# Service difficulty reports: N465UA

A list on [N465UA](https://openairdocs.org/aircraft/N465UA.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 · 124 reports

- [SDR CALA2026101920441](https://openairdocs.org/sdr/CALA2026101920441.md): Battery Pack · faulted · Oct 16, 2026 · N465UA · Airbus A320232 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, RECIEVED FAULT EPSU BATTERY WARNING. VERIFIED BATTERY FAULT ON EPSU 12WL SELF TEST IAW AMM 33-51-38, R & R THE BATTERY PACK, OP CHKD GOOD IAW AMM 33-51-38.
- [SDR CALA2025121812229](https://openairdocs.org/sdr/CALA2025121812229.md): Light · inoperative · Dec 17, 2025 · N465UA · Airbus A320232 · Emergency Lighting
  > SEAT 34ABC EMERGENCY LIGHT INOPERATIVE. R & R THE SEAT MOUNTED FLOOR PROXIMITY LIGHT IAW AMM 33-51-19, OPS CHECKED GOOD.
- [SDR CALA2025072206836](https://openairdocs.org/sdr/CALA2025072206836.md): Frame · cracked · Jul 15, 2025 · N465UA · Airbus A320232 · Fuselage Main, Frame
  > LH FR 35 AT STR 30 FRAME FWD FACE HAS CRACK JUST BELOW FASTENER ADJACENT HOLE 2 IN OUTER FLANGE CRACK EXTENDS FROM FASTENER APPROX.200 IN RADIUS PER HAECO LCQ N/R 9298611/28611 GEN BY V892444 ACCOMPLISHED INTERIM REPAIR AT LH FR35 STGR30L HOLE NO. 2 WITH NO D
- [SDR CALA2025072206835](https://openairdocs.org/sdr/CALA2025072206835.md): Plate · damaged · Jul 15, 2025 · N465UA · Airbus A320232 · Wing, Plate/Skin
  > R/W FUEL PANEL LANDING AT 640KB HAS HOLES OUT OF ROUND PER HAECO LCQ N/R 9298704/28704 GEN BY N078348ESFR COMPLETED AFTER EVALUATION, PERFORMED REPAIR ON ONE OUT OF ROUND HOLE AT RIGHT WING FUEL PANEL 640KB BETWEEN RIBS 15-16 IAW SRM 57-21-11-300-002. REAMED H
- [SDR CALA2025072206834](https://openairdocs.org/sdr/CALA2025072206834.md): Skin · damaged · Jul 15, 2025 · N465UA · Airbus A320232 · Wing, Plate/Skin
  > R/W FUEL PANEL LANDING AT 640LB HAS HOLES OUT OF ROUND PER HAECO LCQ N/R 9298705/28705 GEN BY N078348ESFR COMPLETED AFTER EVALUATION, PERFORMED REPAIR ON ONE OUT OF ROUND HOLE AT RIGHT WING FUEL PANEL 640LB BETWEEN RIBS 16-17 IAW SRM 57-21-11-300-002. REAMED H
- [SDR CALA2025072206833](https://openairdocs.org/sdr/CALA2025072206833.md): None · none · Jul 14, 2025 · N465UA · Airbus A320232 · Standard Practices/Structures
  > COMPLY WITH CFR 121.1109" EX ISTING REPAIR FOUND WITH NO RECORDS AT L/H FR 66-67 STR 24L-26L ACCOMPLISHED INTERIM REPAIR AT LH FR66-67 STGR 24L - 28L WITH NO DEVIATION IAW ECRA 5341-01507. ACCOMPLISH INITIAL INSPECTION OF LH FR 66-67 STGR 24LH ? 28LH REPAIR
- [SDR CALA2025062706001](https://openairdocs.org/sdr/CALA2025062706001.md): Stiffener · cracked · Jun 25, 2025 · N465UA · Airbus A320232 · Fuselage Main, Bulkhead
