# Service difficulty reports: N481UA

A list on [N481UA](https://openairdocs.org/aircraft/N481UA.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 · 103 reports

- [SDR CALA2026062517339](https://openairdocs.org/sdr/CALA2026062517339.md): Battery · faulted · Jun 24, 2026 · N481UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY FWD L MESSAGE REMOVED AND REPLACED FWD LEFT EPSU BATTERY PER AMM 33-51-38-400-002-A. OPS CHECK GOOD.
- [SDR CALA2026022013944](https://openairdocs.org/sdr/CALA2026022013944.md): Fuel Cap · missing · Feb 15, 2026 · N481UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS MISSING FUEL CAP REQUESTING CDL FOR MISSING FUEL CAP. COMPLIED WITH CDL ITEM PLACED ON CDL REPLACED FUEL CAP, OPS CHECK GOOD.
- [SDR CALA2025072106780](https://openairdocs.org/sdr/CALA2025072106780.md): Light · broken · Jul 18, 2025 · N481UA · Airbus A320232 · Emergency Lighting
  > 29C EMERGENCY EXIT LIGHT BROKEN PLACED ON MEL OK TO MEL COMPLIED WITH MEL REMOVED AND REPLACED 29C EMERGENCY EXIT LIGHT REF AMM 33-51-18. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2025070106113](https://openairdocs.org/sdr/CALA2025070106113.md): Slide · faulted · Jun 28, 2025 · N481UA · Airbus A320232 · Escape Slide
  > ACFT L OVERWING SLIDE BLOWN. REMOVED SLIDE FROM ACFT. BLOWN SLIDE PLACED IN AFT CARGO. ALL MX DONE IN REF WITH AMM 25-62-42/401 CONFIG 00 PARTS TRANSACTION ROTABLE PARTS CHG:TT # 1480754 SN OFF 4281 PN OFF 31-2561-9-0001.IPC REFERENCE # MFG SN OFF NOT ON AC M&
- [SDR CALA2025012702043](https://openairdocs.org/sdr/CALA2025012702043.md): Fuel Cap · missing · Jan 26, 2025 · N481UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING... INSTALLED NEW FUEL CAP ASSLY..REF AMM 28-25-41.
- [SDR CALA2025011401900](https://openairdocs.org/sdr/CALA2025011401900.md): Battery Pack · inoperative · Jan 13, 2025 · N481UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY FWD L MESSAGE APPEARS WILIST ACCOMPLIHING TEST ACCOMPLISHED BITE OF EMERGENCY LIGHT SYSTEM REF TSM33-51-00-810-802-A AND MM33-51-00-710-001. OPS CHECKS GOOD. SEE ATTACHED PICTURES.
- [SDR CALA2024080500371](https://openairdocs.org/sdr/CALA2024080500371.md): Acars · faulted · Aug 1, 2024 · N481UA · Airbus A320232 · Data Transmission Auto Call
  > ACARS ACTING UP SEE LOG PAGE 8798710 ACARS INOP IN AIRRESET ACARS SYSTEM REF AMM 23-24-00-710-001 OPS TEST NORMAL.
- [SDR CALA2024061201778](https://openairdocs.org/sdr/CALA2024061201778.md): Floor Support · corroded · Jun 11, 2024 · N481UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT FLOOR BEAM Y765 (FR 66.5-70) REQUIRES REPLACEMENT DUE TO CORROSION REF STS N0064. REMOVED AND REPLACED AFT FLOOR BEAM AT Y765 FR66. 5-FR70 IAW A-320 SRM 51-42-11.
- [SDR CALA2024061201777](https://openairdocs.org/sdr/CALA2024061201777.md): Floor Support · corroded · Jun 11, 2024 · N481UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT Y512.5 (FR 67.5-70) REQUIRES REPLACEMENT DUE TO CORROSION REF STS N0063. REMOVED AND REPLACED AFT FLOOR BEAM Y512.5 FR67.5 -FR70. IAW A320 SRM 51-41-11.
