# Service difficulty reports: N872UA

A list on [N872UA](https://openairdocs.org/aircraft/N872UA.md).

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

- [SDR CALA2026041015250](https://openairdocs.org/sdr/CALA2026041015250.md): Adapter · corroded · Apr 9, 2026 · N872UA · Airbus A319132 · Fuselage Main, Structure
  > VIASAT ADAPTER PLATE HAS MULTI AREAS OF CORROSION MARKED WITH YELLOW DOT. R & R VIASAT ADAPTER PLATE IAW AMM 44-30-02 AND AMM 44-31-02.
- [SDR CALA2026010812818](https://openairdocs.org/sdr/CALA2026010812818.md): Panel · delaminated · Jan 7, 2026 · N872UA · Airbus A319132 · Fuselage Main, Structure
  > PANEL 192AT DELAMINATION LOWER SURFACE EXPOSED DAMAGE DIMENSIONS ARE 3 INCHES LONG BY 1.5 INCHES WIDE. PIC INCLUDED. APPLIED TAPE PER SRM 51-75-12-911002 INSPECT TAPE EACH FLIGHT PERMANENT REPAIR WITHIN 30 DAYS ADD EMP:U116706 INFO: PAINT PEELING OFF. NO DAMGE
- [SDR CALA2025110510912](https://openairdocs.org/sdr/CALA2025110510912.md): Wire · damaged · Nov 5, 2025 · N872UA · Airbus A319132 · Light System Wiring
  > EMERGENCY ROW LIGHT AT SEAT 31C INOP DEFER. REPLACED LIGHT ASSY ON SEAT. NO HELP. MEL 3350C APPROVED, ONLY ONE LIGHT INOP DEFERRED. FOUND BLACK WIRE RUNNING TO THE EMERGENCY LIGHT AT ROW 31C BROKEN AND LAYING UNDER SEAT. WIRE NEEDS REPAIR. SECURED WIRE OUT
- [SDR CALA2025103110777](https://openairdocs.org/sdr/CALA2025103110777.md): Feeder Cable · arced · Oct 28, 2025 · N872UA · Airbus A319132 · Electrical Power System Wiring
  > GENERATOR 2 FAULT AFTER ENGINE START. COMPLIED WITH ECAM. MSG REMAINS. CREW RESET NO HELP. CREW COMPLIED WITH MEL IDG DISCONNECTED PRIOR TO CLEARING. FOUND ARCING ON IDG FEEDER CABLE FIREWALL CONNECTOR, TERMINAL C. REF AD2011-19-01 R1. CABLE REMAINS DIS
- [SDR CALA2025092609287](https://openairdocs.org/sdr/CALA2025092609287.md): Battery Pack · faulted · Sep 25, 2025 · N872UA · Airbus A319132 · Emergency Lighting
  > DURING CABIN EMERGENCY TEST, EPSU BATTERY FWD LEFT SHOWS, TRIED 4 TIMES, NO HELP, REPLACED BATTERY ON UNIT EPSU FWD LT ( FIN 10WL). REMOVAL & INSTALL OF THE BATTERY OF EMERGENCY POWER SUPPLY UNIT (EPSU) IAW TASK 33-51-38, OPS TEST OF THE EMERGENCY LIGHTS I
- [SDR CALA2025081807868](https://openairdocs.org/sdr/CALA2025081807868.md): Power Supply · faulted · Aug 14, 2025 · N872UA · Airbus A319132 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, EPSU AFT LEFT INT LOAD FAULT NOTED AND THREE AFT EXIT MARKERS DO NOT LIGHT UP. REMOVED AFT EPSU.INSTALLED SERVICEABLE CONDITION EPSU INTO AFT LOCATION. OPS CHECK SATISFACTORY AT THIS TIME. REF AIRBUS 319/320 AMM 33-51-38.
