# Service difficulty reports: N892UA

A list on [N892UA](https://openairdocs.org/aircraft/N892UA.md).

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

- [SDR CALA2025102210413](https://openairdocs.org/sdr/CALA2025102210413.md): Fuel Cap · missing · Oct 21, 2025 · N892UA · Airbus A319132 · Fuel Storage
  > AC ARRIVED IN ORD WITH FUEL CAP ASSY MISSING.
- [SDR CALA2025101309936](https://openairdocs.org/sdr/CALA2025101309936.md): Door · no discrepancy · Oct 12, 2025 · N892UA · Airbus A319132 · Emergency Exits
  > REMOVED RIGHT EMERGENCY EXIT HATCH SEAT 21F REF AMM 52-21-11 REPLACED EMERGENCY EXIT HATCH SEAL AT DOOR 21F REF AMM 52-21-18-960-003-A, NO DEFECTS FOUND. REINSTALLED HATCH AT 21F REF AMM 52-21-11-400-001-A, NO DEFECTS NOTED. PERFORMED CABIN PRESSURIZATION REF
- [SDR CALA2025092209081](https://openairdocs.org/sdr/CALA2025092209081.md): Battery Pack · no test · Sep 20, 2025 · N892UA · Airbus A319132 · Emergency Lighting
  > PROCEDURE - EPSU FWD BATTERY FAULT FOUND ON EMERGENCY LIGHTING CHECK. R & R FWD EPSU BATTERY ABOVE FWD ENTRY DOOR. REF: AMM TASK 33-51-38-000-002-A & TASK 33-51-38-400-002-A. OP CHECK GOOD, NO MORE FAULTS SHOWING ON TEST.
- [SDR CALA2025090908662](https://openairdocs.org/sdr/CALA2025090908662.md): Oxygen Panel · unsecure · Sep 5, 2025 · N892UA · Airbus A319132 · Passenger Oxygen System
  > 2R OXYGEN MASK AT FA STATION AFT FALLING DOWN, MASK STILL IN COMARTMENT, SECURED PANEL AT 2R O2 AT FA STATION. MASK DID NOT FALL OUT, PANEL WAS NOT SEATED PROPERLY. REF AMM 35-20-00
- [SDR CALA2025082708186](https://openairdocs.org/sdr/CALA2025082708186.md): Tape · unsecure · Aug 24, 2025 · N892UA · Airbus A319132 · Wing Structure
  > FA REPORTS ABNORMALLY LO UD WHISTLE FROM RIGHT OV ERWING EXIT. SECURED LOOSE TAPE ON RIGHT WING.
- [SDR CALA2025021702338](https://openairdocs.org/sdr/CALA2025021702338.md): Warning Message · false activation · Feb 17, 2025 · N892UA · Airbus A319132 · Door Warning System
  > AFT CARGO DOOR OPEN INDICATION ON CLIMB. CRW REPORTED NORMAL INDICATIONS RETURNED AFTER LANDING. ACCOMPLISHED OPERATIONAL CHECK OF AFT CARGO DOOR PER AMM TASK 52-32-00-710-001-A NO DEFECTS NOTED. CHECKED SENSOR 32WV AND CONNECTOR FOR DEFECTS NONE NOTED.
- [SDR CALA2025021100332](https://openairdocs.org/sdr/CALA2025021100332.md): Scuff Plate · worn · Feb 8, 2025 · N892UA · Airbus A319132 · Nacelle/Pylon, Plate/Skin
  > #1 PYLON BOTTOM SCUFF PLATE AFT OF AFT ENGINE MOUNT HAS WEAR PER HAECO LCQ N/R 9294185/42185. RMVD AND RPLD SCUFF PLATE AFT OF AFT ENGINE MOUNT ON #1 PYLON IAW A319 SRM 54-51-12-300-003 THIS REPAIR REQ SRI EVERY 4900FC 1200FH FROM EMBODIMENT SUBSEQUENT INSP A
- [SDR CALA2025020200262](https://openairdocs.org/sdr/CALA2025020200262.md): Angle · cracked · Jan 31, 2025 · N892UA · Airbus A319132 · Aerodynamic Fairings
  > LH SIDE VERTICAL WING TO BODY STRUCTURE BRACKET IS CRACKED PER HAECO LCQ N/R 9294125/42125 GEN BY V918855
- [SDR CALA2025010601780](https://openairdocs.org/sdr/CALA2025010601780.md): Power Supply · faulted · Jan 3, 2025 · N892UA · Airbus A319132 · Emergency Lighting
  > RIGHT EMERGENCY POWER SUPPLY BATTERY 12WL REQUIRES REPLACEMENT. REPLACED POWER SUPPLY AND BATTERY REF AMM 33-51-38. TESTED NORMAL.PARTS USED: 18-3351-3-0001,QTY:1 31-3350-9-9001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1835569 SN OFF 8208 IPC REFERE
