# Service difficulty reports: N480UA

A list on [N480UA](https://openairdocs.org/aircraft/N480UA.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 · 116 reports

- [SDR CALA2026100920256](https://openairdocs.org/sdr/CALA2026100920256.md): Battery Pack · no test · Oct 7, 2026 · N480UA · Airbus A320232 · Emergency Lighting
  > RAN EMERGENCY LIGHT BATTERY TEST. EPSU LOCATED IN FWD LT. REPLACED EPSU BATTERY IAW AMM 33-51-38-400-002-A.
- [SDR CALA2026041315321](https://openairdocs.org/sdr/CALA2026041315321.md): Fuel Cap · missing · Apr 13, 2026 · N480UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING, PDA 2 REQUIRED IAW GMM 02-30-95
- [SDR CALA2026030214209](https://openairdocs.org/sdr/CALA2026030214209.md): Light · detached · Feb 26, 2026 · N480UA · Airbus A320232 · Exterior Lighting
  > RIGHT RETRACTABLE LANDING, LIGHT HANGING OUT OF RETAINER. LANDING LIGHT RETAINER MISSING. LANDING LIGHT ASSEMBLY ORDERED TO USE THE RETAINER THAT WAS MISSING. 31-3341-9-9001,
- [SDR CALA2025111711281](https://openairdocs.org/sdr/CALA2025111711281.md): Frame · cracked · Oct 27, 2025 · N480UA · Airbus A320232 · Fuselage Main, Frame
  > RIGHT FRM 16 DOUBLE JOGGLE HOLE 6 HAS A CRACK INDICATION IN FRAME LAYER, 2 OCLOCK POSITION VIEWED FROM OUTSIDE, 100% SH. ACCOMPLISHED IMPROVED INTERIM REPAIR AT FR16 DBL JOGGLE HOLE 6 IAW ECRA 5311-02923 REV A PART 1.A.1.
- [SDR CALA2025102310433](https://openairdocs.org/sdr/CALA2025102310433.md): Doubler · cracked · Oct 20, 2025 · N480UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON UPPER FWD SPAR DOUBLER CRACKED AT LT SKIN. REPAIRED THE NR 1 PYLON UPPER FWD SPAR DOUBLER LT SKIN IAW SRM 54 -52-12-300-024.
- [SDR CALA2025101410075](https://openairdocs.org/sdr/CALA2025101410075.md): Spar · cracked · Oct 13, 2025 · N480UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NO.2 PYLON UPPER FWD SPAR DOUBLER HAS CRACKED AT R/H SKIN. GENER ATED BY V919150 ON HAECO LCQ NR 9298226/40226. ESFR INFORMATION UPDATE REPAIR AREA ON #2 PYLON UPPER FWD SPAR DOUBLER AT RT SKIN IAW A3 20 SRM 54-52-12-300-036. ACMP BY V901914
- [SDR CALA2025081107537](https://openairdocs.org/sdr/CALA2025081107537.md): Light · no test · Aug 9, 2025 · N480UA · Airbus A320232 · Emergency Lighting
  > DURING FUNCTION TEST, RECEIVED ERROR MSG "EPSU INT LOAD EMER L" ATA 33-51-38 C/W TEST OF THE EMERGENCY LIGHTS REF AMM: 33-51-00-710-096-A. TEST OK AND NO OTHER FAULTS NOTED AT THIS TIME.
- [SDR CALA2025080707407](https://openairdocs.org/sdr/CALA2025080707407.md): Slide · not reported · Aug 4, 2025 · N480UA · Airbus A320232 · Escape Slide
  > R1 ESCAPE SLIDE ASSEMBLY REPLACED REF AMM 25-62-44. REPLACED R1 ESCAPE SLIDE ASSEMBLY REF AMM 25-62-44. ACP RII INSP REF GMM 09-25-05.
