# Service difficulty reports: N483UA

A list on [N483UA](https://openairdocs.org/aircraft/N483UA.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 2 · 92 reports

- [SDR CALA2026081718696](https://openairdocs.org/sdr/CALA2026081718696.md): Fuel Cap · missing · Aug 7, 2026 · N483UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING
- [SDR CALA2026043015861](https://openairdocs.org/sdr/CALA2026043015861.md): Rail · broken · Apr 27, 2026 · N483UA · Airbus A320232 · Buffet/Galleys
  > LVL 2 DUE TO HISTORY OF FWD GALLEY COFFEEMAKER (M11) INOP. REF. L/PS 8694821, 8683565, 86548211. ACP TSM 25-35-00-810-802-A AND CORRECT FAULTS. VERIFY CM M11 (7055MM) GRDS 9007VN & 9008VN REF. AWM'S 25-31-01, 25-31-02 ARE GOOD. UPDATE LOG WITH FINDINGS AND ALL
- [SDR CALA2026010612722](https://openairdocs.org/sdr/CALA2026010612722.md): Acm · seized · Jan 4, 2026 · N483UA · Airbus A320232 · Cabin Cooling System
  > SHORT FINAL SMELLED SMOK E. AFTER LANDING ECAMS AIR PACK 1 OVERHEAT AND SMOKE DET FAULT. CREW DEBRIEF AND SMOKE. PER CP SMELL WAS DETECTED IN FLIGHT DECK WHICH THEY TOUGHT WAS SOMETHING BURNING IN AN OVEN. LT PACK SHUT DOWN AND FAULT APPEATED. NO SMELL DETE
- [SDR CALA2025121912251](https://openairdocs.org/sdr/CALA2025121912251.md): A/C Pack · overheated · Dec 17, 2025 · N483UA · Airbus A320232 · Cabin Cooling System
  > NR 1 A/C PACK OVERHEAT WITH A BURNING ODOR OF WOOD OR PAPER, NO SMOKE VISABLE. ODOR DISSIPATED WITH PACKS 1 & 2 OFF. ACFT WAS NOT DEICED PRIOR TO DEPARTURE. PERFORMED IDENTIFICATION OF CABIN ODOR IAW TSM 05-50-00-810-831-A, VERIFIED SOURCE OF ODOR AS NR 1 A
- [SDR CALA2025120911949](https://openairdocs.org/sdr/CALA2025120911949.md): Fuel Cap · missing · Dec 7, 2025 · N483UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. APROX 1.2 LBS. APROX 22 SQ INCH. INSTALLED NEW UNDERWING FUEL CAP ASSY IAW AMM 28-25-41-400-007-A, AND AMM 28-25-41-400-006-A. NEW FUEL CAP ASSY IS FLUSH WITH SKIN AND NO LEAKS NOTED FROM THE COUPLING. PLACARD REMOVED.
- [SDR CALA2025102110358](https://openairdocs.org/sdr/CALA2025102110358.md): Rivet · missing · Oct 19, 2025 · N483UA · Airbus A320232 · Engine Air Intake System
  > MISSING RIVET ON NO2 ENG INLET OUTSIDE 11 OCLOCK POS FACING AFT REQUEST CARRY FOR MISSING FASTNER. ONLY 1 MISSING AT THIS TIME. PER SRM DAMAGE IS ZONE K2 AND MAY BE CARRIED FOR 600FH 750FC OR 100 DAYS.
- [SDR CALA2025080407258](https://openairdocs.org/sdr/CALA2025080407258.md): Warning Message · false activation · Jul 31, 2025 · N483UA · Airbus A320232 · Door Warning System
  > DOOR 2R OPEN ECAM. VERIFIED DOOR 2R CLOSES CORRECTLY, DEFERRED 2R OPEN INDICATION PER MEL 5270AV. REPLACED SENSOR 17WV2. SUGGEST TSM 52-13-00-810-804-A FOR FURTHER ISOLATING THE FAULT. CYCLED R2 DOOR MULTIPLE TIMES AND TEST DOOR INDICATION & WARNING SYSTEM
- [SDR CALA2025041503833](https://openairdocs.org/sdr/CALA2025041503833.md): Door · out of adjust · Apr 11, 2025 · N483UA · Airbus A320232 · Service Doors
  > ECAM DOOR R FWD EMER EXIT. CHECKED AND ADJUST FLAP COVER PER AMM 52-11-00. CHECKED AND ADJUST FLAP COVER PER AMM 52-11-00.