- [SDR CALA2024061201776](https://openairdocs.org/sdr/CALA2024061201776.md): Floor Support · corroded · Jun 11, 2024 · N481UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT Y160.5 (FR 68-70) REQUIRES REPLACEMENT DUE TO CORROSION REF STS N0062. REMOVED AND REPLACED AFT FLOOR BEAM AT Y160.5 FR6 8-FR70, IAW SRM 51-42-11.
- [SDR CALA2024061201775](https://openairdocs.org/sdr/CALA2024061201775.md): Stringer · cracked · Jun 11, 2024 · N481UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STR 7 CRACKED BETWEEN FR 63 - FR 64
- [SDR CALA2024031200701](https://openairdocs.org/sdr/CALA2024031200701.md): Relay · faulty · Mar 8, 2024 · N481UA · Airbus A320232 · Airfoil Anti/De-ice System
  > WING ANTI-ICE DISPLAYED AS INOP SYS ON ECAM STATUS PAGE. NO ECAM WARNING, NO FAULT LIGHT - WING ANTI-ICE. CAME ON DURING CLIMBOUT REF LOG 7288701 FOR TROUBLESHOOTING INFO. - TOMC KROWN ITEM UNLOCKED FOR CLEARING ACTION NO STORED FAULTS. NO MESSAGES. REPLACED 5
- [SDR CALA2023120803583](https://openairdocs.org/sdr/CALA2023120803583.md): Actuator · faulty · Dec 7, 2023 · N481UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. - ENG. ENG 1 COMPRESSOR VANE ECAM ON TO ROLL.RTO T/S IAW TSM 75-30-00-810-845-A. PER TOMC ENGINE DESK, THIS IS A POST SB 75-0122 ENGINE. FADEC 1B GIVES THE FAULT ACRONYM SVATK AND THERE ARE 3 MORE OCCURANCES IN F
- [SDR CALA2023112903500](https://openairdocs.org/sdr/CALA2023112903500.md): Fuel Cap · missing · Nov 25, 2023 · N481UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUELER REPORTS FOUND FUEL CAP MISSING. INSTALLED NEW FUEL CAP REF AMM 28-25-41.PARTS USED: 31-2825-9-0001,QTY:1
- [SDR CALA2023101803108](https://openairdocs.org/sdr/CALA2023101803108.md): Unknown · unknown · Oct 17, 2023 · N481UA · Airbus A320232 · Air Distribution System
  > SMELL OR BURNING ELECTRICAL ODOR REPORTED BY MAINTENANCE DURING A/C VITALS CHECK. PERFORMED MAINTENANCE CHECK TSM 05-50-00-810-831-A TYPES 9&10. NO POSSIBLE ODORS SOURCES FOUND.
- [SDR CALA2023062802051](https://openairdocs.org/sdr/CALA2023062802051.md): Hose · inoperative · Jun 25, 2023 · N481UA · Airbus A320232 · Hydraulic System, Main
  > UNABLE TO RAISE GEAR, AIRCRAFT HAS LOST GREEN SYS HYD HYDRAULIC LINE BLOWN OFF LEFT MAIN GEAR. REMOVED AND REPLACED OUTBOARD LOCKSTAY ACTUATOR HOSE UP TO STEP C (1) IAW AMM 32-11-22-400-001-A FUNCTNAL CK REQUIRED WAITING ON TOOLING DRT68864. PARTS USED: 18-32
- [SDR CALA2022040800914](https://openairdocs.org/sdr/CALA2022040800914.md): None · missing · Apr 7, 2022 · N481UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022040800914 SUBMITTED ON 04/08/22.FUELER REPORTS THAT THE FUEL CAP AND LANYARD MISSING ON THE INBOUND ARRIVAL. REPLACED, COUPLING REFUEL UNDERWING MISSING.
