# Service difficulty reports: N891UA

A list on [N891UA](https://openairdocs.org/aircraft/N891UA.md).

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

- [SDR CALA2025071406510](https://openairdocs.org/sdr/CALA2025071406510.md): Oxygen Box · unsecure · Jul 12, 2025 · N891UA · Airbus A319132 · Passenger Oxygen System
  > O2 MASK 27A NOT STOWED FOUND PASSENGER OXYGEN MASK CONTAINER SECURED AND STOWED MASKS NOT DROPPED. FOUND CONTAINER TRIM LOOSE RESECURED IN PLACE IAW AMM 35-21-43
- [SDR CALA2025071006430](https://openairdocs.org/sdr/CALA2025071006430.md): Bulb · missing · Jul 8, 2025 · N891UA · Airbus A319132 · Exterior Lighting
  > RH LANDING LIGHT BULB WAS MISSING IN ARRIVAL IN DENVER. RH LANDING LIGHT ASSY REPLACED ON LP 5481968
- [SDR CALA2025060905368](https://openairdocs.org/sdr/CALA2025060905368.md): Unknown · odor · Jun 7, 2025 · N891UA · Airbus A319132 · Air Distribution System
  > ELEC/SMELL POTIENTIALLY FMOM OVRHD LT 2EF ELEC/SMELL POTIENTIALLY FMOM OVRHD LT 2EF PERFORMED INSPECTION CHECK REF AMM 05-51-10-200-801-C1. NO EVIDENCE OF SMOKE OR PRESENT ODOR WAS NOTED, AND PROVIDED FORM 46.6020 TO THE FLIGHT CREW AND CABIN CREW, FROM THE
- [SDR CALA2024081300416](https://openairdocs.org/sdr/CALA2024081300416.md): Actuator · faulty · Aug 11, 2024 · N891UA · Airbus A319132 · Engine Bleed Air System
  > ENG 1 COMPRESSOR VANEPOST FLT REPORT SUSPECTED LABOR HOURS AND GROUND TIME REQUIRED UPDATE. SEE ATTACHED PICS FOR PRINTOUTS. TROUBLESHOOTING FROM THE PFR SHOWS WARN/MAINT MSG: ENG 1 FADEC AND ENG 1 COMPRESSOR VANE ATA 77-11. INTEROGATED THE LAST LEG REPORT WIT
- [SDR CALA2024080500358](https://openairdocs.org/sdr/CALA2024080500358.md): Cap · missing · Aug 2, 2024 · N891UA · Airbus A319132 · Fuel Storage
  > PDA 2 REF LP 8805737 FUELER REPORTED FUEL CAP MISSING UPON ARRIVAL. ITEM PREVIOUSLY PUT ON CDL 28A FOR MISSING LANYARD. REF LP 8805737.
- [SDR CALA2024071602050](https://openairdocs.org/sdr/CALA2024071602050.md): None · none · Jul 14, 2024 · N891UA · Airbus A319132 · Standard Practices/Structures
  > BIRD STRIKE. INSPECTION REQUIRED PER AMM. BIRD STRIKE ON RIGHT SIDE LOWER NOSE DURING TAKEOFF. NO ABNOR MAL INSTRUMENT INDICATIONS. CW BIRD STRIKE INSP REF AMM 05-51-14 NO DAMAGE OR BIRD STRIKE FOUND. OK FOR SVC
- [SDR CALA2024070101946](https://openairdocs.org/sdr/CALA2024070101946.md): Frame · cracked · Jun 28, 2024 · N891UA · Airbus A319132 · Fuselage Main, Frame
  > R/H FR16 DOUBLE JOGGLE HOLE E HAS A CRACK INDICATION AT 7 O'' CLOCK IN FRAME LAYER. REPAIRED RH FR16 DOUBLE JOGGLE AREA HOLE #E AND HOLE #F (ASSOCIA THE RH FR 16 UPPER DOUBLE JOGGLE HOLES #C #D #E. ACCOMPLISH REPAIER PER HAECO REO-L25281 AIRCRAFT REACHES 32
- [SDR CALA2024070101945](https://openairdocs.org/sdr/CALA2024070101945.md): Frame · damaged · Jun 28, 2024 · N891UA · Airbus A319132 · Fuselage Main, Frame
  > RH FR16 UPPER DOUBLE JOGGLE AREA HOLE D HAS A OUT OF ROUND CONDITION IN SKIN LAYER ONLY. ACCOMPLISH INITIAL INSPECTION OF THE RH FR16 UPP EST REVISION OF ECRA 5311-03232 ON OR BEFORE THE AIRCRAFT REACHES AT INTERVALS NOT TO EXCEED 6,800 FLT CYCLES, DOUBLE J
