# Service difficulty reports: N435UA

A list on [N435UA](https://openairdocs.org/aircraft/N435UA.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 · 141 reports

- [SDR CALA2026052716568](https://openairdocs.org/sdr/CALA2026052716568.md): Wire Harness · damaged · May 26, 2026 · N435UA · Airbus A320232 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHT AT 23C INOPERATIVE. REMOVED AND REPLACED ROW 23ABC EMERGENCY LIGHTING HARNESS, REF AMM 33-51-22, OPS CHECK GOOD.
- [SDR CALA2026050415928](https://openairdocs.org/sdr/CALA2026050415928.md): Battery Pack · discharged · May 2, 2026 · N435UA · Airbus A320232 · Emergency Lighting
  > FOUND EPSU BATTERY EMER COMM L INOPERATIVE. REMOVED AND REPLACED EPSU BATTERY L, REF AMM 33-51-38. OPS CHECK NORMAL. OK TO CONTINUE.
- [SDR CALA2026030214144](https://openairdocs.org/sdr/CALA2026030214144.md): Sensor · faulted · Feb 26, 2026 · N435UA · Airbus A320232 · Cabin Cooling System
  > NR 2 A/C PACK OVERHEAT ECAM MESSAGE ON DESCENT. COMPLETED ECAM PROCEDURE WHICH RESET SYSTEM. YELLOW XX DISPLAYED PLAN TO ACP TSM 21-61-00 AND IF NEEDED APPLY MEL 2152Z. VERIFIED PACK FLOW CONTROL VALVE CLOSED ON ECAM AND APPLIED MEL 2152Z FOR PACK 2. VERI
- [SDR CALA2025111711236](https://openairdocs.org/sdr/CALA2025111711236.md): Circuit Breaker · faulted · Nov 15, 2025 · N435UA · Airbus A320232 · Light System Wiring
  > EMERGENCY EXIT SIGNSILLUMINATED IN CABIN WITH COCKPIT SWITCH INTH E ARMED POSITION PERFORMED CIRCUIT BREAKER RESET. TURNED SEAT BELT SIGN OFF AND TURNED OFF EMERGENCY LIGHTS FROM FLIGHT DECK SWITCH, CABIN EMERGENCY EXIT SIGNS EXTINGUISHED. ARMED EMERGENCY LIGH
- [SDR CALA2025071606634](https://openairdocs.org/sdr/CALA2025071606634.md): Elec Connector · loose · Jul 10, 2025 · N435UA · Airbus A320232 · Door System Wiring
  > DOOR AFT CARGO ECAM. PLACED AFT CARGO DOOR INDICATION ON MEL. VERIFIED AFT CARGO DOOR IS CLOSED AND LATCHED. OK TO CONTINUE. PLR SHOWS AFT CARGO DR SAFETY MECHANICAL PROXIMITY SENSOR (32WV) TGT POS, POSSIBLE SENSOR 32WV OR DOOR HANDLE LINKAGE MAY NEED ADJU
- [SDR CALA2025041603897](https://openairdocs.org/sdr/CALA2025041603897.md): Bottle · overserviced · Apr 14, 2025 · N435UA · Airbus A320232 · Emergency Equipment
  > SLIDE PRESSURE AT DOOR R2 IS SLIGHTLT OVER PRESSURE IN RED BAND. VERIFIED CORRECT SLIDE PRESSURE FOR R2 ESCAPE SLIDE REF AMM 25-62-44
- [SDR CALA2025021402323](https://openairdocs.org/sdr/CALA2025021402323.md): Oxygen Box · damaged · Feb 13, 2025 · N435UA · Airbus A320232 · Passenger Oxygen System
  > O2 MASK FELL IN FWDLAV UPON INSPECTION OF O2 MASK BOX OUTBOARD LATCH SPRING AND ROD GUIDE IS BROKEN AND ROD IS BENT. UNABLE TO LATCH O2 DOOR CLOSED IPC 35-21-01-01E, ITEM 10Z, 10T. PN 807894-214 (M&E 31-3512-3-0004)BOTTLE. PN AH5702-51-U1 (M&E 31-3512-3-0014)C
- [SDR CALA2025012402017](https://openairdocs.org/sdr/CALA2025012402017.md): Power Supply · faulty · Jan 22, 2025 · N435UA · Airbus A320232 · Emergency Lighting
  > DURING TROUBLESHOOTING OF EMERGENCY LIGHTS FOUND LEFT EMERGENCY EXIT POWER SUPPLY 11WL TEST BUTTON INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 11WL, OPS CHECK GOOD REF AMM 33-51-38.
