# Service difficulty reports: N890UA

A list on [N890UA](https://openairdocs.org/aircraft/N890UA.md).

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

- [SDR CALA2026092819846](https://openairdocs.org/sdr/CALA2026092819846.md): Engine · bird ingestion · Sep 28, 2026 · N890UA · Airbus A319132 · Engine (Turbine/Turboprop)
  > BIRD STRIKE. INJESTED IN NR 2 ENGINE. PERFORMED VISUAL INGESTION INSPECTION OF E2 IAW AMM TASK 05-51-19-200-001-A. FOUND BLOOD ON SINGLE BLADE. CLEANED FAN BLADE AS REQUIRED. NO DAMAGE TO FRONT OR BACK OF FAN BLADE NOTED. NO OTHER FLUIDS OR FEATHERS NOTED.BIR
- [SDR CALA2026070817616](https://openairdocs.org/sdr/CALA2026070817616.md): Coupling · missing · Jul 3, 2026 · N890UA · Airbus A319132 · Fuel Storage
  > DURING WALKAROUND INSPECTION DEFUEL/REFUEL COUPLING FOUND MISSING. COMPLIED WITH MAINTENANCE ACTION, PLACED ON CDL 28A.
- [SDR CALA2026063017480](https://openairdocs.org/sdr/CALA2026063017480.md): Unknown · odor · Jun 28, 2026 · N890UA · Airbus A319132 · Air Distribution System
  > ON SHUTDOWN AT GATE WITH APU BLEED AIR ON AIRCRAFT FILLED WITH DIRTY SOCK ODOR. ASSIST CREW WITH ENG RUN USING START CART. DO NOT USE APU BLEED TOMC DEBRIEFED CAPTAIN. CAPTAIN REPORTED THAT HE AND F/O HAD THROAT IRRITATION FROM ODOR. STRONG ODOR WAS REPORTED F
- [SDR CALA2026043015881](https://openairdocs.org/sdr/CALA2026043015881.md): Beam · cracked · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > RT O/W HATCH AFT LATERAL BEAM CRACKED A2NB-MP-2100-522102-01-2-R PER AAR LCQ NON ROUTINE 9294247/20247. REMOVED AND REPLACED AFT LATERAL BEAM ON R/H O/W HATCH IAW A319 SRM 51-42-11.
- [SDR CALA2026043015878](https://openairdocs.org/sdr/CALA2026043015878.md): Beam · cracked · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > RT O/W HATCH FWD LATERAL BEAM CRACKED A3NB-MP-2100-522102-01-2-R PER AAR LCQ NON ROUTINE 9294246/20246. REMOVED AND REPLACED FWD LATERAL BEAM ON R/H O/W HATCH IAW A319 SRM 51-42-11.
- [SDR CALA2026043015876](https://openairdocs.org/sdr/CALA2026043015876.md): Beam · cracked · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > LEFT O/W HATCH AFT LATERAL BEAM CRACKED A3NB-MP-2100-522102-01-2 -L PER AAR LCQ NON ROUTINE 9294249/20249. REMOVED AND REPLACED LATERAL BEAM ON L/H O/W HATCH IAW A319 SRM 51-42-11.
- [SDR CALA2026043015873](https://openairdocs.org/sdr/CALA2026043015873.md): Beam · cracked · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > LEFT O/W HATCH FWD LATERAL BEAM CRACKED A3NB-MP-2100-522102-01-2 -L PER AAR LCQ NON ROUTINE 9294248/20248. REMOVED AND REPLACED FWD LATERAL BEAM ON L/H O/W HATCH IAW A319 SRM 51-42-11.
- [SDR CALA2026043015871](https://openairdocs.org/sdr/CALA2026043015871.md): Plate · damaged · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT FR 66 STGR 12 GUSSET HOLE 2 HAS AN OUT OF LIMITS/OUT OF ROUN D INDICATION PER AAR LCQ NON ROUTINE 9294185/20185. REMOVED AND REPLACED GUSSET PLATE AT FR 66 LT STRG 12 IAW SRM 51-42-11.