- [SDR CALA2025080507298](https://openairdocs.org/sdr/CALA2025080507298.md): Power Supply · faulted · Aug 3, 2025 · N872UA · Airbus A319132 · Emergency Lighting
  > EPSU UNIT EMER R FAULT REF AMM 33-51-38-400-001-A REMOVED AND REPLACED RIGHT OVERWING EXIT EPSU UNIT AND REPLACED EPSU BATTERY FAULT CLEARED OPS CHECKS GOOD.
- [SDR CALA2024121601529](https://openairdocs.org/sdr/CALA2024121601529.md): Power Supply · no test · Dec 14, 2024 · N872UA · Airbus A319132 · Emergency Lighting
  > UNIT FAULT EPSU RIGHT FOUND DURING EMERGENCY LIGHT TEST ACP TSM 33-51-00-810-801-A. FOUND RIGHT OVER WING DOOR EPSU BAD. REPLACED EPSU. REF AMM 33-51-38-400-001-A. OPERATIONAL TEST PASS.
- [SDR CALA2024060501706](https://openairdocs.org/sdr/CALA2024060501706.md): Shear Plate · cracked · May 23, 2024 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CABIN LH SIDE, SHEAR PLATE BETWEEN FR 69 AND FR 70 CRACKED. NO DOT () REMOVED AND REPLACED SHEAR PLATE P/N D5347112420200 REF. SRM 53- 41-17-01-A I.A.W. SRM 51-44-11 SRM 51-42-11 AND D5347418. EMP#: V940362 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT
- [SDR CALA2024060501708](https://openairdocs.org/sdr/CALA2024060501708.md): Floor Support · corroded · May 22, 2024 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT FR 66-69 Y1162 CORRODED AT HARDPOINTS () REMOVED CORROSION IAW SRM 51-74-00 L=0.800" W=0.300" D=0.060" FO MOBILE AT BFM ON NR#: 104028 UNDED TO BE OUT OF LIMITS IAW SRM 53-41-14-283-009. REMOVED AND REPLACED FLOOR BEAM Y1162 AT FR 68-69 IAW 51-42
- [SDR CALA2024060501707](https://openairdocs.org/sdr/CALA2024060501707.md): Floor Support · corroded · May 22, 2024 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FLOOR BEAM FR 64-68 Y512 CORRODED AT HARDPOINT AT FR66 () REMOVE CORROSION I.A.W SRM 51-74-00 L=1.28" D=0.031" FOUND TO BE 104027 OUT LIMIT I.A.W SRM 53-41-14-283. REMOVED AND REPLACED FLOOR BE AM I.A.W SRM 51-42-11 (T93872) SEE ATTACH FORM 44-0008.
- [SDR CALA2023112403461](https://openairdocs.org/sdr/CALA2023112403461.md): Flow Divider · inoperative · Nov 21, 2023 · N872UA · Airbus A319132 · APU Core Engine
  > ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN - APU. PHOTO MULTPLE HISTORY, FUEL CONTROL UNIT, ALREALY REPLASHED PREV. DEACTIVATED AND DEF PER MEL 4910B. MULTPLE HISTORY, FUEL CONTROL UNIT, ALREALY REPLASHED PREV. DEACTIVATED AND DEF PER MEL 49
- [SDR CALA2023030300609](https://openairdocs.org/sdr/CALA2023030300609.md): Hydraulic System · none · Mar 3, 2023 · N872UA · Airbus A319132 · Hydraulic Power System
  > ECAM CAUTION MESSAGE - B ELEC PUMP OVHT MESSAGE INOP - HYD PLUE HYD ELEC. PUMP P/B SW FAULT LT ILLUMINATED- CREW TURNED OFF C/B''S C12 OPENED AT PNL 49VU AND AB09 ON PNL 123VU PER AMM SW PER QRH. 29-12-51-000-001-A FOR BLUE HYD PUMP R&R. REMOVED AND REPLACED B
- [SDR CALA2023020100293](https://openairdocs.org/sdr/CALA2023020100293.md): Sensor · none · Feb 1, 2023 · N872UA · Airbus A319132 · Drag Control System
