# Service difficulty reports: N889UA

A list on [N889UA](https://openairdocs.org/aircraft/N889UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA2026020913642](https://openairdocs.org/sdr/CALA2026020913642.md): Engine · bird ingestion · Feb 3, 2026 · N889UA · Airbus A319132 · Engine (Turbine/Turboprop)
  > LOUD VIBRATIONS AFTER TAKEOFF. ENG INDICATIONS NORMAL. MX FOUND BIRD REMAINS IN NR 1 ENGINE. POTENTIAL BIRD STRIKE, DAMAGE TO TWO FAN BLADES, HOLE IN ENGINE INLET AT APPROX 7 O CLOCK POSITION, AND DAMAGE TO ABRADABLE LINER AT APPROX 5 TO 7 O CLOCK POSITION R
- [SDR CALA2025082708198](https://openairdocs.org/sdr/CALA2025082708198.md): Fuel Cap · missing · Aug 23, 2025 · N889UA · Airbus A319132 · Fuel Storage
  > PDA 2 FUELER FOUND FUEL CAP MISSING SEE LOG PAGE 6024804 FOR CDL
- [SDR CALA2025081207619](https://openairdocs.org/sdr/CALA2025081207619.md): Lgciu · faulted · Aug 9, 2025 · N889UA · Airbus A319132 · Cargo/Baggage Doors
  > FWD CARGO DOOR OPEN ECAM ON LANDING ROLL OUT. INSTALLED INOP STICKER ADJACENT TO THE LOWER ECAM. VERIFIED THE FWD CARGO DOOR IS CLOSED AND LOCKED. PROX SW AND LGCIU IN CASE NEEDED AFTER T/S. UNABLE TO DUPLICATE THE FAULT. REPLACED LGCIU 1 AS A PRECAUTION. O
- [SDR CALA2025080607375](https://openairdocs.org/sdr/CALA2025080607375.md): Warning Message · false activation · Aug 3, 2025 · N889UA · Airbus A319132 · Airborne Auxiliary Power Unit (APU) System
  > CLASSII APU MSG CLEARED WHEN APU MASTER SWITCH ON. FOUND MSG, FUEL LOW PRESS LOW FUEL PRESS SW (5030QM) ON LAST LEG REP. DUE TO HISTORY REQUEST MEL 4900A OK TO MEL COMPLIED WITH MEL 4900A DM MX NOTE FIN 5030QM IS SENSOR P/N FRH100014A (18-2822-3-0017). PERF
- [SDR CALA2025070206149](https://openairdocs.org/sdr/CALA2025070206149.md): Proximity Switch · faulty · Jun 28, 2025 · N889UA · Airbus A319132 · Door Warning System
  > AFT LDG FWD CARGO DOOR ECAM CAME ON BRIEFLY AND WENT OUT ITEM HAS HISTORY. REQUESTING MEL. REF AWM 31-54-46 INSPECT WIRES TO PROX SWITCH FOR CONDITION. CHECK WIRES WITHIN HARNESS 4613VB. ALSO SEE MX TIP 52-019. REMOVED PROXIMITY SWITCH PER AMM-TASK 52-35-13-
- [SDR CALA2025060405263](https://openairdocs.org/sdr/CALA2025060405263.md): Fuel Cap · missing · May 31, 2025 · N889UA · Airbus A319132 · Fuel Storage
  > PDA 2 FUEL CAP FOUND MISSING ON WALK AROUND IN ORD VUSUALLY INSPECTED VACINITY OF REFUEL POINT, NO DAMAGED NOTED. CONTACTED IAH HMC, FUEL CAP HAS YET TO BE LOCATED.
