# Service difficulty reports: N1902U

A list on [N1902U](https://openairdocs.org/aircraft/N1902U.md).

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

- [SDR CALA2026062917383](https://openairdocs.org/sdr/CALA2026062917383.md): Fuel Cap · missing · Jun 24, 2026 · N1902U · Airbus A320232 · Fuel Storage
  > MISSING FUEL CAP, INSTALLED FUEL CAP ASSY IAW AMM 28-25-41.
- [SDR CALA2026012913427](https://openairdocs.org/sdr/CALA2026012913427.md): Hydraulic System · low pressure · Jan 18, 2026 · N1902U · Airbus A320232 · Hydraulic System, Main
  > ECAM HYD G SYS LO PR W/ PTU FAULT LIGHT ALL SYSTEM OPS NORMAL ON ARRIVAL TO ACFT FOUND GREEN HYD PSI INDICATION AT 1800 PSI WITH SYSTEM OFF. GREEN HYD LEAK MEASUREMENT SWITCH WAS SELECTED. TURNED OFF LEAK MEASUREMENT SWITCH. ALL INDICATIONS RETURNED TO NORMA
- [SDR CALA2025110510914](https://openairdocs.org/sdr/CALA2025110510914.md): Slide · no discrepancy · Nov 5, 2025 · N1902U · Airbus A320232 · Standard Practices/Structures
  > DISARM THE OVERWING DOORS OFF-WING ESCAPE SYSTEM. REF. EA 5100-01711 REV AB STEP 2.A.7. TRANSFER REF. NON-ROUTINE 7017956 REARMED OVERWING DOORS PER A320 AMM 52-21-10
- [SDR CALA2025101510131](https://openairdocs.org/sdr/CALA2025101510131.md): Access Panel · missing · Oct 14, 2025 · N1902U · Airbus A320232 · Wing, Plate/Skin
  > FOUND RT UPPER TRAILING EDGE ACCESS PANEL MISSING. INSTALLED ACCESS PANEL IAW IPC 57-51-05-67P.
- [SDR CALA2025041703924](https://openairdocs.org/sdr/CALA2025041703924.md): Cover · unsecure · Apr 15, 2025 · N1902U · Airbus A320232 · Emergency Exits
  > INTERMITTEN LEFT EMERG OVERWING EXIT L2 ECAM CLEARED ON OWN CHECKED AND SECURED DOOR HANDLE COVER, FOLLOWED AMM 05-51-88 WHILE PERFORMING MAINTENANCE.
- [SDR CALA2025041703919](https://openairdocs.org/sdr/CALA2025041703919.md): Target · out of adjust · Apr 15, 2025 · N1902U · Airbus A320232 · Door Warning System
  > LVL 1 DUE TO HISTORY OF LEFT EMERG OVERWING EXIT L-2 ECAM REF. L/PS 4515069, 4507296, 4381132, & 4275868. ACP TSM 52-21-00-810-802-A AND CORRECT FAULTS. IF NO FAULTS REPLACE PROX SW-HANDLE FLAP, L AFT EMER EXIT (21WV1) PER 52-71-13/401 AS PRECAUTION. UPDATE LO
- [SDR CALA2025040803619](https://openairdocs.org/sdr/CALA2025040803619.md): Proximity Sensor · misaligned · Apr 4, 2025 · N1902U · Airbus A320232 · Door Warning System
  > DOOR L AFT EMER EXIT ECAM IN FLIGHT PRESSURIZATION NORM REPEAT W RITE UP FOUND PROX SENSOR TARGET ON HANDLE COVER MISALIGNED. AJUSTED PROX SENSOR TARGET. OPS CHECK GOOD. ECAM INDICATION EXTINGUISHED. REF AMM 52-21-00
- [SDR CALA2025040303483](https://openairdocs.org/sdr/CALA2025040303483.md): Cover · detached · Mar 31, 2025 · N1902U · Airbus A320232 · Emergency Exits
  > DOOR L AFT EMER EXIT ECAM DUE TO COVER FALLING OFF PRESSURIZATIO N NORM VERIFIED ECAM MESSAGE DISPLAYS WHEN LEFT HAMD AFT EMERGENCY EXIT COVER IS REMOVED AND DISAPPEARS WHEN COVER IS INSTALLED. RE-INSTALLED COVER AND SECURED. NO FAULTS NOTED AT THIS TIME.
- [SDR CALA2025022600452](https://openairdocs.org/sdr/CALA2025022600452.md): Skin · corroded · Feb 25, 2025 · N1902U · Airbus A320232 · Wing, Plate/Skin
  > L/H WING UPPER SURFACE CORROSION AT SKIN APROX 3 INCHES FWD OF I /B FWD CORNER OF #1 SPOILER.
