# Service difficulty reports: N331NB

A list on [N331NB](https://openairdocs.org/aircraft/N331NB.md).

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

Page 1 of 4 · 156 reports

- [SDR DALA2026092705362](https://openairdocs.org/sdr/DALA2026092705362.md): Windshield · out of tolerance · Sep 26, 2026 · N331NB · Airbus A319114 · Windshield/Door Rain/Ice Removal
  > DIVERTED DUE TO, DURING CLIMB, ANTI-ICE WINDSHIELD CAUTION APPEARED. ATTEMPTED RESET BUT CAUTION MESSAGE REMAINED. TROUBLESHOT IAW TSM 30-42-00-810-803-A. FOUND LT WINDSHIELD AT 362 K OHMS. R & R LEFT WINDSHIELD IAW AMM 56-11. WHC BITE & WINDOW HEAT OPS NOR
- [SDR DALA2026072304307](https://openairdocs.org/sdr/DALA2026072304307.md): Housing · broken · Jul 21, 2026 · N331NB · Airbus A319114 · Emergency Lighting
  > EMERGENCY LIGHT HOUSING UNDER SEAT 21D IS BROKEN. R & R 21D EMERGENCY LIGHT HOUSING. OPS TESTED GOOD IAW AMM 33-51. (LP: 9613783, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070503905](https://openairdocs.org/sdr/DALA2026070503905.md): Skin · dented · Jul 4, 2026 · N331NB · Airbus A319114 · Passenger/Crew Doors
  > L1 LOWER FORWARD SKIN SECTION REQUIRES PERMANENT REPAIR DENT TYPE 1, ZONE 1, AREA 1, REPAIR SOLUTION PERMANENT WITHIN 8000FC. REFERENCE SRM 52-10-00-283-002 PAGE 17 007 DEF CHECK AIRCRAFT WAS GROUNDED.
- [SDR DALA2026062003683](https://openairdocs.org/sdr/DALA2026062003683.md): Light · damaged · Jun 13, 2026 · N331NB · Airbus A319114 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. AISLE LIGHT HANGING FROM SEAT. RE-SECURED 21D LIGHT ASSY, ALL OPS NORMAL. (LP: 1645205, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026022401326](https://openairdocs.org/sdr/DALA2026022401326.md): Skin · bulged · Feb 23, 2026 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE FR66, STR39L POTABLE WATER SERVICE PANEL FWD LOWER CORNER WITH BULGED SKIN AND SOLID RIVETS WITH CORROSION. CORRECTIVE ACTION: REPLACED POTABLE WATER SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011420800 PER SRM 51-72-11-911-001 AND 51
- [SDR DALA2026022401325](https://openairdocs.org/sdr/DALA2026022401325.md): Skin · bulged · Feb 23, 2026 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE FR66 BETWEEN STR 38R-39R (WASTE) TOILET SERVICE PANEL AFT LOWER CORNER WITH BULGED SKIN. CORRECTIVE ACTION: REPLACED (WASTE) TOILET SERVICE PANEL INTERNAL REINFORCEMENT DOUBLER P/N D5348011521201 PER SRM 51-72-11-911-001 AND 51-42-11- 801-PARG 2
- [SDR DALA2026022301262](https://openairdocs.org/sdr/DALA2026022301262.md): Shear Web · corroded · Feb 22, 2026 · N331NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AIRCRAFT 3131, AFT CABIN, BETWEEN FR 69-70, RH FLOOR SHEAR WEB WITH CORROSION. CORRECTIVE ACTION: REPLACED SHEARPLATE P/N: D5347112420300 I/A/W A319 SRM 51-72-11-911-001 REV 155.00, DATED 17 NOV 25 AND AIRBUS REF.DWG#D53474180. (LP 1463318)
- [SDR DALA2026022001233](https://openairdocs.org/sdr/DALA2026022001233.md): Seat Track · corroded · Feb 19, 2026 · N331NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3131, UPPER FUSELAGE, PAX CABIN, FR 64 TO FR 66 Y=1292 WET AREA SEAT TRACK CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK P/N: 14N00031-101 AT FR64 TO FR66 Y=1292 WET AREA DUE TO CORRODED OUT- LIMITS IAW A319 SRM 51-72-11-911-001 REV 155.00 DATED 17
- [SDR DALA2026022001232](https://openairdocs.org/sdr/DALA2026022001232.md): Fitting · cracked · Feb 19, 2026 · N331NB · Airbus A319114 · Fuselage Main, Structure
  > AIRCRAFT 3131, FLIGHT DECK, WINDSHIELD FRAMING, LT / RT CONTINUITY FITTING CRACKED. CORRECTIVE ACTION: REPLACED CONTINUITY FITTINGS (LH P/N D53111077202009) (RH P/N D5311107720300) IAW DELTA ERA 631770-14AD REV ORIGINAL DATED 10-FEB-26 AND REPAIR DWG R531-1291