- [SDR CALA2026043015868](https://openairdocs.org/sdr/CALA2026043015868.md): Plate · damaged · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L/H FR 66 STGR 14 GUSSET HOLES 4 AND 5 HAVE AN OUT OF LIMITS/OUT OF ROUND INDICATION PER AAR LCQ NON ROUTINE 9294186/20186. REMOVED AND REPLACED GUSSET PLATE AT FR 66 STGR 14L IAW A319 SRM 51-42-11.
- [SDR CALA2026043015866](https://openairdocs.org/sdr/CALA2026043015866.md): Gusset · damaged · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L/H FR 66 STR 15 GUSSET HOLES 1,4 AND 5 HAVE AN OUT OF LIMITS/OU T OF ROUND INDICATION PER AAR LCQ NON ROUTINE 9294187/20187 GENE RATED BY V062335 ESFR DETAILS UPDATED REMOVED AND REPLACED GUSSET PLATE AT FR66 L/H STGR 15L IAW A319 SRM 51-42-11. PERFORMED BY V
- [SDR CALA2026042915846](https://openairdocs.org/sdr/CALA2026042915846.md): Gusset · damaged · Apr 29, 2026 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT FR 68, STR 12 GUSSET HOLES 3 AND 5 HAVE AN OUT OF LIMITS, OUT OF ROUND INDICATION. REMOVED AND REPLACED GUSSET AT FR 68 LH STGR 12L IAW SRM 51 -42-11.
- [SDR CALA2025102410480](https://openairdocs.org/sdr/CALA2025102410480.md): Light · inoperative · Oct 23, 2025 · N890UA · Airbus A319132 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT AT 35C INOPERATIVE. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT AT 36C, OPS CHECK GOOD.
- [SDR CALA2025101710234](https://openairdocs.org/sdr/CALA2025101710234.md): Bolt · missing · Oct 15, 2025 · N890UA · Airbus A319132 · Wheel/Ski/Float
  > PDA 2 REF LP 6620421 #4 MLG TIRE MISSING TIE BOLT. REPLACE NR 4 WHEEL ASSY REF AMM 32-41-00.
- [SDR CALA2025060605331](https://openairdocs.org/sdr/CALA2025060605331.md): Tee Angle · cracked · Jun 4, 2025 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RT AFT TEE ANGLE SHOWS EVIDENCE OF CRACKING. REMOVED AND REPLACED CRACKED RT AFT TEE ANGLE IAW A319 SRM 51-72- 11-911-001 WITH NEW TEE ANGLE.
- [SDR CALA2025040403512](https://openairdocs.org/sdr/CALA2025040403512.md): Safety Valve · malfunctioned · Apr 2, 2025 · N890UA · Airbus A319132 · Cabin Pressure Control System
  > CAB PR LO DIFF PR CAB PR SAFETY VALVE OPEN LO DIFF PR ECAM BELOW 10K AT 6500 FEET CABIN PRESSSURE LO PRESS DIF LIGHT CAME ON ECAM,SEE ASSOCIATED PHOTOS, PILOTS REPORTED FEELING HIGH HUMIDITY, SMELLING ATMOSPHERE, AND HEAT, EARS POPPING, ALL ASSOCIATED SYMPTOM
- [SDR CALA2025012402033](https://openairdocs.org/sdr/CALA2025012402033.md): Unknown · odor · Jan 23, 2025 · N890UA · Airbus A319132 · Air Distribution System
  > STRONG PROPANE/ROTTEN EGG SMELL IN AFT CABIN DESCENDING THRU 1 0000. PASSENGERS NOXIOUS. DEBRIEFED CREW AND CONFIRMED ODOR WAS AT AFT GALLEY AND LAST 2 ROWS. IT LAST APROX 10 MINS, THE ODOR WAS NO LONGER PRESENT BY THE TIME THE ARRIVED AT THE GATE. INSPECTE
