# Service difficulty reports: N479UA

A list on [N479UA](https://openairdocs.org/aircraft/N479UA.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 CALA2026101320342](https://openairdocs.org/sdr/CALA2026101320342.md): Frame · cracked · Sep 28, 2026 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > FRAME 68, STR 8R, ABOVE TOP FASTENER IN WEB HORIZONTAL CRACK ALONG RADIUS APPROX.400 LONG IAW LCQ N/R 9292113/40113. REPAIRED AFT CABIN RT FRAME 68, STR 8R UPPER FRAME IAW SRM 53-41-12-300-012, PAGE 5, FIG 3. PERFORMED HFEC IAW NTM 51-10-08, WITH CRACK INDICA
- [SDR CALA2026041315325](https://openairdocs.org/sdr/CALA2026041315325.md): Fuel Cap · missing · Apr 12, 2026 · N479UA · Airbus A320232 · Fuel Storage
  > PDA 2 SEARCHED GATE AREA AND FUEL CART, FUELER SAID FUEL WAS MISSING AT ARRIVAL PLACED ON CDL 28A SEE LOG 8528973. FUEL CAP MISSING SEARCHED GATE AREA AND FUEL CART, FUELER SAID AIRCRAFT ARRIVED WITH CAP MISSING REQUEST CDL 28A APPLIED CDL 28A REPLACED MISSIN
- [SDR CALA2025060305226](https://openairdocs.org/sdr/CALA2025060305226.md): Check Valve · faulted · Jun 1, 2025 · N479UA · Airbus A320232 · Hydraulic System, Main
  > HYD Y RSVR OVHT ECAM REPORTED BY FLIGHT CREW VIA ARINC TO DISPATCH, CREW C/W QRH AND SHUTOFF HYD Y ENG 2 PUMP. CREW REPORTED THAT THEY HAD NOT RUN THE YELLOW ELECTRIC PUMP. ONLY EDP WAS USED DURING OVERHEAT. OVER HEAT MSG WENT AWAY IN FLIGHT AFTER TURNING OFF
- [SDR CALA2025041403783](https://openairdocs.org/sdr/CALA2025041403783.md): Cover · cracked · Apr 10, 2025 · N479UA · Airbus A320232 · Escape Slide
  > FA ADVISED DOOR 2R SLIDE COVER HAS 2 INCH CRACKED. REPLACED DR 2R SLIDE BUSTLE, REF AMM 25-62-44-400-802-A.
- [SDR CALA2024122301617](https://openairdocs.org/sdr/CALA2024122301617.md): Battery Pack · no test · Dec 20, 2024 · N479UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - BATTERY FAULT AT FWD L EMERGENCY POWER SUPPLY UNIT REMOVED AND REPLACE BATTERY REF AMM 33-51-38-000/400-002-A OPS CHECK GOOD
- [SDR CALA2024111102832](https://openairdocs.org/sdr/CALA2024111102832.md): Skin · dented · Nov 1, 2024 · N479UA · Airbus A320232 · Leading Edge Devices
  > L/H WING SLAT #3 L/E HAS DENT DOT 43-035
- [SDR CALA2024110702806](https://openairdocs.org/sdr/CALA2024110702806.md): Stringer · corroded · Oct 31, 2024 · N479UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CA3NB-05-3-6025) DOT 210-60 AFT CABIN UNDER FLOOR COMPARTMENT FR 66 STGR 41 HAS CORROSION.()
- [SDR CALA2023051201485](https://openairdocs.org/sdr/CALA2023051201485.md): Panel · missing · May 6, 2023 · N479UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 3 #2 ENGINE PHLON OUTBD AFT PANEL 486AR IS MISSING ONE EA SCREW INSTALLED MISSING SCREW ON PANEL 486AR, #2 ENGINE OUTBD PYLON. REF AMM 54-53-11
- [SDR CALA2022110203024](https://openairdocs.org/sdr/CALA2022110203024.md): Panel · inoperative · Nov 2, 2022 · N479UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LTS ILLUMINATED IN CABIN REPLACED AFT LIGHT PANEL PER TASK 23-73-13-400-001-A - OPSCHECK NORMAL
- [SDR CALA2022081002022](https://openairdocs.org/sdr/CALA2022081002022.md): Engine · fire · Aug 9, 2022 · N479UA · Airbus A320232 · Powerplant System
  > DURING HIGH POWER RUN OBSERVED #2 ENGINE FIRE WARNING INDICATION ALONG WITH CONTROL TOWER VISUAL CONFIRMATION. SHUTOFF FUEL CONTROL LEVER AND DEPLOYED #2 ENGINE FIRE SWITCH. CRANKED ENGINE UNTIL FIRE WARNING EXTINGUISHED. FIRE BOTTLES WERE NOT DEPLOYED. VISUAL