- [SDR DALA2026021901183](https://openairdocs.org/sdr/DALA2026021901183.md): Stringer · damaged · Feb 17, 2026 · N331NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > PER FAA AAI FINDING TWO RIVETS AT STRINGER 4R BETWEEN FRAME 36 AND 37 REQUIRE REPLACEMENT DUE TO SUBSTANDARD INSTALLATION. REPAIRED FUSELAGE STRINGER 4R SECTION BETWEEN FR35+47MM AND FR36+381MM DUE TO SUBSTANDARD SOLID RIVETS INSTALLATION I/A/W A319 SRM 53-0
- [SDR DALA2026021201022](https://openairdocs.org/sdr/DALA2026021201022.md): Shear Web · corroded · Feb 11, 2026 · N331NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT CABIN, BETWEEN FR 69-70, LT FLOOR SHEAR WEB WITH LEVEL 2 CORROSION. REPLACED THE SHEAR WEB IAW SRM 51-72- 11-911-001, & 53-41-17-01A, FIG 001, REV 155, & DWG D53474180. (LP 1446287)
- [SDR DALA2026020600876](https://openairdocs.org/sdr/DALA2026020600876.md): Intercostal · cracked · Feb 3, 2026 · N331NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING 7 ON FR 16 RT SIDE, HOLE 1 & 3, WITH CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL IAW SRM 51-72-11-911-001, REV 155, AND DRAWING D5312300, ISSUE E, SHEET 01. FITTING P/N: D53114236201
- [SDR DALA2026020600875](https://openairdocs.org/sdr/DALA2026020600875.md): Door Frame · cracked · Feb 2, 2026 · N331NB · Airbus A319114 · Fuselage Main, Structure
  > WORK CARD 5311-01229-02, UPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING NR 7 ON FR 16 LT SIDE, HOLES 1 & 3, CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL D5311423620091 IAW SRM 51-72-11-911-001, REV 155. AND DWG D5312300, ISSUE E, SH
- [SDR DALA2026021000962](https://openairdocs.org/sdr/DALA2026021000962.md): Fitting · corroded · Jan 29, 2026 · N331NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE ATTACHMENT SPIGOT FITTING OUT OF LIMITS, LEVEL 2 CORROSION. REPLACED NR 1 PYLON LOWER SPIGOT FITTING IAW A319 SRM TASK 54-51-12-300-001. (LP 1443400)
- [SDR DALA2026020100737](https://openairdocs.org/sdr/DALA2026020100737.md): Door Frame · cracked · Jan 29, 2026 · N331NB · Airbus A319114 · Fuselage Main, Structure
  > AD RELATED, A.A. 5311-01216-04, AFT PASSENGER/CREW DOOR, FR68 LT, DOOR STOP FITTING NR 1, HOLE NR 4 (DIA. 0.250") HAD A CRACK INDICATION AT FRAME LAYER. EVALUATE & REPAIR IAW SRM 53-41-12. PERFORMED FREEZE PLUG REPAIR AT FR 68 DOOR FRAME STOP FITTING NR 1 HO
- [SDR DALA2026020100736](https://openairdocs.org/sdr/DALA2026020100736.md): Shear Tie · corroded · Jan 29, 2026 · N331NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT FR 34 BETWEEN STR 41R - 42R FRAME SHEAR TIE CORRODED. REPLACED SHEAR VCLIP P/N: D5323094520000 AT FWD CARGO COMPARTMENT FR 34 BETWEEN STR 41R - STR 42R IAW A319 SRM 51-72- 11-911-001 REV 155.00 DATED 17/NOV/25 AND AIRBUS REFERENCE DRAWIN
- [SDR DALA2026012600546](https://openairdocs.org/sdr/DALA2026012600546.md): Repair · not reported · Jan 22, 2026 · N331NB · Airbus A319114 · Standard Practices/Structures
  > ER/A 496231-14 REVISION B ISSUED FOR FUSELAGE SKIN REPAIR LOCATE D AT FR36 & S-4RH. FOLLOW ON ACTION IS REQUIRED. C/A: PERFORM SECTION II WITHIN SOONER OF 54200FC / 108400FH FROM SECT ION I AND EVERY SOONER OF 5000FC / 10000FH THEREAFTER. ASSOCIATED ER/A 14-49
- [SDR DALA2023120509945](https://openairdocs.org/sdr/DALA2023120509945.md): Unknown · unknown · Dec 5, 2023 · N331NB · Airbus A319114 · Air Distribution System
  > SHIP 3131 ODOR IN FLIGHT DECK WHEN RUNNING APU BLEED. CORRECTIVE ACTION: REMOVED AND RPELACED BOTH RECIRC FILTERS PER A319 AMM 21-21. (5028165)
- [SDR DALA2023120509944](https://openairdocs.org/sdr/DALA2023120509944.md): Unknown · unknown · Dec 5, 2023 · N331NB · Airbus A319114 · Emergency Lighting
  > SHIP 3131 IN SEAT EMERGENCY LIGHT AT 22 DEF DAMAGED. CORRECTIVE ACTION: SECURED EMERGENCY LIGHT PER A319 AMM 33-50. OPS CK GOOD. OK FOR SVC. (5028167)
- [SDR DALA2026012300517](https://openairdocs.org/sdr/DALA2026012300517.md): None · none · Dec 2, 2023 · N331NB · Airbus A319114 · Standard Practices/Structures