- [SDR CALA2025012402016](https://openairdocs.org/sdr/CALA2025012402016.md): Connector · disconnected · Jan 22, 2025 · N435UA · Airbus A320232 · Light System Wiring
  > DURING TROUBLESHOOTING OF EMERGENCY LIGHTS FOUND SEAT MOUNTED ESCAPE PATH LIGHTS ROWS 12ABC TO 22ABC INOPERATIVE. FOUND CONNECTOR 7261VC1 AT SIDEWALL UNDER SEAT 20ABC DISCONNECTED, RESECURRED OPS CHECK OK REF AWM 33-51-07 PAGE 179A AND AMM 33-51-00.
- [SDR CALA2025012402013](https://openairdocs.org/sdr/CALA2025012402013.md): Connector · disconnected · Jan 21, 2025 · N435UA · Airbus A320232 · Light System Wiring
  > DURING CIDS TEST FAULT MESSAGE OCCURED EPSU INT LOAD EMER POST R1 DOOR SLIDE INSTALLATION FOUND RH FWD EMERGENCY DOOR HANDLE LIGHT BURNT OUT, PARTS NIS IAD TESTED RIGHT OVER WING EXIT EMERGENCY POWER SUPPLY UNIT 12WL, FOUND EXTERNAL LIGHT FAULT. FOUND RIGHT F
- [SDR CALA2025011501911](https://openairdocs.org/sdr/CALA2025011501911.md): Battery Pack · no test · Jan 13, 2025 · N435UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - EMERGENCY LIGHT BATTERY PACK AT POSITION # 12 WL. R / H SIDE OUT OF DATE PER W / C A3NB-33-3-6013. REMOVED AND REPLACED (OUT OF DATE) BATTERY PACK AND TESTEDIAW UAL W / C 18-3351-1
- [SDR CALA2024103000965](https://openairdocs.org/sdr/CALA2024103000965.md): Waste Tank · leaking · Oct 27, 2024 · N435UA · Airbus A320232 · Water and Waste System
  > REF LP 9680021, WASTE WATER LEAKED FROM AFT WASTE TANK LEVEL TRANSMITTER BEHIND AFT BULKHEAD, DOWN AND ALONG BELLY SKIN GOING FOWARD BELOW AFT PIT FLOOR, AND COMING OUT FROM FWD DRAIN OF AFT CARGO PIT. LEAK WAS RPRD, NEED TO ACP IN-DEPTH CLEAN UP OF SPILL AN
- [SDR CALA2024091302412](https://openairdocs.org/sdr/CALA2024091302412.md): Skin · corroded · Sep 11, 2024 · N435UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > SKIN AND HOLES UNDER TCAS ANTENNA HAS CORROSION () REMOVED AND REPLACED DAMAGE PARTS, STIFFNER UAD 5323163820, SPLI ISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 108244 CES. UAD 5323164220000 AND UAD 5323164220100. I.A.W. SRM 51-42-1 1 AND DRAWING D23531598
- [SDR CALA2024091602431](https://openairdocs.org/sdr/CALA2024091602431.md): Skin · dented · Aug 26, 2024 · N435UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > RH AFT FUSELAGE AT FRAME 63 & STR 31R, HAS A DENT. MPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF AIRCRAFT FLIGHT CYCLES (FH NOT RELEVANT). ACCOMPLISH REPEAT INS EC/RA 5341-01466 ON OR BEFORE THE AIRCRAFT REACHING 39,907 TOTAL PECTIONS EVERY 6
- [SDR CALA2024091602429](https://openairdocs.org/sdr/CALA2024091602429.md): Fitting · cracked · Aug 10, 2024 · N435UA · Airbus A320232 · Fuselage Main, Structure
  > WHILE ACCOMPLISHING INSPECTION OF L/H AND R/H WINDSHIELD LOWER N ODE AND CONTINUITY FITTING, CRACKS NOTED ON L/H AND R/H FITTINGS. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGH T." () REMOVED AND REPLACED LHS AND RHS CONTINUITY FITTING PER EC
- [SDR CALA2023101303052](https://openairdocs.org/sdr/CALA2023101303052.md): Fuel Cap · missing · Oct 12, 2023 · N435UA · Airbus A320232 · Aircraft Fuel Distribution System
  > PDA 2 FUEL CAP NOT INSTALLED. INSTALLED FUEL CAP PER AMM 28-25-41. RAMP REPORTING A/C ARRIVED WITHOUT FUEL CAP INSTALLED.NO DAMAGE TO AREA NOTED. SUSPECT IMPROPERLY INSTALLED AT PREVIOUS STATION.
