# Service difficulty reports: N280SK, cancelled Jan 24, 2022

A list on [N280SK, cancelled Jan 24, 2022](https://openairdocs.org/deregistered/N280SK-2022-01-24.md).

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

- [SDR UHLA201606030292](https://openairdocs.org/sdr/UHLA201606030292.md): Switch · out of adjust · Jun 3, 2016 · N280SK · Emb EMB145LR · Door Warning System
  > MAIN CABIN DOOR SHOWS OPEN ON THE MFD. ADJUSTED FWD LOCK BOX SWITCH ON MED IAW AMM 52-12-09. OPS CHECK GOOD.
- [SDR UHLA201605250264](https://openairdocs.org/sdr/UHLA201605250264.md): Spring · damaged · May 25, 2016 · N280SK · Emb EMB145LR · Passenger/Crew Doors
  > F/A ADVISES STAIRS SLAM FLAT WHEN RAISING MCD. R & R SPRINGS ON TOP OF MCD IAW AMM 52-10-07. OPS CHECK GOOD.
- [SDR UHLA201510290776](https://openairdocs.org/sdr/UHLA201510290776.md): Handle · unsecure · Oct 29, 2015 · N280SK · Emb EMB145LR · Passenger/Crew Doors
  > THE MAIN ENTRY DOOR HANDLE WAS FOUND NOT SECURE. MAINTENANCE SECURED THE HANDLE IAW AMM 52-11-06 AND ALL OPS CHECKS WERE GOOD.
- [SDR UHLA2015021900146](https://openairdocs.org/sdr/UHLA2015021900146.md): Floor Support · corroded · Feb 19, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE BEAM WAS REPAIRED IAW ETD 2015-145-016197.
- [SDR UHLA2015021500147](https://openairdocs.org/sdr/UHLA2015021500147.md): Floor Support · corroded · Feb 15, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM INBD FLOORBOARD FLANGE AT FRAME 25. THE FLANGE WAS REPAIRED IAW SRM 51-40-024.
- [SDR UHLA2015021400144](https://openairdocs.org/sdr/UHLA2015021400144.md): Shear Tie · cracked · Feb 14, 2015 · N280SK · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING INSPECTION, THE APU FIREWALL SHEAR CLIP WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 8L-9L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015021400143](https://openairdocs.org/sdr/UHLA2015021400143.md): Shear Tie · cracked · Feb 14, 2015 · N280SK · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING INSPECTION, THE RT SHEAR CLIP AT FRAME 80 AND STRINGERS 5R-7R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015021300139](https://openairdocs.org/sdr/UHLA2015021300139.md): Floor Support · corroded · Feb 13, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 22. THE BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015021200142](https://openairdocs.org/sdr/UHLA2015021200142.md): Door Frame · corroded · Feb 12, 2015 · N280SK · Emb EMB145LR · Fuselage Main, Structure
  > DURING INSPECITON, CORROSION WAS FOUND ON THE LOWER SIDE OF THE SERVICE DOOR BOTTOM FRAME. THE FRAME WAS REPAIRED IAW ETD 2015-145-016097.
- [SDR UHLA2015021200140](https://openairdocs.org/sdr/UHLA2015021200140.md): Floor Support · corroded · Feb 12, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LT INBD OMEGA BEAM FLOOR FLANGE. THE FLANGE WAS REPLACED IAW SRM 53-00-10.
- [SDR UHLA2015021100148](https://openairdocs.org/sdr/UHLA2015021100148.md): Structure · corroded · Feb 11, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RT OTBD SILL AT FRAME 18 THROUGH 20. THE SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015021100145](https://openairdocs.org/sdr/UHLA2015021100145.md): Threshold · corroded · Feb 11, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER ON THE CENTER SERVICE DOOR THRESHOLD SILL. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02.
- [SDR UHLA2015021100141](https://openairdocs.org/sdr/UHLA2015021100141.md): Floor Support · corroded · Feb 11, 2015 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT THE LT OMEGA BEAM AND FRAME 20. THE ANGLE WAS REPAIRED IAW SRM 53-21-10.