- [SDR CALA2025032403096](https://openairdocs.org/sdr/CALA2025032403096.md): Landing Gear · malfunctioned · Mar 21, 2025 · N483UA · Airbus A320232 · Landing Gear System
  > AVIATAR REPORTING L/G GEAR NOT DOWNLOCKED, L/G DOOR NOT CLOSED ECAM, CFDS MSG STEERING ELECTRO-HYD MODULE (6GC)- VARGAS TOMC FLAGGED SDR SEE LP 4237214
- [SDR CALA2024082702295](https://openairdocs.org/sdr/CALA2024082702295.md): Battery Pack · no test · Aug 27, 2024 · N483UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L FAULT REMOVED AND REPLACED AFT LEFT BATTERY (13WL) PER REF AMM 33-51-38 OPS CHECK GOOD PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024042901259](https://openairdocs.org/sdr/CALA2024042901259.md): Bulb · missing · Apr 28, 2024 · N483UA · Airbus A320232 · Exterior Lighting
  > PDA 2 REF LOG 7799106 - RIGHT RETRACTABLE LANDING LIGHT BULB AND RETAINER MISSING (DEPARTED AIRCRAFT). PARTS MISSING ARE BULB, RETAINER & GASKET. REF. IPC 33-42-11-01A ITEMS 20, 30 & 40. RETERMINATED REF. TO AWM 33-42-00 AND ESPM 20-48-19. INSTALLED NEW LANDIN
- [SDR CALA2024022200502](https://openairdocs.org/sdr/CALA2024022200502.md): Skin · cracked · Feb 15, 2024 · N483UA · Airbus A320232 · Service Doors
  > DENT FOUND ON EXTERNAL SURFACE OF FWD R1 LOWER AFT EDGE AREA. EVALUATION PERFORMED BY LHT EMP 5T1138 & 5P0052 AS RECORDED ON LTPR NR#5001292157-0010. INSIDE AREA AS PER SRM 52-10-00-283-002. DENT/CRACK DIMENSIONS DOUBLER REPAIR ON FWD DOOR R1 LOWER AFT EDGE AR
- [SDR CALA2023082102606](https://openairdocs.org/sdr/CALA2023082102606.md): Landing Light · missing · Aug 19, 2023 · N483UA · Airbus A320232 · Exterior Lighting
  > PDA 2 RH LANDING LIGHT FOUND MISSING ON ARRIVAL FLT 0511-19 IN MSP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V941601 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V941601 MAC RE
- [SDR CALA2022071101708](https://openairdocs.org/sdr/CALA2022071101708.md): Rub Strip · missing · Jul 11, 2022 · N483UA · Airbus A320232 · Engine Exhaust System
  > SMALL PIECE OF ACOUSTIC LINER DELAMINATING INEXHAUST SECTION OF ENG1 FLIGHT DECK LOTO BAG TO KEEP SHIMS WITH AIRCRAFT. PLACING 10 OF 14. REPLACEMENT/REPAIR ON DIP FOR 100 HRS PER ECRA 7811-01400 PAGE FOUND CNA RUB STRIP MISSING PN 740-1027-501 M&E: 18-7811-3-
- [SDR CALA2022071101689](https://openairdocs.org/sdr/CALA2022071101689.md): Controller · warning message · Jul 11, 2022 · N483UA · Airbus A320232 · Cabin Pressure Controller
  > *EMERGENCY* AT FL340 MASTER WARNINGW/ ECAM CABIN PR EXCESS CAB ALT APPEARED FELT CABIN PR CHANGE SEE LOG PAGE 9011036 FOR WORK ACCOMPLISHED. OPS CHECK GOOD PER LP 9011036. RR OUTFLOW VALVE & PRESSURE CONTROLLER 1 REF. AMM.