- [SDR CALA2025010300022](https://openairdocs.org/sdr/CALA2025010300022.md): Power Supply · no test · Jan 3, 2025 · N892UA · Airbus A319132 · Emergency Lighting
  > AFT LEFT 13WL EMERGENCY POWER SUPPLY REQUIRES REPLACEMENT. REMOVED AND REPLACED POWER SUPPLY PER REF AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2025010601797](https://openairdocs.org/sdr/CALA2025010601797.md): Power Supply · not reported · Jan 2, 2025 · N892UA · Airbus A319132 · Emergency Lighting
  > AFT LEFT 13WL EMERGENCY POWER SUPPLY REQUIRES REPLACEMENT PART INFO UPDATED REMOVED AND REPLACED POWER SUPPLY PER REF AMM 33-51-38 OPS CHECK GOOD
- [SDR CALA2024120201380](https://openairdocs.org/sdr/CALA2024120201380.md): Hydraulic Line · leaking · Dec 2, 2024 · N892UA · Airbus A319132 · Hydraulic System, Main
  > CREW REPORTED LOST YELLOW HYDRAULIC SYSTEM. YELLOW HYD QTY SHOWING ZERO ON HYD PAGE REF LP 3046594 FOR WORK PERFORMED Y HYD RSVR LO LVL COMPLETE FLUID LOSS OPENING AND COLLARING C/BS FOR YELLOW PUMP AND CARGO DOORS. AB03 AB06 AND T12 BREAKERS OPENED. FOUND HYD
- [SDR CALA2024073100337](https://openairdocs.org/sdr/CALA2024073100337.md): Cids · faulted · Jul 28, 2024 · N892UA · Airbus A319132 · Communications System
  > CIDS RESET INFLIGHT FOLLOWED 319 SYS RESET IN FM OPS NOW NORMAL RAN CIDS BITE CHECK THROUGH BOTH FA PANEL AND MCDU REFER AMM 23-73-00-740-005-A ALL TEST OK NO C/B TRIPPED DUE TO HISTORY RAN CIDS FUNC TEST OPS REFER AMM 23-73-00-720-006-A CHECK GOOD NO FAULT NO
- [SDR CALA2024050601328](https://openairdocs.org/sdr/CALA2024050601328.md): Fuel Cap · missing · May 3, 2024 · N892UA · Airbus A319132 · Fuel Storage
  > PDA 2 CAP, COUPLING REFUEL UNDER WING - REPORTED MISSING BY FUEL VENDOR. FUEL CAP IS ON AIRCRAFT FUEL CAP LANYARD IS BROKEN,REPLACED FUEL CAP LANDARD. SEE PHOTOS
- [SDR CALA2024042601244](https://openairdocs.org/sdr/CALA2024042601244.md): Pump · faulted · Apr 23, 2024 · N892UA · Airbus A319132 · Hydraulic Pump (Electric/Engine), Main
  > HYD G RSVR OVHTIN CLIMB. FOLLOWED ECAM SLIGHTLY DECREASED AND FAULT LIGHT EXTINGUISHED BUT ECAM MESSAGE ALONG WITH OVERHEAT WARNING ON HYDROLIC PAGE ON LOWER ECAM WITH REMAINED. ABOUT 15 MINUTES BEFORE TOUCHDOWN, THEY TURNED LEFT FAULT INDICATIONS ON ENG 1 PUM
- [SDR CALA2024042401214](https://openairdocs.org/sdr/CALA2024042401214.md): Transducer · overheated · Apr 21, 2024 · N892UA · Airbus A319132 · Hydraulic System, Main
  > G RSVR OVHT DISPLAYED ON UPPER ECAM SCREEN. - HYD RAN ECAM PROC..OVHT WENT OUT AFTR 10 MINS RECOVERD GRN HYD SYS.. OPS NRML CONSISTENTLY. PERFORMED #2 ENG DRY MOTOR, GREEN INDICATION FLUCTUATED BETWEEN 2450-2700 PSI AND YELLOW PRESSURE MAINTAINED AROUND 2900 P
- [SDR CALA2024040300969](https://openairdocs.org/sdr/CALA2024040300969.md): Repair · inadequate · Apr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > CONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH REF LOG PAGE 7270995 AND ECRA 5330-07 208 PER HAECO LCQ NR 9298002/22002. CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL
- [SDR CALA2024040300968](https://openairdocs.org/sdr/CALA2024040300968.md): Stiffener · cracked · Apr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, Structure
  > UPON INSTALL OF R/H LATERAL SKIN PANEL FOUND SKIN STIFFENER AT L OWER LAP JOINT FR1-2 TO HAVE CRACK AT AFT END. REMOVED AND INSTALLED NEW R/H LATERAL SKIN PANEL SKIN STIFFENER AT LOWER LAP JOINT FR1-2 AS PER A319 SRM 51-42-11.