- [SDR CALA2025072406883](https://openairdocs.org/sdr/CALA2025072406883.md): Engine · malfunctioned · Jul 21, 2025 · N480UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > AT TO POWER SET ENG 1 DO UNT ONLY WENT TO 1.2EPR PULLED LEFT. ENG2 EPR NORM AT 1.46. PREFORMED FAULT ISOLATION REF FIM TASK 75-24-00-810-802B TO STEP 3.B.1 AND FOUND FAULT CODE HCCWAF. ACCOMPLISHED TEST NR 11: HIGH POWER ASSURANCE TEST REF AMM TASK 71-00-00
- [SDR CALA2025072206843](https://openairdocs.org/sdr/CALA2025072206843.md): Actuator · faulted · Jul 19, 2025 · N480UA · Airbus A320232 · Compressor Bleed Valve
  > AT 60 KTS ENG 2 COMP VANE ECAM ON TO PULLED PFR. SEE PHOTO. INSTALLED RIG PIN INTO FRONT OF BEARING HOUSING CRANK UP TO SUB TASK D (3). WORK ACCOMPLISHED ON LOG 5549419, REMOVED ACC ACTUATOR REF MM 75-24-52-000-010-A PARTS USED: 00-0594-3-2278,QTY:1 31-7520-9
- [SDR CALA2025060305227](https://openairdocs.org/sdr/CALA2025060305227.md): Pump · unsecure · Jun 1, 2025 · N480UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > HYD B SYS LO PR IN FLIGH T TURNED BLUE PUMP OFF FOUND EVIDENCE OF HYD LEAK IN LEFT WHEEL WELL AREA AND AFT BELLY - FOUND BLUE PUMP 2074GJ PRESSURE SWITCH EXTREMLY LOOSE AND NOT SAFETY WIRED. SECURED SWITCH REF AMM 29-12-17/401. NO LEAKS NOTED
- [SDR CALA2025041603902](https://openairdocs.org/sdr/CALA2025041603902.md): Life Vest · unsecure · Apr 15, 2025 · N480UA · Airbus A320232 · Life Jacket
  > 1L JUMPSEAT LIFEVEST INBRD AND OUTBRD NEED SECURING RE-SECURED 1L JUMPSEAT I/B & O/B LIFEVESTS AS REQUIRED REF. AMM 25-66-00.
- [SDR CALA2025040403544](https://openairdocs.org/sdr/CALA2025040403544.md): Warning Message · false activation · Apr 2, 2025 · N480UA · Airbus A320232 · Central Warning
  > HYD Y ENG 2 PUMP LO PR ECAM. SERVICED YELLOW HYDRAULIC SYSTEM. RAN YELLOW AND BLUE AND GREEN SYSTEMS WITH APU BOOSTED. CHECKED FOR LEAKS NO LEAK FOUND. RAN THE ENGINE, OPERATED FLIGHT CONTROLS PUSHED BRAKES PADDLES, RECHECKED FOR LEAKS, NO LEAK FOUND AS PER T
- [SDR CALA2025021302312](https://openairdocs.org/sdr/CALA2025021302312.md): Fan · failed · Feb 11, 2025 · N480UA · Airbus A320232 · Air Distribution Fan
  > BLOWER FAULT WITH POPPED BLOWER CB. FOUND AVIOUCS VENT BLOWER CB AD10 POPPED AND WOULD NOT RESET. POST FLIGHT REPORT SHOWED BLOWER FAN 20 HQ FAULT. FAN HAD BURNT ELECTRONICS SMELL.REPLACED BLOWER FAN 20HQ. OPS AND LEAK CHECK GOOD. PARTS USED: 31-2126-9-90
- [SDR CALA2025012201970](https://openairdocs.org/sdr/CALA2025012201970.md): Battery · no test · Jan 21, 2025 · N480UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK - EPSU BAT CAP AFT L FAILED TEST. NEED BATTERY REPLACEMENT. REMOVED AND REPLACED AFT EPSU BATTERY, BITE CHECK PASSED. REF AMM 33-51-38-400-002-A PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024121601522](https://openairdocs.org/sdr/CALA2024121601522.md): Light · malfunctioned · Dec 12, 2024 · N480UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY CABIN LIGHTS AND EMERGENCY EXIT LIGHTS ARE COMING ON A ND OFF INTERMITTENTLY PERFORMED TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001-A. NO FAULTS FOUND LIGHTS FUNCTION NORMAL.
