# Service difficulty reports: N268SK, cancelled Sep 8, 2018

A list on [N268SK, cancelled Sep 8, 2018](https://openairdocs.org/deregistered/N268SK-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.

- [SDR CHQA20140711210](https://openairdocs.org/sdr/CHQA20140711210.md): Light · inoperative · Jul 11, 2014 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX RELAMPED THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20140621190](https://openairdocs.org/sdr/CHQA20140621190.md): Solenoid Valve · failed · Jun 21, 2014 · N268SK · Emb EMB145LR · Landing Gear Door Retract Section
  > CREW REPORTED THAT THERE WAS A LOUD NOISE IN COCKPIT DURING FLIGHT. THE CREW SUSPECTED THAT THE NLG DOORS WERE OPEN. THE ACFT WAS RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NLG DOOR SOLENOID VLV. OPERATIONAL & LEAK CHECKS WERE GOO
- [SDR CHQA20131013369](https://openairdocs.org/sdr/CHQA20131013369.md): A/C Pack · failed · Oct 13, 2013 · N268SK · Emb EMB145LR · Cabin Cooling System
  > CREW REPORTED THAT DURING CRUISE, SMOKE WAS NOTICED IN THE COCKPIT. THE CREW DIVERTED AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED THE ISSUE TO THE PACK 1 SYSTEM. THE PACK 1 SYSTEM WAS DEFERRED. ACM ON THE PACK
- [SDR CHQA20130725190](https://openairdocs.org/sdr/CHQA20130725190.md): Inverter · inoperative · Jul 25, 2013 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE AISLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 2 INVERTER. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130725189](https://openairdocs.org/sdr/CHQA20130725189.md): Inverter · inoperative · Jul 25, 2013 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 INVERTER. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130610209](https://openairdocs.org/sdr/CHQA20130610209.md): Frame · corroded · Jun 10, 2013 · N268SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02.
- [SDR CHQA20120628209](https://openairdocs.org/sdr/CHQA20120628209.md): Support · corroded · Jun 28, 2012 · N268SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE AFT RIGHT FUSELAGE INSIDE ACCESS DOOR 272AR TOILET DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE DISCHARGE CUP IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20120628208](https://openairdocs.org/sdr/CHQA20120628208.md): Frame · damaged · Jun 28, 2012 · N268SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, A HOLE WAS FOUND IN FRAME 65 ON THE RIGHT SIDE NEAR STRINGER 12R. MAINTENANCE INSTALLED A NEW REPAIR DOUBLER IN ACCORDANCE WITH ETD2012-145-009260.
- [SDR CHQA20120605180](https://openairdocs.org/sdr/CHQA20120605180.md): Transducer · disconnected · Jun 5, 2012 · N268SK · Emb EMB145LR · Brake
  > CREW REPORTED LOSS OF BRAKING EFFECTIVENESS ON LANDING ROLL. A BRAKE DEGRADED MESSAGE APPEARED AS WELL. AFTER PUSHING THE BRAKES TO THE FLOOR BRAKES BEGAN WORKING AGAIN. MAINTENANCE FOUND THE RIGHT OUTBOARD MAIN LANDING GEAR WHEEL SPEED TRANSDUCER NOT CONNE
- [SDR CHQA20120203040](https://openairdocs.org/sdr/CHQA20120203040.md): Warning System · false activation · Feb 3, 2012 · N268SK · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED THAT THEY RECEIVED AN EMERGENCY LIGHT NO ARMED EICAS MESSAGE WITH THE EMERGENCY LIGHTS IN THE ARMED POSITION DURING PRE-FLIGHT INSPECTION. MAINTENANCE RESET THE AIRCRAFT'S POWER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201200037](https://openairdocs.org/sdr/CHQA201200037.md): Inverter · inoperative · Jan 30, 2012 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, MULTIPLE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100415](https://openairdocs.org/sdr/CHQA201100415.md): Battery · discharged · Oct 24, 2011 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY FLOOR LIGHTS BETWEEN ROW 8 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100253](https://openairdocs.org/sdr/CHQA201100253.md): Frame · cracked · Jun 12, 2011 · N268SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE DIRECT VISION WINDOW LOWER BEAM. MAINTENANCE REPLACED THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE DIRECT VISIO
- [SDR CHQA201100255](https://openairdocs.org/sdr/CHQA201100255.md): Frame · corroded · Jun 11, 2011 · N268SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, SURFACE CORROSION WAS FOUND ON THE LEFT WINDSHIELD AIRCRAFT FRAME ON THE LOWER OUTBOARD SIDE AROUND THE DOME NUT. MAINTENANCE REPAIRED THE LEFT WINDSHIELD AIRCRAFT FRAME, LOWER OUTBOARD SIDE IN ACCORDANCE WITH ETD2011-145-100872.
