# Service difficulty reports: N860NW

A list on [N860NW](https://openairdocs.org/aircraft/N860NW.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 6 · 269 reports

- [SDR DALA2026050702903](https://openairdocs.org/sdr/DALA2026050702903.md): Wire · damaged · May 7, 2026 · N860NW · Airbus A330223 · Light System Wiring
  > EMERGENCY LIGHT OUT AT SEAT 46B. REPAIRED WIRING AND REPLACED LAMP ASSY PER A330 AMM 33-51. (8601354) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026042002503](https://openairdocs.org/sdr/DALA2026042002503.md): Power Supply · inoperative · Apr 13, 2026 · N860NW · Airbus A330223 · Emergency Lighting
  > AFT GALLEY RT REAR FACING WHITE EMERGENCY LIGHT INOPERATIVE. REPLACED EPSU 16WL IAW AMM 33-51. AIRCRAFT WAS GROUNDED.
- [SDR DALA2026012200513](https://openairdocs.org/sdr/DALA2026012200513.md): Stringer · gouged · Jan 14, 2026 · N860NW · Airbus A330223 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STR 1R FR 60-FR 64 DENT, GOUGE, DAMAGED FASTENER HOLES. REPAIRED PER ERA 627744-14 REV A. (1402097)
- [SDR DALA2026011400334](https://openairdocs.org/sdr/DALA2026011400334.md): Skin · damaged · Jan 14, 2026 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND STRINGER 3R AT FR 61, FR 62 DAMAGED HOLES AND TOOLING DAMAGE. REPAIRED PER ERA 627795-14 REV A. (1400862)
- [SDR DALA2026011400335](https://openairdocs.org/sdr/DALA2026011400335.md): Skin · damaged · Jan 13, 2026 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND STRINGER 3R AT FR 61, FR 62 DAMAGED HOLES AND TOOLING DAMAGE. CORRECTED PER ERA 627795-14 REV A. (1400731)
- [SDR DALA2025110308021](https://openairdocs.org/sdr/DALA2025110308021.md): Bottle · low pressure · Nov 1, 2025 · N860NW · Airbus A330223 · Passenger/Crew Doors
  > SHIP 3360 ESCAPE SLIDE PRESSURE AT 1 LEFT AND 2 LEFT LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLES PER A330 AMM 52-15. OK FOR SERVICE. (7667340)
- [SDR DALA2025102807900](https://openairdocs.org/sdr/DALA2025102807900.md): Indicator · inoperative · Oct 26, 2025 · N860NW · Airbus A330223 · Emergency Equipment
  > SHIP 3360 DOOR 3L SLIDE PRES INDICATION INOP. CORRECTIVE ACTION: REPLACED TERMINAL BOX 308RH2 PER A330 AMM 23-73. OPS CHECK GOOD. (7929179)
- [SDR DALA2025102007675](https://openairdocs.org/sdr/DALA2025102007675.md): Elec Connector · damaged · Oct 20, 2025 · N860NW · Airbus A330223 · Emergency Lighting
  > EMERGENCY LIGHT AT 34AB OUT. REPAIRED CONNECTOR PER A330 AMM 33-51. (7929145)
- [SDR DALA2025100907387](https://openairdocs.org/sdr/DALA2025100907387.md): Frame · damaged · Oct 8, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > TOOLING DAMAGE ON FRAME 24 @ P'4 - BETWEEN BRACKET VIEWED FROM BACK SIDE REF DETAIL W-16 - DD. REPAIRED PER ERA 627851-14 REV ORIG. (1241271)
- [SDR DALA2025100907385](https://openairdocs.org/sdr/DALA2025100907385.md): Frame · damaged · Oct 8, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 TOOLING DAMAGE ON FRAME 23 @ P4 - BETWEEN BRACKET VIEWED FROM BACK SIDE REF DETAIL Y - HH. CORRECTIVE ACTION: REPAIRED PER ERA 627851-14 REV O. (1241638)
- [SDR DALA2025100807353](https://openairdocs.org/sdr/DALA2025100807353.md): Frame · damaged · Oct 7, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > MISDRILLED HOLES AT FRAME 22, L/H SIDE P5 BEHIND ANGLE BRACKET. CORRECTIVE ACTION: REPAIRED PER ERA 627851-14 REV ORIG. (1239805)
- [SDR DALA2025100807352](https://openairdocs.org/sdr/DALA2025100807352.md): Frame · damaged · Oct 7, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > FRAME C70 DETAIL W STR '6 TOOLING DAMAGE ON EXISTING CLIP AND FRAME AROUND NEW FASTENER TAIL AT WIRE BUNDLE. REPAIRED PER ERA 627851-14 REV O. (1239749)
- [SDR DALA2025100807351](https://openairdocs.org/sdr/DALA2025100807351.md): Bracket · damaged · Oct 7, 2025 · N860NW · Airbus A330223 · Fuselage Main, Attach Fittings
  > FRAME C69 STR P'5 BRACKET HAS TOOLING DAMAGE. REPAIRED PER ERA 627851-14 REV O. (1239745)
- [SDR DALA2025100707295](https://openairdocs.org/sdr/DALA2025100707295.md): Bracket · damaged · Oct 6, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > SHIP 3360 BRACKET ON FORWARD SIDE AT FRAME 37.1 HAS TOOLING DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 627851-14 REV. ORIG. (1237970)
- [SDR DALA2025100607248](https://openairdocs.org/sdr/DALA2025100607248.md): Bracket · damaged · Oct 5, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > FRAME 20 DETAIL Z I/B UPPER BRACKET HAS TOOLING DAMAGE. REPLACED BRACKET PER AIRBUS DWG F5397562605000 AND A330 SRM 53-11. (1235742)