- [SDR CALA2024110502799](https://openairdocs.org/sdr/CALA2024110502799.md): Skin · damaged · Nov 4, 2024 · N480UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS DAMAGE 105 INCHES FROM I/B EDGE 5 1/2 INCHES FROM TRAILING EDGE 5 INCHES IN DIAMETER PER HAECO LCQ N/R 9298194/22194 GEN BY V061632 REPAIRED L/H ELEVATOR 105 IN FROM I/B 5.5 IN FROM T/E 5 IN DIA ZONE C IAW A320 SRM 55-21-11-300-
- [SDR CALA2024110502796](https://openairdocs.org/sdr/CALA2024110502796.md): Skin · contaminated · Nov 4, 2024 · N480UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS 176IN FROM INBOARD EDGE 5IN FROM TRAILING EDGE 4IN IN DIAMETER PER HAECO LCQ N/R 9298195/22195 GEN BY V061632 DRILLED WITNESS ON L/H ELEVATOR 176 IN FROM I/B 5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006-A01 PARA
- [SDR CALA2023061401859](https://openairdocs.org/sdr/CALA2023061401859.md): Unknown · unknown · Jun 12, 2023 · N480UA · Airbus A320232 · Landing Gear System
  > WHEEL N/W STRG FAULT APPEARED AFTER EXTENDINGGEAR. LOCKED BY TOMC, MUST HAVE POSITIVE FIX PER TOMC SR MGR DUE CREW DECLARING EMERGENCY CREW REPORTED STEERING AVAILABLE UPON LANDING,RESET NOSE WHEEL STEERING/ANTI SKID SWITCH. PERFORMED GROUND TEST ON BSCU 1&2,
- [SDR CALA2022120703315](https://openairdocs.org/sdr/CALA2022120703315.md): None · none · Dec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/Structures
  > PLANNING TO CONTACT ENGINEEERING AFTER 02APR23, BUT BEFORE 02MAY23 FOR EC/RA 5341-01359 PART 2 STEP 2 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVAL FROM SC1ELBYC COMMENT AFTER 02-APRI
- [SDR CALA2022120703314](https://openairdocs.org/sdr/CALA2022120703314.md): None · none · Dec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/Structures
  > FR66 AND FR68 DOOR STOPS RH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE THE REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 1 AIRCRAFT REACH
- [SDR CALA2022120703313](https://openairdocs.org/sdr/CALA2022120703313.md): None · none · Dec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/Structures
  > PLANNING TO CONTACT ENGINEEERING AFTER 25635 TOTAL FLIGHT CYCLES, BUT BEFORE 25685 TOTAL FLIGHT CYCLES FOR EC/RA 5341-01359 PART 2 STEP 1 INSPECTION REQUIREMENTS. ITEM PLACED ON DIP OK TO CARRY PER ECRA 5341-01359, PLANNING TO CONTACT ENGINEERING TOMC-APPROVAL
- [SDR CALA2022120703312](https://openairdocs.org/sdr/CALA2022120703312.md): None · none · Dec 6, 2022 · N480UA · Airbus A320232 · Standard Practices/Structures
  > FR66 AND FR68 DOOR STOPS LH EXISTING UNDOCUMENTED REPAIRS. REPAIR IS EXPECTED TO BE A PERMANENT SOLUTION WITH INSPECTION OF THE LATEST REVISION OF EC/RA 5341-01359 ON OR BEFORE 02JUN23. REQUIRED. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2, STEP 2 LH FR66 &
- [SDR CALA2022120203262](https://openairdocs.org/sdr/CALA2022120203262.md): Door Frame · damaged · Nov 30, 2022 · N480UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO PROBE INSPECTION OF RHS FR16 #7 DOOR STOP, HOLE#1 AND #3 FOUND WITH REJECTABLE INDICATIONS FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT. AND #3 AND ASSOCIATED HOLES #2 AND #4 AT FR16 RHS DOOR STOP 5311-02919. THERE AFTER REPEAT INSPECTIO
- [SDR CALA2022113003244](https://openairdocs.org/sdr/CALA2022113003244.md): Stop Fitting · cracked · Nov 28, 2022 · N480UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO INSP PF LH FR16 DOOR STOP #7 CRACK INDICATIONS WERE NOTED ON I/B UPPER AND LOWER HOLES, FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT.
- [SDR CALA2022112503218](https://openairdocs.org/sdr/CALA2022112503218.md): Stringer · corroded · Nov 23, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6179 BULK CARGO BET FR63-64 STRINGER 42L IS CORRODED
- [SDR CALA2022111103106](https://openairdocs.org/sdr/CALA2022111103106.md): Doubler · corroded · Nov 9, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > BULK CARGO BETWEEN FRS 63-64, STRG 40L-43L EXISTING DOUBLER HAS CORROSION OR RE-INSPECTION PER SRI. SRI REQUIREMENTS AS FOLLOWS: FIRST INS ER OCCURS 1ST, SUBSEQUENT INSPECTIONS AT INTERVALS OF 2,000FC/4, OR CONCERNING NTM CHAPTERS IAW SRI 53-00-11-205-017, REF
- [SDR CALA2022111103109](https://openairdocs.org/sdr/CALA2022111103109.md): Floor Support · corroded · Nov 9, 2022 · N480UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT FR16 BETWEEN Y254 AND Y765 CORRODED. REMOVED CORROSION IAW SRM 51-42-11 AND FOUND WITHIN ALLOWA BLE LIMITS A-320 SRM 53-11-14-283-007.