- [SDR CALA2024070101944](https://openairdocs.org/sdr/CALA2024070101944.md): Frame · cracked · Jun 28, 2024 · N891UA · Airbus A319132 · Fuselage Main, Frame
  > RH FR16 UPPER DOUBLE JOGGLE AREA HOLE 6 HAS CRACK INDICATION IN FRAME LAYER AT 2 O''CLOCK DIRECTION WITH 100% SCREEN HEIGHT INCLUDING ASSOCIATED HOLE 5) PER ECRA 5311-03232 PT "ACCOMPLISH AND #6 PER PART 2A OF THE LATEST REVISION OF ECRA 5311-03232 ON ES. R
- [SDR CALA2024062801920](https://openairdocs.org/sdr/CALA2024062801920.md): Stop Fitting · cracked · Jun 26, 2024 · N891UA · Airbus A319132 · Fuselage Main, Structure
  > RH FR16 #7 DOOR STOP UPPER AND LOWER IB HOLES HAVE SEVERAL CRACK INDICATIONS, APPEAR TO BE IN INTERCOSTAL LAYER. REMOVED AND REPLACED RH FR16 #7 INTERCOASTAL WITH A REPAIR CODE A0 IAW EA 5311-02164 REV.B AND DWG B2 R531-13118 ISSUE F AND SRM 51-42-11/001.
- [SDR CALA2023050901441](https://openairdocs.org/sdr/CALA2023050901441.md): Windshield · cracked · May 9, 2023 · N891UA · Airbus A319132 · Flight Compartment Windows
  > FO S WINDSHIELD REQUIRES INSPECTION PER AMM 56-11-11, DUE TO LIST DEFECT,EG SCRATCH, CRACK, DELAMINATION, BUBBLES,HEAT DAMAGE LOCATED GIVE LOCATION AND SIZE SEVERE HAIL DAMAGE ENTIRE FO WINDSCREEN. CRACKS EXTEND OVER ENTI RE WINDOW. ADDED PHOTOS OF CRACKED FO'
- [SDR CALA2022113003247](https://openairdocs.org/sdr/CALA2022113003247.md): Stringer · corroded · Nov 28, 2022 · N891UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT FR 57, STRG 43 LFT HAS CORROSION (A3NB 153-4-6179). REMOVED AND REPLACED SECTION OF STRINGER 43 LEFT AT FRAME 57 IAW SRM 53-41-13-300-10.
- [SDR CALA2022113003246](https://openairdocs.org/sdr/CALA2022113003246.md): Stringer · corroded · Nov 28, 2022 · N891UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT PTI STR 43L CORRODED FWD AND AFT OF FR 60 (A3NB-53-4-6179). REMOVED AND REPLACED SECTION OF STR 43 LEFT AT FRAME 60 IAW SRM 53-41-13-300-10.
- [SDR CALA2022111603144](https://openairdocs.org/sdr/CALA2022111603144.md): Fitting · corroded · Nov 15, 2022 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA R2 DOOR STILL HAVE CORROSION AT FR 66 AND FR68 AND FWD AND AFT CONNER FITTINGS HAS CORROSION (SUPPORT TASK). REMOVED AND REPLACED R2 DOOR SILL AND FWD AND AFT CONNER FITTING IAW A319 SRM 51-72-11.
- [SDR CALA2022111603140](https://openairdocs.org/sdr/CALA2022111603140.md): Stringer · corroded · Nov 14, 2022 · N891UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT FR 57 STR32LFT HAS CORROSION. GENERATED AT HAECO L CQ PER NR 9296402 (30402) BY V927281 {A3NB-153-4-6173}
- [SDR CALA2022111103120](https://openairdocs.org/sdr/CALA2022111103120.md): Door Sill · corroded · Nov 10, 2022 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA LH 2 DOOR SILL HAS CORROSION AT FR 68 2EA PLACES. REMOVED AND REPLACED WITH NEW LH L-2 DOOR SILL AT FR 66-68 IAW A 319 SRM 51-72-11-911-001.