- [SDR CALA2022012400216](https://openairdocs.org/sdr/CALA2022012400216.md): Frame · corroded · Jan 24, 2022 · N481UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > AFT CARGO FR56 - FR58 40L CORRODED A3NB-53-4-6179 PER NR9290621/ 28621 GEN BY V061629 STR IAW A320SRM 53-00-13-300-001 AND IAW A320SRM 51-42-10/001. REPAIR IN AFT CARGO FR56-58 STR 40L REQUIRE AN SRI, SRI TIME OF ADL/REPAIR EMBODIMENT SUBSEQUENT INSP AT INTERV
- [SDR CALA2022012000190](https://openairdocs.org/sdr/CALA2022012000190.md): Plate · cracked · Jan 19, 2022 · N481UA · Airbus A320232 · Fuselage Structure (General)
  > LH PRESSURE PNL FRAME 36 HOLES 2,3,4,5,6,7,9,10,15,20,21,22,23,2 4,26,27 AND 28 ARE CRACKED IN THE PRESSURE PNL AD2018-06-04 GEN BY V061633 AT HAECO LCQ PER NR 9290732 (28732). ACP REPAIR INSTRUCTIONS PER REO L-23537 REV IR WITH NO DEVIATION 63,512 TOTAL A/C F
- [SDR CALA2022012000189](https://openairdocs.org/sdr/CALA2022012000189.md): Plate · cracked · Jan 19, 2022 · N481UA · Airbus A320232 · Fuselage Structure (General)
  > RH PRESSURE PNL FRAME 36 HOLES 4,6,7,8,9,13,14,16,17,18,20,22,25 AND 26 ARE CRACKED IN THE PRESSURE PANEL AD2018-06-04 GEN BY V0 61633 ACCOMPLISHED REPAIR INSTRUCTIONS ON RH FR36 PRESSURE PANEL PER R ON OR BEFORE 69,512 TOTAL AIRCRAFT FLIGHT CYCLES OR 146,671
- [SDR CALA2022011700158](https://openairdocs.org/sdr/CALA2022011700158.md): Stringer · corroded · Jan 15, 2022 · N481UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO FR56 - FR58 40L CORRODED A3NB-53-4-6179 PER NR9290621/ 28621 GEN BY V061629 STR IAW A320SRM 53-00-13-300-001 AND IAW A320SRM 51-42-10/001. REPAIR IN AFT CARGO FR56-58 STR 40L REQUIRE AN SRI, SRI TIME OF ADL/REPAIR EMBODIMENT SUBSEQUENT INSP AT INTERV
- [SDR CALA2022011400126](https://openairdocs.org/sdr/CALA2022011400126.md): Intercostal · cracked · Jan 12, 2022 · N481UA · Airbus A300* · Fuselage Main, Frame
  > L1 DOOR FRAME 16 STOP #7 INBOARD LOWER HOLE IS CRACKED IN THE IN TERCOASTAL AT 5 O''CLOCK AND THE INBOARD UPPER HOLE IS CRACKED IN THE WEB AT 11 O''CLOCK AND INTERCOASTAL AT 5 O''CLOCK. SUPPORT TASK AD 2019-20-10 GENERATED BY V061633 AT HAECO LCQ PER NON ROUTI
- [SDR CALA2022010500028](https://openairdocs.org/sdr/CALA2022010500028.md): Stringer · corroded · Jan 4, 2022 · N481UA · Airbus A300* · Waste Disposal System
  > 171/172 EVIDENCE OF CORROSION ON FR66 STR41L GENERATED BY V50 2040 AT HAECO LCQ PER NON ROUTINE 9290216 (28216) (A3NB-53-3-627 9) REMOVED STRINGER SECTION AT STRG41L FR66 A320 SRM 51-42-11. REC IEVED STRINBGER MATERIAL & COUPLING DAN50B11 T73511 PO1043697 FO
- [SDR CALA2022010300006](https://openairdocs.org/sdr/CALA2022010300006.md): Stringer · corroded · Jan 2, 2022 · N481UA · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO FR56 - FR59 STGR 42L. A3NB-53-4-6179. GENERATED BY V06 61629 AT HAECO LCQ PER NR 9290618 (28618) CUT OUT CORRODED STRINGER SECTION AND REMOVED 1EA SHEAR WEB IAW 53-41-13-300-010, SRM 51-21-11/001, SRM 51-23-11/001 ANDSRM 51-4 A320 SRM 53-41-13-300-01