- [SDR CALA2022110403034](https://openairdocs.org/sdr/CALA2022110403034.md): Floorbeam · corroded · Nov 4, 2022 · N480UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT FR16 BETWEEN Y254 AND Y765 CORRODED. REMOVED CORROSION IAW A-320 SRM 51-42-11 AND FOUND WITHIN ALLOWA BLE LIMITS UAW A-320 SRM 53-11-14-283-007 L=1.900" W=1.350" D=.0 40" T93987,T93998 EMP#: V936039 WORK ACCOMPLISHED AT ST ENGINEER ING OF M
- [SDR CALA2022102402915](https://openairdocs.org/sdr/CALA2022102402915.md): None · cracked · Oct 22, 2022 · N480UA · Airbus A300* · Fuselage Main, Plate/Skin
  > DURING ROTO INSP OF LH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED ON FASTER HOLE. REAPIR BEFORE NEXT FLIGHT
- [SDR CALA2022102402913](https://openairdocs.org/sdr/CALA2022102402913.md): None · corroded · Oct 22, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > BULK CARGO BET FR57 -5 STRINGER 37R IS CORRODED
- [SDR CALA2022102402914](https://openairdocs.org/sdr/CALA2022102402914.md): None · cracked · Oct 22, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING ROTO INSP OF RH FRAME FOOT AT FR43 CRACK INDICATION WAS NOTED OF FASTENER HOLE. REPAIR BEFORE NEXT FLIGHT
- [SDR CALA2022101802826](https://openairdocs.org/sdr/CALA2022101802826.md): Stringer · corroded · Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > BULK CARGO STRINGER 41L BET FR63-64 IS CORRODED. REMOVED AND REPLACED STRG 41L IAW A320 SRM 51-42-11/001, RECEIVE D NEW STRG 41L P/N=D5347041821600 B/N:0003899727. EMP# V936039 W ORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 38657.
- [SDR CALA2022101802825](https://openairdocs.org/sdr/CALA2022101802825.md): Stringer · corroded · Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > BULK CARGO BET FR63-64 STRINGER 43L IS CORRODED REMOVED AND REPLACED STRG 43L IAW A320 SRM 51-42-11/001, RECEIVE D NEW STRG 43L P/N:D5347041822000, B/N=0003900958. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM O N NR# 38665.
- [SDR CALA2022101802822](https://openairdocs.org/sdr/CALA2022101802822.md): Seat Track · corroded · Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6038) CABIN SEAT TRACK -Y1292 FR20 CORRODED. DOT NO.1 7-23() SEAT TRACK -Y1292 BETWEEN FR1224 REPLACED IAW A320 SRM 51-42-11. EMP# V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF M OBILE AT BFM ON NR# 38978.
- [SDR CALA2022101802821](https://openairdocs.org/sdr/CALA2022101802821.md): Floor Support · corroded · Oct 14, 2022 · N480UA · Airbus A320232 · Fuselage Main, Structure
  > (A3NB-53-3-6038) CABIN FLOOR SUPPORT FR21 Y254 TOP SURFACE CORRO DED. DOT NO.17-19() REMOVED AND REPLACED FLOOR SUPPORT Y254 IAW A320 SRM 51-42-11/00 1. RECEIVED NEW FLOOR SUPPORT P/N=D5311281820401 B/N=0003925620 EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERI
- [SDR CALA2022101202771](https://openairdocs.org/sdr/CALA2022101202771.md): Seat Track · corroded · Oct 12, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6038) CABIN SEAT TRACK -Y1292 FR20 CORRODED. DOT NO.1 7-23() SEAT TRACK -Y1292 BETWEEN FR1224 REPLACED IAW A320 SRM 51-42-11. EMP# V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF M OBILE AT BFM ON NR# 38978.
- [SDR CALA2022101202770](https://openairdocs.org/sdr/CALA2022101202770.md): Floor Support · corroded · Oct 12, 2022 · N480UA · Airbus A320232 · Fuselage Main, Structure
  > (A3NB-53-3-6038) CABIN FLOOR SUPPORT FR21 Y254 TOP SURFACE CORRO DED. DOT NO.17-19() REMOVED AND REPLACED FLOOR SUPPORT Y254 IAW A320 SRM 51-42-11/00 1. RECEIVED NEW FLOOR SUPPORT P/N=D5311281820401 B/N=0003925620 EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERI
- [SDR CALA2022101002753](https://openairdocs.org/sdr/CALA2022101002753.md): Seat Track · corroded · Oct 8, 2022 · N480UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK -Y765 FR20 CORRODED.
