# Service difficulty reports: N260JX

A list on [N260JX](https://openairdocs.org/aircraft/N260JX.md).

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

- [SDR 4DPA2024031000001](https://openairdocs.org/sdr/4DPA2024031000001.md): Pump · leaking · Mar 10, 2024 · N260JX · Emb EMB135LR · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED- ON CLIMB OUT EICAS MESSAGE CAME ON FOR HYDRAULIC QUANTITY. RAN QRH. THEN LATER HYDRAULIC SYSTEM 2 FAILURE. CORR ACTION- MX R&R'D ENG 2 PUMP AFTER IT WAS INSPECTED AND FOUND LEAKING. OPS AND LEAK CHECK GOOD.
- [SDR V0XD20230526001](https://openairdocs.org/sdr/V0XD20230526001.md): Panel · cracked · May 26, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > UPPER LATERAL MOUNTING BRACKET ON UPPEER LH SIDE OF COCKPIT CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED OVERHEAD PANEL (FRAME) AND REPLACED WITH NEW OVERHEAD PANEL (FRAME) PN 123-07751-005 AT LH SIDE OF COCKPIT UPPERSIDE IAW EMB 145 SRM 51-40-02 SEE AVMA
- [SDR V0XD20230524001](https://openairdocs.org/sdr/V0XD20230524001.md): Skin Panel · cracked · May 25, 2023 · N260JX · Emb EMB135LR · Fuselage Main, Plate/Skin
  > LEFT HAND WINDSHIELD OUTBOARD POST SKIN IS CRACKED AT UPPER SIDE. CORRECTIVE ACTION: REPAIRED L/H WINDSHIELD OUTBOARD POST SKIN IAW EMB SB 145-53-0079 REV. 1 DATED 07NOV 2012. SEE AVAMAX W.O. 81054 W.C. 2189
- [SDR V0XD20230518003](https://openairdocs.org/sdr/V0XD20230518003.md): Seat Track · corroded · May 18, 2023 · N260JX · Emb EMB135LR · Fuselage, Seat/Cargo Attach Fittings
  > SIGNS OF CORROSION ON LH UPPER SEAT TRACK AT FRM 20- FRM 23. CORRECTIVE ACTION: REMOVED AND REPLACED L/H UPPER SEAT TRACK AT FRM 20 - FRM 23 IAW EMB 135/145 AMM 53-01-06.
- [SDR V0XD20230516002](https://openairdocs.org/sdr/V0XD20230516002.md): Unknown · unknown · May 16, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > MULTIPLE DENTS IN AREA AFT OF FRM 19 STGR 11-12L. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR BY CUTTING OUT DAMAGED AREA FABRICATED AND INSTALLED REAPIR DOUBLER AND FILLER IAW EMB 145 SRM 51-40-02 AND ETD 2023-145-011847. SEE AVMAX WO:81054 WC: 2191
- [SDR V0XD20230516001](https://openairdocs.org/sdr/V0XD20230516001.md): Seat Track · corroded · May 16, 2023 · N260JX · Emb EMB135LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE FLOOR SEAT TRACK AT Y=479.0 FRM 36 TO FRM 47 HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED R/H FLOOR SEAT TRACK AT FRM 36-FRM 47 IAW EMB 135/145 AMM 53-01-06. SEE AVMAX WO: 81054 WC:2215
- [SDR V0XD20230515001](https://openairdocs.org/sdr/V0XD20230515001.md): Seat Track · corroded · May 15, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > CORROSION ON R/H UPPER SEAT TRACK AT FRM 19 TO FRM 22. CORRECTIVE ACTION: REMOVED AND REINSTALLED NEW SEAT TRACK ON R/H SIDEWALL AT FRM 19 TO FRM 22 IAW EMB 135/145 AMM 53-01-06.
- [SDR V0XD20230508003](https://openairdocs.org/sdr/V0XD20230508003.md): Support · corroded · May 8, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > BAGGAGE COMPT. FLOOR SILL CRACKED RH FWD AREA 8.5" AFT OF LAV TO BAGGAGE AREA WALL. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT SILL P/N 145-25422-003 RH FWD AFT OF LAV TO BAGGAGE AREA IAW EMB 145 SRM 51-20-03, SRM 51-40-02. SEE AVMAX WO 81054 WC 1172
- [SDR V0XD20230508002](https://openairdocs.org/sdr/V0XD20230508002.md): Profile · corroded · May 8, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > LH AISLE FLOOR GUSSETTCORROSION FS 32.5 TO FS 35.5, Y = 479.0. CORRECTIVE ACTION: RMEOVED AND REPLACED LH AISLE FLOOR GUSSETT FRM 32.5 TO FRM 35.5 IAW EMB 145 SRM 51-40-02 NDT INSPECTION PERFORMED BY BARON NDT LLC. FAA CRS# SNDR545D REPORT # S042023-2 DATED 20
- [SDR V0XD20230508001](https://openairdocs.org/sdr/V0XD20230508001.md): Profile · corroded · May 8, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > RH AISLE FLOOR GUSSETT FRM 35-36(APPROX.) SHOWS SIGNS OF CORROSION. CORRCTIVVE ACTION: REMOVED DAMAGED PROFILE (GUSSETT) AND INSTALLED NEW PROFILE P/N 135-00076-002 RH SIDE FLOOR GUSSETT FRM 32-36 IAW EMB 145 SRM 51-20-03 & 51-40-02.