- [SDR CALA2022050901186](https://openairdocs.org/sdr/CALA2022050901186.md): None · none · May 9, 2022 · N483UA · Airbus A320232 · Hydraulic Quantity Indicator
  > *EMERGENCY*G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD LOCKED FOR FIX UNLOCKING FOR UPDATE ON SDAC''S ITEM LOCKED FOR FERRY.TOMC SMITH REPLACED SDAC1 & SDAC2 PER AMM 31-55-34-400-001-A. PERFORMED GND PERFORMED MAINTENANCE TAXI AND ENGINE RUN AT 75% POWER
- [SDR CALA2022050601162](https://openairdocs.org/sdr/CALA2022050601162.md): Valve · failed · May 6, 2022 · N483UA · Airbus A320232 · Hydraulic Quantity Indicator
  > G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD FAULT-OVER HEAT INDICATION EXTINGUISHED AFTER 6 MIN WITH SYSTEM SECURED. ACP TEM 29-11-00-810-802A UP TO UP THROUGH ITEM 3. COULD NOT DUPICATE OVERHEAT. NEED TO ACP ITEM 4D. R/R ENGINE PUMP FIRE -VALVE IAW AMM
- [SDR CALA2022050401132](https://openairdocs.org/sdr/CALA2022050401132.md): Ptu · failed · May 4, 2022 · N483UA · Airbus A320232 · Hydraulic Quantity Indicator
  > G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD SEE PREVIOUS HISTORY CASE DRAIN FILTER (1084GM). UNLOCKED FOR UPDATE T/S REF TSM 29-11-00-810-802-A. AFTER RUNNING GREEN HYD SYSTEM, FOUND THE PTU EXTREMELY HOT. 40GA, 41GA AND 49GA WERE COOL TO THE TOUCH. SUSP
- [SDR CALA2022010300011](https://openairdocs.org/sdr/CALA2022010300011.md): Lens · missing · Jan 3, 2022 · N483UA · Airbus A300* · Exterior Lighting
  > PDA 2 UPON MX WALK-AROUND, FOUND RT RETRACTABLE LANDING LIGHT LENS/LAMP MISSING. REF LOG PAGE #7727304. GMM 02-30-95 REQUEST MEL 3340BB FOR RIGHT RETRACTABLE LANDING LIGHT INOP, REF PLACED ON MEL 3340BB PER TOMC. DDP COMPLIED WITH. L/P 7727304. DDP COMPLIED W
- [SDR CALA2021060700803](https://openairdocs.org/sdr/CALA2021060700803.md): Outflow Valve · damaged · Jun 7, 2021 · N483UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > SKIN VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. - V ENT REMOVED AND REPLACED SKIN AIR OUTFLOW VALVE OPS CHECKS GOOD REF AMM 21-26-53-400-001-A ROTABLE PARTS CHANGE WAS INDICATED - TT # 1939473 SN OFF 3533 VALVE, SKIN AIR OFF 31-2125-9-0001 3533 ON 31-2125-9
- [SDR CALA2021041400448](https://openairdocs.org/sdr/CALA2021041400448.md): Frame · cracked · Apr 12, 2021 · N483UA · Airbus A320232 · Fuselage Main, Frame
  > FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HAS CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER LCQ 9298605/24605. REPAIRED FLT DECK RH FR4 UPPER ATT
- [SDR CALA2021041400447](https://openairdocs.org/sdr/CALA2021041400447.md): Fitting · cracked · Apr 12, 2021 · N483UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HA S CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER HAECO LCQ 9298605/24605 GENERATED BY V892422 REPAIRED
- [SDR CALA2021041400446](https://openairdocs.org/sdr/CALA2021041400446.md): Fitting · cracked · Apr 12, 2021 · N483UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HA S CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER HAECO LCQ 9298605/24605 GENERATED BY V892422 REPAIRED
- [SDR CALA2021032200361](https://openairdocs.org/sdr/CALA2021032200361.md): Stringer · corroded · Mar 21, 2021 · N483UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT INTERNAL FUSELAGE STR31R HAS CORROSION AT FR65, JUST BELOW O UTFLOW VALVE. PER HAECO NR 9298127/24127. REMOVED AND REPLACED STINGER 3/R AT FR64-FR67 IAW A320 SRM 51-72 -11-911-001.