- [SDR UHLA2015021000149](https://openairdocs.org/sdr/UHLA2015021000149.md): Frame · misinstalled · Feb 10, 2015 · N280SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, THE WORKING RIVETS ON FRAME 79 BETWEEN STRINGERS 4R AND 6R WERE REPLACED IAW ETD 2015-145-017668.
- [SDR CHQA20141229362](https://openairdocs.org/sdr/CHQA20141229362.md): Switch · faulty · Dec 29, 2014 · N280SK · Emb EMB145LR · Pneumatic Distribution System
  > THE CREW REPORTED THAT THEY RECEIVED A BLEED 2 VLV CLOSED MSG IN FLIGHT. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE BLEED SYS 2 PUSHBUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130628251](https://openairdocs.org/sdr/CHQA20130628251.md): Battery · inoperative · Jun 28, 2013 · N280SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE MAIN ENTRY DOOR EMERGENCY EXIT SIGN WAS FOUND NOT TO ILLUMINATE. MX REPLACED THE EMERGENCY LIGHT INVERTER BATTERY NR 1 AFTER WHICH ALL OPS CHECKS WERE FOUND TO BE GOOD.
- [SDR CHQA20130520173](https://openairdocs.org/sdr/CHQA20130520173.md): Relay · failed · May 20, 2013 · N280SK · Emb EMB145LR · Rudder Control System
  > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCH
- [SDR CHQA20130520172](https://openairdocs.org/sdr/CHQA20130520172.md): Relay · failed · May 20, 2013 · N280SK · Emb EMB145LR · Rudder Control System
  > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCH
- [SDR CHQA20130520171](https://openairdocs.org/sdr/CHQA20130520171.md): Pressure Switch · malfunctioned · May 20, 2013 · N280SK · Emb EMB145LR · Rudder Control System
  > CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCH
- [SDR CHQA20130321093](https://openairdocs.org/sdr/CHQA20130321093.md): Fitting · cracked · Mar 21, 2013 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACKED SHEAR CLIP WAS FOUND AT FRAME 38 FROM STRINGERS 21L TO 21R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20130318094](https://openairdocs.org/sdr/CHQA20130318094.md): Fitting · cracked · Mar 18, 2013 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH 53-31-04.
- [SDR CHQA20130316095](https://openairdocs.org/sdr/CHQA20130316095.md): Skin · corroded · Mar 16, 2013 · N280SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 38 AND 39 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-01.
- [SDR CHQA20130316092](https://openairdocs.org/sdr/CHQA20130316092.md): Skin · corroded · Mar 16, 2013 · N280SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 37 AND 38 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-01.
- [SDR CHQA20130128032](https://openairdocs.org/sdr/CHQA20130128032.md): Light · damaged · Jan 28, 2013 · N280SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY LIGHTING STRIP THAT IS FARTHEST AFT WAS FOUND TO HAVE A BROKEN LEAD. THE EMERGENCY FLOOR LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20120329111](https://openairdocs.org/sdr/CHQA20120329111.md): Hinge · cracked · Mar 29, 2012 · N280SK · Emb EMB145LR · Ailerons
  > DURING INSPECTION, THE LEFT AILERON DAMPER HINGE WAS FOUND TO BE CRACKED. THE LEFT AILERON DAMPER HINGE WAS REPLACED IAW SRM 51-40-08 AND 51-40-02.
- [SDR CHQA20120301070](https://openairdocs.org/sdr/CHQA20120301070.md): Acm · failed · Mar 1, 2012 · N280SK · Emb EMB145LR · Cabin Cooling System
  > CREW REPORTED THAT THERE WAS SMOKE IN THE CABIN AND COCKPIT DURING TAKEOFF. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED THE FAULT ISOLATION MANUAL TASK WITH NO DEFECTS NOTED. THE CREW THEN REPORTED A BURNING SME
- [SDR CHQA201100413](https://openairdocs.org/sdr/CHQA201100413.md): Inverter · inoperative · Oct 24, 2011 · N280SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER ABOVE THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100256](https://openairdocs.org/sdr/CHQA201100256.md): Relay · burned · Jun 28, 2011 · N280SK · Emb EMB145LR · Pitot/Static Anti-Ice System
  > CREW REPORTED THAT DURING FLIGHT RECEIVED A PITOT 3 INOPERATIVE MESSAGE ON THE EICAS FOLLOWED SHORTLY BY AN UNUSUAL ODOR IN THE FLIGHT DECK. THE CREW DIVERTED TO KIAD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE PITOT 3 CURRENT SENSOR RELAY K0057 AND S
- [SDR CHQA201100202](https://openairdocs.org/sdr/CHQA201100202.md): Skin · damaged · May 27, 2011 · N280SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING INSPECTION, A PREVIOUS BLEND ON THE RIGHT CENTER FUSELAGE SKIN, SECTION I BETWEEN FRAME 16-17 AND STRINGER 19R-20R, WAS FOUND TO BE OUT OF LIMITS. THE DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-01.