  > A/C LOST ALL ROLLSPOILERS DURING CLB LOCKING FOR DETAILS ON REPAIR CREW REPORTED ROLL WAS "SLUGGISH" ON CLIMB. ON APPROACH, ROLL SPOILER OPERATION RETURNED. UNLOCKING FOR SIGN OFF REPLACED AOA SENSOR P/N: C16291AB PER AMM 34-11-19-400-001-A. 40-0595-3-4206,QT
- [SDR CALA2022101402818](https://openairdocs.org/sdr/CALA2022101402818.md): None · missing · Oct 14, 2022 · N872UA · Airbus A300* · Aircraft Fuel System
  > PDA 2 FUEL CAP MISSING ADDED PICS ADDED PICS INSTALLED FUEL COUPLING CAP REF 28-11-43 TOMC NOTIFIED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1829128 SN OFF 7027 CAP, COUPLING R OFF 31-2825-9-0001 7027 ON 31-2825-9-0001 1836
- [SDR CALA2022080101935](https://openairdocs.org/sdr/CALA2022080101935.md): Fuel Cap · missing · Jul 31, 2022 · N872UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/01/22. ON ARRIVAL MEX FOUND MISSING REFUEL/DEFUEL COUPLING CAP. REPLACED MISSING CAP.
- [SDR CALA2021040600429](https://openairdocs.org/sdr/CALA2021040600429.md): Door Sill · damaged · Apr 5, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CGO DOOR SILL PLATE SURFACE 6EA ATT SCREW HOLE FOUND ELONGAT ED AT FR55A-FR59 STGR38 REF NON-ROUTINE NO.: 9429297, SPEC NO.A3NB-53-4-6179. AFT CGO DOOR SILL REPAIRED AS PER ECRA 5341-01239 REV A AND RELATED COVER SHEET, CONNECTION SHEET & FIT TINGS REPLA
- [SDR CALA2021040500426](https://openairdocs.org/sdr/CALA2021040500426.md): Battery · discharged · Apr 5, 2021 · N872UA · Airbus A319132 · Emergency Lighting
  > 10WL ESPU BATTERY FOUND LOW VOLTAGE REF NON-ROUTINE NO.: 9430735, REPLACED 10WL ESPU BATTERY & BITE CHEC K EPSU FOUND TEST ''OK'', REF TO AMM 33-51-38-000-002-A REV 110 & AMM 33-51-38-400-002 REV 110 AND AMM 33-51-00-710-001-A REV 110.
- [SDR CALA2021040500425](https://openairdocs.org/sdr/CALA2021040500425.md): Battery · discharged · Apr 5, 2021 · N872UA · Airbus A319132 · Emergency Lighting
  > 12WL ESPU BATTERY FOUND LOW VOLTAGE REF NON-ROUTINE NO.: 9430738, REPLACED 12WL ESPU BATTERY & BITE CHEC K ESPU FOUND TEST ''OK'', REF TO AMM 33-51-38-000-002-A REV 110 & AMM 33-51-38-400-002 REV 110 AND AMM 33-51-00-710-001-A REV 110.
- [SDR CALA2021040500424](https://openairdocs.org/sdr/CALA2021040500424.md): Door Sill · damaged · Apr 5, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CGO DOOR SILL PLATE SURFACE 6EA ATT SCREW HOLE FOUND ELONGAT ED AT FR55A-FR59 STGR38 REF NON-ROUTINE NO.: 9429297, ORIGINATED BY EMP V906550, SPEC NO.A3NB-53-4-6179. PERFORMED BY EMP V906550, AFT CGO DOOR SILL REPAIRED AS PER ECRA 5341-01239 REV A AND RELA
- [SDR CALA2021040500423](https://openairdocs.org/sdr/CALA2021040500423.md): Battery · discharged · Apr 5, 2021 · N872UA · Airbus A319132 · Emergency Lighting
  > 13WL ESPU BATTERY FOUND LOW VOLTAGE REFER NON-ROUTINE NO:9430739. REPLACED 13WL ESPU BATTERY & BITE CHECK E SPU FOUND TEST "OK" REF TO AMM 33-51-38-000-002-A REV.110 & AMM 33-51-38-400-002 REV.110 AND AMM 33-51-00-710-001-A REV.110.