- [SDR CALA2023021300427](https://openairdocs.org/sdr/CALA2023021300427.md): Fuel Cap · missing · Feb 13, 2023 · N435UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 FUEL CAP MISSING. INSTALLED NEW FUEL CAP. PARTS USED: 31-2825-9-0001,QTY:1
- [SDR CALA2022042901103](https://openairdocs.org/sdr/CALA2022042901103.md): None · damaged · Apr 29, 2022 · N435UA · Airbus A320232 · Doors
  > COCKPIT DOOR ''FAULT'' LIGHT AND DOOR CONTROLLER ''TOP STRIKE'' OR LOWER STRAKE LIGHT IS ON REPEAT WRITE UP.CAME ON ENROUTE REPLACED TOP STRICKER NO HELP REMOVED PINS AND SECURED REF DDPC/W NUMBER REF WDM 52-51-02 DEFFERED TOP STRICKER ROTABLE PARTS CHANGE WAS
- [SDR CALA2022030100544](https://openairdocs.org/sdr/CALA2022030100544.md): Light · failed · Mar 1, 2022 · N435UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - EMERGENCY LIGHT SYSTEM TEST FAILS. DISPLAYS "ESPU INT LOAD AFT L" RESET ESPU 13WL POWER REF TSM 33-51-00. EMERGENCY LIGHTING OPS CHECK GOOD REF AMM 33-51-00.
- [SDR CALA2022020800345](https://openairdocs.org/sdr/CALA2022020800345.md): Stringer · corroded · Feb 8, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STR44 POSSIBLE CORROSION FWD OF FR34 (A3NB-53-3-6105) GENERATED BY V079881 AT HAECO LCQ PER NR 9292507 (30507) REMOVED AND REPLACED STRINGER 44 AT FWD CARGO IAW A320 SRM 51-72 -11-911-001 AND SRM 51-72-11-911-002. MECH V929087 INSP BY N0785 70
- [SDR CALA2022020800344](https://openairdocs.org/sdr/CALA2022020800344.md): Stringer · corroded · Feb 7, 2022 · N435UA · Airbus A320232 · Fuselage Main, Frame
  > AFT PIT STR 32R BETWEEN FRAME 62 & 63 HAS CORROSION.SUPPORT TASK GENERATED BY:V061334 AT HAECO LCQ PER NON ROUTINE 9292561 (3056 1) REMOVED AND REPLACED SECTION OF STRINGER 32R BETWEEN FR 62 & 63 IAW A320 SRM 53-00-13-300-001.