- [SDR CALA2021122902465](https://openairdocs.org/sdr/CALA2021122902465.md): Stringer · corroded · Dec 28, 2021 · N481UA · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO FR63- FR64 STRGR 41L CORRODED (A3NB-53-4-6179) GENERAT ED BY: V061629 AT HAECO LCQ PER NON ROUTINE 9290619 (28619) BLENDED OUT CORROSION AFT CARGO STGR 412 FR63-FR64 IAW A320 SRM DEPTH GAUGE TLC-2596 DUE 07OCT22. REMOVED AND REPLACED STRG WITH RESTOR
- [SDR CALA2021122702440](https://openairdocs.org/sdr/CALA2021122702440.md): Stringer · corroded · Dec 23, 2021 · N481UA · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO FR 58 - FR 59 STGR 33L CORRODED. TIME OF ADL/REPAIR EMBODIMENT AT 60,000 FC / 120,000 FH WHICHEVE ACCOMPLISHED ON HAECO NR 9290613. R IS ACHIEVED FIRST IAW SRI 53-00-13-205-001 TABLE 004. ALL WORK ACCOMPLISHED STGR SPLICE REPAIR AT FR 58 - FR 59 STGR
- [SDR CALA2021122302436](https://openairdocs.org/sdr/CALA2021122302436.md): Frame · corroded · Dec 23, 2021 · N481UA · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO FR 58 - FR 59 STGR 33L CORRODED. TIME OF ADL/REPAIR EMBODIMENT AT 60,000 FC / 120,000 FH WHICHEVE ACCOMPLISHED ON HAECO NR 9290613. R IS ACHIEVED FIRST IAW SRI 53-00-13-205-001 TABLE 004. ALL WORK ACCOMPLISHED STGR SPLICE REPAIR AT FR 58 - FR 59 STGR
- [SDR CALA2021122302432](https://openairdocs.org/sdr/CALA2021122302432.md): Frame · cracked · Dec 22, 2021 · N481UA · Airbus A300* · Doors
  > R/H AFT EMER EXIT R/H LOAD TRANSMITTING PROFILE (FRAME) CRACKED PER 9290537/28537 GEN BY V077960 SPEC A3NB-52-4-6031 RMVD AND RPLD CRACKED R/H AFT EMERGENCY EXIT R/H LOAD TRANSMITTI NG PROFILE (FRAME)IAW A320 SRM 51-72-11-001 AND 51-42-11-001 BY MECH V061742 I
- [SDR CALA2021122302431](https://openairdocs.org/sdr/CALA2021122302431.md): Frame · cracked · Dec 22, 2021 · N481UA · Airbus A300* · Doors
  > R/H FWD EMER EXIT R/H LOAD TRANSMITTING PROFILE (FRAME) CRACKED SPEC A3NB-52-4-6031 PER 9290538/28538 GEN BY V077960 RMVD AND RPLD CRACKED R/H FWD EMER EXIT R/H LOAD TRANSMITTING PR OFILE (FRAME)IAW A320 SRM 51-72-11-001 51-42-11-001 BY MECH V061 742 INSP BY V
- [SDR CALA2021122302430](https://openairdocs.org/sdr/CALA2021122302430.md): Stringer · corroded · Dec 22, 2021 · N481UA · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO FR58-FR60 STGR 35R CORRODED(A3NB-53-4-6179) GENERATED BY: V061629 AT HAECO LCQ PER NON ROUTINE 9290612 (28612) REMOVED CORRODED SECTION ON STRINGER 35R FROM FR58-FR60. FABRICA MECHANIC V913405 INSPECTED BY V892285 TED NEW STRINGER SECTION AND COUPLIN
- [SDR CALA2019121602216](https://openairdocs.org/sdr/CALA2019121602216.md): Placard · missing · Dec 16, 2019 · N481UA · Airbus A320232 · Placards and Markings
  > YELLOW SYSTEM BRAKE ACCUMULATOR PRESSURE PLACKARD MISSING INSTALLED NEW YELLOW SYSTEM BRAKE ACCUMULATOR PRESSURE PLACARD IAW AMM 11-00-00.
- [SDR CALA2019092301625](https://openairdocs.org/sdr/CALA2019092301625.md): Skin · gouged · Sep 22, 2019 · N481UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE EXT SKIN GOUGES AND DENT AT FR 21 STR 17L 18L PER NR LP 9292413. REPAIRED DAMAGED SKIN AT LT FR21 STR 17, 18L IAW ECRA 5311-02248 NO FURTHER ACTION REQUIRED.