  > FR1 PRESSURE BULKHEAD L/H SIDE 2ND STIFFENER FROM THE TOP FOUND TO BE CRACKED. REMOVED AND REPLACED STIFFENER AT FR1 PRESSURE BULKHEAD IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025062605905](https://openairdocs.org/sdr/CALA2025062605905.md): Stringer · corroded · Jun 23, 2025 · N465UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER HAS EXFOLIATION CORROSION R/H FR64-65 STR 31R (PSE/MAJOR REPAIR) A3NB-05-3-6024. REMOVED S31R DUE TO 100% MATERIAL LOSS IAW SRM 51-42-11/ 001.LOCATED & DRILLED NEW REPLACEMENT PARTS D5348004721202 & D53 47105220590 IAW SRM 51-44-11/001. INS
- [SDR CALA2025062305819](https://openairdocs.org/sdr/CALA2025062305819.md): Door Sill · corroded · Jun 21, 2025 · N465UA · Airbus A320232 · Fuselage Main, Structure
  > FWD CARGO ENTRY DOOR SILL HAS CORROSION. REMOVED AND REPLACED FWD CARGO ENTRY DOOR SILL IAW A320SRM 51-72-11. R & R FWD CARGO ENTRY DOOR SILL IAW SRM 51-72-11 CAT A.
- [SDR CALA2025071506569](https://openairdocs.org/sdr/CALA2025071506569.md): Stringer · gouged · Jun 19, 2025 · N465UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 40R GOUGED APPROX 7 INCHES FWD OF FRAME 48.
- [SDR CALA2025062605895](https://openairdocs.org/sdr/CALA2025062605895.md): Seat Track · corroded · Jun 12, 2025 · N465UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 51-42
- [SDR CALA2025061105460](https://openairdocs.org/sdr/CALA2025061105460.md): Beam · corroded · Jun 8, 2025 · N465UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR 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.
- [SDR CALA2025061105457](https://openairdocs.org/sdr/CALA2025061105457.md): Window Frame · cracked · Jun 5, 2025 · N465UA · Airbus A320232 · Fuselage Main, Structure
  > WINDSHIELD 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
- [SDR CALA2025060205169](https://openairdocs.org/sdr/CALA2025060205169.md): Rib · corroded · May 30, 2025 · N465UA · Airbus A320232 · Elevator, Spar/Rib
  > L/H ELEVATOR CORROSION AT O/B RIB T/E AS MARKED PER HAECO LCQ N/R 9298575/28575 GEN BY V899045 ESFR COMPLETED RMVD AND RPLD CORRODED O/B RIB ON THE L/H ELEVATOR IAW A320 SRM 51-42-11.
- [SDR CALA2025052905080](https://openairdocs.org/sdr/CALA2025052905080.md): Seat Track · corroded · May 27, 2025 · N465UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FWD FLOOR BEAM UPPER SURFACE CORRODED @ FRAME 16 AND CENTERLINE (C/L) REMOVED AND REPLACED FLOOR BEAM Y-81 AT BETWEEN FR12-16 IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025062705990](https://openairdocs.org/sdr/CALA2025062705990.md): Panel · cracked · May 25, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LH BETWEEN FR58-59 STRINGER 31L HAS CRACKE D SLOPE PNL SUPPORT PROFILE. REMOVED AND REPLACED NEW PROFILE PANEL FROM AFT CARGO L/H BTW FR 58 TO FR59 STR 31L IAW A320 SRM 51-42-11.
- [SDR CALA2025052704959](https://openairdocs.org/sdr/CALA2025052704959.md): Angle · cracked · May 22, 2025 · N465UA · Airbus A320232 · Wing Miscellaneous Structure
  > LEFT WING FIXED L/E FR15 HAS CRACKED SMALL ANGLE AT INNER BAY R & R ANGLE AT LH WING FR15 INNER BAY IAW A320 SRM 51-72-11 -911-001.
