOOR FWD HINGE AND ACTUATOR FITTING HOLES FOUND WITH SHEARED FASTENERS. REVISION OF ECRA 5330-07326 ON OR BEFORE 23-AUG-25. CARIED TO ACCOMPLISH A PERMANENT REPAIR ON THE LH MLG DOOR ACTUATOR FITTING REPAIRED HOLES L3 & L9 PER PART 3 OF THE LATEST OK TO
- [SDR CALA2024090302346](https://openairdocs.org/sdr/CALA2024090302346.md): Fitting · damaged · Aug 30, 2024 · N431UA · Airbus A320232 · Landing Gear Doors
  > LMLG DOOR FWD ACTUATOR FTG LOWER FWD HOLE AND SURROUNDING FLANGE DAMAGED COMMON TO KEEL BEAM. REMOVED & REPLACED FWD ACTUATOR FITTING AT LH DOOR MLG IAW A320 DRAWING REPAIR R533 70501 AND SRM 51-42-11/001.
- [SDR CALA2024082602269](https://openairdocs.org/sdr/CALA2024082602269.md): Stringer · corroded · Aug 22, 2024 · N431UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AREA STRG 25RH BETWEEN FRM 67 CORRODED (A3NB-05-3 -6199). REMOVED AND REPALCED STRINGER SECTION @25RH BETWEEN FR67 AND 66 IAW UAL A320 SRM 53-41-13-300-004.
- [SDR CALA2024082602268](https://openairdocs.org/sdr/CALA2024082602268.md): Stringer · corroded · Aug 22, 2024 · N431UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AREA STRG 26RH CORRODED BETWEEN FRM 65 AND FRM 66 (A3 NB-05-3-6199). REMOVED AND REPALCED STRINGER SECTION 26RH BETWEEN FRAME 65 AND 66 IAW UAL A320 SRM 53-41-13-300-004.
- [SDR CALA2024031900788](https://openairdocs.org/sdr/CALA2024031900788.md): Vsv · faulty · Mar 17, 2024 · N431UA · Airbus A320232 · Engine Bleed Air System
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS NORMAL. - ENG 1 ENG 1 COMPRESSOR VANE DURING TAKE OFF ROLL REJECT AT 80 KNOTS COMPLETED FADEC 1A AND 1B TEST AND GROUND SCAN. FADEC 1B TEST SHOWS MSG CHB VSV ACT/HC/ EEC1. BOTH 1A AND 1B SHOW AT
- [SDR CALA2023090602727](https://openairdocs.org/sdr/CALA2023090602727.md): Fuel Cap · missing · Sep 5, 2023 · N431UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 FUELER REPORTED FUEL CAP MISSING ON AIRCRAFT 4631. ARRIVED DENVER FLIGHT 2130-5SEP2023 FROM MEM SCEPTRE SHOWS FUEL CAP M&E 31-2825-9-0001 M&E S/N 1537 MFG PART # 0727540 MFG S/N C191537. MISSING CAP WAS ADDRESSED ON LOG PAGE 5669069. REPLACED FUEL CAP RE
- [SDR CALA2023082502634](https://openairdocs.org/sdr/CALA2023082502634.md): Linkage · out of adjust · Aug 23, 2023 · N431UA · Airbus A320* · Cargo/Baggage Doors
  > HIGH SPEED REJECTED TO DUE TO AFT CARGO DOOR OPEN INDICATION. PER CREW RTO AT 100 KNOTS. TS FOUND AFT CARGO DOOR FLAP LINKAGE OUT OF ADJUSTMENT. ADJUSTED PER AMM 52-32-11-820-002. REINSTALLED AND OPERATED AFT CARGO DOOR HANDLE. OPS CK OK. INDICATION IS NORMAL.