- [SDR CHQA201100194](https://openairdocs.org/sdr/CHQA201100194.md): Frame · corroded · May 27, 2011 · N280SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65, BETWEEN STRINGERS 15L AND 17L. THREE AREAS WERE FOUND WITH THE DEEPEST DAMAGE BEING 0.022" DEEP. THE DAMAGE WAS BLENDED OUT, AND A 0.051" DOUBLER INSTALLED PER EMBRAER ETD 2011-145-100340 WITH NO FURTHER DE
- [SDR CHQA201100216](https://openairdocs.org/sdr/CHQA201100216.md): Skin · dented · May 21, 2011 · N280SK · Emb EMB145LR · Elevator, Plate/Skin
  > DURING INSPECTION THE LOWER CONTROL SURFACE OF THE LEFT ELEVATOR WAS FOUND TO BE DENTED APPROXIMATELY AT YH-1280.00. THE DENT WAS REPAIRED IN ACCORDANCE WITH ETD2011-145/100372 REV A.
- [SDR CHQA201100218](https://openairdocs.org/sdr/CHQA201100218.md): Beam · corroded · May 20, 2011 · N280SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE LOWER BEAM. THE CARGO FLOOR STRUCTURE LOWER BEAM WAS REPLACED; THE NEW PART WAS INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.
- [SDR CHQA200900199](https://openairdocs.org/sdr/CHQA200900199.md): Uplock Switch · faulty · Sep 6, 2009 · N280SK · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 3075, LGA TO RIC. ON TAKEOFF THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE NOSE GEAR INDICATION SHOWED YELLOW CROSS HATCHES AND A LANDING GEAR LEVER DISAGREE MESSAGE WAS PRESENT ON EICAS. THE HANDLE WAS CYCLED WITH THE SAME RESU
- [SDR CHQA200900147](https://openairdocs.org/sdr/CHQA200900147.md): Controller · inoperative · Jun 28, 2009 · N280SK · Emb EMB145LR · Cabin Pressure Controller
  > THE ACFT HAD THE AUTO PRESSURIZATION MODE DEFERRED WHEN IT DEPARTED. DURING CLIMB-OUT, WHILE CLIMBING THROUGH 9,000 FT THE CABIN ALTITUDE INDICATED 8,500 FT. THE CREW LEVELED OFF AT 10,000FT THEN DESCENDED TO 9,000FT. THE CREW WAS UNABLE TO PRESSURIZE THE C
- [SDR CHQA200900127](https://openairdocs.org/sdr/CHQA200900127.md): Inverter · inoperative · May 19, 2009 · N280SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION THE EMERGENCY FLOOR LIGHTS NR 4, 6, 7, 8 WERE FOUND INOP. THE NR 4 FLOOR PROXIMITY LIGHT STRIP AND NR 4 INVERTER WERE REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY.
- [SDR CHQA200900029](https://openairdocs.org/sdr/CHQA200900029.md): Proximity Sensor · faulty · Jan 21, 2009 · N280SK · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 3008, CMH TO LGA - DURING INITIAL CLIMB-OUT AFTER GEAR RETRACTION, THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS, AND WITHIN 1 MINUTE A ENG 1-2 REV DISAGREE. THE QRH CHECKLISTS WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT BACK AT CMH.