- [SDR CALA2025052704958](https://openairdocs.org/sdr/CALA2025052704958.md): Support · excess play · May 22, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD PIT FWD WALL RH I/B VERTICAL SUPPORT HAS EXCESSIVE PLAY AND WEAR AT UPPER ATTACHMENT. SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-29-300-002. R & R MEMBER ASSY VERTICAL ON FWD PIT FWD WALL RH IB SUPPORT HAS EXCESSIVE PLAY AND WEAR AT UPPER ATTACHEMENT
- [SDR CALA2025052304925](https://openairdocs.org/sdr/CALA2025052304925.md): Bonding Plate · broken · May 21, 2025 · N465UA · Airbus A320232 · Horizontal Stabilizer Structure
  > RH THS T/E HINGE FITTING #1 HAS A BROKEN BONDING PLATE. REPLACED RH THS T/E HINGE FITTING #1 BONDING PLATE IAW A320 SRM 51-42-11/001 AND ACMP BONDING TEST AND THE RESISTANCE IN RH THS T/E HING FITTING #1 BONDING PLATE IS IN LIMITS IAW A320 AMM 20-2 8-00-869-0
- [SDR CALA2025052304924](https://openairdocs.org/sdr/CALA2025052304924.md): Panel · worn · May 21, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT L/H FR49 BETWEEN STRINGER 32L-34L HAS ELONGATED FASTENER HOLE AT SLOPE PANEL SUPPORT PROFILE. REMOVED AND REPLACED SLOPE PROFILE PNL IAW 51-42-11/001.
- [SDR CALA2025052104892](https://openairdocs.org/sdr/CALA2025052104892.md): Floor Support · corroded · May 20, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT Y 512.5 AT FR 68-70 HAS CORROSION. CABIN FLOOR SUPPORT Y512.5 AT FR68-70 RMVD + RPLCD IAW A320 SRM 51- 72-11-911-001 + 51-42-11/001.
- [SDR CALA2025052104891](https://openairdocs.org/sdr/CALA2025052104891.md): Support · cracked · May 20, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT L/H BETWEEN FR 54-58 STRINGER 31L HAS CRA CKED AT SLOPE PANEL SUPPORT PROFILE. R & R NEW PROFILE PNL ON AFT CARGO FR54 TO FR58 STR31L IAW A320 SRM 51-42-11.
- [SDR CALA2025052004854](https://openairdocs.org/sdr/CALA2025052004854.md): Seat Track · corroded · May 19, 2025 · N465UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FWD FLOOR SEAT TRACK CORRODED AT FR 20 AND Y-1292 R/H. R & R MAIN CABIN FWD FLOOR SEAT TRACK BETWEEN FRAME 12-24 Y -292 RH IAW A320 SRM 51-42-21.
- [SDR CALA2025052004853](https://openairdocs.org/sdr/CALA2025052004853.md): Seat Track · corroded · May 19, 2025 · N465UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FWD FLOOR SEAT TRACK CORRODED AT FR 20 AND Y-765 R/H. R & R MAIN CABIN FWD FLOOR SEAT TRACK FRAME 12-24 Y-765 RH IAW SRM 51-42-11 A320.
- [SDR CALA2025051904793](https://openairdocs.org/sdr/CALA2025051904793.md): Floor Support · corroded · May 18, 2025 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT Y765 AT FR 64-66 HAS CORROSION. FLOOR SUPPORT Y765 AT FR64-66 REMOVED & REPLACED IAW A320 SRM 51-72-11-911-001 & 51-42-11/001.
- [SDR CALA2025051904792](https://openairdocs.org/sdr/CALA2025051904792.md): Floorbeam · corroded · May 18, 2025 · N465UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM Y 765 AT FR 66-70 HAS CORROSION. ESFR COMPLETE CABIN FLOOR BEAM Y765 AT FR 66-70 REMOVED & REPLACED IAW A320 SR M 51-72-11-911-001 & 51-42-11/001.
