# Service difficulty reports: N871UA

A list on [N871UA](https://openairdocs.org/aircraft/N871UA.md).

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

- [SDR CALA2026042315650](https://openairdocs.org/sdr/CALA2026042315650.md): Skin · cracked · Apr 22, 2026 · N871UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > RIGHT FR 35 STR 30 HOLE 2 HAS CRACK INDICATION IN FWD SKIN LAYER, 70% S.H. AT 8 O CLOCK POSITION. UPDATED PERFORMED INTERIM REPAIR ON RH FR 35 STR 30 HOLE 2 IAW ECRA 5331-03188 PART 1 INTERIM REPAIR.
- [SDR CALA2026092319695](https://openairdocs.org/sdr/CALA2026092319695.md): Skin · cracked · Jan 10, 2026 · N871UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > FRAME 35, STR 30L, HOLE NR 2 HAD A CRACK INDICATION IN FWD & AFT SKINS LAYERS, 100 PERCENT S.H AT 4 AND 5 OCLOCK POSITION. ACCOMPLISHED AN INTERIM REPAIR IAW ECRA 5331-03189, PART 1.1.
- [SDR CALA2026010212595](https://openairdocs.org/sdr/CALA2026010212595.md): Stringer · corroded · Dec 27, 2025 · N871UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY CORROSION BETWEEN FR 57 & 58, S41L. REMOVED & REPLACED CORRODED S41L, FR 56 - 59, AFT CARGO IAW SRM 51-42-11 CAT A & SRM 51-72-11.
- [SDR CALA2026010212594](https://openairdocs.org/sdr/CALA2026010212594.md): Stringer · corroded · Dec 27, 2025 · N871UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT BULK CARGO COMP CORROSION BETWEEN FR 62 AND 63, STRINGER 42L. REMOVED & REPLACED CORRODED STGR 42L FR61-64 AT AFT CARGO IAW SRM 51-42-11 CAT A & SRM 51-72-11-911-001.
- [SDR CALA2026010212593](https://openairdocs.org/sdr/CALA2026010212593.md): Stringer · corroded · Dec 27, 2025 · N871UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT CORROSION BETWEEN FR 56 AND FR 57 AT STR 42L PER AAR LCQ N/R 9292875/28875. REMOVED & REPLACED CORRODED STGR 42L FR54-FR60 AT AFT CARGO IAW SRM 51-42-11 CAT A & SRM 51-72-11.
- [SDR CALA2025122912492](https://openairdocs.org/sdr/CALA2025122912492.md): Stringer · corroded · Dec 26, 2025 · N871UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT CORROSION BETWEEN FR 58 AND FR 59 AT STR 43L. REMOVED AND REPLACED STRINGER 43L FR 54.5 - FR 58.5 IAW SRM 51-42-11/001.
- [SDR CALA2025121912249](https://openairdocs.org/sdr/CALA2025121912249.md): Tie Down · corroded · Dec 16, 2025 · N871UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FWD CARGO TORSION BOX COVER HAS CORROSION UNDER TIE DOWN FITTINGS. R & R TORSION BOX COVER AT FWD CARGO IAW SRM 51-42-11/001.
- [SDR CALA2025121712181](https://openairdocs.org/sdr/CALA2025121712181.md): Skin · dented · Dec 14, 2025 · N871UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > TOOLING DAMAGE FOUND ON UPPER FUSELAGE RT SIDE JUST BELOW RUDDER AT FR80 - FR81 STGR 3R. PERFORMED DOUBLER REPAIR ON UPPER FUSEAGE RH SIDE JUST BELOW RUD DER AT FR80-FR81 STGR 3R IAW SRM 53-51-11-300-010 REPAIR IS A CAT A.
- [SDR CALA2025121512121](https://openairdocs.org/sdr/CALA2025121512121.md): Angle · cracked · Dec 13, 2025 · N871UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RH AFT TI-ANGLE IS CRACKED. REMOVED AND REPLACED TI-ANGLE AT FR42 RH STG 42RH IAW A319 SRM 5 1-72-11-911-001.
- [SDR CALA2025121112027](https://openairdocs.org/sdr/CALA2025121112027.md): Stringer · corroded · Dec 9, 2025 · N871UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT BULK CARGO BAY, CORROSION BETWEEN FR 59 & 60 S43R. REMOVED AND REPLACED S43R AT FR 59 TO 64 IN THE AFT BULK CARGO BAY IAW SRM 51-42-11/001.