- [SDR CALA2021032200360](https://openairdocs.org/sdr/CALA2021032200360.md): Door Sill · corroded · Mar 21, 2021 · N483UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOORSILL CORRODED UNDER GIRT BAR PLATES AT FR66 AND FR68. PER HAECO NR 9298466/24466. GENERATED BY V079529 REMOVED AND REPLACED L2 DOOR SILL AT FR66-FR68 IAW UAL A320 SRM 51-72-11-911-001 BY MECH V914232
- [SDR CALA2021031900331](https://openairdocs.org/sdr/CALA2021031900331.md): Stringer · damaged · Mar 17, 2021 · N483UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT BILGE AREA BETWEEN FR63 AND FR64 STGR42L HAS CORROSION ON ST RG PER HAECO LCQ NON-ROUTINE 24719/9298719 PER MECH V061640 REMOVED AND REPLACED STR42L FR 60-64 IAW A320 SRM 51-42-11 PARA 2E&F & SRM 51-72-11 CAT A REPAIR PER MECH V061640
- [SDR CALA2021031900330](https://openairdocs.org/sdr/CALA2021031900330.md): Stringer · damaged · Mar 17, 2021 · N483UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE AREA BETWEEN FR C63 AND C64 STR 41L REMOVED DOT HN-24. PER MECH V061640 REMOVED AND REPLACED STRINGER 41L FR60-694 IAW A320 SRM 51-42-11 PARA LE&F AND SRM 51-72-11 CAT A REPAIR REMOVED DOT HN-29
- [SDR CALA2021031900329](https://openairdocs.org/sdr/CALA2021031900329.md): Frame · corroded · Mar 17, 2021 · N483UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO BILGE AREA FR C63 STR 41R TO STR 42R HAS CORROSION AND BARE METAL DOT HN-23 PE HAECO NON ROUTINE 24672/9298672 REMOVED AND REPLACED STR 42R IAW A320 SRM 51-42-11 PARA 2E & F, STRINGER 41R WAS REPLACED ON N/R 24667 FR60-64 & SRM 51-72-11. C AT A REPAI
- [SDR CALA2021031900328](https://openairdocs.org/sdr/CALA2021031900328.md): Stringer · corroded · Mar 17, 2021 · N483UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STR41R WITH FR59 HAS CORROSION. PER HAECO NON-ROUTINE 24667/9298667 BY MECH V061640 REMOVED AND REPLACED STR 41R FR 58-64 IAW A320 SRM 51-42-11 PARA 2E&F. CAT A REPAIR REMOVED DOT E555
- [SDR CALA2021031000279](https://openairdocs.org/sdr/CALA2021031000279.md): Door Sill · corroded · Mar 8, 2021 · N483UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN AT FR68 DOOR SILL IS CORRODED AT SEVERAL AREAS AND HAS ENLARGED FASTENER HOLE PER HAECO LCQ NON ROUTINE. REMOVED & REPLACED R2 DOOR SILL (FR66-FR68) IAW A320 SRM 51-72-1 1-911-001.
- [SDR CALA2021011100037](https://openairdocs.org/sdr/CALA2021011100037.md): Engine · stalled · Jan 11, 2021 · N483UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. ENGINE 2 APPROXIMATELY 3000 FT ON DEPT FELT MINOR THRUST REDUCTION FOLLOWED BY ENG 2 STALL ECAM, ECAM CLEARED AND TH REF TO TSM TASK:71-00-00-810-809-A SURGE OR ST
- [SDR CALA2020020870328](https://openairdocs.org/sdr/CALA2020020870328.md): Skin · dented · Feb 2, 2020 · N483UA · Airbus A320232 · Wing, Plate/Skin
  > DURING SERVICE CHECK WALK AROUND FOUND DENT ON RIGHT WING INBOARD FLAP 8 INCH FROM WING ROOT. DENT MESURE L= 7 INCH W= 1.25 D= 0.113 PLACING DAMAGE ON A DIP IN REF TO SRM 57-52-00-283-027 FIGURE 1 COLUMN 3. APPLIED HIGH SPEED TAPE TO THE DAMAGED AREA TO BE RE
- [SDR CALA2019080401300](https://openairdocs.org/sdr/CALA2019080401300.md): Outflow Valve · malfunctioned · Aug 2, 2019 · N483UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > VENT SKIN VALVE FAULT RESET CBS CFDS TEST PASSED OPS CK MM 21-26-00-710-001 A
- [SDR CALA2018022000714](https://openairdocs.org/sdr/CALA2018022000714.md): Battery · faulted · Feb 20, 2018 · N483UA · Airbus A320232 · Emergency Lighting
  > EEL FWD LEFT BATTERY FAULT. REPLACED FWD LEFT EEL BATTERY IAW AMM 33-51-38.