- [SDR CALA2022020400317](https://openairdocs.org/sdr/CALA2022020400317.md): Stringer · corroded · Feb 3, 2022 · N435UA · Airbus A320232 · Fuselage Main, Frame
  > A3NB-AFT PIT STR 32R BETWEEN FRAME 62 & 63 HAS CORROSION GENERAT ED BY:V061334 @ HAECO LCQ PER NON ROUTINE: 9292561 (30561) REMOVED SECTION OF STRINGER 32RT INSTALLED SECTION OF STRINGER 3 2RT. INSTALLED STRINGER & SPLICE BETWEEN 62-63RT. IAW A320 DISREGARD TH
- [SDR CALA2022013100281](https://openairdocs.org/sdr/CALA2022013100281.md): Stringer · corroded · Jan 31, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO BLIGE AREA 43R REPAIR CORRODED FR 22-27 REMOVED EXISTING REPAIR CUT & TRIMMED SECTION OF REPAR AND INSTA LLED REPAIR IN FWD CARGO PIT BETWEEN FR 26-27-RT ON STRINGER 42R T IAW SRM 51-72-11 AND SRM 53-21-13-300-003
- [SDR CALA2022012400205](https://openairdocs.org/sdr/CALA2022012400205.md): Stringer · corroded · Jan 22, 2022 · N435UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT CORROSION AT STR 40R BETWEEN FR58-FR64. GENERATED BY V061334 ON HAECO LCQ NR 9292527/30527 REMOVED AND REPLACED STRINGER 40RIGHT IN AFT CARGO PIT FRAME 58-64RT IAW A320 SRM 51-72-11. PERFORMED BY V913406 AND INSP BY V892285.
- [SDR CALA2022012400204](https://openairdocs.org/sdr/CALA2022012400204.md): Plate · corroded · Jan 22, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO PIT SILL TORSION BOX COVER CORROSION SEVERAL PLACES. G ENERATED BY V061334 ON HAECO LCQ NR 9292520/30520 REMOVED AND REPLACED AFT CARGO TORSION BOX COVER SHEET IAW A320 SRM 51-72-11. PERFORMED BY V052030 AND INSP BY V892285.
- [SDR CALA2022012400203](https://openairdocs.org/sdr/CALA2022012400203.md): Stringer · corroded · Jan 22, 2022 · N435UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO PIT CORR AT 41R BETWEEN FR 58-59 GENERATED BY V061334 A3NB-05-3-6024 HAECO LCQ PER NON ROUTINE# 9292528 (30528) REMOVED AND REPLACED STRINGER 41 RIGHT IN AFT CARGO PIT FR58-64 PERFORMED BY:V092030 INSP BY:V061334.
- [SDR CALA2022011800183](https://openairdocs.org/sdr/CALA2022011800183.md): Stringer Splice · corroded · Jan 18, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STRINER SPLICE STR41L FR30-FR31 CORRODED GENERATED BY V079881 ON HAECO LCQ NR 9292493/30493. ORGINAL LP 7776370 REMOVED & REPLACED STRINGER SPLICE ON STG 41L BETWEEN FR 30-31 I AW A320 SRM 51-72-11 ADD EMP:V061765
- [SDR CALA2022011800167](https://openairdocs.org/sdr/CALA2022011800167.md): Stringer · corroded · Jan 16, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO BILGE AREA STR 42R REPAIR CORRODED FR26-27 GENERATED B Y V079881 ON HAECO LCQ NR 9292468/30468. ORGINAL LP#7776381. REPAIR STRINGER ASSY PER SRM 51-72-11 & 53-21-13-300-003 ADD EMP:V063868
- [SDR CALA2022011700161](https://openairdocs.org/sdr/CALA2022011700161.md): Splice · corroded · Jan 16, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STRINER SPLICE STR41L FR30-FR31 CORRODED GENERATED BY V079881 ON HAECO LCQ NR 9292493/30493. ORGINAL LP 7776370 REMOVED & REPLACED STRINGER SPLICE ON STG 41L BETWEEN FR 30-31 I AW A320 SRM 51-72-11 ADD EMP:V061765
- [SDR CALA2022011700160](https://openairdocs.org/sdr/CALA2022011700160.md): Splice · corroded · Jan 15, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STRINER SPLICE STR42L FR30-FR31 CORRODED GENERATED BY V079881 ON HAECO LCQ NR 9292492/30492 FWD CARGO STRINGER STR 42L FR30-FR31 CORRODED