- [SDR DALA2025090406558](https://openairdocs.org/sdr/DALA2025090406558.md): Skin · dented · Aug 25, 2025 · N860NW · Airbus A330223 · Service Doors
  > (4R) OUTER SKIN, BOTTOM EDGE FOUND DENTED. COMPLIED WITH ERA 501981-14 REV. B. (1163409)
- [SDR DALA2025082206260](https://openairdocs.org/sdr/DALA2025082206260.md): Bleed Valve · faulted · Aug 21, 2025 · N860NW · Airbus A330223 · APU Bleed Air System
  > ATO DUE TO ENG THRUST LOSS BLEED CONFIG ECAM MSG WHEN T/O POWER WAS SELECTED. R & R APU BLEED VALVE. OPS CHECK GOOD. (7355668)
- [SDR DALA2025072805645](https://openairdocs.org/sdr/DALA2025072805645.md): Skin · mechanic error · Jul 26, 2025 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > SHIP 3360 WHILE DISBONDING STGR 3R, TOOLING MARKS WERE CREATED ON SKIN AT FR 61. CORRECTIVE ACTION: REPAIRED PER PRI 627795-14 REV 1. (1106308)
- [SDR DALA2025072805643](https://openairdocs.org/sdr/DALA2025072805643.md): Shear Tie · gouged · Jul 26, 2025 · N860NW · Airbus A330223 · Fuselage Internal Mounting Structure
  > SHIP 3360 FR60 AFT SIDE OF FRAME U-CHANNEL SKIN SUPPORT IN BETWEEN STR1L AND STR2L GOUGED AT FWD INBD RADIUS. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-11. (1107157)
- [SDR DALA2025073005716](https://openairdocs.org/sdr/DALA2025073005716.md): Skin · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > SHIP 3360 STRINGER 3R AND FUSELAGE SKIN REWORK, FR 60-62. REPAIRED PER ERA 627795-14.
- [SDR DALA2025073005715](https://openairdocs.org/sdr/DALA2025073005715.md): Stringer · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Longeron/Stringer
  > SHIP 3360 STRINGER 3L REPAIR, FR 60 - FR 64. INSPECTED AND REPAIRED PER ERA 627504-14. (1105529)
- [SDR DALA2025072805650](https://openairdocs.org/sdr/DALA2025072805650.md): Skin · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > SHIP 3360 DAMAGE FOUND ON INTERNAL SIDE SKIN AT FASTENER HOLE INBOARD OF STR 3L BETWEEN FR 61 AND FR 62. CORRECTIVE ACTION: REPAIRED PER ERA 627562-14 REV O. (1105056)
- [SDR DALA2025072805649](https://openairdocs.org/sdr/DALA2025072805649.md): Tee Angle · mechanic error · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > SHIP 3360 T-CHORD P/N: F53491904239 (ITEM 25) LOCATED AT FR 61-FR 62 BETWEEN STR 2R AND STR 3R IS MISDRILLED. CORRECTIVE ACTION: REPAIRED PER ERA 627645-14 REV O. (1105041)
- [SDR DALA2025072805648](https://openairdocs.org/sdr/DALA2025072805648.md): Tee Angle · mechanic error · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > SHIP 3360 T-CHORD P/N: F53491904238 LOCATED AT FR 61-FR 62 BETWEEN STR 2L AND STR 3L IS MISDRILLED. CORRECTIVE ACTION: REMOVED AND REPLACED REF A330 SRM 51-42-11. (1105038)
- [SDR DALA2025072805647](https://openairdocs.org/sdr/DALA2025072805647.md): Stringer Clip · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Attach Fittings
  > SHIP 3360 FRAME 63 STR 1R CLIP ASSY (PN: F5349190100700) HAS TOOLING DAMAGE AND ELONGATED HOLES. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV O. (1105019)
- [SDR DALA2025072805646](https://openairdocs.org/sdr/DALA2025072805646.md): Support Angle · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > SHIP 3360 FRAME 63 STR 2R SUPPORT CLIP (PN: F5349190920900 ITEM 75) HAS ELONGATED HOLES AND TOOLING DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV O. (1105006)
- [SDR DALA2025072805644](https://openairdocs.org/sdr/DALA2025072805644.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 3L - 2L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: INSTALLED NEW FRAME PER A330 SRM 53-11. (1106019)
- [SDR DALA2025072805642](https://openairdocs.org/sdr/DALA2025072805642.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3L - 4L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106119)
- [SDR DALA2025072805641](https://openairdocs.org/sdr/DALA2025072805641.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3L - 2L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106104)
- [SDR DALA2025072805640](https://openairdocs.org/sdr/DALA2025072805640.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 1L - 2L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106098)
- [SDR DALA2025072805639](https://openairdocs.org/sdr/DALA2025072805639.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 1R - 1L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106092)
- [SDR DALA2025072805638](https://openairdocs.org/sdr/DALA2025072805638.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3R - 4R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: INSTALLED NEW FRAME PER A330 SRM 53-11. (1106086)
