# Service difficulty reports: N265SK, cancelled Sep 8, 2018

A list on [N265SK, cancelled Sep 8, 2018](https://openairdocs.org/deregistered/N265SK-2018-09-08.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 2 · 77 reports

- [SDR UHLA2015040200327](https://openairdocs.org/sdr/UHLA2015040200327.md): Attach Fitting · damaged · Apr 2, 2015 · N265SK · Emb EMB145 · Trailing Edge Flaps
  > DURING INSPECTION, ON THE LT WING, THE OTBD FLAP ROLLER ATTACHMENT ON THE RIB INBD SIDE WAS FOUND TO BE DAMAGED. THE FLAP ROLLER ATTACHMENT WAS REPAIRED IAW ETD 2015-145-031617.
- [SDR UHLA2015032700316](https://openairdocs.org/sdr/UHLA2015032700316.md): Track · corroded · Mar 27, 2015 · N265SK · Emb EMB145 · Nose/Tail Landing Gear
  > DURING INSPECTION, THE LT UPPER HALF BEARING TRACK ON THE NLG LEG WAS FOUND TO BE CORRODED. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179.
- [SDR UHLA2015032200326](https://openairdocs.org/sdr/UHLA2015032200326.md): Skin · damaged · Mar 26, 2015 · N265SK · Emb EMB145 · Rudder, Plate/Skin
  > DURING INSPECTION, DAMAGE ON THE RUDDER 2, LT LOWER SKIN WAS REPAIRED IAWETD 2015-145-030496-B.
- [SDR UHLA2015032600325](https://openairdocs.org/sdr/UHLA2015032600325.md): Frame · cracked · Mar 26, 2015 · N265SK · Emb EMB145 · Fuselage Main, Frame
  > DURING INSPECTION, A CRACK WAS FOUND AT FRAME 75 AND STRINGERS 2R AND 2L. THE CRACK WAS REPAIRED IAW ETD 2015-145-029344.
- [SDR UHLA2015032500315](https://openairdocs.org/sdr/UHLA2015032500315.md): Track · corroded · Mar 25, 2015 · N265SK · Emb EMB145 · Nose/Tail Landing Gear
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RT UPPER HALF BEARING TRACK OF THE NLG LEG. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179.
- [SDR UHLA2015032400322](https://openairdocs.org/sdr/UHLA2015032400322.md): Frame · cracked · Mar 24, 2015 · N265SK · Emb EMB145 · Fuselage Main, Frame
  > DURING INSPECITON, A CRACK WAS FOUND ON THE LT FLANGE AT FRAME 67. THE AREA WAS REPAIRED IAW ETD2015-145-028481, REV A.
- [SDR UHLA2015032400321](https://openairdocs.org/sdr/UHLA2015032400321.md): Frame · cracked · Mar 24, 2015 · N265SK · Emb EMB145 · Fuselage Main, Frame
  > DURING INSPECTION, THE LT REAR FUSELAGE, END FRAME 66, AT THE LOWER BEAM, WAS FOUND TO BE CRACKED. THE BEAM WAS REPAIRED IAW ETD2015-145-028481, REV A.
- [SDR UHLA2015032300314](https://openairdocs.org/sdr/UHLA2015032300314.md): Floor Support · corroded · Mar 23, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RT REAR FUSELAGE SILL BETWEEN FRAME 71 AND FRAME 73. THE SILL WAS REPLACED IAW SRM 51-40-03.
- [SDR UHLA2015032300313](https://openairdocs.org/sdr/UHLA2015032300313.md): Floor Support · corroded · Mar 23, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT REAR FUSELAGE SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032300312](https://openairdocs.org/sdr/UHLA2015032300312.md): Floor Support · corroded · Mar 23, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE III LT FLOOR STRUCTURE SILL NR 6 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032300311](https://openairdocs.org/sdr/UHLA2015032300311.md): Floor Support · corroded · Mar 23, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE IV LT FLOOR STRUCTURE SILL NR 7 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-02.
- [SDR UHLA2015032100318](https://openairdocs.org/sdr/UHLA2015032100318.md): Mount · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Main, Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD RT GALLEY FITTING INBD AND OTBD. THE INBD AND OTBD RT GALLEY FLOOR FITTINGS WERE REPLACED IAW AMM 20-10-01.
- [SDR UHLA2015032100317](https://openairdocs.org/sdr/UHLA2015032100317.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE EMERGENCY EQUIPMENT STOWAGE SEAT TRACK FITTING WAS FOUND TO BE CORRODED. THE FITTING WAS REPLACED IAW AMM 25-26-03.