- [SDR CALA2017122004547](https://openairdocs.org/sdr/CALA2017122004547.md): Generator · odor · Dec 20, 2017 · N483UA · Airbus A320232 · Waste Disposal System
  > FLIGHT ATTENDANTS REPORT SCORCHED PLASTIC SMELL COMING FROM AFT GALLEY OR LAVS. REPLACED WASTE VACUUM GENERATOR PER AMM 38-31-64. OPS CHECKS GOOD, NO BURNING SMELL NOTED.
- [SDR CALA2017112004168](https://openairdocs.org/sdr/CALA2017112004168.md): Battery Pack · no test · Nov 20, 2017 · N483UA · Airbus A320232 · Emergency Lighting
  > OPS CHECK OF THE CABIN EMERGENCY LIGHT BATTERY CAPACITY FAILED. REPLACED THE BATTERY PACK, AND TESTED OK.
- [SDR CALA2017110603963](https://openairdocs.org/sdr/CALA2017110603963.md): Cids · malfunctioned · Nov 6, 2017 · N483UA · Airbus A320232 · Emergency Lighting
  > EXIT SIGN REMAINS ILLUMINATED FOR ENTIRE TIME IN EXIT ROW RESET CIDS. PERFORMED CIDS SYSTEM TEST. NO FAULTS. NO PREVIOUS L EG FAULTS. ACCOMPLISHED OPERATIONAL TEST OF THE EMERGENCY LIGHTS. PER AMM 33-51-00-710-001-A. SYSTEM CHECK NORMAL. OPERATED EMERGENCY LI
- [SDR CALA2016110295885](https://openairdocs.org/sdr/CALA2016110295885.md): Actuator · leaking · Oct 29, 2016 · N483UA · Airbus A320232 · Drag Control Actuator
  > LOW SPEED ABORTED TAKEOFF (70KTS) DUE TO B HYD SYS LOW QTY ECAM. FOUND NR 3 SPOILER ACT LEAKING. R&R AND TESTED PER AMM.
- [SDR CALA2016082395673](https://openairdocs.org/sdr/CALA2016082395673.md): Power Supply · failed · Aug 18, 2016 · N483UA · Airbus A320232 · Emergency Lighting
  > ON FWD FAP HAD MESSAGE FOR EPSU FAIL FWD. ON BATTERY POWER SUPPLY HAD MESSAGE UNIT FAILED. REMOVED AND REPLACED FWD L1 DOOR EMERGENCY LIGHT POWER SUPPLY.
- [SDR CALA2015091094285](https://openairdocs.org/sdr/CALA2015091094285.md): Regulator Valve · faulty · Sep 8, 2015 · N483UA · Airbus A320232 · Pneumatic Distribution System
  > AFTER TAKEOFF CREW LOST BOTH ENG BLEEDS & CROSS BLEED VLV, STARTED APU FOR BLEED, DIVERTED. ACCOMPLISHED BMC BITE CHECKS OK. ACCOMPLISH FAULT CHECK OF CROSS BLEED VLV POSITION CONTROL OK. REPLACED PRESS REGULATOR VLV. OPERATIONS CHECKED GOOD.
- [SDR CALA2015010692901](https://openairdocs.org/sdr/CALA2015010692901.md): Unknown · odor · Jan 3, 2015 · N483UA · Airbus A320232 · Air Distribution System
  > RAMP REPORTS BURNING WIRING SMELL IN FWD CARGO BIN. PERFORMED GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT. OPERATED NESTING SYS FULL TRAVEL NO DEFECTS NOTED. NO BURNING SMELL DETECTED.
- [SDR CALA2014102792612](https://openairdocs.org/sdr/CALA2014102792612.md): Epsu · inoperative · Oct 25, 2014 · N483UA · Airbus A320232 · Emergency Lighting
  > RIGHT EMER LIGHTS TEST FAIL WITH MSG EPSU EMER RT. REPLACED EPSU & BATTERY AT RT OVERWING DOOR IAW AMM 33-51-38. OPERATIONS CHECKED OK.