- [SDR V0XD20230503002](https://openairdocs.org/sdr/V0XD20230503002.md): Gusset · corroded · May 3, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > RH GUSSETT PLATE AT Y = 479.0 AND FRM 60 HAS SIGNS OF CORROSION. EVAL CORRECTIVE ACTION: REMOVE AND REPLACED R/H GUSSETT PLATE P/N 145-26437-001 @ Y = 479.0 FR 60 IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02 SEE AVMAX WO 81054 WC 1200
- [SDR V0XD2023050300001](https://openairdocs.org/sdr/V0XD2023050300001.md): Gusset · corroded · May 3, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > R/H AISLE GUSSET UNDER SEAT TRACK AT FRM 35 TO FRM 39 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED R/H GUSSET IAW EMB 145 SRM 51-40-09, 51-40-02.
- [SDR V0XD20230502003](https://openairdocs.org/sdr/V0XD20230502003.md): Floor Support · corroded · May 2, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > R/H AISLE GUSSET SHOWS SIGNS OF CORROSION FROM FRM 39 TO FRM 45. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL FROM FRM 39- FRM 45 R/H SIDE IAW EMB 145 SRM 51-40-02. SEE AVMAX WO: 81054 WC: 1201
- [SDR V0XD20230502002](https://openairdocs.org/sdr/V0XD20230502002.md): Floor Support · corroded · May 2, 2023 · N260JX · Emb EMB135LR · Fuselage Miscellaneous Structure
  > RH FLOOR SILL APROX. FRM 35-41 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED RH FLOOR SILL AT FRM 35 - FRM 41 IAW EMB 145 SRM 51-40-02 SEE AVMAX WO: 81054 WC: 1186
- [SDR V0XD20230502001](https://openairdocs.org/sdr/V0XD20230502001.md): Floor Support · corroded · May 2, 2023 · N260JX · Emb EMB135LR · Fuselage Miscellaneous Structure
  > EVALUATE SURFACE CORROSION ON RH FLOOR SILL FRM 22-25. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED FLOOR SILL AT RH SIDE FROM FRM 22-25 IAW EMB 145 SRM 51-40-02 SEE AVMAX WO: 81054 WC: 1202
- [SDR V0XD20230501001](https://openairdocs.org/sdr/V0XD20230501001.md): Angle · bent · May 1, 2023 · N260JX · Emb EMB135LR · Fuselage Miscellaneous Structure
  > FLOOR BEAM SUPPORT ANGLE BENT AT FRM 67 LBL16 UNDER BAGGAGE DOOR FLOOR PANEL 271FF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T, ANGLES AND PLATE IAW EMB 145 SRM 51-40-02 & EMB 145 SRM 51-20-03. SEE AVMAX WO 81054 WC 1168
- [SDR V0XD20230426002](https://openairdocs.org/sdr/V0XD20230426002.md): Floor Support · corroded · Apr 26, 2023 · N260JX · Emb EMB135LR · Fuselage Miscellaneous Structure
  > RH FLOOR SILL AT FRM 25-31 AND FRM 35-36 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED SILL AND EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-22-10 REPLACED SILL AT RH FLOOR FROM FRM 25-35 IAW EMB145 SRM 51-40-02, 51-40-09. SEE AVMAX
- [SDR V0XD20230426001](https://openairdocs.org/sdr/V0XD20230426001.md): Profile · corroded · Apr 26, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > L/H AISLE FLOOR GUSSET HAS SIGNS OF CORROSION FROM FRM 23.5 TO FRM 32.5. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET IAW EMB 135/145 SRM 51-40-02.
- [SDR V0XD20230424004](https://openairdocs.org/sdr/V0XD20230424004.md): Seat Track · corroded · Apr 24, 2023 · N260JX · Emb EMB135LR · Fuselage, Seat/Cargo Attach Fittings
  > L/H AISLE SEAT TRACK FLOOR GUSSET CORRODED AT FRM 20 TO FRM 24. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR GUSSET ( DIGITAL LEFT) IAW EMB 135 SRM 51-20-03, 51-40-02. SEE AVMAX WO 81054 WC 1181
- [SDR V0XD20230424003](https://openairdocs.org/sdr/V0XD20230424003.md): Support · cracked · Apr 24, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > LH PRECOOLER AFT MOUNTING BRACKET CRACKED BEYOND STOP DRILL. CORRECTIVE ACTION: REMOVED AND REPLACED LH PRECOOLER AFT MOUNTING BRACKET PART # 145-31654-001 BATCH # 167-211 IAW EMB 135/145 SRM 51-40-02 SEE AVMAX WO 81054 WC 4033
- [SDR V0XD20230424002](https://openairdocs.org/sdr/V0XD20230424002.md): Unknown · bent · Apr 24, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > BAGGAGE AREA FLOOR BEAM CREASED AND BENT AT FRM 65 2'5" FROM BAGGAGE DOOR SURROUND UNDER FLOOR PANEL 271BF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T ON FRM 65 UNDER APNEL 271BF IAW EMB 135 SRM 51-40-02 SEE AVMAX WO 81054 WC 1170.