- [SDR CALA2025051604728](https://openairdocs.org/sdr/CALA2025051604728.md): Skin · contaminated · May 13, 2025 · N465UA · Airbus A320232 · Elevator, Plate/Skin
  > RIGHT HAND ELEVATOR UPPER SIDE HAS LIQUID INGRESS AT 145 FROM END BOARD, 11 TRAILING EDGE,.5 DIAMATOR. REPAIRED R/H ELEV UPPER SIDE AT 145 FROM END BOARD 11 T/E.5 DIA AS REQUIRED IAW A320 SRM 55-21-11-300-004 REPAIR CATEGORY A.
- [SDR CALA2025051604727](https://openairdocs.org/sdr/CALA2025051604727.md): Skin · contaminated · May 13, 2025 · N465UA · Airbus A320232 · Elevator, Plate/Skin
  > LEFT HAND ELEVATOR UPPER SIDE HAS LIQUIS INGRESS AT 135 FRIN END BOARD, 6 TRAILING EDGE, 2 DIAMATOR. REPAIRED L/H ELEV UPPER SIDE AT 135 FROM END BOARD.6 T/E 2 DIA AS REQUIRED IAW A320 SRM 55-21-11-300-004 REPAIR CATEGORY A.
- [SDR CALA2024110400990](https://openairdocs.org/sdr/CALA2024110400990.md): Actuator · faulty · Oct 31, 2024 · N465UA · Airbus A320232 · Flight Control System
  > REF ELAC 2 PITCH TRIM FAULTS. PFRS FAULTING THS ACTR POS ERROR 9CEOF ELAC2/IDEFCS 1. IF FAULT REPEATS, REPLACE THE "PITCH TRIM ACTUATOR" (AN LRU ON THE TRIMMABLE HORIZONTAL ACTUATOR) PER AMM 27-44-57. **REF TSM 27-93-00-810-836, PRE SB 27-1248. CARRIED BY EL
- [SDR CALA2024080200347](https://openairdocs.org/sdr/CALA2024080200347.md): Latch · faulty · Jul 22, 2024 · N465UA · Airbus A320232 · Fluid Service Doors
  > AFT POTABLE WATER LATCH BROKEN SERCURED DOOR 172AR TOILET SERVICE DOOR CLOSED REF MT 52-028 REF MT 52-028 PANEL 172AR. ISSUE DEFERRAL PER GMM 05-30-05 FOR THE RELAIR/REPLACEMENT WITH A RECHECK PRIOR TO EA FLIGHT CORRECTION. ITS THE TOILET SERVICE DOOR. OK TO A
- [SDR CALA2024021500430](https://openairdocs.org/sdr/CALA2024021500430.md): Fuel Cap · missing · Feb 10, 2024 · N465UA · Airbus A320232 · Fuel Storage
  > FUEL CAP REPORTED MISSING. NO LEAK AT FUEL COUPLING. COMPLIED WITH CDL 28A. STICKER APPLIED AND NO LEAK AT FUEL COUPLING. INSTALLED NEW FUEL CAP PER AMM 28-25-41-499-005-A. OPS CHECK GOOD.