- [SDR CALA2025022400406](https://openairdocs.org/sdr/CALA2025022400406.md): Stringer · corroded · Feb 20, 2025 · N1902U · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMP STR 41R CORRODED BETWEEN FR 58 AND FR 59. ACCOMPLISHED REPAIR ON AFT CARGO COMP STR 41R BETWEEN FR 58 AND FR 59 PER HAECO REO-L25363 REV IR WITH NO DEVIATIONS AS DIRECTED BY ECRA 5341-01475.
- [SDR CALA2025020200252](https://openairdocs.org/sdr/CALA2025020200252.md): Skin · gouged · Jan 23, 2025 · N1902U · Airbus A320232 · Fuselage Main, Plate/Skin
  > ACFT L/H AFT FUSELAGE EXTERIOR HAS GOUGE IN LOCATION ZONE 160 ST A 28296 FR 60 BETWEEN STR 37-38 LEFT PER HAECO LCQ NON ROUTINE 9 296795/40795 GENERATED BY V901665 WITH INSPECTION REQUIREMENTS PER SRI 53-41-11-205-146. REPAIR IS FROM REPAIR EMBODIMENT WITH INT
- [SDR CALA2025010600043](https://openairdocs.org/sdr/CALA2025010600043.md): Door Frame · cracked · Jan 4, 2025 · N1902U · Airbus A320232 · Fuselage Main, Structure
  > L/H FWD EMERGENCY EXIT HATCH HAS CRACKS ON FRAME AS MARKED. REMOVED AND REPLACED ANGLE SEGMENT AT LH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025010600042](https://openairdocs.org/sdr/CALA2025010600042.md): Door Frame · cracked · Jan 4, 2025 · N1902U · Airbus A320232 · Fuselage Main, Structure
  > L/H AFT EMERGENCY EXIT HATCH HAS CRACKS ON FRAME AS MARKED. GENE RATED BY V926223 ON HAECO LCQ NR 9296437/40437. REMOVED AND REPLACED SEGMENT AT LH AFT EMERGENCY EXIT DOOR IAW A 320 SRM 51-72-11-911-001. ACMP BY MECH V947030 INSP BY V077960
- [SDR CALA2025010600041](https://openairdocs.org/sdr/CALA2025010600041.md): Web · cracked · Jan 4, 2025 · N1902U · Airbus A320232 · Fuselage Main, Structure
  > RT AFT EMERGENCY EXIT DOOR WEB CRACKED. REMOVED AND REPLACED ANGLE SEGMENT AT RH AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025010600044](https://openairdocs.org/sdr/CALA2025010600044.md): Web · cracked · Jan 4, 2025 · N1902U · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT FWD EMERGENCY EXIT DOOR WEB CRACKED. REMOVED AND REPLACED ANGLE SEGMENT AT RH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2024112001202](https://openairdocs.org/sdr/CALA2024112001202.md): Battery Pack · no test · Nov 17, 2024 · N1902U · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - BATTERY PACK AT RIGHT DADO PANEL, BELOW OVERWING EXITS HAS FAULT. CHECKED ALL CABIN EMERGENCY LIGHTS - ON, RESET 4 EMERGENCY LIGHT BATTERY CHARGING C/B, OP CK AGAIN, PASSED. REF. SUBTASK 23-73-00-
- [SDR CALA2024111301127](https://openairdocs.org/sdr/CALA2024111301127.md): Wire · pulled · Nov 11, 2024 · N1902U · Airbus A320232 · Light System Wiring
  > SEAT 35C EMERGENCY PATH LIGHT WIRING PULLED FROM LIGHT. REF. LP 9832120 FOR TRIM BROKEN OFF. REPLACED SEAT 35C EMERGENCY ISLE PATH LIGHT. OPS CHECK GOOD.
- [SDR CALA2024100402564](https://openairdocs.org/sdr/CALA2024100402564.md): Bolt · sheared · Oct 3, 2024 · N1902U · Airbus A320232 · Wheel/Ski/Float
  > PDA 2 AIRCRAFT ARRIVED WITH 2 WHEEL HALF BOLTS SHEARED/MISSING FROM #1 MLG WHEEL. TRANSFERED TO TCM LOG PAGE 9448167 01 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. AIRCRAFT ARRIVED WITH 2 WHEEL HALF BOLTS SHEARED/MISSING IN
- [SDR CALA2024012500228](https://openairdocs.org/sdr/CALA2024012500228.md): Fuel Cap · missing · Jan 24, 2024 · N1902U · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISSING ON INBOUND ENGINEERING NOTIFIED. FUELER REPORTS AIRCRAFT CAME TO GATE WITHOUT FUEL CAP APPLIED CDL 28A FOR MISSING FUEL CAP NO LEAKS NOTED DEFERRED IAW CDL 28A DISPATCH DESK: 22 NAME: JV DATE: 24-JAN-24- FUEL CAP MISSING.