- [SDR CALA2025041703931](https://openairdocs.org/sdr/CALA2025041703931.md): Vent · bird ingestion · Apr 13, 2025 · N889UA · Airbus A319132 · Fuselage Structure (General)
  > BIRD CAUGHT IN PAC AIR VENT UNDER AIRCRFT. FOUND BIRD WHOLE AND INTACT IN LOUVER PANEL, ACCESSED THRU RIGHT WHEEL WELL MLDG DOOR FOR RETRIEVAL, NO ABNORMAL SMELLS OR INDICATIONS NOTED IN CABIN OR FLIGHT DECK, PERFORMED BIRD STRIKE INSPECTION REF AMM 05-51-
- [SDR CALA2024112001215](https://openairdocs.org/sdr/CALA2024112001215.md): Unknown · odor · Nov 20, 2024 · N889UA · Airbus A319132 · Air Distribution System
  > INBOUND CREW REPORTED TO TOMC AFTER PARKING AT GATE FLT ATT REPORTED AN ELECTRICAL ODOR FROM AFT OF ACFT, THEN ALSO NOTED AN OILY SMELL. AFTER ARRIVING AT GATE SMELL WENT AWAY. PERFORM AMM 05-51-10-200-801-C1 FOUND NO ELECTRICAL ODOR THROUGHOUT AFT AND FWD CAB
- [SDR CALA2024102500927](https://openairdocs.org/sdr/CALA2024102500927.md): Fuel Cap · missing · Oct 24, 2024 · N889UA · Airbus A319132 · Fuel Storage
  > PDA 2 REPORTED BY FUELER. FUEL CAP IS MISSING REF LOG 9577959 FOR DEFFERAL
- [SDR CALA2023081602548](https://openairdocs.org/sdr/CALA2023081602548.md): None · none · Aug 14, 2023 · N889UA · Airbus A319132 · Standard Practices/Structures
  > CREW REPORTED REJECTED TAKEOFF DUE TO BIRD STRIKE. INSPECTED BRAKES NO DAMAGE NOTED. BRAKE TEMPS DID NOT EXCEED 410 DEGREES F. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-14/601. NO DAMAGE TO AIRCRAFT NOTED, ONLY BIRD STRIKE EVIDENCE WAS TO FO WINDOW. CLEAN
- [SDR CALA2023012000152](https://openairdocs.org/sdr/CALA2023012000152.md): Stringer · corroded · Jan 18, 2023 · N889UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BETWEEN FR52 AND FR53 STGR42L HAS CORROSION PER HAECO LCQ NON-ROUTINE 9294437/38437. WORK ACCOMPLISHED IAW ECRA 5340-02090, CAT A. NO FURTHER ACTION REQUIRED. HAECO NON ROUTINE AND ASSOCIATED ECRA REVIEWED NO ISSUES.
- [SDR CALA2023011800139](https://openairdocs.org/sdr/CALA2023011800139.md): Slide · no test · Jan 17, 2023 · N889UA · Airbus A319132 · Escape Slide
  > AFT RIGHT HAND SLIDE FAILS EMERGENCY LIGHT TEST. PER HAECO LCQ N ON-ROUTINE 9294652/38652, SPEC: A3NB-33-3-6 015. REMOVED AND REPLACED R/H AFT (R2 DOOR) SLIDE-RAFT PACK ASSEMBLY IAW AMM TASK 25-62-44-000-804-A AND AMM TASK 75-67-44- 400-803-A. OPS CHECKED GO
- [SDR CALA2023011000075](https://openairdocs.org/sdr/CALA2023011000075.md): Skin · corroded · Jan 9, 2023 · N889UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > AFT CARGO BETWEEN FR54 AND FR55 STGR42L HAS CORROSION PER HAECO LCQ N/R 9294442/38442 BLENDED OUT CORR AT AFT CARGO BTWEEN FR54-FR55 STGR42L IAW A319 AND REPAIR ANGLE IAW A319 SRM 53-41-13-300-010 FIG 2 TREAT PRIME SRM 51-74-00-001 MAT ORIGINAL IS.142 MAT LOS
- [SDR CALA2023010600043](https://openairdocs.org/sdr/CALA2023010600043.md): Fitting · corroded · Jan 4, 2023 · N889UA · Airbus A319132 · Fuselage Structure (General)
  > SUPPORT TASK FWR CARGO DOOR LOWER CUT-OUT #6 FITTING FWD LUG HAVE CORROSION AROUND BUSH PER HAECO LCQ NON-ROUTINE 9294486/38486 GENERATED BY V061682. REMOVED AND REPLACED NEW FITTING ON FWD CARGO DOOR LOWER CUT OUT #6 FITTING FWD LUG IAW A319 SRM 51-72-11-911-
- [SDR CALA2022123003532](https://openairdocs.org/sdr/CALA2022123003532.md): Shear Web · corroded · Dec 28, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RH FR69-70 SHEAR WEB SUPPORT IS CORRODED A3NB-05-3-6056 PER NR 9 294323/38323. RMVD AND RPLD NEW SHEAR WEB SUPPORT ON RH FR69-FR70 AFT CABIN IA W SRM 51-72-11-911-001.
- [SDR CALA2022123003531](https://openairdocs.org/sdr/CALA2022123003531.md): Shear Web · corroded · Dec 28, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RH FR69-70 SHEAR WEB IS CORRODED A3NB-05-3-6056 PER NR9294322/38 322. RMVD AND RPLD NEW SHEAR WEB ON RH FR69-70 AFT CABIN IAW SRM 51-7 2-11-911-001.