- [SDR CALA2024040300963](https://openairdocs.org/sdr/CALA2024040300963.md): Repair · inadequate · Apr 2, 2024 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > CONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL FROM FR 1 - FR 12 PN D531100752010 3 STEP 6 OF ECRA INSTRUCTS TO CLOSE DIP
- [SDR CALA2023031700770](https://openairdocs.org/sdr/CALA2023031700770.md): Unknown · corroded · Mar 15, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > AFT CARGO PIT L/H FR64 BETWEEN STRINGERS 43L-44 HAS CORROSION ON SKIN DOUBLER (A3NB-53-4-6179). GENERATED BY V919150 AT HAECO LC Q PER NR 9298610 (20610). 5341-01376. WORK ACCOMPLISHED BY LCQ EMP V932428. ACCOMPLISH PER PART 2 OF LATEST REVISION OF EC/RA 5341-
- [SDR CALA2023031300708](https://openairdocs.org/sdr/CALA2023031300708.md): Stop · cracked · Mar 10, 2023 · N892UA · Airbus A319132 · Fuselage Main, Structure
  > FR 68 RH DOOR STOP #1 LOWER IB HOLE HAS CRACK INDICATION IN FRAM E LAYER 6 O''CLOCK DIRECTION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9298588/20588 REAMED FREEZE PLUG TO.2820" PER SRM 53-41-12-300-011. REAMED 5340-01734 STEP 9. PER SRI 53-41-12-205-010 INSPECTI
- [SDR CALA2023031000684](https://openairdocs.org/sdr/CALA2023031000684.md): Stop · cracked · Mar 10, 2023 · N892UA · Airbus A319132 · Fuselage Main, Structure
  > FR 68 RH DOOR STOP #1 LOWER IB HOLE HAS CRACK INDICATION IN FRAM E LAYER 6 O''CLOCK DIRECTION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9298588/20588 REAMED FREEZE PLUG TO.2820" PER SRM 53-41-12-300-011. REAMED 5340-01734 STEP 9. PER SRI 53-41-12-205-010 INSPECTI
- [SDR CALA2023022700557](https://openairdocs.org/sdr/CALA2023022700557.md): Nut Plate · corroded · Feb 25, 2023 · N892UA · Airbus A319132 · Fuselage Main, Frame
  > FR68 LH FWD FACE AT NUT PLATE HOLE HAS CORROSION PER HAECO LCQ N R 9298794/20794 GENERATED BY V061680 SPEC: A3NB-53-3-6222. =.030", REM''ING MTL =.068", MAX ALLOWABLE REM''ING MTL =.050", HFEC AND ROTO INSPECTED AREA AND NUT PLATE HOLE IAW 51-10-08 REPAIR F
- [SDR CALA2023022700551](https://openairdocs.org/sdr/CALA2023022700551.md): Plate · corroded · Feb 24, 2023 · N892UA · Airbus A319132 · Fuselage Main, Floor Beam
  > AFT WET AREA L2 DOOR SILL PLATE AFT CORNER HAS CORROSION FR68-68 PER HAECO LCQ NR 9298668/20668 GENERATED BY V926223 SPEC: A3NB-5 3-3-6222 RMVD AND RPLD AFT WET AREA L2 DOOR SILL IAW UAL SRM 51-72-11 BY MECH V061742 INSP BY V061334
- [SDR CALA2023022700550](https://openairdocs.org/sdr/CALA2023022700550.md): Door Sill · corroded · Feb 24, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR SILL HAS CORROSION SPOTS ON UPPER SURFACE GENERAT ED AT HAECO LCQ PER NR 9298573 (20573) BY V919150. {A3NB-53-3-61 05} REMOVED AND REPLACED FWD CARGO DOOR SILL IAW A319 SRM 51-42-11-0 01. TREATED, PRIMED, AND TOP COAT AREA IAW A319 SRM 51-23-11-
- [SDR CALA2023022400527](https://openairdocs.org/sdr/CALA2023022400527.md): Plate · corroded · Feb 22, 2023 · N892UA · Airbus A319132 · Fuselage Main, Floor Beam
  > AFT WET AREA R-2 DOOR SILL PLATE HAS CORROSION FWD END FR 66-68 PER HAECO LCQ NR 9298673/20673 GENERATED BY V926223 SPEC: A3NB-5 3-3-6222. REPAIRED R-2 DOOR SILL PLATE IAW 53-41-14-300-001 ADD EMP:V940814 REPAIRED R-2 DOOR SILL PLATE IAW 53-41-14-300-001