- [SDR CALA2023070702181](https://openairdocs.org/sdr/CALA2023070702181.md): Stringer · corroded · Jul 5, 2023 · N890UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER 43 L/H HAS CORROSION FROM FR55-58 A3MB-53 -4-6179 PER HAECO LCQ NON ROUTINE 9292446/22446 GENERATED BY V92 6223 PERFORMED STRINGER SPLICE REPAIR AT AFT CARGO PIT STRG.43 LH BTW FRAME 55-58 I.A.W. A319 SRM 53-41-13-300-010 PER MECH V06161
- [SDR CALA2023070502166](https://openairdocs.org/sdr/CALA2023070502166.md): Stringer · corroded · Jul 4, 2023 · N890UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER L/H HAS CORROSION FR 55-56 (A3NB-53-4-617 9) GENERATED AT HAECO LCQ PER NR 9292458 (22458) BY MECH V926223 REMOVED AND REPLACED OK STRINGER FR 54-56 LT IAW A319 SRM 53-41- 13-300-10 ACMP BY MECH V052030 INSP V937268
- [SDR CALA2023062602001](https://openairdocs.org/sdr/CALA2023062602001.md): Frame · cracked · Jun 23, 2023 · N890UA · Airbus A319132 · Fuselage Main, Frame
  > RH FRAME 16 UPPER DOUBLE JOGGLE AREA, HOLE B HAS A CRACK INDICATION IN FRAME LAYER (AD RELEATED SUPPORT TASK)(AD 2022-08-08) GENERATED AT HAECO LCQ PER NR 9292265 (22265) BY MECH V892444.
- [SDR CALA2023062602000](https://openairdocs.org/sdr/CALA2023062602000.md): Stringer · corroded · Jun 23, 2023 · N890UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > STR30R FROM FR65-FR66 BELOW OUTFLOW VALVE CORRODED (A3NB-53-3-61 85) GENERATED AT HAECO LCQ PER NR 9292607 (22607) BY MECH V07988 1 REMOVED AND REPLACED STR30 R/H SIDE FR 64-67 BELOW 007 FLOW VALV E IAW A319 SRM 51-75-11-911-001 AND A319 SRM 51-42-11/001 ACMP
- [SDR CALA2023062101971](https://openairdocs.org/sdr/CALA2023062101971.md): Floor Support · unknown · Jun 19, 2023 · N890UA · Airbus A319132 · Fuselage Structure (General)
  > RIGHT HAND SUPPORT UNDER SHEAR PLATE HAS OUT OF ROUND HOLES (A3N B-53-3-6187) GENERATED AT HAECO LCQ PER NR 9292589 (22589) BY ME CH V052030 REMOVED AND REPLACED R/H AFT SHEAR PLATE SUPPORT IAW A319 SRM 57 -42-11/001 PER MECH V061630 INSP V061757
- [SDR CALA2023061901917](https://openairdocs.org/sdr/CALA2023061901917.md): Stringer · unknown · Jun 17, 2023 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > MAIN CABIN STRINGER 23RT HAS ENLONGATED HOLE FR 68-69 RT (A3NB-5 3-3-6187AFT) GENERATED AT HAECO LCQ PER NR 9292596 (22596) BY ME CH V052030 REMOVED & REPLACED RT SIDE STRINGER 23R BETWEEN FRAMES 68-69 IAW A319 SRM 51-72-11 ACCMP BY MECH V052030 INSP BY V91312
- [SDR CALA2023061901915](https://openairdocs.org/sdr/CALA2023061901915.md): Shear Plate · corroded · Jun 17, 2023 · N890UA · Airbus A319132 · Fuselage Structure (General)
  > AFT LH SHEAR PLATE HAS CORROSION AT FRM 70 (A3NB-53-3-6187) GENE RATED AT HAECO LCQ PER NR 9292373 (22373) BY MECH V937268 REMOVED AND REPLACED LH SHEAR PLATE AT FRM 70 IAW A319 SRM 51-72 -11 DOT REMOVED MECH V052030 INSP BY V940824