- [SDR CALA2023122803746](https://openairdocs.org/sdr/CALA2023122803746.md): Door Seal · stuck · Dec 23, 2023 · N465UA · Airbus A320232 · Passenger/Crew Doors
  > CABIN DOOR 1R HAS A DEAFENING SQUEEL. AT ALT NO CHANGE. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED CHECK DOOR SEAL MAC RELATED WORK ORDER 000000003093189 AND PRTR MAC RELATED WORK ORDER 000000003093189 AND PRTR FOR DEBRIS OR SLIDE BUSTLE
- [SDR CALA2023051501491](https://openairdocs.org/sdr/CALA2023051501491.md): Fuel Cap · missing · May 12, 2023 · N465UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS FUEL CAP MISSING REF LP 4569687 FOR ACTIONS TAKEN. PDA ENTERED INTO HISTORY. INSTALLED NEW CAP PARTS USED: 31-2825-9-0001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1201727 SN OFF 0687
- [SDR CALA2023021300416](https://openairdocs.org/sdr/CALA2023021300416.md): Coupling · detached · Feb 11, 2023 · N465UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 FUELER REPORTED ACFT ARIVED WITH FUEL CAP MISSING. SN OFF CAP MISSING C192092 NOTIFIED TOMC ABOUT FUEL CAP PDA
- [SDR CALA2022050901193](https://openairdocs.org/sdr/CALA2022050901193.md): None · smoke · May 9, 2022 · N465UA · Airbus A320232 · Fire Detection
  > *EMERGENCY* LAV F SMOKE DETECTOR - SMOKE PERFORMED A VISUAL INSP OF SMOKE DETC, PERFORMED SDCU SELF TEST NO FOULTS FOUND AT THIS TIME OK TO CONTINUE
- [SDR CALA2021033000399](https://openairdocs.org/sdr/CALA2021033000399.md): Transceiver · failed · Mar 30, 2021 · N465UA · Airbus A320232 · Air Collision Avoidance System
  > BOTH XPDR SYS FAILED AIR RETURN TO DENDUE TO INTL FLT TCAS FAULT DISPLAYED AT ENGINE START. REF TSM TASKS 34-43-00-810-820 AND 34-43-00-810-821-A, REF LMC LP 6055083 FOR GUIDANCE TO REPLACE TCAS COMPUTER. ACCOMPLISHED BITE TEST OF INSTALLED TCAS COMPUTER IAW A
- [SDR CALA2020091501109](https://openairdocs.org/sdr/CALA2020091501109.md): Pump · failed · Sep 15, 2020 · N465UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > LT ENG G HYD PUMP PR LOECAM COMPLETE. PTU WORKED REMOVED AND REPLACED ENGINE DRIVEN HYD PUMP, REF 29-11-51. COMPLETED UP TO STEP 4.E.(6), NEED TO CONTINUE WITH STEP 4.F, AMM 29-11-51-400-010-A 13. ADD EMP:U093933. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1
- [SDR CALA2020091501099](https://openairdocs.org/sdr/CALA2020091501099.md): Coupling · damaged · Sep 11, 2020 · N465UA · Airbus A320232 · Hydraulic System, Main
  > MAIN HYD SUPPLY LINE, CPLG HALF IPC 29-11-06-01A ITEM 10, WILL NOT SELF SAFETY. M 32-2911-3-0023. THIS IS THE CONNECTION USED TO DISCONNECT THE HYD SUPPLY LINE DURING ENGINE CHANGE. REPLACED NR 1 ENGINE SELF SEALING HALF COUPLING OF THE GREEN PUMP SUCTION (
- [SDR CALA2019091301528](https://openairdocs.org/sdr/CALA2019091301528.md): Door Sill · corroded · Sep 9, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT DOOR SILL UPPER SURFACE HAS SPOTS OF CORROSION A3N B-53-4-6179. PER NON ROUTINE 9296490 REMOVED AND REPLACED AFT CARGO DOOR SILL PLATE FOR ELONGATED HOLES IAW SRM 51-42-11-801.
- [SDR CALA2019091301525](https://openairdocs.org/sdr/CALA2019091301525.md): Doubler · corroded · Sep 9, 2019 · N465UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > AFT CARGO LT FR63-64 AIRPHONE DOUBLER HAS CORRSION NTERNAL SURFACE STR41L PER NON ROUTINE 9296857. REMOVED AND REPLACED AIRPHONE DOUBLER LT FR63-64 STR 41L IAW SRM 53-00-11-300-029 THIS IS A CAT B REPAIR WITH A SRI INSP AT 21200 FC/42400FH FROM EMBODIMENT AND
- [SDR CALA2019091301524](https://openairdocs.org/sdr/CALA2019091301524.md): Doubler · corroded · Sep 9, 2019 · N465UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > AFT CARGO RT FR63-64 AIRPHONE DOUBLER HAS CORROSION INTENAL SKIN PER NON ROUTINE 9296858. REMOVED AND REPLACED RT AIRPHONE DOUBLER FR 63-64 STR 41R IAW SRM 53-00-11-300-049 THIS IS A CAT B REPAIR W/ A SRI INSP AT 20000FC/40000FH FROM EMBODIMENT AND SUBSEQUENT
- [SDR CALA2019091301523](https://openairdocs.org/sdr/CALA2019091301523.md): Door Sill · corroded · Sep 9, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT DOOR SILL WEB UPPER SURFACE HAS SPOTS OF CORROSION A3NB-53-4-6179. PER NON ROUTINE 9 296491 AFT CARGO DOOR SILL WEB REMOVED AND REPLACED FOR ELONGATED HOLES IAW SRM 51-42-11-801.