- [SDR CALA2022100702733](https://openairdocs.org/sdr/CALA2022100702733.md): Stringer · corroded · Oct 6, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.
- [SDR CALA2022100602723](https://openairdocs.org/sdr/CALA2022100602723.md): Stringer · corroded · Oct 5, 2022 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.
- [SDR CALA2019080501313](https://openairdocs.org/sdr/CALA2019080501313.md): Stringer · corroded · Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER 43 LEFT BETWEEN FRAME 56-58 HAS CORROSION. FOUND STRINGER OUT OF LIMITS PER SRM 53-00-13-300-002. PERFORMED STRINGER REPAIR IAW SRM 53-00-13-300-001, SHT. 02, COUPLING TYP E 1.
- [SDR CALA2019080501312](https://openairdocs.org/sdr/CALA2019080501312.md): Stringer · corroded · Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT FR 31-33 STRINGER 43R HAS CORROSION. FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-21-13-283-001. PER FORMED STRINGER REPAIR IAW SRM 53-00-13-300-001 SHEET 01, COUPLI NG TYPE 1.
- [SDR CALA2019080501311](https://openairdocs.org/sdr/CALA2019080501311.md): Stringer · corroded · Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STR 42RT BETWEEN FR62-64 HAS CORROSION. FOUND STRINGER TO BE OUT OF LIMITS PER SRM 53-00-13-300-002. PER FORMED STRINGER REPAIR PER SRM 53-00-13-300-001 SHEET 02, COUPLI NG TYPE 1.
- [SDR CALA2019080501310](https://openairdocs.org/sdr/CALA2019080501310.md): Stringer · corroded · Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER 42 LEFT BETWEEN FRAMES 54-56 HAS CORROSIO N PER HAECO LCQ NR LP 9294479 GENERATED BY V052030 UPON FURTHER EVAL STRG 42L BETWEEN FR 54-56 FOUND TO BE OUT OF L IMTS WITH ESS THAN.031IN REMAINING MATERIAL REMOVED AND REPALCE D STR 42L FR 5
- [SDR CALA2019080501309](https://openairdocs.org/sdr/CALA2019080501309.md): Threshold · corroded · Aug 4, 2019 · N480UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO THRESHOLD SPLICE PLATE HAS CORROSION. REMOVED AND REPLACED DISCREPANT FWD CARGO THRESHOLD PLATE IAW SRM 51-42-11-001 AND 51-72-11.
- [SDR CALA2019080101285](https://openairdocs.org/sdr/CALA2019080101285.md): Cleat · corroded · Aug 1, 2019 · N480UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FWD CARGO FR 31-32 STGR 40R-41R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT FR 31-32 STR 40R-41R IAW SRM 51- 72-11.
- [SDR CALA2019072901266](https://openairdocs.org/sdr/CALA2019072901266.md): Web · cracked · Jul 26, 2019 · N480UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN LT FLOOR WEB IS CRACKED AT FR68-69 JUST AFT OF L2 DOOR SILL ON REF 9294422 SPEC A3NB-53-3-6222. REMOVED, FABRICATED & INSTALLED NEW FLOOR WEB AT FRAME 68-69 JUS T AFT OF L2 DOOR SILL IAW SRM 51-42-11-001 PARA E, H, F & SRM 51-31-00-801, SRM 51-23-11-
- [SDR CALA2017072802386](https://openairdocs.org/sdr/CALA2017072802386.md): Lamp · inoperative · Jul 26, 2017 · N480UA · Airbus A320232 · Emergency Lighting
  > RIGHT FWD OVERWING EXIT LIGHT FWD LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-15. OPS CHECKED GOOD.
- [SDR CALA2016121900001](https://openairdocs.org/sdr/CALA2016121900001.md): Battery · faulted · Dec 19, 2016 · N480UA · Airbus A320232 · Emergency Lighting
  > CIDS REPORTED LEFT AND RIGHT BATT PACK FAULTS. REMOVED AND REPLACED LEFT AND RIGHT EMERGENCY LIGHT BATTERY PACKS. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N480UA/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 = 'N480UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N480UA/reports

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