- [SDR CHQA200800207](https://openairdocs.org/sdr/CHQA200800207.md): Inverter · inoperative · Oct 19, 2008 · N280SK · Emb EMB145LR · Emergency Lighting
  > FLIGHT 3084, CMH TO DCA. DURING INSPECTION THE EMERGENCY EXIT SIDEWALL LIGHT AT SEATS 12 D&F WAS INOP. MAINTENANCE FOUND THE NR 4 INVERTER INOP AND WAS REPLACED. AFTER REPLACEMENT, THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY.
- [SDR CHQA200600060](https://openairdocs.org/sdr/CHQA200600060.md): Carbon Seal · defective · May 12, 2006 · N280SK · Emb EMB145LR · Turbine Engine Oil System
  > NORMAL FLIGHT UNTIL CLIMBING THROUGH FL300, NOTICED OIL PRESSURE FOR NR 2 ENGINE WAS IN THE AMBER RANGE ON THE EICAS. CHECKED QUANTITY OF OIL ON NR 2 ENGINE, NOTICED ONLY 3 QUARTS (8 QUARTS OBSERVED DURING AFTER START CHECK). PRESSURE FELL TO 19 PSI IN THE R
- [SDR CHQA20050192](https://openairdocs.org/sdr/CHQA20050192.md): Wire · broken · Nov 5, 2005 · N280SK · Emb EMB145LR · Emergency Lighting
  > AFT STRIP EMERGENCY FLOOR LIGHTING HAS BROKEN WIRES. REPLACED AFT EMERGENCY LIGHTING STRIP IAW MM 33-26-06. OPS TEST GOOD.
- [SDR CHQA200500139](https://openairdocs.org/sdr/CHQA200500139.md): Radio · inoperative · Aug 9, 2005 · N280SK · Emb EMB145LR · VHF Communications System
  > FLIGHT 3143 - GSP-LGA - DURING DESCENT, AN ODOR SIMILAR TO ELECTRICAL BURNING WAS NOTICED FOLLOWED BY COM 1 FAILING. REMOVED AND REPLACED THE NR 1 INTEGRATED COM UNIT IAW EMB 145 AMM 23-00-01. OPS CHECK GOOD.
- [SDR CHQA200500126](https://openairdocs.org/sdr/CHQA200500126.md): Engine · unserviceable · Jul 12, 2005 · N280SK · Emb EMB145LR · Engine (Turbine/Turboprop)
  > AFTER STARTING DESCENT OUT OF 16,000 FT, HEAT-TYPE ODOR NOTED SHORTLY AFTER MAKING INITIAL POWER REDUCTION. ODOR SUBSIDED AND ATTRIBUTED TO OCCASIONAL PACK SMELL. SOP UNTIL AFTER PASSING APPROX 400 AGL. A/C CONFIGURED AND SET FOR NORMAL VMC ILS. NR 1 ENGINE
- [SDR CHQA200500082](https://openairdocs.org/sdr/CHQA200500082.md): Engine · failed · Apr 13, 2005 · N280SK · Emb EMB145LR · Engine (Turbine/Turboprop)
  > DURING LATE STAGES OF CLIMB, AT APPROX 24500 FT., NOTICED A SPIKE IN NR 2 ITT OF 911 C. FOR 1 SEC. REDUCED THRUST ON NR 2, ITT RETURNED TO GREEN RANGE. LEVELED OFF AT FL260 & SET TO CRUISE. SET POWER TO SAME N1 TO ALLOW CHK OF ENG PARAMS. BOTH N1 SETTINGS 80.5
- [SDR CHQA200400563](https://openairdocs.org/sdr/CHQA200400563.md): Engine · leaking · Oct 9, 2004 · N280SK · Emb EMB145LR · Engine (Turbine/Turboprop)
  > DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS ABORTED AND THE SMOKE DISSIPATED RAPIDLY AND CLEARED AFTER POWER REDUCTION. ALL TEMPERATURES WERE NO
- [SDR CHQA200400562](https://openairdocs.org/sdr/CHQA200400562.md): Carbon Seal · leaking · Oct 6, 2004 · N280SK · Emb EMB145LR · Turbine Engine Oil System
  > FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. THE TAKEOFF WAS ABORTED AND THE PLANE WAS EVACUATED ON THE TAXIWAY. MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SMOKE TO COMING FROM

## 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 = 'N280SK' AND deregistration_id = 'N280SK-2022-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N280SK-2022-01-24/reports

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