# Service difficulty reports: N895UA

A list on [N895UA](https://openairdocs.org/aircraft/N895UA.md).

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

- [SDR CALA2026100620140](https://openairdocs.org/sdr/CALA2026100620140.md): Pressure Switch · low pressure · Oct 3, 2026 · N895UA · Airbus A319132 · Hydraulic Pump (Electric/Engine), Main
  > HYD G ENG1 PUMP LO PR. UPON RETURN TO GATE MOTORED LEFT ENGINE FOUND ENGINE DRIVEN PUMP (GREEN) PRODUCING 3000 PSI WITH LOW PRESSURE ECAM INDICATION. VERIFIED LOW PRESSURE INDICATION ISSUE. FOUND EDP CASE DRAIN FILTER DPI NOT EXTENDED. REPLACED EDP PRESSURE S
- [SDR CALA2026090719275](https://openairdocs.org/sdr/CALA2026090719275.md): Unknown · odor · Sep 6, 2026 · N895UA · Airbus A319132 · Air Distribution System
  > FLT ATTS REPORTED AN ODOR COMING FROM AFT LAVS, OFF & ON DURING FLT. COMPLETED A TOILET OPS CHECK OF BOTH AFT LAVS & FOUND NO DISCREPANCIES AT THIS TIME. NO SMELL WAS EVIDENT UPON ARRIVAL TO AIRCRAFT. COMPLETED AN EXTERIOR INSPECTION OF WASTE VACUUM VENT POR
- [SDR CALA2026082018766](https://openairdocs.org/sdr/CALA2026082018766.md): Lanyard · detached · Aug 15, 2026 · N895UA · Airbus A319132 · Fuel Storage
  > FUEL CAP REPORTED MISSING BY FLIGHT CREW. FUEL CAP PLACED ON CDL 28A. FOUND FUEL CAP IS STILL INSTALLED BUT FUEL CAP LANYARD WAS NOT ATTACHED. REATTACHED FUEL, CAP LANYARD AS REQUIRED.
- [SDR CALA2026081518643](https://openairdocs.org/sdr/CALA2026081518643.md): Fuel Cap · missing · Aug 15, 2026 · N895UA · Airbus A319132 · Fuel Storage
  > MISSING FUEL CAP
- [SDR CALA2026031014462](https://openairdocs.org/sdr/CALA2026031014462.md): Light · intermittent · Mar 7, 2026 · N895UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY EXIT RED LIGHT OVER CAPT SIDE WINDOW EXIT INTERMITTENTLY ILLUMINED. VERIFIED RED LIGHT IS A SIDEWALL ILLUMINATION LIGHT PART OF THE BRUCE MOOD LIGHTING SYSTEM ACCOMPLISHED SYSTEM RESET REF AMM 33-28-00, NO HELP. APPLIED MEL 3320A. VERIFIED RED L
- [SDR CALA2025082708165](https://openairdocs.org/sdr/CALA2025082708165.md): Wire · broken · Aug 24, 2025 · N895UA · Airbus A319132 · Light System Wiring
  > EMERGENCY LIGHT AT ROW 35CBA INOP. FOUND BROKEN WIRE, REPAIRED WIRE PER AIRBUS 319/320 ESPM 20-43-11-01. OPS CHECK GOOD
- [SDR CALA2025032403128](https://openairdocs.org/sdr/CALA2025032403128.md): Lamp · inoperative · Mar 21, 2025 · N895UA · Airbus A319132 · Emergency Lighting
  > EXIT LIGHT ABOVE L1 DOOR INOP. RE LAMPED L1 DOOR EXIT LIGHT IAW A319 AMM 33-51-00-710-001-A V073952 RESEATED CONNECTOR 2671VC IAW A319 ESPM 20-44-10-02 PERFORMED OP CHECK GOOD IAW A319 AMM 33-51-00-710-001-A
- [SDR CALA2025013002113](https://openairdocs.org/sdr/CALA2025013002113.md): Battery · no test · Jan 26, 2025 · N895UA · Airbus A319132 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - PTP SHOWS FAULT: "EPSU EMER AFT L". CORRECTION: SHOWS " EPSU BATTERY AFT L". REMOVED AND REPLACED AFT L EPSU BATTERY 13WL REF AMM 33-51-38-000-002-A AND TASK 33-51-38-400-002-A. OPS CK GOOD. NO FAU