- [SDR CALA2022062001540](https://openairdocs.org/sdr/CALA2022062001540.md): Priority Valve · leaking · Jun 20, 2022 · N479UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > HYD Y ENG 2 PUMP LO PRECAM.YELLOW HYD SYSTEM LOST ALL FLUID DURING CRUISE. LEAK FOUND AT PRIORITY VALVE YELLOW SYS. R AND R YELLOW PRIORITY VALVE LEAK TEST IS GOOD NO DEFECT NOTICE AT THIS TIME. ADD EMP:U102061 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1124690
- [SDR CALA2022032500794](https://openairdocs.org/sdr/CALA2022032500794.md): Relay · odor · Mar 25, 2022 · N479UA · Airbus A320232 · Air Conditioning System
  > FLIGHT CREW REPORTED TO HMC SMOKE IN THE COCKPIT UPDATING TO REFLECT SDR ITEM DEBREIFED CREW AND FOUND C/B E8 ON 49VU TRIPPED.. REF AWM 31-68-04,31-68-05,31-68-06,31-68-07,,31-61-07..FOUND TESTS PASSED.EIS DMC SWITCHING CKS NORMAL..CIRCUIT BRKR STAYS RELAY BO
- [SDR CALA2022031700668](https://openairdocs.org/sdr/CALA2022031700668.md): Power Supply · inoperative · Mar 15, 2022 · N479UA · Airbus A320232 · Emergency Lighting
  > PASSENEGER SEAT ROWS 10, 11 AND 38 EMERGENCY LIGHTS FAIL TO ILLU MINATE PER HAECO LCQ NON ROUTINE 9298752/36752 GENERATED BY V061 627. TROUBLESHOT IAW A320 AWM 35-51-06 & 35-51-08. REMOVED & REPLACED AND 33-51-00-710-001-A. PERFORMED BY MECH V920292 INSPECTED
- [SDR CALA2022031400658](https://openairdocs.org/sdr/CALA2022031400658.md): Battery Pack · weak · Mar 13, 2022 · N479UA · Airbus A320232 · Lighting System
  > 13WL FAILS CAPACITY CHECK A3NB-33-3-6013 PER HAECO LCQ NON ROUTI NE 9298024/36024 GENERATED BY V039706
- [SDR CALA2022022800507](https://openairdocs.org/sdr/CALA2022022800507.md): Stringer · corroded · Feb 24, 2022 · N479UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO FR34 STR41 RT STRINGER HAS CORROSION (A3NB-05-3-6013) GENERATED AT HAECO LCQ PER NONROUTINE 9298365 (36365) BY N078592 REMOVED AND REPLACED STR 34 FR30-35 L/H IAW A320 SRM 51-72-11-91 1-001 PERFORMED BY:V061616 INSP BY:V919150
- [SDR CALA2022022100463](https://openairdocs.org/sdr/CALA2022022100463.md): Intercostal · cracked · Feb 19, 2022 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > R1 FR16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APPE ARS TO BE IN FRAME LAYER AT 5 O''CLOCK. GENERATED BY V892444 PER NR 9298275/36275 INSPECTIONS AT RH FR16 AT DOOR STOP FITTING #1 HOLE#3 AND #4 PER REACHES 38,829 TOTAL ACFT FC.PERFORM REPEAT INSP
- [SDR CALA2022022100462](https://openairdocs.org/sdr/CALA2022022100462.md): Skin · cracked · Feb 19, 2022 · N479UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FR 35 STR 30 LH CRACK INDICATIONS NOTED IN FASTENER HOLE #2 FRAM E,AFT SKIN FWD SKIN LAYERS AND HOLE #3 FRAME LAYER ONLY. 5331-02848 PART 1.1. ACCOMPLISH PERMANENT REPAIR AT LH FR 35 STR BEFORE 16AUG2022. ALL WORK ACCOMPLISHED ON HAECO NR 9298178 AND 30 HOLES
- [SDR CALA2022021800427](https://openairdocs.org/sdr/CALA2022021800427.md): Stringer · corroded · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO BILGE STRINGER 42 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298691 (36691) REMOVED AND REPLACED STR42 L/H AT FR57 IAW A320 SRM 51-72-11-911 -001.PERFORMED BY V061765,INSPECTED BY: V061334.