- [SDR CALA2025120811889](https://openairdocs.org/sdr/CALA2025120811889.md): Web · corroded · Dec 5, 2025 · N871UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL AREA FLOOR WEB NEAR AFT GIRT BAR FITTING CORRODED FR68 S32L PERFORMED REPAIR ON L2 DOOR SILL AT FR68 IAW SRM 53-41-14-3 00-001. REPAIR IS 2 CAT A NO FUTHER ACTIONS REQUIRED.
- [SDR CALA2025120811883](https://openairdocs.org/sdr/CALA2025120811883.md): Web · corroded · Dec 5, 2025 · N871UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > DOOR SILL AREA, FLOOR WEB NEAR AFT GIRT BAR FITTING CORRODED. REMOVED DAMAGE AND R2 DOOR SILL AREA FLOOR WEB IAW SRM 53-41-14-300-001 CAT A.
- [SDR CALA2025120511811](https://openairdocs.org/sdr/CALA2025120511811.md): Floorbeam · corroded · Dec 4, 2025 · N871UA · Airbus A319132 · Fuselage Main, Floor Beam
  > AFT FLOORBEAM, FRAME 68 LT CORRODED. AFT FLOORBEAM REMOVED & REPLACED IAW SRM 51-4 2-11.
- [SDR CALA2025120511809](https://openairdocs.org/sdr/CALA2025120511809.md): Seat Track · corroded · Dec 4, 2025 · N871UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > Y-765 LT FR 64-70 SEAT TRACK CORRODED OUT OF LIMITS AT FR68. REMOVED & REPLACED THE SEAT TRACK IAW SRM 51-72 -11-911.
- [SDR CALA2025120211646](https://openairdocs.org/sdr/CALA2025120211646.md): Fitting · deformed · Nov 28, 2025 · N871UA · Airbus A319132 · Passenger/Crew Doors
  > R-2 DOOR FRAME AFT LOWER CORNER KNICKS & SCRATCHES. REMOVED AND REPLACED DISCREPANT R2 FR 68 CORNER FITTING IAW SRM 51-42-11-001.
- [SDR CALA2025112711528](https://openairdocs.org/sdr/CALA2025112711528.md): Seat Track · corroded · Nov 26, 2025 · N871UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LT +Y1292 BETWEEN FR35-39 HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK AT FR35-39 IAW SRM 51-42-11-001/51-72-11.
- [SDR CALA2025112711526](https://openairdocs.org/sdr/CALA2025112711526.md): Fitting · corroded · Nov 26, 2025 · N871UA · Airbus A319132 · Emergency Equipment
  > AFT FLOOR LT WEB AT FR 66 FWD OF GIRT BAR FITTING CORROSION. PERFORMED FITTING REPAIR AT FR 66 WEB FWD OF GIRT BAR IAW SRM 53-41-14-300-001.
- [SDR CALA2025111911332](https://openairdocs.org/sdr/CALA2025111911332.md): Floorbeam · corroded · Nov 12, 2025 · N871UA · Airbus A319132 · Fuselage Main, Floor Beam
  > AFT FLOORBEAM AT FR 68 RT CORROSION. REMOVED AND REPLACED AFT FLOORBEAM -Y1162, FRAME 68 RT IAW SRM 51-72-11-911.
- [SDR CALA2025101610177](https://openairdocs.org/sdr/CALA2025101610177.md): Slide · unserviceable · Oct 14, 2025 · N871UA · Airbus A319132 · Escape Slide
  > 2L DOOR SLIDE ARM LEVER DIFFICULT TO USE REMOVED SLIDE REQUEST INSPECTION DOOR 2 LEFT PART NUMBER VERIFY ON NEW SLIDE. ACP RII PART NUMBER VERIFICATION OF L2 SLIDE REF IPC 25-62-04-51 FIG. ITEM 10C. SLIDE RAFT PN D30665-709 SN L25765 IS OK TO INSTALL DOOR 2L.
- [SDR CALA2025090208384](https://openairdocs.org/sdr/CALA2025090208384.md): Engine · faulty · Aug 24, 2025 · N871UA · Airbus A319132 · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTED AT FLIGHT LEVEL 260 ENGINE 2 WAS HEAR TO HAVE AT LEAST 2 LOUD BANGS FOLLOWED BY THE ENGINE 2 STALL ECAM. FLIGHT ATTENDANTS REPORTED LOUD BANGING AS WELL. EXAMINE ENG 2 EXHAUST AND FOUND METAL PIECES PER TSM 75-30-00-810-828-B WILL REQUIRE
- [SDR CALA2025031802904](https://openairdocs.org/sdr/CALA2025031802904.md): Bottle · unknown · Mar 12, 2025 · N871UA · Airbus A319132 · Service Doors