- [SDR CALA2019091301522](https://openairdocs.org/sdr/CALA2019091301522.md): Stringer · corroded · Sep 9, 2019 · N465UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT BETWEEN FR63-64 STRINGER 41R HAS CORROSION PER NON ROUTINE 9296502. REMOVED AND REPLACED STR 41 FROM FR 58 TO 64 IAW SRM 51-42- 11-801 PG 9-19.
- [SDR CALA2019090601494](https://openairdocs.org/sdr/CALA2019090601494.md): Stringer · corroded · Aug 31, 2019 · N465UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STR42R FR33-34 HAS CORROSION AROUND REMOVED FASTENER F ROM CARD 40838 PER NON ROUTINE 9296903 ACCOMPLISHED CAT B REPAIR ON STR 42R FR 33-34 FWD CARGO IAW SRM 53-21-13-300-004, REPAIR REQUIRES INSPECTION AT 60,000 FC/120,000 FH WICHEVER OCCURES FIRST
- [SDR CALA2019090201468](https://openairdocs.org/sdr/CALA2019090201468.md): Support · corroded · Aug 29, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FR28 BETWEEN STR 37R TO 38R TIE DOWN SUPPORT HAS CORROSION PER NON ROUTINE 9296966. REMOVED AND REPLACED TIE DOWN SUPPORT AT FR28 BETWEEN STR 37R-38 R IAW SRM 51-72-11.
- [SDR CALA2019090201467](https://openairdocs.org/sdr/CALA2019090201467.md): Support · corroded · Aug 29, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FR28 BETWEEN STR37R TO 38R TIE DOWN SUPPORT HAS CORROSION PER NON ROUTINE 9296966. REMOVED AND REPLACED TIE DOWN SUPPORT AT FR28 BETWEEN STR 37R-38 R IAW SRM 51-72-11.
- [SDR CALA2019082601436](https://openairdocs.org/sdr/CALA2019082601436.md): Door Sill · corroded · Aug 25, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN RH DOOR SILL CORRODED AT FR68 GIRT BAR FITTING. REMOVED AND REPLACED AFT CABIN R/H DOOR SILL AT FR68 GIRT BAR FI TTING IAW SRM 51-72-11-911-001.
- [SDR CALA2019082601434](https://openairdocs.org/sdr/CALA2019082601434.md): Fitting · corroded · Aug 23, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R2 DOOR AFT CORNER FITTING IS CORRODED. REMOVED AND REPLACED AFT CABIN R2 DOOR AFT CORNER FITTING IAW SRM 51-72-11-911-001.
- [SDR CALA2019082301424](https://openairdocs.org/sdr/CALA2019082301424.md): Fitting · corroded · Aug 22, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR FWD CORNER FITTING CORRODED. REMOVED AND REPLACED R2 DOOR FWD CORNER FITTING IAW SRM 51- 72-11-911-001.
- [SDR CALA2019082301412](https://openairdocs.org/sdr/CALA2019082301412.md): Door Sill · corroded · Aug 21, 2019 · N465UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN L2 DOOR SILL IS CORRODED AT FR68. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-911-001.

Next page: https://openairdocs.org/aircraft/N465UA/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 = 'N465UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N465UA/reports

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