- [SDR CALA2019092301622](https://openairdocs.org/sdr/CALA2019092301622.md): Door · cracked · Sep 20, 2019 · N481UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR LOWER SECTION HAS IMPACT DAMAGE BENDS AND CRACKS PER HANGAR NR 9292419. CUT OUT L1 DOOR LOWER SECTION IMPACT DAMAGE. FAB DOUBLER AND FILLER RELACED DAMAGED PARTS LOCATED, DRILLED AND INSTALLED DOUBLER FILLER AND REPLACED PARTS ALL WRK PERFORMED IAW ECR
- [SDR CALA2019092301619](https://openairdocs.org/sdr/CALA2019092301619.md): Skin · dented · Sep 20, 2019 · N481UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD OF THE F/H LATERAL AVIONICS COMPARTMENT DOOR (13") FUSELAGE SKIN IS CREASED FR11-12 STR 35-36R ON REF 9292408. CUT OUT DAMAGED AREA AND INSTALLED REINFORCING REPAIR DOUBLER AT FR 11-12, STR 35R-36R IAW SRM 53-11-11-300-041. PERFORMED HFEC AT CUTOUT IAW NTM
- [SDR CALA2019092301604](https://openairdocs.org/sdr/CALA2019092301604.md): Cover Plate · dented · Sep 16, 2019 · N481UA · Airbus A320232 · Passenger/Crew Doors
  > L-1 DOOR HAS CREASE @ UPPER DOOR STOP (SUPPORT TASK) PER NR#9292502. REMOVED AND REPLACED UPPER L-1 DOOR COVER PLATE PNL IAW SRM 51-42-11-801 DWG D52110475 SRM 51-44-11-0611 AND SRM 5 1-25-00.
- [SDR CALA2019090901510](https://openairdocs.org/sdr/CALA2019090901510.md): Power Supply · failed · Sep 8, 2019 · N481UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATT 11WL FAILS DATE INSPECTION. EMERGENCY LIGHT EPSU 13WL FAILS OP TEST A3NB-33-3-6016 PER NR 929031. PARTS TRANSACTION INFORMATION PERFORMED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249123 SN OFF 8876 IPC REFERENCE # 3350-01431A POWER SUPP
- [SDR CALA20190821396](https://openairdocs.org/sdr/CALA20190821396.md): Shear Web · cracked · Aug 19, 2019 · N481UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L-2 DOOR FRAME 68 MINUS 8 INCHES AT FLOOR SUPPORT HAS CRACK IN S TRUCTURE. REMOVED CRACKED SHEAR WEB AFT OF FR68 AT FLOOR IAW SRM 51-4 2-11-001 FABRICATED AND INSTALLED NEW SHEAR WEB IAW A320 SRM 51- 42-11-001, 51-44-11-801 AND 51-28-11.
- [SDR CALA2017120404324](https://openairdocs.org/sdr/CALA2017120404324.md): Switch · inoperative · Dec 4, 2017 · N481UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT SWITCH LIGHT ON OVRHD PANEL INOP RELAMPED EMERGENCY EXIT SW OPS CK''ED OK
- [SDR CALA2016031495213](https://openairdocs.org/sdr/CALA2016031495213.md): Connector · loose · Mar 12, 2016 · N481UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHTS OPERATIONAL TEST FAILED. EPSU LT FAILED. FOUND EPSU LT FWD MSG, RESET CONNECTOR ON FWD LT EMER LIGHT POWER SUPPLY & SYS CHECKED GOOD NOW. TESTED OK.
- [SDR CALA2016020395072](https://openairdocs.org/sdr/CALA2016020395072.md): Flap · faulted · Feb 1, 2016 · N481UA · Airbus A320232 · Trailing Edge Flap Control System
  > F CTL FLAP SYS 1 FAULT. CYCLED CB B6 - B7, NO HELP. REPLACED SFCC1 COMPUTER PERM 27-51-34, SYS OPERATIONS OK. POST FLIGHT REPORT, FAULTED SFCC1.