- [SDR UHLA2015032100310](https://openairdocs.org/sdr/UHLA2015032100310.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV RT FLOOR STRUCTURE SILL NR 6. THE SILL WAS REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-02.
- [SDR UHLA2015032100309](https://openairdocs.org/sdr/UHLA2015032100309.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 5. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100308](https://openairdocs.org/sdr/UHLA2015032100308.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 4. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100307](https://openairdocs.org/sdr/UHLA2015032100307.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE SILL NR 3. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100306](https://openairdocs.org/sdr/UHLA2015032100306.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II RT FLOOR STRUCTURE SILL NR 2. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100305](https://openairdocs.org/sdr/UHLA2015032100305.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II RT FLOOR STRUCTURE SILL NR 1. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100304](https://openairdocs.org/sdr/UHLA2015032100304.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III RT FLOOR STRUCTURE GUSSET NR 5. THE GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100303](https://openairdocs.org/sdr/UHLA2015032100303.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RT FLOOR STRUCTURE GUSSET NR 2. THE GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100302](https://openairdocs.org/sdr/UHLA2015032100302.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II LT FLOOR STRUCTURE GUSSET NR 3. THE GUSSET WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100301](https://openairdocs.org/sdr/UHLA2015032100301.md): Floor Support · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE 2 LT FLOOR STRUCTURE NR 2 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032100300](https://openairdocs.org/sdr/UHLA2015032100300.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT OTBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100299](https://openairdocs.org/sdr/UHLA2015032100299.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT OTBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100298](https://openairdocs.org/sdr/UHLA2015032100298.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT INBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100297](https://openairdocs.org/sdr/UHLA2015032100297.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT INBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100296](https://openairdocs.org/sdr/UHLA2015032100296.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT INBD SEAT TRACK NR 2 WAS FOUND TO BE CORRODED FROM FRAME 30 TO FRAME 35. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100295](https://openairdocs.org/sdr/UHLA2015032100295.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE RT INBD SEAT TRACK NR 1 WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100294](https://openairdocs.org/sdr/UHLA2015032100294.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LT OTBD SEAT TRACK NR 5 WAS FOUND TO BE CORRODED FROM FRAME 47 TO FRAME 52. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06.
- [SDR UHLA2015032100293](https://openairdocs.org/sdr/UHLA2015032100293.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LT INBD SEAT TRACK NR 4 WAS FOUND TO BE CORRODED FROM FRAME 35 TO FRAME 47. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06.
- [SDR UHLA2015032100292](https://openairdocs.org/sdr/UHLA2015032100292.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LT INBD SEAT TRACK NR 3 WAS FOUND TO BE CORRODED FROM FRAME 30 TO FRAME 35. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06.
- [SDR UHLA2015032100291](https://openairdocs.org/sdr/UHLA2015032100291.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LT INBD SEAT TRACK NR 2 WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032100290](https://openairdocs.org/sdr/UHLA2015032100290.md): Seat Track · corroded · Mar 21, 2015 · N265SK · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LT INBD SEAT TRACK NR 1 WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 24. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.
- [SDR UHLA2015032000320](https://openairdocs.org/sdr/UHLA2015032000320.md): Structure · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Cargo/Baggage Doors
  > DURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR LOWER L-SHAPE AT FRAME 65 - 68. THE L-SHAPE WAS REPAIRED IAW ETD2015-145-032521.
- [SDR UHLA2015032000319](https://openairdocs.org/sdr/UHLA2015032000319.md): Beam · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Cargo/Baggage Doors
  > DURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR LOWER BEAM. THE BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032000289](https://openairdocs.org/sdr/UHLA2015032000289.md): Structure · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Fuselage Main, Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE RIGHT HAND MIDDLE BEAM AT FRAME 23. THE BEAM WAS REPAIRED IAW ETD2015-145-028592.
- [SDR UHLA2015032000288](https://openairdocs.org/sdr/UHLA2015032000288.md): Channel · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRANCE DOOR FLOOR STRUCTURE FORWARD AND AFT OF THE U-SHAPE. THE FORWARD AND AFT U-SHAPE WERE REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032000287](https://openairdocs.org/sdr/UHLA2015032000287.md): Doubler · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Fuselage Main, Structure
  > DURING INSPECTION, THE CENTER FUSELAGE I FLOOR STRUCTURE RIGHT HAND BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. THE DOUBLER WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015032000286](https://openairdocs.org/sdr/UHLA2015032000286.md): Channel · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER FUSELAGE I, SERVICE DOOR BOTTOM CHANNEL WAS FOUND TO BE CORRODED. THE CHANNEL WAS REPAIRED IAW SRM 53-21-02.