- [SDR CALA2023022400526](https://openairdocs.org/sdr/CALA2023022400526.md): None · cracked · Feb 22, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > R/H OVERWING EMERGENCY EXIT HAS CRACK AT INNER BOTTOM ANGLE-WEB PER HAECO LCQ NR 9298411/20411 SPEC: A3NB-05-3-6168. GENERATED B Y V919150. REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT INNER, BOTTOM ANGLE-WEB IAW SRM 51-42-11 AND DWG# 0522-79010 ADD EMP:V9
- [SDR CALA2023021600446](https://openairdocs.org/sdr/CALA2023021600446.md): None · corroded · Feb 15, 2023 · N892UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR26 BETWEEN STRINGERS 41R-42R CLEAT HAS CORROSION DOT M067. PER HAECO LCQ NONROUTINE 9298576/20576. GENERATED BY V919150. SPEC: A3NB-53-3-6105. FOUND CLEAT CORRODED AT FR26 BETWEEN STRINGERS 41R-42R TO BE OUT IAW A319 SRM 51-44-11/001A AND I
- [SDR CALA2023020100282](https://openairdocs.org/sdr/CALA2023020100282.md): Intercostal · none · Jan 31, 2023 · N892UA · Airbus A319132 · Fuselage Main, Frame
  > AD RELATED TASK (2022-02-11) RH FR16 DOOR STOP #7 INBD LOWER HOL E, #3. HAS A CRACK INDICATION IN THE INTERCOSTAL LAYER AT 6 O;CL OCK POSITION, REPAIRE BEFORE NEXT FLIGHT PER HAECO LCQ NR 929845 2/20452 GENERATED BY V061671. REMOVED AND REPLACED FR16 R/H #7 IN
- [SDR CALA2019021700256](https://openairdocs.org/sdr/CALA2019021700256.md): Angle · cracked · Feb 14, 2019 · N892UA · Airbus A319132 · Emergency Exits
  > RH EMERGENCY EXIT HATCH FORWARD LOWER SEGMENT 1 IS CRACKED 16TH FASTENER FROM TOP =.110" LONG A3NB-52-3-6096 PER HAECO LCQ NR 9 296229 GENERATED BY V061633 REMOVED AND REPLACED DISCREPENT FRAME ANGLE ON R/H EMERGENCY EXI T HATCH AT FWD LOWER SEGMENT IAW A319
- [SDR CALA2019021700255](https://openairdocs.org/sdr/CALA2019021700255.md): Angle · cracked · Feb 14, 2019 · N892UA · Airbus A319132 · Emergency Exits
  > LH EMERGENCY EXIT HATCH FORWARD LOWER SEGMENT 1 IS CRACKED 15TH, 16TH AND 17TH FASTENER FROM TOP =.5" LONG AND AFT LOWER SEGMEN T 1 IS CRACKED AT 17TH FASTENER FROM TOP =.0250" LONG A3NB-52-3 -6096 PER HAECO LCQ NR 9296228 GENERATED BY V061633 REMOVED AND RE
- [SDR CALA2017032700739](https://openairdocs.org/sdr/CALA2017032700739.md): Threshold · cracked · Mar 27, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT PIT THRESHOLD CRACKED AT FASTENER HOLE BETWEEN FR57-FR58. REMOVED AND REPLACED THRESHOLD PLATE IAW SRM 51-42-11.
- [SDR CALA2017032700738](https://openairdocs.org/sdr/CALA2017032700738.md): Plate · corroded · Mar 27, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CORROSION IN AFT CARGO DOORWAY AT FS 58 AROUND TIE DOWN. REMOVED AND REPLACED WEB SEAT PLATE AND SPLICER PLATE IAW SRM 51-42-11.
- [SDR CALA2017032600729](https://openairdocs.org/sdr/CALA2017032600729.md): Floor Support · corroded · Mar 26, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT AT FR59 H AS ELONGATED HOLE & CORROSION. REMOVED DAMAGE & REPLACED FLOOR SUPPORT AREA AT FR59 IAW TD18027 8508/006/2017 NR A.
- [SDR CALA2017032500725](https://openairdocs.org/sdr/CALA2017032500725.md): Structure · corroded · Mar 25, 2017 · N892UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CORROSION AT R2 DOOR SILL AREA FR 65-66. REPAIRED CORROSION ON R2 DOOR SILL AREA FR65-66 IAW A319 SRM 53- 41-14 FIG 201 & PARA 5A.

## 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 = 'N892UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N892UA/reports

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