- [SDR CALA2022120503274](https://openairdocs.org/sdr/CALA2022120503274.md): Frame · cracked · Dec 2, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 35 LT SIDE IN OPEN FASTENER HOLE LOWER AND MORE AFT AT LEVEL OF STGR30, CRACK DIRECTION IS 5 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) AND ANGLE FITTING AT S-30LH IAW PART 2A OF LATEST REVISION OF 104,772 TFH. ACCOMPLISHED INTERIM
- [SDR CALA2022120503273](https://openairdocs.org/sdr/CALA2022120503273.md): Fitting · corroded · Dec 2, 2022 · N431UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > CORROSION REAR SPAR STOP RETRACTION JACK FITTING LOC MLG BAY ON LH WING. SEE AEROMAN NON ROUTINE 2022-360095. REQUIRED, PERFORMED SCEPTRE ENTRY ON LOGPAGE #3119101 REMOVED AND REPLACED JACK ANCHORAGE FITTING LOCATED ON MLG UPDATE SDR YES SIDE UPPER SURFACE A
- [SDR CALA2022112503225](https://openairdocs.org/sdr/CALA2022112503225.md): Fitting · corroded · Nov 25, 2022 · N431UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > CORROSION REAR SPAR STOP RETRACTION JACK FITTING LOC MLG BAY ON LH WING. SEE AEROMAN NON ROUTINE 2022-360095. REQUIRED, PERFORMED SCEPTRE ENTRY ON LOGPAGE #3119101 REMOVED AND REPLACED JACK ANCHORAGE FITTING LOCATED ON MLG UPDATE SDR YES SIDE UPPER SURFACE A
- [SDR CALA2022112503212](https://openairdocs.org/sdr/CALA2022112503212.md): Frame · cracked · Nov 24, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE AT VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-359865 3 OF THE LATEST REVISION OF EC/RA #5310-08051 ON OR BEFORE THE T ENGINNE
- [SDR CALA2022111603143](https://openairdocs.org/sdr/CALA2022111603143.md): Fitting · damaged · Nov 15, 2022 · N431UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON RH FR 66 AFT DOOR STOP FITTING. SEE AEROMAN 2022-360051 ATTACHMENT HOLES PER PART 2 OF LATEST REVISION OF ECRA 5341- CONTACT ENGINEERING AFTER 90,645 TOTAL AIRCRAFT FLIGHT CYCL
- [SDR CALA2022111603142](https://openairdocs.org/sdr/CALA2022111603142.md): Fitting · damaged · Nov 15, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > FOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON LH FR 66 AFT DOOR STOP FITTING SEE AEROMAN NON ROUTINE 2022-360050 ATTACHMENT HOLES PER PART 2 OF LATEST REVISION OF ECRA 5341-01 CONTACT ENGINEERING AFTER 90,645 TOTAL FLIGHT
- [SDR CALA2022110403035](https://openairdocs.org/sdr/CALA2022110403035.md): None · none · Nov 4, 2022 · N431UA · Airbus A320232 · Standard Practices/Structures
  > ADDITIONAL DATA IS NEEDED TO EVALUATED ON EXISTING DOUBLER AS PER ECRA 5330-06364 (LP 6821164) SEE AEROMAN NON ROUTINE 2022-359932 INSPECTION REQUIREMENTS FOR REINFORCING REPAIR GENERATE ANOTHER DIP THAT REFERENCE THE LOGPAGE 78,000 FC BUT BEFORE AIRCRAFT REAC
- [SDR CALA2022110203026](https://openairdocs.org/sdr/CALA2022110203026.md): Frame · cracked · Nov 2, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 36 PRESSURE PANEL IN OPEN FASTENER HOL ES NUMBER 6, 7, 10, 11, 12, 13, 14, 17, 18 AND 19 INBOARD OF BEA M -Y1292, HOLES ARE OUTSIDE THE REPAIR ALLOWABLE CUT-OUT AREA, C ONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEX
- [SDR CALA2022110203025](https://openairdocs.org/sdr/CALA2022110203025.md): Frame · cracked · Nov 2, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 36 PRESSURE PANEL IN OPEN FASTENER HOL ES NUMBER 6, 7, 10, 11, 12, 13, 14, 17, 18 AND 19 INBOARD OF BEA M -Y1292, HOLES ARE OUTSIDE THE REPAIR ALLOWABLE CUT-OUT AREA, C ONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEX
- [SDR CALA2022102402927](https://openairdocs.org/sdr/CALA2022102402927.md): None · cracked · Oct 23, 2022 · N431UA · Airbus A320232 · Fuselage Structure (General)
  > CRACK PLATE LOC. BTW FR68TO FR69 L/H SIDE AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-359949 REPLACED NEW PLATE LOC. BTW FR 68 TO FR69 L/H SIDE AT AFT GALLY AREA IAW A320 SRM 51-42-11-001 AND A320 SRM 51-72-11-911- 001, DWG D53480019
- [SDR CALA2022102402918](https://openairdocs.org/sdr/CALA2022102402918.md): Skin · cracked · Oct 22, 2022 · N431UA · Airbus A320232 · Fuselage Structure (General)