- [SDR V0XD20230424001](https://openairdocs.org/sdr/V0XD20230424001.md): Unknown · bent · Apr 24, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > BAGGAGE AREA FLOOR BEAM BENT AT FRM 68 2' 5" FROM BAGGAGE DOOR SURROUND UNDER FLOOR PANEL 271BF. CORRECTIVE ACTION: REMOVED AND REPLACED PROFILE T LOCATED AT FRM 68 UNDER PANEL 271BF IAW SRM 51-40-02 SEE AVMAX WO 81054 WC 1169
- [SDR V0XD20230421001](https://openairdocs.org/sdr/V0XD20230421001.md): Unknown · corroded · Apr 21, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > L/H SIDE FLOOR SILL HAS SIGNS OF CORROSION BETWEEN FRM 20- FRM 24. CORRECTIVE ACTION: REMOVED DAMAGED FLOOR SILL AND INSTALLED NEW FLOOR SILL ON L/H SIDE FROM FRM 18- FRM 23 IAW EMB 135 SRM 51-40-02. SEE AVMAX WO 81054 WC 1180
- [SDR V0XD20230417001](https://openairdocs.org/sdr/V0XD20230417001.md): Unknown · chafed · Apr 17, 2023 · N260JX · Emb EMB135LR · Fuselage Structure (General)
  > BAGGAGE COMPARTMENT FLOOR SILL CHAFED R/H AFT BETWEEN FRM 70- FRM 71. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL AT R/H AFT BETWEEN FRM 70 TO FRM 71 IAW EMB 135 SRM 51-40-02.
- [SDR 4DPA2023011000001](https://openairdocs.org/sdr/4DPA2023011000001.md): Autopilot Sys · failed · Jan 10, 2023 · N260JX · Emb EMB135LR · Autopilot System
  > ISSUE-CREW REPORTED AROUND 1000 FEET ON TAKEOFF INTO IMC WITH THE LEFT SEAT PILOT FLYING, SCREENS 1, 2, 3, AND 4 AND ISIS WENT OUT. AUTOPILOT FAILED, FD NOT VISIBLE ON SINGLE REMAINING SCREEN, AND NAV 2 WENT OUT AND NEVER CAME BACK. ONE OR TWO OF THE FAILED LE
- [SDR 4DPA2022110300001](https://openairdocs.org/sdr/4DPA2022110300001.md): Proximity Switch · failed · Nov 3, 2022 · N260JX · Emb EMB135LR · Landing Gear Position and Warning
  > CREW REPORTED-RCVD CAS MESSAGE “LG AIR/GND FAIL.” GEAR WOULD NOT RETRACT WHEN GO-AROUND WAS INITIATED. MESSAGE CLEARED UPON TOUCHDOWN. CORR ACTION- REMOVED AND REPLACED NLG PROXIMITY SWITCH PERFORMED TWO GEAR SWINGS ALL OPS TESTS GOOD.
- [SDR 4DPA2021060200001](https://openairdocs.org/sdr/4DPA2021060200001.md): Hinge · broken · Jun 2, 2021 · N260JX · Emb EMB135LR · Pressure Regulator/Outflow Valve
  > AFTER TAKEOFF CAB ALT PRESSURE WAS AMBER AND ROSE WITH THE AIRCRAFT. IT LEAKED AT ABOUT 9800 FT AND THE AIRCRAFT ALTITUDE WAS APPROX 11.3. WE DESCENDED BACK TO 10000 AND THE CAB ALT HELD WITHIN 200 FT WHATEVER ALT THEY WERE AT. COMPLETED EMB 135 AMM 21-31-00
- [SDR 4DPA20210602](https://openairdocs.org/sdr/4DPA20210602.md): Hinge · broken · Jun 2, 2021 · N260JX · Emb EMB135LR · Cabin Pressure Control System
  > DISC: AFTER TAKEOFF CABIN ALT PRESSURE WAS AMBER AND ROSE WITH THE AIRCRAFT. IT LEAKED AT ABOUT 9800FT AND THE AIRCRAFT ALTITUDE WAS APPROX 11.3FT. THAT DESCENDED BACK TO 10000FT AND THE CABIN ALT HELD WITHIN 200FT WHATEVER ALT THEY WERE AT. CORR ACTION: COMPL
- [SDR 4DPA2020060940001](https://openairdocs.org/sdr/4DPA2020060940001.md): Relay · failed · Jun 4, 2020 · N260JX · Emb EMB135LR · Landing Gear Door Retract Section
  > NOSE LANDING DOORS NEVER CLOSED AFTER PUTTING THE GEAR UP. WE FELT THE VIBRATION AND THE NOISE EVEN AFTER WE TRIED TO PUT THE GEAR UP AND DOWN AGAIN. REMOVED AND REPLACED FAULTY DOOR CONTROL RELAY K0642.

## 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 = 'N260JX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N260JX/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.