  > INSTALLED SAFETY PIN IN DOOR 1R SLIDE BOTTLE. REMOVED AND STOWED SAFTETY PIN FROM DOOR 1R SLIDE BOTTLE. REF AMM 25-62-44-400.PARTS USED: 17-2562-3-0001,QTY:1 REMOVED AND STOWED SAFETY PIN FROM DOOR 1R SLIDE BOTTLE. REF AMM 25-62-44-400. ADD EMP:U414042 ACP
- [SDR CALA2025022702494](https://openairdocs.org/sdr/CALA2025022702494.md): Girt Bar · out of alignment · Feb 25, 2025 · N871UA · Airbus A319132 · Emergency Equipment
  > DOOR 2R CONTROL SHAFT LEVERS DO NOT ENGAGE CORRECTLY IN THE HOLES OF THE GIRT BAR DURING INITIAL SLIDE INSTALLATION. UPON LOWERING DOOR CONTROL HANDLE, GIRT BAR WILL MOVE INBOARD CAUSING MISALIGNMENT. REF. AMM 25-62-44/401 CONFIG 00 DOOR 2R, WITH SLIDE INSTALL
- [SDR CALA2025020302174](https://openairdocs.org/sdr/CALA2025020302174.md): Lanyard · broken · Jan 31, 2025 · N871UA · Airbus A319132 · Cabin Equipment/Furnishings
  > CORD HANGING UNDER BELLY AT LEFT PACK FOUND DOOR 195BB LANYARD BROKEN. REMOVED LANYARD. REQUEST NEF. OK TO APPLY MEL 2522FC....TOCM SMITH DDP COMPLIED WITH. INSTALLED LANYARD. THIS ACTION CLEARS THE NEF.
- [SDR CALA2024120301396](https://openairdocs.org/sdr/CALA2024120301396.md): Cap · missing · Dec 1, 2024 · N871UA · Airbus A319132 · Fuel Storage
  > PDA 2 FUEL COUPLING CAP MISSING ON ARRIVAL. NOTIFIED TOMC.REFER LP 3051957 FUEL CAP MISSING. INSTALLED REFUEL/DEFUEL COUPLING CAP REF AMM 28-25-41-400-005-A.
- [SDR CALA2024061700003](https://openairdocs.org/sdr/CALA2024061700003.md): Medical Kit · open · Jun 17, 2024 · N871UA · Airbus A319132 · Emergency Equipment
  > ENHANCED EMERGENCY MEDICAL KIT INSPECTION {A3NB-25-3-6260} - ENHANCED EMERGENCY MEDICAL KIT IS INCOMPLETE AND LESS THAN 160 DAYS (EXP OCT 2024) NIS AT MEX ENHANCED EMERGENCY MEDICAL KIT IS INCOMPLETE/INOPERATIVE REQUEST MEL OK TO APPLY MEL 2560AF FOR INCOMPLET
- [SDR CALA2023101803109](https://openairdocs.org/sdr/CALA2023101803109.md): Skin · damaged · Oct 4, 2023 · N871UA · Airbus A319132 · Trailing Edge Flaps
  > R/WING O/B FLAP TAILING EDGE, INBD OF FAIRING 632BB HAS SKIN THAT IS SEPERATED DOT 202-200 REPAIRED R/WING O/B FLAP T/E DAMAGED AREA 3.5"X 3.5" DISBOND IAW SRM 57-53-00-300-120 AND SRM 51-77-11-911-023 STA:ST ENGINEERIN G BFM
- [SDR CALA2022020400311](https://openairdocs.org/sdr/CALA2022020400311.md): Anchor Fitting · corroded · Feb 3, 2022 · N871UA · Airbus A319132 · Wing, Attach Fittings
  > RH ANCHORAGE FITTING IS PITTED ON TOP SIDE BETWEEN FITTING & BUS HING ON HAECO LCQ REF 9296023/44023 SPEC A3NB-32-3-6078. NR GENE RATED BY V892442 BUSHING AND REAMED TO REMOVE PITTING FINAL HOLE SIZE 4.172", REMOVED MATERIAL.024 AND FINAL LUG THICKNESS 1.468"
- [SDR CALA2022020100291](https://openairdocs.org/sdr/CALA2022020100291.md): Fitting · corroded · Feb 1, 2022 · N871UA · Airbus A319132 · Wing Structure
  > RH ANCHORAGE FITTING IS PITTED ON TOP SIDE BETWEEN FITTING & BUS HING ON HAECO LCQ REF 9296023/44023 SPEC A3NB-32-3-6078. NR GENE RATED BY V892442
- [SDR CALA2022020100290](https://openairdocs.org/sdr/CALA2022020100290.md): Fitting · corroded · Feb 1, 2022 · N871UA · Airbus A319132 · Wing Structure
  > L/H ANCHORAGE FITTING HAS PITTING CORROSION ON UPPER SURFACE BET WEEN FITTING CHAMFER & BUSHING SLEEVE ON HAECO LCQ REF 9296027/4 4027 SPEC A3NB-32-3-6078. NR GENERATED BY V892429 REMOVED & REPLACED LH ANCHORAGE FITTING IAW A319 SRM 57-26-13-30 0-026 AT HAECO

## 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 = 'N871UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N871UA/reports

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