  > CRACK INDICATION ON FRAME 35 RH SIDE IN OPEN FASTENER HOLE LOWER AND MORE AFT AT LEVEL OF STGR30, CRACK DIRECTION IS 2 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-359824 SKIN, AND FR35 LAYARS ONLY) AND F5 AT FR35 AND F5 AT FR35 AND RE
- [SDR CALA2022101202775](https://openairdocs.org/sdr/CALA2022101202775.md): Flange · cracked · Oct 12, 2022 · N431UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION FOUND ON WEB HORIZONTAL FLANGE RADII LOWER POSITION OF FR.68 STR.22R L=0.787 INCH APPROX. SEE AEROMAN NON ROUTINE 2022-359838 22 PER PART 2A OF THE LATEST REVISION EC/RA 5341-01339 ON OR INSPECTION ON THE FASTENER HOLE AND EXTERNAL SURFACES OF
- [SDR CALA2022101202774](https://openairdocs.org/sdr/CALA2022101202774.md): Frame · cracked · Oct 12, 2022 · N431UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 12 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-359849 PER PART 2.A OF THE LATES REV. EC/RA 5341-0
- [SDR CALA2022101202773](https://openairdocs.org/sdr/CALA2022101202773.md): Stop Fitting · unknown · Oct 12, 2022 · N431UA · Airbus A320232 · Fuselage Main, Structure
  > FOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON RH FR 68 AFT DOOR STOP FITTING. SEE AEROMAN NON ROUTINE 2022-360057 FR.68 STR.22 PER PART 2.A OF THE LATES REVISION OF EC/RA #5341- INITIAL INSPECTION ON THE FASTENER HOLES AND
- [SDR CALA2022101202772](https://openairdocs.org/sdr/CALA2022101202772.md): Stop Fitting · unknown · Oct 12, 2022 · N431UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > FOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON LH FR 68 AFT DOOR STOP FITTING SEE AEROMAN NON ROUTINE 2022-360056 B. GENERATE A DIP LOGPAGE TO ACCOMPLISH REACHES 50,045 TOTAL A/C (FC) PERFOM REPEAT REVISION OF EC/RA# 5341-0
- [SDR CALA2022100602709](https://openairdocs.org/sdr/CALA2022100602709.md): Frame · corroded · Oct 5, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > CORROSION FRAME 20 AT LEVEL STR23R IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-359976 REPLACED FR 20 LOC BTW STR 5 TO STR 31 RH SIDE IAW EA #53-0389-22 COVER REV 0 AND EC/RA #5311-02889 THIS REPAIR IS CATEGORY A, ADDITIONAL INSPECTION IS NOT REQUIRED PERFO
- [SDR CALA2022100602703](https://openairdocs.org/sdr/CALA2022100602703.md): Skin · none · Oct 4, 2022 · N431UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > ADDITIONAL DATA IS NEEDED TO EVALUATED ON EXISTING DOUBLER AS PER ECRA 5330-06364 (LP 6802117). SEE AEROMAN 2022-359933. ARE L=1.372IN W=1328IN, USED MATERIAL IN REPAIR DOUBLER IS CLAD INTERVALS TBD INSPECTION METHOD TBD ASPER SRI 53-11-11-205-051, 2024T3-0.0
- [SDR CALA2022100602700](https://openairdocs.org/sdr/CALA2022100602700.md): Floorbeam · corroded · Oct 4, 2022 · N431UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 AT AFT GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359946. REPLACED FLOOR BEAM STRUCTURE Y+765 LOCATED FR66 TO FR70 IAW NTM 51-90-00. PERFORMED SCEPTRE AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND ENTRY ON LOGPAGE
- [SDR CALA2022100602699](https://openairdocs.org/sdr/CALA2022100602699.md): Floorbeam · corroded · Oct 4, 2022 · N431UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM Y-189 LOC.BTW F20 TO TR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359893. REPLACED FOORBEAM -Y189 LOC BTW FR20 TO FR24 AT FWD GALLEY AREA OF CORROSION ARE L=2.360 IN W=0.878 IN D=0.010 IN TOOL USED I.A.W SRM A320 51-72-11-911-001 A
- [SDR CALA2022100602698](https://openairdocs.org/sdr/CALA2022100602698.md): Seat Track · corroded · Oct 4, 2022 · N431UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359890. REMOVED AND REPLACED SEAT TRACK-Y1292 LOC. BTW FR12 TO FR24 AT DITIONAL DAMAGE I.A.W. NTM 51-90-00. PERFORMED SCEPTRE ENTRY INE 2022-359890. FWD GALLEY A
- [SDR CALA2022100602694](https://openairdocs.org/sdr/CALA2022100602694.md): Floorbeam · corroded · Oct 3, 2022 · N431UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y1292 LOC BTW FR68 TO FR69 AT AFT GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359948. REPLACED FLOOR STRUCTURE LOCATED FR68 TO FR69 -Y1292 SCEPTRE ENTRY ON LOGPAGE NUMBER IS: 9185702. MEASURES AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DRA