- [SDR CALA2022021800426](https://openairdocs.org/sdr/CALA2022021800426.md): Stringer · corroded · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO BILGE STRINGER 40 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298690 (36690) REMOVED AND REPLACED STR40 L/H FR47-57 IAW A320 SRM 51-72-11-911 -001 PERFORMED BY:V061630 INSPECTED BY:V061334
- [SDR CALA2022021800424](https://openairdocs.org/sdr/CALA2022021800424.md): Intercostal · cracked · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > L1 FR 16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APP EARS TO BE IN INTERCOASTAL LAYER AT 3 O''CLOCK. SUPPORT TASK GENE RATED BY:V892444 AT HAECO LCQ PER NR:9298272 (36272) PERFORMED INTERCOASTAL REPLACEMENT AT L1 FR16, STOP FITTING #1 IAW EA5311-0
- [SDR CALA2022021800423](https://openairdocs.org/sdr/CALA2022021800423.md): Intercostal · cracked · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > L1 FR 16 DOOR STOP #7 HAS CRACK INDICATION IN UPPER IB HOLE, APP EARS TO BE INTERCOASTAL LAYER AT 4 O''CLOCK. SUPPORT TASK. GENERA TED BY V892444 AT HAECO LCQ PER NR:9298273 (36273). PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT L1 FR16, STOP FITTI NG #7. IAW E
- [SDR CALA2022021800422](https://openairdocs.org/sdr/CALA2022021800422.md): Intercostal · cracked · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > R1 FR16 DOOR STOP #7, HAS CRACK INDICATION IN UPPER IB HOLE AT 5 O''CLOCK. GENERATED BY:V892444 AY HAECO LCQ PER NR:9298276 (3627 6) SUPPORT TASK.. PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT R1 FR 16, STOP FITT ING #7 IAW EA 5311-02164.002 & REPAIR DWG R5311
- [SDR CALA2022021800421](https://openairdocs.org/sdr/CALA2022021800421.md): Plate · corroded · Feb 17, 2022 · N479UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > AFT CARGO PIT R/H DOOR SILL SUPPORT BOX BETWEEN FR52A-56, HAS CO RROOSION ON UPPER SURFACE.A3NB-05-3-6023. GENERATED BY V919150 A T HAECO LCQ PER NR:9298328 (36328) REMOVED 7 REPLACED AFT CARGO PIT R/H DOOR SILL SUPPORT FR52A-56 IAW A320 SRM 51-72-11 PERFORMED
- [SDR CALA2022020800343](https://openairdocs.org/sdr/CALA2022020800343.md): Plate · corroded · Feb 7, 2022 · N479UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO DOOR SILL WEBB FR25 TO FR28 HAS SPOTS OF CORROSION. G ENERATED BY:N075892 @HAECO LCQ PER NON ROUTINE 9298330(36330) A3 NB-53-3-6105.
- [SDR CALA20190821395](https://openairdocs.org/sdr/CALA20190821395.md): Outflow Valve · faulted · Aug 19, 2019 · N479UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > FLIGHT CREW REPORTED AVIONICS VENT SKIN VALVE FAULT ALONG WITH BLOWER FAULT. TOMC UPDATE- PRECAUTIONARY REMOVE AND REPLACE 22HQ SKIN AIR OUTLET VLV. REF TSM TASK 21-26-00-810-84-A, TESTED AEVC ON MCDU, TESTED OK, LAST LEG REPORT, SKIN AIR OUTLET V 22HQ AND ISO
- [SDR CALA2019052000797](https://openairdocs.org/sdr/CALA2019052000797.md): Epsu · faulty · May 19, 2019 · N479UA · Airbus A320232 · Emergency Lighting
  > MIDDLE OVERHEAD EMERGENCY LIGHT INTERMITTENTLY TURNS ON UNCOMMAN DED A3NB-33-3-6012 PER NR 9290608 T/S MIDDLE OVERHEAD EMERGENCY LIGHTS AND FOUND LT EPSU (11WL) TO BE BAD REMOVED AND REPLACED LT EPSU (11WL) IAW AMM 33-51-34-000-001-A AND 33-51-38-400-001-A OP
- [SDR CALA2019051300769](https://openairdocs.org/sdr/CALA2019051300769.md): Shear Plate · not reported · May 5, 2019 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT AFT SHEAR PLATE @FR 68-69 A3NB-53-3-6222 PER NR 92 90327 REMOVED AND REPLACED SHEAR PLATE @FR 68-69 IAW A320 51-42-11 PER NR 9290327 WORK ACCOMPLISHED.