- [SDR CALA2022011700159](https://openairdocs.org/sdr/CALA2022011700159.md): Splice · corroded · Jan 15, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STRINER SPLICE AT STR43L FR31 CORRODED GENERATED BY V0 79881 ON HAECO LCQ NR 9292489/30489 REMOVED AND REPLACED FWD CARGO SPLICE ON STRINGER 43 LEFT BETWEE N FRAME 30-31 IAW SRM 51-72-11
- [SDR CALA2022011400150](https://openairdocs.org/sdr/CALA2022011400150.md): Stringer Splice · corroded · Jan 13, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO STRINER SPLICE STR42L FR30-FR31 CORRODED GENERATED BY V079881 ON HAECO LCQ NR 9292492/30492 FWD CARGO STRINGER STR 42L FR30-FR31 CORRODED
- [SDR CALA2022011200115](https://openairdocs.org/sdr/CALA2022011200115.md): Cleat · corroded · Jan 11, 2022 · N435UA · Airbus A300* · Fuselage Structure (General)
  > FWD CARGO BILGE HAS CORRODED CLEAT AT FR28 STR41R-42R. PER HAECO LCQ NR 9292476/30476 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO PIT AT FR28 STR 41R-42RT IAW A320 SRM 51-72-11
- [SDR CALA2022011200110](https://openairdocs.org/sdr/CALA2022011200110.md): Cleat · corroded · Jan 10, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO BILGE HAS CORRODED CLEAT @ FR26 STR44-STR43L. PER HAEC O LCQ NR 9292464/30464 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO FR 26 STR 44-43LT IAW A3 20 SRM 51-72-11
- [SDR CALA2022011200109](https://openairdocs.org/sdr/CALA2022011200109.md): None · corroded · Jan 10, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO TORSION BOX UPPER SKIN HAS CORROSION AT MULTIPLE FASTE NER HOLES. PER HAECO LCQ NR 9292518/30518 GENERATED BY V079881 REMOVED AND REPLACED FWD CARGO TORSION BOX SKIN IAW A320 ARM 51- 72-11 INSTALLED FWD CARGO PROFILE PANEL IAW A320 SRM 51-22-11
- [SDR CALA2022011200108](https://openairdocs.org/sdr/CALA2022011200108.md): None · corroded · Jan 10, 2022 · N435UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO BILGE FR28 STR43R-STR42R HAS CORRODED CLEAT. PER HAECO LCQ NR 9292470/30470 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO FR28RT BETWEEN 43R-42R I AW A320 SRM 51-72-11
- [SDR CALA2022010700060](https://openairdocs.org/sdr/CALA2022010700060.md): Frame · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Main, Frame
  > FWD CARGO FR33 STR40L-STR41L HAS CORRODED CLEAT REMOVED AND REPLACED CLEAT AT FR33 STR40L-STR41L IAW ARM 51-75-1 2-911-001 ADD EMP:V052030
- [SDR CALA2022010700049](https://openairdocs.org/sdr/CALA2022010700049.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR29 STR43R-STR42R CLEAT IS CORRODED. REMOVED AND REPLACED CLEAT IN FWD CARGO FR 29 STR43R-STR42R IAW S RM 51-42-17.
- [SDR CALA2022010700048](https://openairdocs.org/sdr/CALA2022010700048.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR33 STR41R-STR42R HAS CORRDED CLEAT. REMOVED AND REPLACED CLEAT IN FWD CARGO FR 33 STR41R-STR42R IAW ARM 51-77-11.
- [SDR CALA2022010700047](https://openairdocs.org/sdr/CALA2022010700047.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Standard Practices/Structures
  > FWD CARGO FR33 STR40R-41R HAS CORRDED CLEAT. REMOVED AND REPLACED CLEAT IN FWD CARGO FR33 STR40R-STR41R IAW 5 1-72-11.
- [SDR CALA2022010700046](https://openairdocs.org/sdr/CALA2022010700046.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR33 STR41L-STR42L HAS CORRODED CLEAT. REMOVED AND REPLACED VLEAT AT FR 33 STR41L AND STR42L IAW SRM 51 -42-11-511-001.
- [SDR CALA2022010700045](https://openairdocs.org/sdr/CALA2022010700045.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR33 STR42L-STR43L HAS CORRODED CLEAT. REMOVED AND REPLACED CLEAT AT FR 33 STR42L-STR43L IAW SRM 51-75- 12-911-001.