- [SDR CALA2022100302649](https://openairdocs.org/sdr/CALA2022100302649.md): Doubler · damaged · Oct 3, 2022 · N431UA · Airbus A320232 · Fuselage Main, Frame
  > THIS REPAIR IS CATERGORY B INSPECTION THRESHOLD FROM EXCEEDING 37,500FC OR 80,000FH WICHEVER OCCURS FIRST INSTALLED TIME OF ADL FC 60,000; FH 120,000 SUBSEQUENT INSPECTION AT DOT IAW GMM 06-35-05. EVALUATED EXISTING REPAIR ON EXTERNAL SKIN FUSELAGE LH SIDE LOC
- [SDR CALA2022092302455](https://openairdocs.org/sdr/CALA2022092302455.md): Frame · corroded · Sep 23, 2022 · N431UA · Airbus A300* · Passenger Compartment Windows
  > CORROSION FRAME 20 AT LEVEL STR23R IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-359976 REPLACED FR 20 LOC BTW STR 5 TO STR 31 RH SIDE IAW EA #53-0389-22 COVER REV 0 AND EC/RA #5311-02889 THIS REPAIR IS CATEGORY A, ADDITIONAL INSPECTION IS NOT REQUIRED PERFO
- [SDR CALA2022090502281](https://openairdocs.org/sdr/CALA2022090502281.md): None · cracked · Sep 5, 2022 · N431UA · Airbus A300* · Fuselage Structure (General)
  > CRACK INDICATION ON MAIN DOOR KEEL BEAM HINGE FITTING RH SIDE IN FWD LUG WEB RADIUS,CRACK LENGTH= 0.230 INCH APPROX, IN MAIN WHEEL WELL (1EA). SEE AEROMAN NON ROUTINE 2022-360084 REPLACED HINGE FITTING LOC MAIN DOOR RH SIDE KEEL BEAM AREA IAW A320 SRM 51-72-1
- [SDR CALA2022082902215](https://openairdocs.org/sdr/CALA2022082902215.md): Plate · cracked · Aug 29, 2022 · N431UA · Airbus A300* · Cabin Equipment/Furnishings
  > CRACK PLATE LOC. BTW FR68TO FR69 L/H SIDE AT AFT GALLEY AREA.REPLACED NEW PLATE LOC. BTW FR 68 TO FR69 L/H SIDE AT AFT GALLY AREA.
- [SDR CALA2022081902123](https://openairdocs.org/sdr/CALA2022081902123.md): Seat Track · corroded · Aug 17, 2022 · N431UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION SEAT TRACK -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359891. REMOVED AND REPLACED SEAT TRACK Y765 LOC.BTW FR12 TO FR24 AT FWD ION ON AREA AND NOT FOUND ADDITIONAL DAMAGE I.A.W. NTM 51-90- 2023. GALLEY AREA IN PASSEN
- [SDR CALA2022081202056](https://openairdocs.org/sdr/CALA2022081202056.md): Seat Track · corroded · Aug 12, 2022 · N431UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION SEAT TRACK -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359891. REMOVED AND REPLACED SEAT TRACK Y765 LOC.BTW FR12 TO FR24 AT FWD ION ON AREA AND NOT FOUND ADDITIONAL DAMAGE I.A.W. NTM 51-90- 2023. GALLEY AREA IN PASSEN
- [SDR CALA2022081202055](https://openairdocs.org/sdr/CALA2022081202055.md): Seat Track · corroded · Aug 12, 2022 · N431UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION SEAT TRACK -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359890. REMOVED AND REPLACED SEAT TRACK-Y1292 LOC. BTW FR12 TO FR24 AT DITIONAL DAMAGE I.A.W. NTM 51-90-00. PERFORMED SCEPTRE ENTRY INE 2022-359890. FWD GALLEY A
- [SDR CALA2022080801982](https://openairdocs.org/sdr/CALA2022080801982.md): Fitting · corroded · Aug 5, 2022 · N431UA · Airbus A300* · Fuselage Structure (General)
  > CORROSION CENTER FITTING PASSENGER CREW DOOR AT AFT GALLEY AREA LH SIDE. SEE AEROMAN NON ROUTINE 2022-360080. REMOVED AND REPLACED CENTER FITTING PASSENGER AREA IAW NTM 51-90-00. PERFORMED SCEPTRE ENTRY ON LOGPAGE SEP-29-2022 CREW DOOR AT AFT GALLEY AREA LH SI
- [SDR CALA2022080501971](https://openairdocs.org/sdr/CALA2022080501971.md): Fitting · corroded · Aug 5, 2022 · N431UA · Airbus A320232 · Passenger/Crew Doors
  > CORROSION CENTER FITTING PASSENGER CREW DOOR AT AFT GALLEY AREA LH SIDE. SEE AEROMAN NON ROUTINE 2022-360080. REMOVED AND REPLACED CENTER FITTING PASSENGER AREA IAW NTM 51-90-00. PERFORMED SCEPTRE ENTRY ON LOGPAGE SEP-29-2022 CREW DOOR AT AFT GALLEY AREA LH SI

Next page: https://openairdocs.org/aircraft/N431UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N431UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N431UA/reports

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