- [SDR CALA2014062791344](https://openairdocs.org/sdr/CALA2014062791344.md): Door Seal · dirty · Jun 26, 2014 · N483UA · Airbus A320232 · Emergency Exits
  > HISSING NOISE AT EMER EXIT PLUG DOOR AT 20A. INSPECTED & CLEANED FWD LT HATCH SEAL & SEAL MATING SURFACE & OUTSIDE HANDLE GASKET IAW MT 53-004 & MM 52-21-11-000-001-A. NO SEAL OR GASKET DAMAGE NOTED.
- [SDR CALA2014061391257](https://openairdocs.org/sdr/CALA2014061391257.md): Slide · deployed · Jun 10, 2014 · N483UA · Airbus A320232 · Escape Slide
  > RIGHT OVERWING SLIDE DEPLOYED. REPLACED RT OVERWING SLIDE IAW AMM 25-62-42-400-001-A. REPLACED RT OVERWING INFLATION RESERVOIR IAW AMM 25-62-46-400-001-A. INSTALLED EMER EXIT HATCH IAW AMM 52-21-11-400-001-A.
- [SDR CALA2014060591216](https://openairdocs.org/sdr/CALA2014060591216.md): Skin · damaged · Jun 2, 2014 · N483UA · Airbus A320232 · Rudder, Plate/Skin
  > RUDDER PN 5547100001400 SN TS-1274 WAS FOUND TO HAVE WATER INGRESS & DISBOND DAMAGE. ACCOMPLISHED ALL REPAIRS IAW ECRA 5541-01046 REV A. WORK ACCOMPLISHED ON WU'S 49575, 49576, 49577, 49578, 49579 & 49580. CURRENT PTT 41377 PTC 17871. REPAIR TO RUDDER SID
- [SDR CALA2014051991061](https://openairdocs.org/sdr/CALA2014051991061.md): Support · corroded · May 19, 2014 · N483UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FRAME 60 - FRAME 70 CIRCUMFERENTIAL SUPPORT FOUND CORRODED. R & R SUPPORT FRAME D5347112320200 IAW A320 51-72-11.
- [SDR CALA2014051991060](https://openairdocs.org/sdr/CALA2014051991060.md): Door Sill · corroded · May 16, 2014 · N483UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN CABIN R2 LOWER SILL HAS CORROSION ON FRAME 68. CORROSION FOUND BEYOND OEM LIMITS. FABRICATED & INSTALLED REPAIR PLATE IAW SRM53-41-14 FIG 101 & 201. THIS REPAIR WAS CIR'D & ACCEPTED.
- [SDR CALA2014051391013](https://openairdocs.org/sdr/CALA2014051391013.md): Attach Fitting · chafed · May 11, 2014 · N483UA · Airbus A320232 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT ACTUATOR ATTACH FITTING IS CHAFED. BLENDED CHAFED AREA. ORIGINAL THICKNESS WAS 0.200 & REMAINING THICKNESS IS 0.198. MATERIAL LOSS IS 0.002. THIS REPAIR REQUIRES SRI INSP IAW SRI 52-30-00-1-005-00 TABLE 105. FIRST INSPECTION IS DUE AT 6
- [SDR CALA2014021090340](https://openairdocs.org/sdr/CALA2014021090340.md): Fairing · unsecure · Feb 7, 2014 · N483UA · Airbus A320232 · Aerodynamic Fairings
  > LOUD HUMMING SOUND AROUND ROW 22. INSPECTED SEALS ON BOTH LT & RT SIDE, NO DEFECTS FOUND. TAPED FAIRINGS 191DT & 192DT. CREW ON FLIGHT 330 7 REPORTED NO HUMMING.
- [SDR CALA2013121393676](https://openairdocs.org/sdr/CALA2013121393676.md): Cone · cracked · Dec 12, 2013 · N483UA · Airbus A320232 · Engine Collector/Tailpipe/Nozzle
  > 8 INCH CRACK IN NR 2 ENG EXHAUST CONE ALONG A PREVIOUS WELD. REPLACED EXHAUST CONE.

Next page: https://openairdocs.org/aircraft/N483UA/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 = 'N483UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N483UA/reports

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