- [SDR CALA2022122803506](https://openairdocs.org/sdr/CALA2022122803506.md): Angle · corroded · Dec 27, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL AT FR68 HAS CORROSION A3NB-05-3-6056 PER NR9294333/ 3833 R2 DOOR SILL AT FR68 REPAIRED IAW SRM 53-41-14-300-081 REPAIR PR INCEPLE 7.
- [SDR CALA2022122603484](https://openairdocs.org/sdr/CALA2022122603484.md): Stop Fitting · cracked · Dec 23, 2022 · N889UA · Airbus A319132 · Fuselage Main, Structure
  > RH FR16, DOOR STOP#1, IB LOWER HOLE HAS CRACK INDICATION IN FR LAYDER @ 9 O''CLOCK. REMOVED AND REPLACED R/H FR16 INTERCOSTAL AT THE #1 DOOR STOP PO SITION IAW AIRBUS DWG R53113118 FLOW CHART 2.
- [SDR CALA2022122303470](https://openairdocs.org/sdr/CALA2022122303470.md): Shear Web · corroded · Dec 22, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT FRAMES 69-70 SHEAR WEB WAS CORRODED. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-72-11-911-001.
- [SDR CALA2022122303469](https://openairdocs.org/sdr/CALA2022122303469.md): Floor Support · corroded · Dec 22, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT FRAMES 69-70 SHEAR WEB SUPPORT IS CORRODED. REMOVED AND REPLACED THE SHEAR WEB SUPPORT IAW SRM 51-72-11-911-001.
- [SDR CALA2022122103457](https://openairdocs.org/sdr/CALA2022122103457.md): Shear Plate · cracked · Dec 20, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) AFT CARGO PIT FR54 TO FR55, STGR38L, SHEAR PLATE BUCKLED AND CRACKED. PER HAECO LCQ N/R 9294552/38552 GENERATED B Y V925324. REMOVED AND REPLACED AFT CARGO PIT FR54L TO FR55L STGR38L SHEAR V925324 INSP V061704. PLATE (WED) IAW A319 SRM 51-42-11-
- [SDR CALA2022122103456](https://openairdocs.org/sdr/CALA2022122103456.md): Door Sill · corroded · Dec 20, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FWR AREA AT FR 66 HAVE CORR. AROUND HO LE. PER HAECO LCQ N/R 9294490/38490. R2 DOOR SILL FWR AREA AT FR66 HAS BEEN REPAIRED IAW A319 SRM 53- 41-14-300-001 REPAIR PRINCIPLE 6. DOT REMOVED.
- [SDR CALA2022121903411](https://openairdocs.org/sdr/CALA2022121903411.md): Door Sill · corroded · Dec 16, 2022 · N889UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FR66 HAS CORROSION AROUND NUT PLATE HOLE. SPEC: A3N B-05-3-6056. PER HAECO LCQ NON-ROUTINE 9294319/38319 GENERATED B Y V061680. L2 DOOR SILL FR66 AREA OF CORROSION AROUND NUTPLATE FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14-283-002. DAMANGE RE
- [SDR CALA2022121203354](https://openairdocs.org/sdr/CALA2022121203354.md): Stop Fitting · cracked · Dec 10, 2022 · N889UA · Airbus A319132 · Fuselage Main, Structure
  > AD RELATED SUPPORT TASK (AD 2022-02-11): RH FR 16, DOOR STOP #7 IB UPPER HOLE HAS CRACK INDICATION IN FR LAYER @ 7 O''CLOCK. "REP AIR BEFORE NEXT FLIGHT" PER HAECO LCQ NON-ROUTINE 9294289/38289 GENERATED BY V892444.
- [SDR CALA2022121203353](https://openairdocs.org/sdr/CALA2022121203353.md): Stop Fitting · cracked · Dec 10, 2022 · N889UA · Airbus A319132 · Fuselage Main, Structure
  > AD RELATED SUPPORT TASK (AD 2022-02-11): LH FR 16, #7 DOOR STOP, IB LOWER HOLE HAS CRACK INDICATION IN INTERCOSTAL LAYER @ 9 O''C LOCK. PER HAECO LCQ NON-ROUTINE 9294288/38288. GENERATED BY V892 444.