- [SDR CALA2021040500422](https://openairdocs.org/sdr/CALA2021040500422.md): Battery · discharged · Apr 5, 2021 · N872UA · Airbus A319132 · Emergency Lighting
  > 11WL ESPU BATTERY FOUND LOW VOLTAGE REFER NON-ROUTINE NO:9430736. REPLACED 11WL ESPU BATTERY & BITE CHECK E SPU FOUND TEST "OK".REF TO AMM 33-51-38-000-002-A REV.110 & AMM 33-51-38-400-002 REV.110 AND AMM 33-51-002-710-001-A REV.110.
- [SDR CALA2021040100405](https://openairdocs.org/sdr/CALA2021040100405.md): Skin · cracked · Mar 30, 2021 · N872UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FUS AT TAIL CONE UPPER SURFACE FRAME 80 FOUND SKIN CRACK REF NON -ROUTINE NR.: 9429743, ORIGINATED BY EMP, SPEC NR: A3NB- 53-3-6145. PERFORMED BY EMP. THE FUS AT TAIL CONE UPPER SKIN (FR80 AREA) REPAIRED AS PER SRM 53-51-11-300-010 REV 135. RII BY TA768.
- [SDR CALA2021033000403](https://openairdocs.org/sdr/CALA2021033000403.md): Light · cracked · Mar 30, 2021 · N872UA · Airbus A319132 · Passenger/Crew Doors
  > LH EMERGENCY DOOR AREA LIGHT LOCK (70WL1) FOUND CRACKED REF NON ROUTINE NO.: 9429158, SPEC NO A3NB-05 -3-6170. LH EMERGENCY DOOR AREA LT 70WL1 REPLAC ED AS PER AMM 33-51-11-000-001-A REV 110 & AMM 33-51-11-400-001- A REV 110.
- [SDR CALA2021033000387](https://openairdocs.org/sdr/CALA2021033000387.md): Stringer · damaged · Mar 27, 2021 · N872UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CARRY OUT CHECK FWD CARGO STRINGER AT LOC. FR30-FR34, S41R, THE RESULT FOUND WITHOUT REPAIR RECORD (CURRENT R/T=0.064") REF NON- ROUTINE NO.: 9431172, ORIGINATED BY EMP V906550, REF TASK CARD J OB NO: TTN0405 - LOG 5788027. PERFORMED BY EMP V906550, FWD CARGO
- [SDR CALA2021033000381](https://openairdocs.org/sdr/CALA2021033000381.md): Stringer · damaged · Mar 26, 2021 · N872UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CARRY OUT NDT CHECK FWD CARGO STRINGER AT LOC FR29-FR34,S43L,THE RESULT FOUND OUT OF LIMIT ALLOWABLE DAMAGE AS PER SRM CURRENT R /T=0.031" REF NON-ROUTINE NO.9431190,ORIGINATED BY EMP V906550, REF TASK CARD JOB NO:TTN0553,LOG 5788027. PERFORMED BY EMP V906550,
- [SDR CALA2021032600380](https://openairdocs.org/sdr/CALA2021032600380.md): Stop Fitting · cracked · Mar 26, 2021 · N872UA · Airbus A319132 · Fuselage Main, Structure
  > CRACK SIGNAL ON A HOLE AT THE LOWER SIDE OF STOP FITTING AT LOC. FR68, REF ECRA 5100-03044, CSN INTERNAL REPAIR LIST, FIG.15, IT EM 12, REF NON-ROUTINE NO.: 9430350, ORIGINATED BY EMP V905987, LOG 5788027. PERFORMED BY EMP V902597, GVI ACCOMPLISHED WITH NIL FI
- [SDR CALA2021032600377](https://openairdocs.org/sdr/CALA2021032600377.md): Stringer · damaged · Mar 26, 2021 · N872UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CARRY OUT CHECK FWD CARGO STRINGER AT LOC. FR30-FR34, S41R, THE RESULT FOUND WITHOUT REPAIR RECORD (CURRENT R/T=0.064") REF NON- ROUTINE NO.: 9431172, ORIGINATED BY EMP V906550, REF TASK CARD J OB NO: TTN0405 - LOG 5788027. PERFORMED BY EMP V906550, FWD CARGO