- [SDR CALA2023101303050](https://openairdocs.org/sdr/CALA2023101303050.md): Skin · damaged · Mar 25, 2023 · N1902U · Airbus A320232 · Fuselage Main, Plate/Skin
  > AC LOOKS TO HAVE HAD A TAIL SRIKE PERFORMED INSPECTION AFTER TAIL RUNWAY IMPACT IAW AMM 05-51-21-200-001-A. DAMAGE FINDINGS ARE RECORDED IN LOG PAGES: 4165760, 4170493, 4170498, 4170504, 4170511, 4170529, 4170541, 4171124, 4170552 & 4170560. COMPLIED WITH REQU
- [SDR CALA2023020100297](https://openairdocs.org/sdr/CALA2023020100297.md): None · failed · Feb 1, 2023 · N1902U · Airbus A320232 · Lighting System
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - LEFT PASSENGER CABIN EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED LEFT EMERGENCY LIGHT BATTERY IAW AMM 33-51-38
- [SDR CALA2022113003259](https://openairdocs.org/sdr/CALA2022113003259.md): Circuit Breaker · tripped · Nov 30, 2022 · N1902U · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > HYD B SYS LOW PRESSURE ECAM ON BLUE QUANTITY. ACCOMPLISHED INSPECTION CHECK OF BLUE HYD SYSTEM. NO LEAKS DETECTED, HYD RESERVOIR PRESSURE WITHIN THE LIMITS, ONLY FOUND B HYD ELEC PUMP CIRCUIT BREAKER TRIPPED, PUSHED IN AND NO OTHER FAULTS FOUND.
- [SDR CALA2022071801808](https://openairdocs.org/sdr/CALA2022071801808.md): None · missing · Jul 18, 2022 · N1902U · Airbus A320232 · Engine Cowl Flaps
  > PDA 3 #2 ENG AIR INTAKE COWL OUTER LIP AT INBD SIDE (11 O-CLOCK POS) HAS ONE RIVET HEAD BROKEN OFF / MISSING -- SEE PHOTO ADDED PHOTO INSTALLED NEW FASTENER REF AIRBUS SRM 51-42-00.
- [SDR CALA2022062201549](https://openairdocs.org/sdr/CALA2022062201549.md): Frame · cracked · Jun 20, 2022 · N1902U · Airbus A320232 · Fuselage Main, Structure
  > RH FRAME 68 #1 DOOR STOP, HOLE 3 (LOWER INBOARD) HAS A CRACK IND ICATION IN FRAME LAYER. GENERATED BY V892444 ON HAECO LCQ NR 929 2252/38252 SIZE.4658" AND INSTALLED FREEZE PLUG AND REPAIR SPLICE IAW SRM E 205 NUM 010 TABLE 006 AREA 2 INSPECTION THRESHOLD FRO
- [SDR CALA2022021600407](https://openairdocs.org/sdr/CALA2022021600407.md): Light · faulty · Feb 16, 2022 · N1902U · Airbus A320232 · Lighting System
  > CHRONIC ISSUE EMERGENCY LIGHTS ON IN ARMED POSITION. REF TSM 33-51-00-810-881-A FOR TROUBLESHOOTING. PILOT REPORTS ONLY LEFT SIDE OF AIRCRAFT IS COMING ON. PLEASE REF TSM 33-51-00-810- 881A FOR TROUBLE SHOOTING. SUSPECT WIRING ISSUE TO LEFT SIDE OF AIRCRAFT. P
- [SDR CALA2021090801534](https://openairdocs.org/sdr/CALA2021090801534.md): Rivet · missing · Sep 8, 2021 · N1902U · Airbus A320232 · Engine Air Intake System
  > PDA 3 #2 ENG AIR INTAKE COWL OUTER LIP SKIN HAS ONE RIVET HEAD BROKEN OFF/MISSING AT 7 O-CLOCK POS AFT LOOKING FORWARD-- SEE PHOTO PHOTO ADDED REPLACED DAMAGED FASTNER WITH NEW FASTNER WITH NEW FASTNER REF. EC/RA 7111-01387.
- [SDR CALA2021061400871](https://openairdocs.org/sdr/CALA2021061400871.md): Vent Line · leaking · Jun 14, 2021 · N1902U · Airbus A320232 · Wash Water System
  > REF LP 6472922 CREW REPORTS WATER LEAK IN FWD GALLEY COMING FROM BEHAND THE COFFEE MAKER. SHUT OFF WATER AND LEAK STOPPED. REF LP 6472922, SERVICED WATER FULL REMOVED COFFEE MAKER WITH ENG RUNNING FOUND WATER POURING OUT OF THE CHECK VALVE VENT LINE BEHIND THE
- [SDR CALA2018070301540](https://openairdocs.org/sdr/CALA2018070301540.md): Shear Plate · corroded · Jun 22, 2018 · N1902U · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FR70 STR 23L SHEAR PLATE SUPPORT WEB CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW SRM 51-42-11-0 01.

## 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 = 'N1902U' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N1902U/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.