- [SDR DALA2025072805637](https://openairdocs.org/sdr/DALA2025072805637.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 3R - 4R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106076)
- [SDR DALA2025072805636](https://openairdocs.org/sdr/DALA2025072805636.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 2R - 3R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106055)
- [SDR DALA2025072805635](https://openairdocs.org/sdr/DALA2025072805635.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 1R - 2R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106048)
- [SDR DALA2025072805634](https://openairdocs.org/sdr/DALA2025072805634.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 1L - 1R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106045)
- [SDR DALA2025072805633](https://openairdocs.org/sdr/DALA2025072805633.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 2L - 1L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106037)
- [SDR DALA2025072805632](https://openairdocs.org/sdr/DALA2025072805632.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR62 FROM STR 4L - 3L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1106005)
- [SDR DALA2025072805631](https://openairdocs.org/sdr/DALA2025072805631.md): Skin · damaged · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > SHIP 3360 TOOLING DAMAGE FOUND ON THE SKIN ADJACENT TO STR R1 AT FR 63. CORRECTIVE ACTION: REPAIRED PER ERA 627916-14 REV ORIGINAL. (1105858)
- [SDR DALA2025072805630](https://openairdocs.org/sdr/DALA2025072805630.md): Skin · mechanic error · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Plate/Skin
  > SHIP 3360 WHILE DISBONDING STR 1R, TOOLING MARKS WERE CREATED ON SKIN 8" AFT OF FR60 1" OB OF STR 1R. CORRECTIVE ACTION: REPAIRED PER ERA 627744-14 REV O. (1105844)
- [SDR DALA2025072805629](https://openairdocs.org/sdr/DALA2025072805629.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3L - 4L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105300)
- [SDR DALA2025072805628](https://openairdocs.org/sdr/DALA2025072805628.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3L - 2L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105299)
- [SDR DALA2025072805627](https://openairdocs.org/sdr/DALA2025072805627.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 1L - 2L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105297)
- [SDR DALA2025072805626](https://openairdocs.org/sdr/DALA2025072805626.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 1R - 1L REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105295)
- [SDR DALA2025072805625](https://openairdocs.org/sdr/DALA2025072805625.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 1R - 2R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 AMM 53-11. (1105294)
- [SDR DALA2025072805624](https://openairdocs.org/sdr/DALA2025072805624.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3R - 2R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105290)
- [SDR DALA2025072805623](https://openairdocs.org/sdr/DALA2025072805623.md): Frame · not reported · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Frame
  > SHIP 3360 FR63 FROM STR 3R - 4R REQUIRES HFEC ROTO TEST OF OPEN HOLES FROM FASTENER REMOVAL. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 53-11. (1105269)
- [SDR DALA2025072505592](https://openairdocs.org/sdr/DALA2025072505592.md): Door Frame · misinstalled · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Structure
  > SHIP 3360 FR 64 L2-R2 HAS INCORRECT FASTENERS. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV ORIGINAL. (1104867)
- [SDR DALA2025072505591](https://openairdocs.org/sdr/DALA2025072505591.md): Door Frame · misinstalled · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Main, Structure
  > SHIP 3360 FR 63 - R2 HAS INCORRECT FASTENERS. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV ORIGINAL. (1104860)
- [SDR DALA2025072505590](https://openairdocs.org/sdr/DALA2025072505590.md): Bracket · misinstalled · Jul 25, 2025 · N860NW · Airbus A330223 · Fuselage Miscellaneous Structure
  > SHIP 3360 FR 64 BRACKET BETWEEN R2-3 HAS INCORRECT FASTENERS. CORRECTIVE ACTION: REPAIRED PER ERA 627465-14 REV ORIGINAL. (1104853)

Next page: https://openairdocs.org/aircraft/N860NW/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 = 'N860NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N860NW/reports

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