- [SDR CALA2023061201823](https://openairdocs.org/sdr/CALA2023061201823.md): Door Sill · corroded · Jun 11, 2023 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 PAX DOOR SILL AFT CORNER ANGLE FITTINGS HAS CORROSION (A3NB-5 3-3-6187) GENERATED AT HAECO LCQ PER NR 9292370 (22370) BY MECH V937268 REMOVED AND REPLACED L2 PAX DOOR SILL CORNER ANGLE FITTING IAW A 319 SRM 51-42-11/001 PER MECH V061616 INSP V921658
- [SDR CALA2023061201822](https://openairdocs.org/sdr/CALA2023061201822.md): Door Sill · corroded · Jun 11, 2023 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 PAX DOOR SILL AFT CORNER ANGLE FITTING HAS CORROSION(A3NB-53- 3-6187) GENERATED AT HAECO LCQ PER NR 9292372(22372) BY MECH V93 7268 REMOVED AND REPLACED AFT CORNER FITTING ON R-2 DOOR SILL IAW A31 9 SRM 51-42-11/001 PER MECH V061616 INSP V921658
- [SDR CALA2023060901803](https://openairdocs.org/sdr/CALA2023060901803.md): Angle · corroded · Jun 7, 2023 · N890UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO, FRAME 26 STR40R, SHEAR TIE HAS CORROSION (A3NB-53-3-6 105) PER HAECO LCQ NON ROUTINE 9292310/22310 GENERATED BY V06160 3 REMOVED AND REPLACED FWD CARGO FR26 STG40R SHEAR TIE - CLEAT - I AW A319 SRM 51-72-11-911-001 AND SRM 51-72-11-911-002 MECH V917
- [SDR CALA2022032300747](https://openairdocs.org/sdr/CALA2022032300747.md): None · cracked · Mar 21, 2022 · N890UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > RH FR68 DOOR STOP NO. 1 LOWER IB HOLE NO. 3 HAS CRACK INDICATION IN FRAME LAYER @ 6 OCLOCK DIRECTION ON HAECO LCQ REF 9292086/34 086 AD RELATED SUPPORT TASK. NR GENERATED BY V892444 REPAIR AND REQUIRES REINSPECTION AT 19,700 FC (FH NOT RELEVANT) FIG 001 SHEET
- [SDR CALA2022032100736](https://openairdocs.org/sdr/CALA2022032100736.md): Stop · cracked · Mar 21, 2022 · N890UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > RH FR68 DOOR STOP NO. 1 LOWER IB HOLE NO. 3 HAS CRACK INDICATION IN FRAME LAYER @ 6 OCLOCK DIRECTION ON HAECO LCQ REF 9292086/34 086 AD RELATED SUPPORT TASK. NR GENERATED BY V892444 REPAIR AND REQUIRES REINSPECTION AT 19,700 FC (FH NOT RELEVANT) FIG 001 SHEET
- [SDR CALA2022031400646](https://openairdocs.org/sdr/CALA2022031400646.md): Floor Support · corroded · Mar 12, 2022 · N890UA · Airbus A319132 · Fuselage Structure (General)
  > RH SUPPORT ANGLE AT FRAME 70 CORRODED ON HAECO LCQ REF 9292288/3 4288 SPEC A3NB-7-3-603. NR GENERATED BY V077956 REMOVED & REPLACED R/H SUPPORT ANGLE AT FR70 IAW A319 SRM 51-72- 11 AT HAECO LCQ ON HANGAR NR 9292288/34288 PERFORMED BY MECH V91 3215 RII INSP PER
- [SDR CALA2022031400645](https://openairdocs.org/sdr/CALA2022031400645.md): None · corroded · Mar 12, 2022 · N890UA · Airbus A319132 · Fuselage Main, Structure