- [SDR CALA2022110403047](https://openairdocs.org/sdr/CALA2022110403047.md): Stringer · corroded · Nov 3, 2022 · N891UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT PIT: STR43L CORRODED @ FR65 (A3NB-53-4-6179) GENERATED BY REMOVED SECTION OF STRINGER 43 LEFT BETWEEN FR65&66, INSPECTION INSPECTION METHOD TBD IAW A319 SRI 53-00-13-205-001 REPAIR BETWEEN 65 AND 66 IAW A319 SRM 53-00-13-300-001. REQUIRES SRI INSPECTION TH
- [SDR CALA2022110403046](https://openairdocs.org/sdr/CALA2022110403046.md): Panel · corroded · Nov 3, 2022 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA RH SHEAR PLATE HAVE CORROSION BETWEEN FR 69 AND FR 70 PER HAECO LCQ NON ROUTINE 9296512/30512 GENERATED BY REMOVED AND REPLACED AFT SHEAR WRB R/H SIDE WRT AREA FR69-70 IAW A319 SRM 57-42-11/001 PARA E AND F PERFORMED BY
- [SDR CALA2022110403045](https://openairdocs.org/sdr/CALA2022110403045.md): Panel · corroded · Nov 3, 2022 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA LH SHEAR PLATE BETWEEN FR 69 AND FR 70 HAVE CORROSION PER HAECO LCQ NON ROUTINE 9296508/30508 GENERATED BY REMOVED AND REPLACED SHEAR WRB AFT WRT AREA L/H FR69 AND 70 PERF ORMED BY
- [SDR CALA2021081101311](https://openairdocs.org/sdr/CALA2021081101311.md): Warning Message · false activation · Aug 9, 2021 · N891UA · Airbus A319132 · Central Warning
  > FLIGHT CREW REPORTED SEVERAL ANTI ICE PROBE MESSAGES PRESENT, CFDS SHOWS CAPT/FO PITOT PROBES FAULTING PFR IS FAULTING BOTH PITOTS AS WELL AS F/O STATIC AND F/O TAT. ACCMP TSM 30-31-00-810-804-A AND 30-31-00-810-869-A. PHC1 NOT CURRENTLY FAULTING AND HAS 115 A
- [SDR CALA2021072801213](https://openairdocs.org/sdr/CALA2021072801213.md): Bolt · missing · Jul 28, 2021 · N891UA · Airbus A319132 · Trailing Edge Flaps
  > PDA 3 LEFT WING #2 FLAP TRACK FAIRING 531CB BOLT COVER MISSING ON INBOARD SIDE. INSTALLED COVER ON INBOARD SIDE OF FAIRING 531CB..REF IPC 57-55-11-14H
- [SDR CALA2021011100031](https://openairdocs.org/sdr/CALA2021011100031.md): Actuator · defective · Jan 9, 2021 · N891UA · Airbus A319132 · Compressor Bleed Valve
  > ENGINE 2 EXPERIENCED SIGNIFICANT STALLS ON CLIMB AT CLIMB POWER. ECAM CLEARED. LANDED W/BOTH ENGINE, REF ATTACHED PICTURES FOR FAILURES ON PFR AND FADEC 2B BOTH FADEC CHANNELS FOR NUMBER 2 ENGINE SELF TESTED FINE. ONLY FADEC 2B HAS FAILURES FOR LAST LEG ACC
- [SDR CALA2020110901257](https://openairdocs.org/sdr/CALA2020110901257.md): Light · broken · Nov 8, 2020 · N891UA · Airbus A319132 · Emergency Lighting
  > PASSENGER SEAT 23 & 24 SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERABLE ON HAECO LCQ, REF 9290432.
- [SDR CALA2020010600101](https://openairdocs.org/sdr/CALA2020010600101.md): Skin · corroded · Jan 6, 2020 · N891UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AROUND LAV VENT AFT FUSELAGE, A/C RIGHT SIDE. VERFIED REPAIR DOUBLER ITEM 1 MATERIAL 0.071 2024T3,P.O# 9747831, REPAIR FILLERS ITEM 2,3 MATERAIL 0.063 2024T3 P.O# 8546450 AND VERFIED INTERNAL DOUBLER P/N D5348019320401 AS REF TO SRM 53-41 -11-
- [SDR CALA2018012700363](https://openairdocs.org/sdr/CALA2018012700363.md): Battery · faulty · Jan 27, 2018 · N891UA · Airbus A319132 · Emergency Lighting
  > FWD LT EMERGENCY POWER SUPPLY UNIT BATTERY FOUND FAULTY DURING EMERGENCY LIGHT TEST. REPLACED EMERGENCY LIGHT BATTERY PER AMM 33-51-38, OPERATIONAL TEST GOOD, OK FOR SERVICE.