- [SDR CALA2019050700706](https://openairdocs.org/sdr/CALA2019050700706.md): Door Sill · corroded · May 5, 2019 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION L-2 DOOR SILL I/B OF AFT GIRT PLATE A3NB-5 3-3-6222 PER NR 9290355. REPAIRED AREA ON L2 DOOR SILL I/B OF AFT GIRT PLATE IAW SRM 51-42-11 AND 53-41-14-300-001 THIS IS A CATEGORY A REPAIR NO REINSPECT REQUIRED PER NR 9290355.
- [SDR CALA2019050700701](https://openairdocs.org/sdr/CALA2019050700701.md): Door Sill · corroded · May 5, 2019 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION AT FWD AND AFT I/B SIDE OF R-2 DOOR SILL A 3NB-53-3-6222 PER NR 9290351. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001 PER NR 9290351.
- [SDR CALA2018020200462](https://openairdocs.org/sdr/CALA2018020200462.md): Cover · cracked · Feb 2, 2018 · N479UA · Airbus A320232 · Emergency Equipment
  > RIGHT OVERWING EMER EXIT SLIDE COVER CRACKED. REPLACED RIGHT OVERWING SLIDE PER AMM25-62-42-400. ALL OPS CKS GOOD.
- [SDR CALA2018010500064](https://openairdocs.org/sdr/CALA2018010500064.md): Switch · malfunctioned · Jan 5, 2018 · N479UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. RESET NO SMOKING LIGHTS TO ON POSITION
- [SDR CALA2017121804518](https://openairdocs.org/sdr/CALA2017121804518.md): Power Supply · inoperative · Dec 18, 2017 · N479UA · Airbus A320232 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EPSU AND BATTERY REF AMM 33-51-38. OPS CHECK GOOD. OK FOR SVC.
- [SDR CALA2017120104285](https://openairdocs.org/sdr/CALA2017120104285.md): Power Supply · no test · Dec 1, 2017 · N479UA · Airbus A320232 · Emergency Lighting
  > RIGHT EMER LIGHT POWER SUPPLY FAILED SYSTEM TEST DURING 2 SERVICE CHECK. REPLACED RH EPSU REF AMM 33-51-38 OPS CHK OK
- [SDR CALA2017051901468](https://openairdocs.org/sdr/CALA2017051901468.md): Oven · contaminated · May 19, 2017 · N479UA · Airbus A320232 · Buffet/Galleys
  > F/A REPORTED AFT GALLEY OVEN R42 BURNT SMELL AND PLASTIC MELTED TO FAN GUARD. MELTED PLASTIC FOUND AT OVEN FAN GRILL. REMOVED PLASTIC, OPS CHECK GOOD. NO MORE SMELL.
- [SDR CALA2015102094682](https://openairdocs.org/sdr/CALA2015102094682.md): Stringer · corroded · Oct 19, 2015 · N479UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, STRINGER 43L IS CORRODED, BETWEEN FRAME 58 - 59. R & R STRINGER 43L IAW SRM 51-42-11.
- [SDR CALA2014032090650](https://openairdocs.org/sdr/CALA2014032090650.md): Fitting · corroded · Mar 19, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR AFT FRAME 68 & STRINGER 23 HAS CORROSION. REMOVED CORROSION & FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.
- [SDR CALA2014032090649](https://openairdocs.org/sdr/CALA2014032090649.md): Skin · damaged · Mar 19, 2014 · N479UA · Airbus A320232 · Wing, Plate/Skin
  > RT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.
- [SDR CALA2014032090648](https://openairdocs.org/sdr/CALA2014032090648.md): Skin · damaged · Mar 19, 2014 · N479UA · Airbus A320232 · Wing, Plate/Skin
  > LT WING FUEL PANEL LANDING 540MB HAS FOUR EACH SCREW HOLES GOUGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.
- [SDR CALA2014022590465](https://openairdocs.org/sdr/CALA2014022590465.md): Door Frame · corroded · Feb 25, 2014 · N479UA · Airbus A320232 · Fuselage Main, Structure
  > R2 DOOR AFT FRAME 68 & STATION 23 HAS CORROSION. REMOVED CORROSION, FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.