  > AFT CABIN RIGHT AFT SHEAR WEB HAS CORROSION ON HAECO LCQ REF 929 2269/34269 SPEC A3NB-53-3-6222. NR GENERATED BY V077956 REMOVED & REPLACED AFT SHEAR WEB AT R/H FR70 IAW A319 SRM 51-72- 11-911-001 AT HAECO LCQ ON HANGAR NR 9292269/34269 PERFORMED BY MECH V9132
- [SDR CALA2021031900345](https://openairdocs.org/sdr/CALA2021031900345.md): Extinguisher · discharged · Mar 19, 2021 · N890UA · Airbus A319132 · Fire Bottle, Fixed
  > INADVERTENT DISCHARGE OF FWD CARGO FIRE BOTTLE ACOMPLISHED STEP 3 A 1,2. STEP 3 B PULLED CIRCUT BREAKERS C06, T19, T18. STEP 3 C 1,2 3. STEP 3 D,1 REMOVED FIRE EXTINGUISHER BOTTLE. BOTTLE. LOGPAGE 6010175 CREATED TO COVER INSPECTION WEIGH IN OF NEW ACP AMM
- [SDR CALA2020100901171](https://openairdocs.org/sdr/CALA2020100901171.md): Exciter · inoperative · Oct 9, 2020 · N890UA · Airbus A319132 · APU Engine Fuel and Control
  > APU AUTOSHUT DOWN DURING START. REPEAT ISSUE. PLACED ON DEFFERAL DISPATCH DESK: 28 NAME: BB DATE: 28-SEP-20- NOC DESK: 320 NAME: RUPP DATE: 28-SEP-20. OK TO PLACE APU ON MEL 4910B AND COMPLY WITH ALL MAINTENANCE PROCEDURES, AS REQUIRED. PLACED ON DEFFERAL.
- [SDR CALA2020033000742](https://openairdocs.org/sdr/CALA2020033000742.md): Skin · dented · Mar 29, 2020 · N890UA · Airbus A319132 · Leading Edge Devices
  > RAMPER REPORTED DENT ON LT WING #3 SLAT L/E. DENT LOCATED APPROX 47" FROM IB EDGE OF #3 SLAT TOP SKIN NOSE AREA. MEASURES APPROX 2.5"CHORDWISE AND 5" SPANWISE WITH A DEPTH OF 0.135". PERFORMED TEMP FILL REPAIR REF SRM 57-40-00-300-023 PARA E. PLACED ON DIP TO
- [SDR CALA2018032600997](https://openairdocs.org/sdr/CALA2018032600997.md): Skin · dented · Mar 24, 2018 · N890UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT FRAMES 23 - 24, STRINGER 42L. REPAIRED IAW SRM 53-00-11-300-042, FIG 20144.
- [SDR CALA2017100203418](https://openairdocs.org/sdr/CALA2017100203418.md): Flashlight · no test · Oct 2, 2017 · N890UA · Airbus A319132 · Emergency Equipment
  > FWD INBD F/A FLASHLIGHT IS NOT TESTING AND CONSIDERED INOPERATIVE. REPLACED THE FLASHLIGHT AND HOLDER, TESTED OK
- [SDR CALA2017070202089](https://openairdocs.org/sdr/CALA2017070202089.md): Wire · broken · Jul 2, 2017 · N890UA · Airbus A319132 · Light System Wiring
  > ROW 20 EMER SIGN WIRES EXPOSED AND BROKEN. REPLACED CABIN WALL MOUNTED EMERG EXIT LIGHT ASSY AT ROW 21 LEFT SIDE REF AMM 33-51-13-000-001-A, OP CHECKS GOOD. VERIFIED EEL INSTALLATION OP CK OK.
- [SDR CALA2017060501730](https://openairdocs.org/sdr/CALA2017060501730.md): Lanyard · misrouted · Jun 5, 2017 · N890UA · Airbus A319132 · Escape Slide
  > L2 DOOR WILL NOT ARM. FOUND ROUTING OF FWD SLIDE RIBBON OBSTRUCTING DOOR LOCKING MECHANISM. ROUTED, OPS CHECKED GOOD AT THIS TIME. ACFT OK FOR CONTINUE D SERVICE.

## 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 = 'N890UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N890UA/reports

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