# Service difficulty reports: N4888U

A list on [N4888U](https://openairdocs.org/aircraft/N4888U.md).

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

- [SDR CALA2025071406563](https://openairdocs.org/sdr/CALA2025071406563.md): Charger · faulted · Jul 13, 2025 · N4888U · Airbus A319132 · Battery/Charger System
  > WHILE PERFORMING STAR CHECK, BCL 1 AND BATTERY 1 FAULTS APPEARED. SMOKE SMELL IN COCKPIT, SMOKE COMING FROM BAT 1. FAULT FIR BAT 1 AND BCL 1 ON ECAM. R/R #1 MAIN BAT IAW AMM 24-38-51/401. R/R #1 BCL IAW AMM 24-38-34/401. NO FAULTS NOTED AT THIS TIME. A/C OK FO
- [SDR CALA2025051604718](https://openairdocs.org/sdr/CALA2025051604718.md): Warning Message · false activation · May 12, 2025 · N4888U · Airbus A319132 · Door Warning System
  > LVL-2 CHRONIC AFT CARGO DOOR ECAM IN FLT. AHM INDICATED THE AFT CGO DOOR POS SW TARGETS OUT OF RIG. PLS ADJ PROX SW 32WV, 34WV, 12MJ IAW AMM 52-71-00-820-003,004. INSPECT PROX SW FOR DAMAGE, RPL AS REQUIRED REF IPC 52-35-04-13A, 52-71-04-17. RECORD YOUR FINDIN
- [SDR CALA2024100702590](https://openairdocs.org/sdr/CALA2024100702590.md): Door Sill · corroded · Sep 25, 2024 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL AT FR 68 HAS CORROSION ON EXISTING REPAIR AND JUST O/B OF EXISTING REPAIR.
- [SDR CALA2024061001760](https://openairdocs.org/sdr/CALA2024061001760.md): Fuel Cap · missing · Jun 6, 2024 · N4888U · Airbus A319132 · Fuel Storage
  > PDA 1 FUEL CAP MISSING. REF LOGPQGE 8202050, FUEL CAP MISSING. REPLACED FUEL CAP.
- [SDR CALA2023112303454](https://openairdocs.org/sdr/CALA2023112303454.md): Sensor · dirty · Nov 21, 2023 · N4888U · Airbus A319132 · Passenger/Crew Doors
  > AFTER TAKEOFF THRUSTSET...ECAM - DOOR R AFT CABIN WOULD LIKE TO APPLY MEL 5270C WOULD LIKE TO APPLY MEL 5270A APPLIED MEL 5270A AND INSTALLED INOP STICKER DISPATCH DESK: 38 NAME: NF DATE: 21-NOV-23- MEL 5270A APPROVED. MEL 5270C USE 5270A. *DM* RECOMMEND TS
- [SDR CALA2023091802814](https://openairdocs.org/sdr/CALA2023091802814.md): Line · leaking · Sep 15, 2023 · N4888U · Airbus A319132 · Hydraulic System, Main
  > LEFT MAIN GEAR DOOR ACTUATOR HYD FLEX LINE LEAKING.LOCATION NEAR PROX SWITCH 33GA.SEE PICTURES. INSTALLED NEW LEFT MLG GEAR DOOR ACTUATOR HYD FLEX LINE (2763GM) IN REF. TO AMM 32-31-38. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME.
- [SDR CALA2023051501519](https://openairdocs.org/sdr/CALA2023051501519.md): Skin · damaged · May 14, 2023 · N4888U · Airbus A319132 · Trailing Edge Flaps
  > RIGHT WING IB FLAP BOTTOM SKIN HAS EXPOSED COMPOSITE PER HAECO L CQ NR 9292364/38364 GENERATED BY V921755 ACCOMPLISHED REPAIR PER HAECO REO - L24430 REV IR WITH NO DEVIAT ACCMP BY MECH V955356 INSP BY V916884 IONS NOTE: HAECO REO-L24430 REV IR IS INCLUDED WITH
- [SDR CALA2023051501501](https://openairdocs.org/sdr/CALA2023051501501.md): Skin · punctured · May 13, 2023 · N4888U · Airbus A319132 · Trailing Edge Flaps
  > RIGHT WING, INBRD FLAP CENTER BOX LOWER SKIN AT RIB 5 PUNCTURED. ORIGINAL LP4580291 CLOSED INADVERTENTLY. ACCOMPLISHED REPAIR PER HAECO REO - L24430 REV IR WITH NO DEVIAT IONS NOTE: HAECO REO-L24430 REV IR IS INCLUDED WITHIN ECRA AS FI GURES 1-14 FOR REFERENCE
- [SDR CALA2022051601257](https://openairdocs.org/sdr/CALA2022051601257.md): None · faulty · May 16, 2022 · N4888U · Airbus A319132 · Fuselage Structure (General)
  > 2000FT ON TAKEOFF AIRBLEED 1 FAUT FOLLOWEDBY AIR BLEED 2 FAULT.R ESET BLEEDS BUT BOTH LOCKED FOR POSITIVE FIX UNLOCKING FOR FIX POST FLIGHT REPORT FAULTED E1 PRESSURE REGULATOR VALVE (PRV) REMOVED & REPLACED REF AMM 36-11-52-400-010-B.PERFORMED POWER ASSURANCE
- [SDR CALA2022011800180](https://openairdocs.org/sdr/CALA2022011800180.md): Fuel Cap · missing · Jan 18, 2022 · N4888U · Airbus A319132 · Aircraft Fuel System
  > PDA 2 REDFUEL CAP MISSING APON ARRIVAL IAH FLT 2227 DEFERAL REQUESTED CDL 28A ALREADY ON CDL7833343 MISSING CAP REFERENCED IN LOG PAGE 7833343