  > REPETITIVE INTERNAL HFEC AND EXTERNAL LFEC, SEC II OF ER/A 604182-14 REV. A. PERFORMED REPETITIVE INTERNAL H.F.E.C. AND EXTERNAL L.F.E.C. OF ER/A 604182-14 REV A, DATED 03-DEC-23, SECTION II, STEPS 3 AND 4. FOUND NO CRACKS. (LP: 0092463)
- [SDR DALA2023041202861](https://openairdocs.org/sdr/DALA2023041202861.md): Unknown · unknown · Apr 10, 2023 · N331NB · Airbus A319114 · Emergency Lighting
  > AIRCRAFT 3131, EMERGENCY LIGHTS AT ROW 26 & 27 INOP. CORRECTIVE ACTION: REPAIRED WIRE AT CONNECTOR 9159VC. (LP 4765500)
- [SDR DALA2023011100209](https://openairdocs.org/sdr/DALA2023011100209.md): Acm · seized · Jan 10, 2023 · N331NB · Airbus A319114 · Cabin Cooling System
  > SHIP 3131 - AIR PACK 1 OVHT DISPLAYED ON ECAM TEMERATURE WAS UNCONTROLLABLE MAX OUTLET COCKPIT TEMP WAS 134. THERE WAS A PLASTIC ODOR. CORRECTIVE ACTION: REPLACED ACM 10HM1 PER A319 AMM 21-52-21 LEAK & OPS TEST OK. (9397947)
- [SDR DALA2022121207999](https://openairdocs.org/sdr/DALA2022121207999.md): Skin · damaged · Dec 7, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - PREVIOUS HAIL DAMAGE FUSELAGE/SKIN/ FS 57 TO 63 / S-5R TO S-5L. REPAIRED PER ER/A 604182-14. (2529074)
- [SDR DALA2022121207998](https://openairdocs.org/sdr/DALA2022121207998.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 58, 2.6 INCHES AFT, 3.3 INCHES OUTBOARD 4R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527154)
- [SDR DALA2022120907993](https://openairdocs.org/sdr/DALA2022120907993.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 60. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527169)
- [SDR DALA2022120907992](https://openairdocs.org/sdr/DALA2022120907992.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 58. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527159)
- [SDR DALA2022120907991](https://openairdocs.org/sdr/DALA2022120907991.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 59. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527151)
- [SDR DALA2022120907990](https://openairdocs.org/sdr/DALA2022120907990.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 59, 4.2 INCHES AFT,.200 INCHES OUTBOARD 4R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527149)
- [SDR DALA2022120907989](https://openairdocs.org/sdr/DALA2022120907989.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 60. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527148)
- [SDR DALA2022120907988](https://openairdocs.org/sdr/DALA2022120907988.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 60,.300 INCHES AFT, 1.25 INCHES INBOARD 5R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527145)
- [SDR DALA2022120907987](https://openairdocs.org/sdr/DALA2022120907987.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 60, 7.25 INCHES AFT,.600 INCHES INBOARD 5R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527144)
- [SDR DALA2022120907986](https://openairdocs.org/sdr/DALA2022120907986.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 60, 4.0 INCHES AFT, 2.5 INCHES OUTBOARD 3R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527141)
- [SDR DALA2022120907985](https://openairdocs.org/sdr/DALA2022120907985.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 4.3 INCHES FWD, 3.4 INCHES INBOARD 3R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527138)
- [SDR DALA2022120907984](https://openairdocs.org/sdr/DALA2022120907984.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 5.7 INCHES FWD, 3.1 INCHES INBOARD 3R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527136)
- [SDR DALA2022120907983](https://openairdocs.org/sdr/DALA2022120907983.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 6.5 INCHES FWD, 1.7 INCHES OUTBOARD 3R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527133)