- [SDR UHLA2015032000285](https://openairdocs.org/sdr/UHLA2015032000285.md): Fitting · corroded · Mar 20, 2015 · N265SK · Emb EMB145 · Water and Waste System
  > DURING INSPECTION, THE TOILET WASTE VALVE WAS FOUND TO BE CORRODED AROUND THE FITTING. THE FITTING WAS REPLACED IAW AMM 38-32-04 AND SRM 51-40-02.
- [SDR UHLA2015031900324](https://openairdocs.org/sdr/UHLA2015031900324.md): Frame · cracked · Mar 19, 2015 · N265SK · Emb EMB145 · Fuselage Main, Frame
  > DURING INSPECTION, THE LT AND RT HAND FRAME 10 WERE FOUND TO BE CRACKED. THE LT AND RT FRAME 10 WERE REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015031900323](https://openairdocs.org/sdr/UHLA2015031900323.md): Skin · loose · Mar 19, 2015 · N265SK · Emb EMB145 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, LOOSE RIVETS WERE FOUND ON THE LT AND RT FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3L-8L AND 3R-8R. THE SKIN WAS REPAIRED IAW ETD 2015-145027458, REV 8.
- [SDR CHQA20140808239](https://openairdocs.org/sdr/CHQA20140808239.md): Light · disconnected · Aug 8, 2014 · N265SK · Emb EMB145 · Emergency Lighting
  > DURING INSPECTION THE EMER FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE AT ROW 6. THE EMER LIGHT FLOOR STRIP WAS DEFERRED. THE DEFERRAL WAS CLEARED IN 8/8/14 WHEN MAINTENANCE RECONNECTED THE EMER LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER
- [SDR CHQA20140125022](https://openairdocs.org/sdr/CHQA20140125022.md): Battery · discharged · Jan 25, 2014 · N265SK · Emb EMB145 · Emergency Lighting
  > CREW REPORTED THAT DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROW 8 WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130614207](https://openairdocs.org/sdr/CHQA20130614207.md): Light · inoperative · Jun 14, 2013 · N265SK · Emb EMB145 · Emergency Lighting
  > DURING INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX PERFORMED AN ADJUSTMENT OF THE LIGHT AFTER WHICH ALL OPS CHECKS WERE SUCCESSFULLY COMPLETED.
- [SDR CHQA20130614206](https://openairdocs.org/sdr/CHQA20130614206.md): Light · inoperative · Jun 14, 2013 · N265SK · Emb EMB145 · Emergency Lighting
  > DURING INSPECTION, THE LEFT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND TO BE INOPERATIVE. MX PERFORMED AN ADJUSTMENT OF THE LIGHT. OPS CHECKED SUCCESSFUL.
- [SDR CHQA20130327096](https://openairdocs.org/sdr/CHQA20130327096.md): Pdu · failed · Mar 27, 2013 · N265SK · Emb EMB145 · Trailing Edge Flap Actuator
  > CREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE ON THE FINAL APPROACH WITH FLAP CHANNEL 2 ON MEL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO KJFK. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FLAP CHANNEL 1 TO BE AT FAULT AND RE-A
- [SDR CHQA201100378](https://openairdocs.org/sdr/CHQA201100378.md): Inverter · inoperative · Sep 21, 2011 · N265SK · Emb EMB145 · Emergency Lighting
  > DURING INSPECTION, THE FORWARD SIDE OF THE EXIT LOCATOR, AT THE EXIT ROW, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AC TO DC INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100141](https://openairdocs.org/sdr/CHQA201100141.md): Computer · inoperative · Apr 19, 2011 · N265SK · Emb EMB145LR · Ground Proximity System
  > CREW REPORTED GPWS FAIL, TERRAIN INOP, AND RADIO ALTIMETER 1 FAIL MESSAGES AND DIVERTED TO CMH DUE TO WEATHER WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 RADIO ALTIMETER COMPUTER WITH NO FURTHER DEFECTS NOTED.

Next page: https://openairdocs.org/deregistered/N265SK-2018-09-08/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 = 'N265SK' AND deregistration_id = 'N265SK-2018-09-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N265SK-2018-09-08/reports

---
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