- [SDR CHQA201100254](https://openairdocs.org/sdr/CHQA201100254.md): Floor Support · cracked · Jun 11, 2011 · N268SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100252](https://openairdocs.org/sdr/CHQA201100252.md): Floor Support · cracked · Jun 11, 2011 · N268SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100251](https://openairdocs.org/sdr/CHQA201100251.md): Floor Support · cracked · Jun 11, 2011 · N268SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION A CRACK WAS FOUND ON THE MID OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE MID OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.
- [SDR CHQA201100050](https://openairdocs.org/sdr/CHQA201100050.md): Check Valve · damaged · Mar 7, 2011 · N268SK · Emb EMB145LR · Cabin Pressure Control System
  > FLT CREW REPORTED WHILE CLIMBING THROUGH FL270, RECEIVED A "CABIN" AURAL WARNING. NO RELATED EICAS MESSAGES DISPLAYED. CABIN PRESSURE INDICATED OVER 10,000FT & REPORTED TO BE CLIMBING TO 11,000FT. MEMORY ITEMS FOLLOWED & ACFT BEGAN DESCENT TO 10,000FT & DEC
- [SDR CHQA201000174](https://openairdocs.org/sdr/CHQA201000174.md): Light · inoperative · Sep 1, 2010 · N268SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, TWO FLOOR PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. THE FLOOR PROXIMITY LIGHTS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA200900220](https://openairdocs.org/sdr/CHQA200900220.md): Connector · broken · Oct 12, 2009 · N268SK · Emb EMB145LR · Light System Wiring
  > DURING INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE FOUND A BROKEN WIRE AT THE OVERWING LAMP RECEPTACLE. THE CONNECTOR WAS REPLACED AND THE EMERGENCY LIGHT OPERATED NORMALLY.
- [SDR CHQA200800194](https://openairdocs.org/sdr/CHQA200800194.md): Connector · loose · Oct 5, 2008 · N268SK · Emb EMB145LR · Light System Wiring
  > MAINTENANCE FOUND THE BACK SIDE OF THE CENTER AISLE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE RESET THE CONNECTOR ON THE LIGHT AND THE SYSTEM OPS CHECKED GOOD.
- [SDR CHQA200500204](https://openairdocs.org/sdr/CHQA200500204.md): Smoke · detected · Dec 2, 2005 · N268SK · Emb EMB145LR · Air Distribution System
  > TOOK OFF FROM DCA WITH NO PROBLEMS. AT 1500 FT, BROUGHT FLAPS UP AND WENT TO CLIMB THRUST, NOTICED COCKPIT SEEMED A LITTLE HAZY. F/O OFFICER NOTICED HAZE. HAZE STARTED TO GET THICKER. F/A ATTENDANT SAW SMOKE OR HAZE IN THE CABIN. DIVERTED TO IAD. RAN ALL
- [SDR CHQA200500205](https://openairdocs.org/sdr/CHQA200500205.md): Light · burned out · Dec 2, 2005 · N268SK · Emb EMB145LR · Emergency Lighting
  > EMERGENCY FLOOR LIGHT STRIP THIRD BACK INOPERATIVE. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW MM 33-60-00. NO FURTHER DEFECTS NOTED.
- [SDR CHQA200500067](https://openairdocs.org/sdr/CHQA200500067.md): Wire · broken · Mar 30, 2005 · N268SK · Emb EMB145LR · Light System Wiring
  > EMERGENCY EXIT LIGHT IDENTIFIER IS INOPERATIVE. TROUBLESHOT PROBLEM TO A BROKEN WIRE AT W192-8588-22 PRIOR TO SPLICE SP9048 REF EMB AWM 33-50-50. REQUIRED REWIRE IAW EMB 145AMM 20-31-00. OPS CHECK GOOD IAW CHQ JC E33-50-00-710-001.
- [SDR CHQA200500024](https://openairdocs.org/sdr/CHQA200500024.md): Carbon Seal · leaking · Jan 31, 2005 · N268SK · Emb EMB145LR · Turbine Engine Oil System
  > FLIGHT 3217 - LGA-PHL - WHILE EN ROUTE A LAV SMOKE MASTER WARNING APPEARED ON EICAS. THE APPROPRIATE QRH CHECKLIST WAS COMPLETED. THE FLIGHT ATTENDANT CHECKED THE LAV AND SAW NO SMOKE OR FIRE AND NO SMELL WAS PRESENT ANYWHERE IN THE AIRCRAFT. THE EICAS MESS
- [SDR CHQA200500021](https://openairdocs.org/sdr/CHQA200500021.md): Smoke Detector · malfunctioned · Jan 28, 2005 · N268SK · Emb EMB145LR · Smoke Detection
  > FLIGHT 3083 - ROC-DCA - AFTER BOARDING THE AIRCRAFT TAXIED TO THE DEICE PAD FOR DEICING. AFTER THREE MINUTES THE BLEEDS AND PACKS WERE TURNED ON AND THE AIRCRAFT DEPARTED NORMALLY. DURING CLIMB OUT AT 10,000 FEET, A LAV SMOKE WARNING WAS ON EICAS. THE FLIGH
- [SDR CHQA200500018](https://openairdocs.org/sdr/CHQA200500018.md): Carbon Seal · leaking · Jan 25, 2004 · N268SK · Emb EMB145LR · Turbine Engine Oil System
  > FLIGHT 3063 - LGA-SYR - EN ROUTE TO SYR A SMELL OF BURNING PLASTIC OR AN ELECTRICAL FIRE WAS NOTED IN THE COCKPIT AND CABIN. THE ODOR MADE EYES WATER AND THROAT SORE. LANDED IN SYR WITHOUT EVENT. MAINTENANCE FOUND NR 0 CARBON SEAL LEAKING ON THE LEFT HAND E

## 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 = 'N268SK' AND deregistration_id = 'N268SK-2018-09-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N268SK-2018-09-08/reports

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