- [SDR CALA2022060801455](https://openairdocs.org/sdr/CALA2022060801455.md): Battery · no test · Jun 7, 2022 · N889UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY BATTERY (13WL) CAPACITY TEST FAILURE AS NOTED ON LTPR NR# 5001159309-0010. EPSU BATTERY(13WL)FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY LOG PAGE:8769258. WORK ACCOMPLISHED BY V933645 AND INSPECTED BY TEST AND REQUIRES REPLACEMENT.PERFORMED REPLACE
- [SDR CALA2022060801454](https://openairdocs.org/sdr/CALA2022060801454.md): Battery · inoperative · Jun 7, 2022 · N889UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY BATTERY (12WL) CAPACITY TEST FAILURE AS NOTED ON LTPR NR# 5001159309-0010. EPSU BATTERY(12WL)FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY LOG PAGE:8769243. WORK ACCOMPLISHED BY V933645 AND INSPECTED BY TEST AND REQUIRES REPLACEMENT.PERFORMED REPLACE
- [SDR CALA2022060801453](https://openairdocs.org/sdr/CALA2022060801453.md): Battery · inoperative · Jun 7, 2022 · N889UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY BATTERY (11WL) CAPACITY TEST FAILURE AS NOTED ON LTPR NR# 5001159309-0010. EPSU BATTERY(11WL)FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY TEST SATISFACTORY.LOG PAGE:8768658. WORK ACCOMPLISHED BY V933645 TEST AND REQUIRES REPLACEMENT.PERFORMED REPLAC
- [SDR CALA2022060801452](https://openairdocs.org/sdr/CALA2022060801452.md): Battery · failed insp · Jun 7, 2022 · N889UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY BATTERY (10WL) CAPACITY TEST FAILURE AS NOTED ON LTPR NR#5001159309-0010. ESPU BATTERY(10WL)FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY P/N OFF:AD-3214-31- S/N OFF:273398,P/N ON:AD-3214-31, S/N ON: TEST AND REQUIRES REPLACEMENT.PERFORMED REPLACEMEN
- [SDR CALA2021042200526](https://openairdocs.org/sdr/CALA2021042200526.md): Unknown · odor · Apr 22, 2021 · N889UA · Airbus A319132 · Powerplant System
  > STRONG SMELL OF OILFUMES INFLIGHT... ESPECIALLY AT LOWER ALTITUD ES.ONLY IN COCKPIT. ASED ON FLIGHT CREW SMOKE/ODOR IN THE PLANE (NOTABLY FLIGHT DECK) WORKING TSM TASK 71-00-00-810-801-A, # 1 ENGINE FOR EVIDENCE OF OIL LEAK. LOCKING FOR SIGNOFF CONCURRENCE WI
- [SDR CALA2020032700729](https://openairdocs.org/sdr/CALA2020032700729.md): Connector · damaged · Mar 24, 2020 · N889UA · Airbus A319132 · Light System Wiring
  > (SUPPORT TASK) L-38-004 EEPL HARNESS CONNECTING SEATS 23 AND 24 HAS DAMAGED CONNECTOR AT SEAT 24. REMOVED AND REPLACED CONNECTOR ON EEPL HARNESS AT SEAT ROW 24 24 L/H IAW A319 ESPM 20-44-29 PB 0101 CONFIG 01, CONTINUITY CHECK GOOD IAW A319 ESPM 20-52-21-760-00
- [SDR CALA2020032700728](https://openairdocs.org/sdr/CALA2020032700728.md): Connector · damaged · Mar 24, 2020 · N889UA · Airbus A319132 · Light System Wiring
  > AAR N/R S/N 9829261.(SUPPORT TASK) L-38-003 EEPL HARNESS CONNECT ING SEATS 21 AND 22 HAS DAMAGED CONNECTOR AT SEAT 21 RESEATED CONTACTS IN SEAT CONNECTOR AT SEAT 21 EEPL HARNESS IAW A319 ESPM 20-49-29-0101-01 OPS TEST PERFORMED ON CC 17-3351-1-79 07 SEQ 427
- [SDR CALA2018012700362](https://openairdocs.org/sdr/CALA2018012700362.md): Panel · delaminated · Jan 27, 2018 · N889UA · Airbus A319132 · Emergency Equipment
  > LT OVER WING SLIDE "193AT" AFT EDGE OF SLIDE PANEL DELAMINATED. REPLACED LT OVER WING SLIDE ASSY REF AMM 25-62-42.
- [SDR CALA2017051201379](https://openairdocs.org/sdr/CALA2017051201379.md): Light · inoperative · May 12, 2017 · N889UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS CHECK FAULTS 33-51-38 EPSU EXT LOAD EMER R. FOUND RT AFT EXTERIOR OVERWING EXIT LIGHT WITH ONE BULB BURNED OUT. RELAMPED AND OPS CHECKED EMERGENCY LIGHTS REF AMM 33-51-00-7 10-001-A. ALL LIGHT CHECK GOOD.

## 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 = 'N889UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N889UA/reports

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