- [SDR CALA2017111004017](https://openairdocs.org/sdr/CALA2017111004017.md): Mount · misinstalled · Nov 10, 2017 · N891UA · Airbus A319132 · Emergency Equipment
  > COCKPIT FLASHLIGHT BRACKET IS MOUNTED UPSIDE DOWN. CANNOT PREFLIGHT TEST BUTTON. REPOSITIONED THE FLASHLIGHT MOUNT 180 DEGREES. SECURED AND TESTED GOOD.
- [SDR CALA2017111004016](https://openairdocs.org/sdr/CALA2017111004016.md): Battery · inoperative · Nov 10, 2017 · N891UA · Airbus A319132 · Emergency Equipment
  > COCKPIT FLASHLIGHT TESTED BAD. ONE RED FLASH INSTEAD OF GREEN. FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY AND THE FLASHLIGHT TESTED NORMAL.
- [SDR CALA2017102703797](https://openairdocs.org/sdr/CALA2017102703797.md): Unknown · vibration · Oct 27, 2017 · N891UA · Airbus A319132 · Standard Practices/Structures
  > AT FL280, HEARD VIBRATION NOISES LIKE PROPS OUT OF SYNC. THEN HEARD LOUD TONE NOISE FOR 4-5 SECONDS. THEN SMELLED AN ELECTRICAL BURNING ODOR FOR A FEW SECONDS. NO ECAMS OR ANY FAULTS. CREW REPORTED THE VIBRATION AND ODOR DISSIPATED.
- [SDR CALA2017072102334](https://openairdocs.org/sdr/CALA2017072102334.md): Slide · dislodged · Jul 21, 2017 · N891UA · Airbus A319132 · Escape Slide
  > MX NOTIFIED THAT SIDE PACK HANGING OUT OF SLIDE COVER ON L1 DOOR. MX FOUND DOOR ARMED AND DOOR 3/4 OPEN. SLIDE NOT DEPLOYED, CYL FOR DAMPER AND EMERGENCY OPERATION PRESSURE AT ZERO. R&R L1 DOOR SLIDE/RAFT IAW AMM 25-62-44-000-012-A / 25-62-44-400 -007-A. OPS C
- [SDR CALA2017071702277](https://openairdocs.org/sdr/CALA2017071702277.md): Cover · unsecure · Jul 17, 2017 · N891UA · Airbus A319132 · Emergency Lighting
  > LEFT WING EMERG EXIT COVER FELL OFF. RE-INSTALLED PANEL.
- [SDR CALA2017062301970](https://openairdocs.org/sdr/CALA2017062301970.md): Warning System · false activation · Jun 23, 2017 · N891UA · Airbus A319132 · Door Warning System
  > L FWD EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR COVER OFF SEEMS LOOSE NO ECAM MSGS NOTED, ALL DOORS SHOW GREEN ON CFDS, COULD NOT FIND ANYTHING LOOSE ON DOOR.
- [SDR CALA2017010496060](https://openairdocs.org/sdr/CALA2017010496060.md): Threshold · corroded · Dec 17, 2016 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO FRAMES 55-59 DOOR THRESHOLD IS CORRODED. REPLACED THE THRESOLD IAW SRM 51-72-11, & 51-42-11.
- [SDR CALA2016121696043](https://openairdocs.org/sdr/CALA2016121696043.md): Door Sill · corroded · Dec 15, 2016 · N891UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CORROSION ON THE L2 DOOR SILL FRAME 66. FABRICATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, TOPCOATED, AND INSTALLED THE REPAIR IAW SRM 53-41-14 PAR 2 FIG 001.
- [SDR CALA2016121696042](https://openairdocs.org/sdr/CALA2016121696042.md): Fitting · corroded · Dec 15, 2016 · N891UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > CORROSION FWD CARGO BAY RT CROSSBEAM END FITTING FRAME 27 STRINGER 39 - 42R. REMOVED CORROSION IAW SRM 51-24-00. REMOVED AND REPLACED THE END FITTING IAW SRM 51-72-11.

## 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 = 'N891UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N891UA/reports

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