- [SDR CALA2014022590464](https://openairdocs.org/sdr/CALA2014022590464.md): Skin · gouged · Feb 22, 2014 · N479UA · Airbus A320232 · Wing, Plate/Skin
  > RT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. HOLE REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.
- [SDR CALA2014022590463](https://openairdocs.org/sdr/CALA2014022590463.md): Skin · gouged · Feb 22, 2014 · N479UA · Airbus A320232 · Wing, Plate/Skin
  > LT WING FUEL PANEL LANDING 540 MB HAS FOUR EACH SCREW HOLES GOUGED. HOLES REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.
- [SDR CALA2014022590462](https://openairdocs.org/sdr/CALA2014022590462.md): Frame · damaged · Feb 22, 2014 · N479UA · Airbus A320232 · Fuselage Main, Frame
  > LT AVIONICS COMPARTMENT NLG DOG HOUSE CROSS BEAM FRAME 16 HAS ELONGATED SLOT ATTACH HOLE. REWORKED HOLE LT SIDE NLG COMPARTMENT BETWEEN LT AVIONICS DOOR & DOG HOUSE FAME 16. REAMED ELONGATED HOLE, FABRICATED & INSTALLED INSERT & REPAIRED WASHERS IAW ECRA 531
- [SDR CALA2014022190411](https://openairdocs.org/sdr/CALA2014022190411.md): Sill · corroded · Feb 18, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AT FRAME 66, REPLACED R2 DOOR SILL.
- [SDR CALA2014021790387](https://openairdocs.org/sdr/CALA2014021790387.md): Stringer · corroded · Feb 16, 2014 · N479UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 41R, FRAME 58 - 64 HAS CORROSION. REPLACED STRINGER IAW SRM 51-42-11 ON TIMCO NR 39450.
- [SDR CALA2014021790386](https://openairdocs.org/sdr/CALA2014021790386.md): Sill · corroded · Feb 14, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CORROSION PRESENT AT L2 DOOR SILL FWD GIRT BAR ATTACH POINT FRAME 66. R & R L2 DOOR SILL PN D534800420601 IAW A320 SRM 51-42-11 PG 7, PARA 5 & 6 & PG 25 PARA 7.
- [SDR CALA2014021290363](https://openairdocs.org/sdr/CALA2014021290363.md): Structure · gouged · Feb 11, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REPAIRED MED R1 FWD GIRT BAR FITTING AREA GOUGE IN TWO PLACES IAW SRM 53-11-14 FIG 108. ACP HFEC IAW NTM'S 51-10-01 PB 6 & 51-10-04 PB 4, NO DISCREPANCIES. FABRICATED & INSTALLED TWO EACH REPAIR WASHERS FWD INBD & OTBD HOLES IAW SRM 53-11-14 FIG 108.
- [SDR CALA2014021090339](https://openairdocs.org/sdr/CALA2014021090339.md): Fitting · corroded · Feb 9, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REPAIRED R1 DOOR SILL FWD GIRT BAR FITTING AFT TWO EACH HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACCOMPLISHED HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.
- [SDR CALA2014021090338](https://openairdocs.org/sdr/CALA2014021090338.md): Fitting · corroded · Feb 9, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REPAIRED L1 DOOR SILL FWD GIRT BAR FITTING TWO EACH AFT HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.
- [SDR CALA2014021090337](https://openairdocs.org/sdr/CALA2014021090337.md): Fitting · corroded · Feb 9, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REPAIRED L1 DOOR SILL FWD GIRT BAR FITTING FWD OTBD HOLE CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLE IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.
- [SDR CALA2013121693732](https://openairdocs.org/sdr/CALA2013121693732.md): Power Supply · inoperative · Dec 15, 2013 · N479UA · Airbus A320232 · Emergency Lighting
  > DURING TEST ITEM 31 OF JIC 4-2020 FAILED BATTERY CAPACITY TEST. MESSAGE DISPLAYED AS FOLLOWS EPSU BAT CAP FWD L, EMER R EMER L, AFT L. TEST COMPLETION AT "CIDS" SHOWS BATTERY FAULT AT "EMERG PWR SUPPLY UNIT". 10WL LOCATED ABOVE CEILING DOOR FWD LT. REPLACED

Next page: https://openairdocs.org/aircraft/N479UA/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 = 'N479UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N479UA/reports

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