- [SDR CALA2021032600376](https://openairdocs.org/sdr/CALA2021032600376.md): Stringer · out of limits · Mar 26, 2021 · N872UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CARRY OUT NDT CHECK FWD CARGO STRINGER AT LOC FR29-FR34,S43L,THE RESULT FOUND OUT OF LIMIT ALLOWABLE DAMAGE AS PER SRM CURRENT R /T=0.031" REF NON-ROUTINE NO.9431190,ORIGINATED BY EMP V906550, REF TASK CARD JOB NO:TTN0553,LOG 5788027. PERFORMED BY EMP V906550,
- [SDR CALA2021031900341](https://openairdocs.org/sdr/CALA2021031900341.md): Tail Cone · cracked · Mar 19, 2021 · N872UA · Airbus A319132 · Aerodynamic Fairings
  > FUS AT TAIL CONE UPPER SURFACE FRAME 80 FOUND SKIN CRACK REF NON -ROUTINE NO.: 9429743, SPEC NO: A3NB- 53-3-6145. PERFORMED BY EMP V905985, THE FUS AT TAIL CONE UPPER SKIN (FR80 AREA) REPAIRED AS PER SRM 53-51-11-300-010 REV 135.
- [SDR CALA2021031200316](https://openairdocs.org/sdr/CALA2021031200316.md): Door Sill · corroded · Mar 12, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN R2 DOOR SILL PANEL FOUND CORROSION AT FR68 REF NON-ROUTINE NO.: 9428433 - ORIGINATED BY EMP: V902597, SPEC NO: A3NB-53-3-6 187. PERFORMED BY EMP V902597, CABIN R2 DOOR SILL PANEL AT FR68 REPAI RED AS PER SRM 53-41-14-300-001 REV 135. RII BY TA377.
- [SDR CALA2021031000296](https://openairdocs.org/sdr/CALA2021031000296.md): Door Sill · corroded · Mar 10, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN R2 DOOR SILL PANEL FOUND CORROSION AT FR68 REF NON-ROUTINE NO.: 9428433, SPEC NO: A3NB-53-3-6 187. CABIN R2 DOOR SILL PANEL AT FR68 REPAI RED AS PER SRM 53-41-14-300-001 REV 135.
- [SDR CALA2021031000287](https://openairdocs.org/sdr/CALA2021031000287.md): Door Sill · corroded · Mar 9, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN L2 DOOR SILL PANEL FOUND CORROSION AT FR68 REF NON-ROUTINE NO.: 9428449, ORIGINATED BY EMP: V902597, SPEC NO.: A3NB-53-3-6 187. PERFORMED BY EMP V902597, CABIN L2 DOOR SILL PANEL FR68 REPAIR A S PER SRM 53-41-14-300-001 REV 135,RII BY TA729. THIS ITEM IS
- [SDR CALA2021030500261](https://openairdocs.org/sdr/CALA2021030500261.md): Panel · corroded · Mar 4, 2021 · N872UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN L2 DOOR SILL PANEL FOUND CORROSION AT FR68 REF NON-ROUTINE NO.: 9428449, ORIGINATED BY EMP: V902597, SPEC NO.: A3NB-53-3-6 187. PERFORMED BY EMP V902597, CABIN L2 DOOR SILL PANEL FR68 REPAIR A S PER SRM 53-41-14-300-001 REV 135,RII BY TA729.

## 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 = 'N872UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N872UA/reports

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