- [SDR CALA2025011401896](https://openairdocs.org/sdr/CALA2025011401896.md): Battery Pack · no test · Jan 11, 2025 · N895UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT LH EMERGENCY BATTERY DID NOT PASS TEST. REPLACED AFT LH EMERGENCY BATTERY. OPS CHECK GOOD. REF AMM 33-51-38-000-002-A. PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2025011401894](https://openairdocs.org/sdr/CALA2025011401894.md): Battery Pack · no test · Jan 11, 2025 · N895UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LH EMERGENCY BATTERY DID NOT PASS TEST. INSTALLED NEW EMERGENCY BATTER AT FWD LH POSITION. OPS CHECK GOOD. REF AMM TASK 33-51-38-000-002-A.
- [SDR CALA2024121201477](https://openairdocs.org/sdr/CALA2024121201477.md): Unknown · odor · Dec 10, 2024 · N895UA · Airbus A319132 · Air Distribution System
  > ACRID SMELL AFTER T/O IN FLIGHT DECK. UPDATING WITH SMOKE ODOR FORM PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-10-200-801-C1. NO ODOR SMOKE OR FUMES FOUND. PER TOMC REQUEST RAN ENGINE WITH PACKS AND CROSSBLEED. COULD NOT DUPLICATE FAULT. NO HISTORY AND CA
- [SDR CALA2024111501155](https://openairdocs.org/sdr/CALA2024111501155.md): Fuel Cap · missing · Nov 15, 2024 · N895UA · Airbus A319132 · Fuel Storage
  > PDA 2 RAMP REPORT FUEL CAP MISSING. INSP'D AREA, NO DAMAGE FOUND. CHAIN LANYARD MISSING WITH CAP. INSTALLED MISSING FUELING CAP, AND CHAIN LANYARD.PARTS USED: 1356545,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1356545 SN OFF 2121 CAP, COUPLING R OF
- [SDR CALA2024102900952](https://openairdocs.org/sdr/CALA2024102900952.md): Unknown · odor · Oct 26, 2024 · N895UA · Airbus A319132 · Air Distribution System
  > UNABLE TO OPERATE DUE TO LOGPAGE NUMBER 9672781 PILOT IN COMMAND: UNKNOWN.REFERENCE LOG PAGE: 9672781 DATE AND TIME: 25OCT24 19:46 (26OCT24 02:46Z) AIRCRAFT: 4895 FLIGHT: 1787FROM: DEN TO: OMA PILOT COMMENTS: DEN-OMA. GLUE FUME SMELL NO FURTHER MAINTENANCE ACT
- [SDR CALA2024040400973](https://openairdocs.org/sdr/CALA2024040400973.md): Unknown · fumes · Apr 2, 2024 · N895UA · Airbus A319132 · Air Distribution System
  > STRONG ELECT ODOR IN AFT CABIN EMERGENCY DECLARED.... CONTAMINATED AT LEVEL C AIR DUCT AND ECS AT LEVEL C. LOCAL FIRE DEPARTMENT PERFOMED A IINFERED TEST FOR HEAT AND CARBON MONOXIDE TEST. BOTH WERE NORMAL. CONTACT TOMC 847-700-9980. PERFORM AMM INSPECTION
- [SDR CALA2024011200083](https://openairdocs.org/sdr/CALA2024011200083.md): Unknown · unknown · Jan 10, 2024 · N895UA · Airbus A319132 · Cargo/Baggage Doors
  > AFT CARGO DOOR OPEN INDICATION ON TAKE OFF, NO LOSE OF CABIN PRESSURIZATION... ADJUSTED AFT CARGO DOOR BOTTOM SENSOR TARGET PER AMM 52-71-12--400 34WV OPS CHECK DOOR. NO FAULTS FOUND. NO LIGHT ON OPS CHECK PER 52-71-00-710-001.
- [SDR CALA2023121303635](https://openairdocs.org/sdr/CALA2023121303635.md): Lens · wrong part · Dec 7, 2023 · N895UA · Airbus A319132 · Lighting System
  > F/A SAYS EMER EXIT SIGN OVER ROW 1 - DOES NOTHAVE REQUIRED ARROW S REMOVED AND REPLACED CABIN ROW 1 OVERHEAD EXIT LENS.REF ASM 33-51-01-15G. INSPECTED LIGHT SHADE, CK''D INSTALLATION AND SECURITY REF GMM 09-10-05.
- [SDR CALA2023050101309](https://openairdocs.org/sdr/CALA2023050101309.md): Stringer · corroded · Apr 30, 2023 · N895UA · Airbus A319132 · Fuselage Structure (General)
  > AFT CARGO CORROSION FOUND ON UNDERFLOOR BAY STRINGER 43L IN BETW EEN FRAME 62-63. PERFORMED REPAIR AT AFT CARGO UNDER FLOOR BAY STR 43L BETWEEN FR AME 62-63 IAW A319 SRM 53-41-13-300-010.