- [SDR CALA2022010700043](https://openairdocs.org/sdr/CALA2022010700043.md): Shear Tie · corroded · Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FR33 STR40L-STR41L HAS CORRODED CLEAT REMOVED AND REPLACED CLEAT AT FR33 STR40L-STR41L IAW ARM 51-75-1 2-911-001 ADD EMP:V052030
- [SDR CALA2020011300143](https://openairdocs.org/sdr/CALA2020011300143.md): Hydraulic Line · chafed · Jan 11, 2020 · N435UA · Airbus A320232 · Hydraulic System, Main
  > HYD Y ENG2PUMP LO PRECAM PRESENTED DURINGAPP PHASE. UPON ARRIVAL OBSERVED EVIDENCE OF HYD LEAK COMING FROM #2 ENG PYLON DRAIN. AS PER CERW VERBAL ENG PUMP WAS OPERATED FOR APPROX 1 MINUTE BEFORE THEY TURNED IT OFF. REF AMM 29-00-00-280-006-A01. LEAKING IN #2 P
- [SDR CALA2019031100378](https://openairdocs.org/sdr/CALA2019031100378.md): Shear Plate · cracked · Mar 8, 2019 · N435UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RIGHT SIDE SHEAR PLATE IS CRACKED AT FWD JOGGLE. REF NR 99833891 REMOVED AND REPLACED RIGHT SIDE SHEAR PLATE AT WET AREA PER REF SRM 51-42-11.
- [SDR CALA2019030800366](https://openairdocs.org/sdr/CALA2019030800366.md): Stringer · corroded · Mar 6, 2019 · N435UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA STGR 40R HAS EVIDENCE OF SURFACE CORROSION.AROUND FASTENERS BETWEEN FR 58 AND 60. MKD 126-017. REF. N/R:99833879 PERFORMED, LOCATED, DRILLED AND INSTALLED REPAIR AT AFT CARGO COMP BETWEEN FR. 59-60 IAW SRM 51-42-11, 53-00-13 FI
- [SDR CALA2019030800365](https://openairdocs.org/sdr/CALA2019030800365.md): Stringer · corroded · Mar 6, 2019 · N435UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA STR 40R PREVIOUS REPAIR HAS EVIDENCE OF SURFACE CORROSION. BETWEEN FR 61 AND 60. MKD 126-016 REF. N/R:99833878 REPAIRED AFT CARGO COMPT. BILGE AREA STR 40R BETWEEN FR62 TO FR 60 AS PER SRM 53-00-13 REF. N/R:99833878.
- [SDR CALA2019030800364](https://openairdocs.org/sdr/CALA2019030800364.md): Stringer · corroded · Mar 6, 2019 · N435UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA STGR 39R HAS EVIDENCE OF SURFACE CORROSION AROUND PREVIOUS REPAIR FASTENERS BETWEEN FR59 AND FR60 - MKD. REF N/R:99833912 LOCATED, DRILLED AND INSTALLED NEW SPLICE ANGLE AT AFT CARGO COMP FR 59-60 USING P/N:2001T79511 IAW SRM 5
- [SDR CALA2019030800363](https://openairdocs.org/sdr/CALA2019030800363.md): Door Sill · corroded · Mar 6, 2019 · N435UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 SILL BEAM CORRODED AT FR66. REF. N/R:99830115 REMOVED AND REPLACED R2 DOOR SILL BEAM PIN 31-2098-3-2394 PO #1590766 IAW SRM 53-41-14, 51-44-11 AND 51-42-11. R2 DOOR GIRT BAR FITTING ADJUSTMENT WILL ACCOMPLISH ON N/R 99833908. REF.99830115.
- [SDR CALA2018022700825](https://openairdocs.org/sdr/CALA2018022700825.md): Battery · no test · Feb 27, 2018 · N435UA · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY LIGHT BATTERIES FAILED CABIN EMERGENCY LIGHTS OPS CHECK IAW TASK CARD 18-2428-1-6192, ITEM 27. REPLACED THE BATTERIES. PERFORMED EMERGENCY LIGHT SYS CHECK AND TESTED GOOD IAW 33-51-38, TASK CARD 18-2428-1-6192, ITEM 27.

Next page: https://openairdocs.org/aircraft/N435UA/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 = 'N435UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N435UA/reports

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