- [SDR CALA2014071191413](https://openairdocs.org/sdr/CALA2014071191413.md): Ils System · faulted · Jul 5, 2014 · N481UA · Airbus A320232 · Localizer/VOR System
  > ILS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ACCOMPLISHED CHRONIC REVIEW. ACCOMPLISHED MT 34-001. OPERATIONS CHECKED GOOD.
- [SDR CALA2014042590898](https://openairdocs.org/sdr/CALA2014042590898.md): Seal · worn · Apr 24, 2014 · N481UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR.005. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED REP
- [SDR CALA2014042590897](https://openairdocs.org/sdr/CALA2014042590897.md): Seal · worn · Apr 24, 2014 · N481UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 ON LOWER SPAR. NR 2 PYLON LOWER SPAR REPAIRED WITH EXTENDED CHAFE PLATE.
- [SDR CALA2014041490818](https://openairdocs.org/sdr/CALA2014041490818.md): Stringer · corroded · Apr 13, 2014 · N481UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION IN AFT PIT BILGE AREA ON LOWER LT SKIN STRINGER 40L BETWEEN FRAME 56 & FRAME 58. CORROSION WAS BEYOND LIMITS IAW SRM 53-41-13 PG 101. INSTALLED STRINGER REPAIR & SPLICE ON STRINGER 41L IAW SRM 53-00-13 PG 211-212 & FIG 201.
- [SDR CALA2014041490817](https://openairdocs.org/sdr/CALA2014041490817.md): Skin · dented · Apr 12, 2014 · N481UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTED AT FRAME 61 & STRINGER 42L - 43L. MEASURED THE DENTED AREA & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-41-11 DIA 103. CUT OUT DENTED AREA & INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-00-11 FIG 209.
- [SDR CALA2014040890780](https://openairdocs.org/sdr/CALA2014040890780.md): Seal · worn · Apr 5, 2014 · N481UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR.005 INCHES. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INST
- [SDR CALA2014040890779](https://openairdocs.org/sdr/CALA2014040890779.md): Stringer · corroded · Apr 5, 2014 · N481UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION IN AFT PIT BILGE AREA ON STRINGER 41L FROM FRAME 63 - 64. REPLACED SECTION OF STRINGER 41L BETWEEN FRAME 62 - 63L TO FRAME 64, NEW SPLICE BETWEEN FRAME 61 - 63 & CLEAT FRAME 63 STRINGER 61 IAW SRM 53-00-13 FIG 201 & SRM 51-42-11 PG 25-27. REPAIR AT
- [SDR CALA2014040890778](https://openairdocs.org/sdr/CALA2014040890778.md): Stringer · corroded · Apr 5, 2014 · N481UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION IN AFT PIT BILGE AREA ON LT SKIN STRINGERS & FASTENERS BETWEEN FRAMES 53 - 55 & STRINGER 41 - 44L. REMOVED FACTORY SPLICE AT FRAME 53. REMOVED STRINGER 41L FROM FRAME 53 TO FRAME 59. INSTALLED NEW STRINGER 41L FROM FRAME 53 TO FRAME 59 & FACTORY S
- [SDR CALA2014040890777](https://openairdocs.org/sdr/CALA2014040890777.md): Stringer · corroded · Apr 5, 2014 · N481UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION IN AFT PIT BILGE AREA ON STRINGER 42R FROM FRAME 63 - 64. REPAIR REQUIRES SRI INSP AT DEFINED INTERVALS. REMOVED SECTION OF STRINGER 42R BETWEEN FRAME 62 - 63. INSTALLED FABRIC REPAIR STRINGER 42 BETWEEN 62 - 64 & INSTALLED FABRICATED SPLICE STRING
- [SDR CALA2014040890776](https://openairdocs.org/sdr/CALA2014040890776.md): Seal · worn · Apr 5, 2014 · N481UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 INCHES ON LOWER SPAR. HFEC OF WORKED AREA IAW NTM 51-10-20 PB6 NO CRACKS FOUND. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED EXTENDE

Next page: https://openairdocs.org/aircraft/N481UA/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 = 'N481UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N481UA/reports

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