- [SDR DALA2022120907982](https://openairdocs.org/sdr/DALA2022120907982.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 2.9 INCHES FWD,.600 INCHES OUTBOARD 3R. CORRECTIVE ACTON: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527131)
- [SDR DALA2022120907981](https://openairdocs.org/sdr/DALA2022120907981.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 1.1 INCHES AFT, 2.2 INCHES INBOARD 4R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527130)
- [SDR DALA2022120907980](https://openairdocs.org/sdr/DALA2022120907980.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 62, 2.5 INCHES FWD, 1.6 INCHES INBOARD 4R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527129)
- [SDR DALA2022120907979](https://openairdocs.org/sdr/DALA2022120907979.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 62, 11.7 INCHES AFT, 0.5 INCHES INBOARD 1R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527127)
- [SDR DALA2022120907978](https://openairdocs.org/sdr/DALA2022120907978.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 62, 4.4 INCHES AFT, 1.2 INCHES INBOARD 2L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527125)
- [SDR DALA2022120907977](https://openairdocs.org/sdr/DALA2022120907977.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 62, 2.4 INCHES FWD, 1.6 INCHES OUTBOARD 3L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527123)
- [SDR DALA2022120907976](https://openairdocs.org/sdr/DALA2022120907976.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 2.7 INCHES FWD, 2.9 INCHES OUTBOARD 3L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527118)
- [SDR DALA2022120907975](https://openairdocs.org/sdr/DALA2022120907975.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 61, 4.6 INCHES FWD, 3.3 INCHES OUTBOARD 3L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527114)
- [SDR DALA2022120907974](https://openairdocs.org/sdr/DALA2022120907974.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 58, 3.8 INCHES AFT, 1.3 INCHES OUTBOARD 4L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527113)
- [SDR DALA2022120907973](https://openairdocs.org/sdr/DALA2022120907973.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 57, 8 INCHES AFT, 1.1 INCHES OUTBOARD 3L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527112)
- [SDR DALA2022120907972](https://openairdocs.org/sdr/DALA2022120907972.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - HAIL DAMAGE FRAME 57 2.2 INCHES AFT, 2.7 INCHES INBOARD 3L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527109)
- [SDR DALA2022120907971](https://openairdocs.org/sdr/DALA2022120907971.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - EXTERIOR FUSELAGE SKIN, HAIL DAMAGE BETWEEN FRAME 61-62, OTBD OF STR 2R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527106)
- [SDR DALA2022120907970](https://openairdocs.org/sdr/DALA2022120907970.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - EXTERIOR FUSELAGE SKIN, HAIL DAMAGE BETWEEN FRAME 61-62, OTBD OF STR 1L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527103)
- [SDR DALA2022120907969](https://openairdocs.org/sdr/DALA2022120907969.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - EXTERIOR FUSELAGE SKIN, HAIL DAMAGE BETWEEN FRAME 61-62, INBD OF STR 2L. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527101)
- [SDR DALA2022120907968](https://openairdocs.org/sdr/DALA2022120907968.md): Skin · damaged · Dec 6, 2022 · N331NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3131 - EXTERIOR FUSELAGE SKIN, HAIL DAMAGE BETWEEN FRAME 60-61, BETWEEN STR 3R-4R. CORRECTIVE ACTION: WORK ACCOMPLISHED ON DELTA ER/A 604182-14. (2527097)

Next page: https://openairdocs.org/aircraft/N331NB/reports.md?page=2

## 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 = 'N331NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N331NB/reports

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