- [SDR CALA2021101401885](https://openairdocs.org/sdr/CALA2021101401885.md): None · none · Oct 14, 2021 · N4888U · Airbus A319132 · Landing Gear Brake System
  > HOT BRAKES DUE TO RTO APPLIED COOLING FANS IAW MT 32-10 AND JNSPECTED BRAKES IAW AMM 32-40-00, NO DEFECTS NOTED. OKAY FOR SERVICE.
- [SDR CALA2019120762142](https://openairdocs.org/sdr/CALA2019120762142.md): Fuel Cap · missing · Dec 3, 2019 · N4888U · Airbus A319132 · Fuel Storage
  > PDA 2 FUELER REPORTED FUEL CAP MISSING ON ARRIVAL FUEL CAP MISSING. NO LEAKS NOTED REQUEST CDL DISPATCH DESK: 29 NAME: PA APPROVED FOR CDL 28A C/W DDP PLACED ON CDL 28A
- [SDR CALA2018030800862](https://openairdocs.org/sdr/CALA2018030800862.md): Skin · dented · Mar 6, 2018 · N4888U · Airbus A319132 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ON THE REAR SKIN OF THE TAIL ZONE ACCESS PANEL BETWEEN FRAMES 73 - 74, STRINGERS 26 - 27R. REMOVED AND REPLACED THE PREVIOUS REPAIR IAW SR M 53-00-11-300-015.
- [SDR CALA2018021700673](https://openairdocs.org/sdr/CALA2018021700673.md): Door Sill · corroded · Feb 17, 2018 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY, FORWARD CARGO DOOR SILL FOUND CORRODED, FRAMES 24A - 28. REMOVED AND REPLACED THE FWD CARGO DOOR SILL IAW SRM 51-4 2-11, PARA 2.D, 2.E, AND 2.F.
- [SDR CALA2018021600638](https://openairdocs.org/sdr/CALA2018021600638.md): Shear Tie · corroded · Feb 13, 2018 · N4888U · Airbus A319132 · Fuselage Internal Mounting Structure
  > FORWARD CARGO BAY, CORROSION ON THE SHEAR TIE AT FORWARD FACE OF FRAME 29, FOUND TO BE OUT OF LIMITS IAW 51-73-11-001. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.
- [SDR CALA2018021600637](https://openairdocs.org/sdr/CALA2018021600637.md): Shear Tie · corroded · Feb 13, 2018 · N4888U · Airbus A319132 · Fuselage Internal Mounting Structure
  > CORROSION ON THE SHEAR TIE AT FORWARD FACE OF FRAME 29, FOUND OUT OF LIMITS IAW 51-73-11-001. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11-911-001.
- [SDR CALA2018021100593](https://openairdocs.org/sdr/CALA2018021100593.md): Door Sill · corroded · Feb 11, 2018 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CABIN L2 DOOR STILL AT FRAME 68 HAS SPOT OF CORROSION ON FASTENER HOLE. INSTALLED REPAIR AT AFT CABIN L2 DOOR SILL FR68 IB NUTPLATE AREA IAW SRM 53-41-14-300-001 FIG 20101.
- [SDR CALA2018020900521](https://openairdocs.org/sdr/CALA2018020900521.md): Fitting · corroded · Feb 9, 2018 · N4888U · Airbus A319132 · Fuselage Main, Attach Fittings
  > R2 DOOR, FRAME 66 LOWER FWD CORNER FITTING HAS CORROSION. REMOVED AND REPLACED THE FITTING IAW 51- 42-11-001, PAR 2 E AND 2F.
- [SDR CALA2018020900520](https://openairdocs.org/sdr/CALA2018020900520.md): Threshold · corroded · Feb 9, 2018 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO THRESHOLD COVER HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-283-003. REMOVED AND REPLACED THE THRESHOLD IAW SRM 51-42-11-001.
- [SDR CALA2018020500493](https://openairdocs.org/sdr/CALA2018020500493.md): Door Sill · corroded · Feb 5, 2018 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CABIN R2 DOOR SILL AT FRAME 68 HAS SPOT OF CORROSION. REPAIRED AFT CABIN R2 DOOR SILL AT FRAM 68 IAW SRM 53-41-14 -300-001 PAR 2.A REPAIR PRINCIPLE 7 FIG 20101.
- [SDR CALA2018020400472](https://openairdocs.org/sdr/CALA2018020400472.md): Fitting · corroded · Feb 4, 2018 · N4888U · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FR 68 AFT CORNER FITTING HAS CORROSION. REMOVED AND REPLACED R-2 DOOR SILL AFT CORNER FITTING AT FR-68 P N D5348004220702 PO NR1038193.6 IAW SRM 51-72-11-911-001.

## 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 = 'N4888U' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N4888U/reports

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