- [SDR CALA2023040601049](https://openairdocs.org/sdr/CALA2023040601049.md): Fitting · cracked · Apr 5, 2023 · N895UA · Airbus A319132 · Fuselage Main, Frame
  > LH FRAME 16 #7 DOOR STOP, IB UPPER AND LOWER HOLES HAVE CRACK IND ICATIONS IN INTERCOSTAL LAYERS IN 6 OCLOCK DIRECTION AD2022-02-1 1 PER HAECO LCQ NR9294490/30490 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT L/H FR16 STOP #7 INTERCOSTAL IAW A319 EA 531
- [SDR CALA2023040601048](https://openairdocs.org/sdr/CALA2023040601048.md): Intercostal · cracked · Apr 5, 2023 · N895UA · Airbus A319132 · Fuselage Main, Frame
  > FR 16 RH #7 DOOR STOP, IB UPPER AND LOWER HOLES HAVE CRACK INDIC ATIONS IN INTERCOSTAL LAYERS. 9 OCLOCK IB DIRECTION AD 2022-02-1 1 PER HAECO LCQ NR 9294489/30489 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT R/H FR16 STOP #7 INTERCOSTAL IAW A319 EA 581
- [SDR CALA2021052400721](https://openairdocs.org/sdr/CALA2021052400721.md): Access Panel · missing · May 23, 2021 · N895UA · Airbus A319132 · Wing, Plate/Skin
  > UPON ARRIVAL TO FLL RIGHT WING ACCESS PANEL FOR SPOILER ACUATOR NUMBER 675GB IS MISSING.PANEL OUTBOAD OF WING UNDERSIDE REF IPC 57-51-05-25K. ITEM NUMBER 40 MFG PART NUMBER D5754600900900A. FOR INFO. FURTHER DETAILS AWAITED.
- [SDR CALA2019072901277](https://openairdocs.org/sdr/CALA2019072901277.md): Accelerometer · inoperative · Jul 29, 2019 · N895UA · Airbus A319132 · Flight Control System
  > AIRCRAFT CLIMBS UNLESS FORWARD PRESSURE IS KEPT ON STICK. NOT NORMAL SEE TSM TASK 27-30-00-810-853-A, PFR SHOWS ACCLRM 4 12CE4 FAILED. TOMC RECOMENDS REPLACING 12CE3 AND 12CE4 REMOVED #3 AND #4 FLIGHT CONTROL ACCELEROMETER 27-92-16 REPLACED BOTH FLT CONT ACCEL
- [SDR CALA2019062201034](https://openairdocs.org/sdr/CALA2019062201034.md): Shear Plate · corroded · Jun 20, 2019 · N895UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT SHEAR PLATE CORRODED BETWEEN FRAMES 69 - 70, STRINGER 23L. REMOVED & REPLACED THE AFT SHEAR PLATE IAW A31 9 51-42-11-001 P6 & 51-72-11-911-001 P 1-3.
- [SDR CALA2019062201033](https://openairdocs.org/sdr/CALA2019062201033.md): Shear Plate · corroded · Jun 20, 2019 · N895UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RIGHT AFT SHEAR PLATE CORRODED BETWEEN FRAMES 69 - 70, STRINGER 23R. REMOVED & REPLACED THE SHEAR PLATE IAW SRM 51-42-11-001 P.6 & 51-72-11-911-001 P1-3.
- [SDR CALA2017063002015](https://openairdocs.org/sdr/CALA2017063002015.md): Fitting · corroded · Jun 29, 2017 · N895UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL SUPPORT FITTTING BETWEEN FRAMES 56 - 57 HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED THE DOOR SILL FITTING IAW SRM 51-42-11-001, PARAGRAPH E, AND F.
- [SDR CALA2017063002013](https://openairdocs.org/sdr/CALA2017063002013.md): Panel · corroded · Jun 27, 2017 · N895UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY CORROSION HAS PREVIOUS GRINDED OUT IN SEVERAL AREAS FROM FRAME 58R TO 56R (COVER S HEET). REMOVED AND REPLACED AFT CARGO COMPARTMENT COVER SHEET FROM FRAME 55 TO FRAME 59 IAW A319 SRM 51-42-11-001 PARAGRAPH E AND F.

## 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 = 'N895UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N895UA/reports

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