# Service difficulty reports: N284SK, cancelled Jul 31, 2018

A list on [N284SK, cancelled Jul 31, 2018](https://openairdocs.org/deregistered/N284SK-2018-07-31.md).

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

- [SDR UHLA201606040294](https://openairdocs.org/sdr/UHLA201606040294.md): Lens · missing · Jun 4, 2016 · N284SK · Emb EMB145LR · Emergency Lighting
  > RIGHT OVERWING EXIT EMERGENCY LIGHT PROTECTIVE LENS MISSING. R & R RT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10.
- [SDR CHQA20131025379](https://openairdocs.org/sdr/CHQA20131025379.md): Bleed Valve · faulty · Oct 25, 2013 · N284SK · Emb EMB145LR · Compressor Bleed Valve
  > CREW REPORTED THAT THEY RECEIVED A BLEED ONE VALVE CLOSED MESSAGE AFTER TAKEOFF. FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 1 VALVE. OPS CHECKED WERE GOOD WITH NO FURTHER DEFECT
- [SDR CHQA20130831340](https://openairdocs.org/sdr/CHQA20130831340.md): Mount · damaged · Aug 31, 2013 · N284SK · Emb EMB145LR · APU Cowling/Containment
  > DURING INSPECTION, AN APU SHUNT MOUNTING BOLT ATTACHMENT WAS FOUND TO BE DAMAGED. THE SHUNT CONNECTION BAR HOLES AT FRAME 80 WERE REPAIRED IAW ETD 2013-145-034328.
- [SDR CHQA20130424128](https://openairdocs.org/sdr/CHQA20130424128.md): O-Ring · leaking · Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution System
  > CREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MESSAGE ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINT 20 AND 22. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20130424127](https://openairdocs.org/sdr/CHQA20130424127.md): O-Ring · leaking · Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution System
  > CREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MESSAGE ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOINT 20 AND 22. OPERATIONAL AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA20121115442](https://openairdocs.org/sdr/CHQA20121115442.md): Frame · damaged · Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE A PERMANENT REPAIR OF A LIGHTNING BURN AT FRAME 13 ON STRINGER 19L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-007033.
- [SDR CHQA20121115439](https://openairdocs.org/sdr/CHQA20121115439.md): Skin · damaged · Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE A PERMANENT REPAIR WAS COMPLETED OF A LIGHTNING BURN ON FRAME 23 ABOVE STRINGER 20L IN ACCORDANCE WITH ETD2012-145-007041. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.
- [SDR CHQA20121115441](https://openairdocs.org/sdr/CHQA20121115441.md): Fitting · cracked · Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE REPLACED THE UPPER SHEAR CLIP AND REPAIRED THE LOWER SHEAR CLIP IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20121115440](https://openairdocs.org/sdr/CHQA20121115440.md): Fitting · cracked · Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE REPLACED THE UPPER SHEAR CLIP AND REPAIRED THE LOWER SHEAR CLIP IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20121027438](https://openairdocs.org/sdr/CHQA20121027438.md): Angle · damaged · Nov 15, 2012 · N284SK · Emb EMB145LR · Wing Miscellaneous Structure
  > DURING HEAVY MAINTENANCE A PERMANENT REPAIR WAS COMPLETED ON THE RIGHT LOWER WING TRAILING EDGE IN ACCORDANCE WITH ETD 2012-145-015393B.
- [SDR CHQA20121112424](https://openairdocs.org/sdr/CHQA20121112424.md): Stringer · corroded · Nov 12, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 14. THE STRINGER WAS REPLACED.
- [SDR CHQA20121111423](https://openairdocs.org/sdr/CHQA20121111423.md): Support Fitting · corroded · Nov 11, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BETWEEN STRINGERS 21R AND 20R AT FRAME 12. THE AILERON TORQUE TUBE SUPPORT WAS REPLACED.
- [SDR CHQA20121031420](https://openairdocs.org/sdr/CHQA20121031420.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LEFT SIDE WALL SEAT TRACK FROM FRAME 30 THROUGH FRAME 33 WAS FOUND TO BE CORRODED. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 30 THROUGH 33 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031419](https://openairdocs.org/sdr/CHQA20121031419.md): Attach Bracket · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE AFT FLOOR ATTACH BRACKET AT THE PASSENGER DOOR THRESHOLD. THE AFT FLOOR ATTACH BRACKET AT THE PASSENGER DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH 51-40-02.
- [SDR CHQA20121031418](https://openairdocs.org/sdr/CHQA20121031418.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 41 THROUGH FRAME 47. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 41 THROUGH FRAME 47 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031417](https://openairdocs.org/sdr/CHQA20121031417.md): Gusset · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM DIGITAL FROM FRAME 20 THROUGH FRAME 23. THE CENTER OMEGA BEAM GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20121031416](https://openairdocs.org/sdr/CHQA20121031416.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 51. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 51 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031415](https://openairdocs.org/sdr/CHQA20121031415.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 28. THE LEFT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 28 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031414](https://openairdocs.org/sdr/CHQA20121031414.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 42 THROUGH FRAME 50. THE LEFT SIDE WALL SEAT TRACK SUPPORT FROM FRAME 42 THROUGH FRAME 50 WAS REPAIRED IN ACCORDANCE WITH SRM 51-30-03, 51-20-03, AND 51-40-02.
- [SDR CHQA20121031413](https://openairdocs.org/sdr/CHQA20121031413.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE LEFT CENTER OMEGA BEAM SEAT TRACK AT FRAME 31 WAS FOUND TO BE CORRODED. THE LEFT-HAND CENTER OMEGA BEAM SEAT TRACK AT FRAME 31 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031412](https://openairdocs.org/sdr/CHQA20121031412.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, THE CENTER OMEGA BEAM SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 41 THROUGH FRAME 47. THE CENTER OMEGA BEAM SEAT TRACK FROM FRAME 41 THROUGH FRAME 47 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031411](https://openairdocs.org/sdr/CHQA20121031411.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121031410](https://openairdocs.org/sdr/CHQA20121031410.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20121131409](https://openairdocs.org/sdr/CHQA20121131409.md): Seat Track · corroded · Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
- [SDR CHQA20120227064](https://openairdocs.org/sdr/CHQA20120227064.md): Battery · discharged · Feb 27, 2012 · N284SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION THE LEFT FORWARD FAIRING EMERGENCY LIGHT AND THE NUMBER 1 AISLE LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTER DEFECTS NOTED.
- [SDR CHQA201100459](https://openairdocs.org/sdr/CHQA201100459.md): Light · inoperative · Nov 24, 2011 · N284SK · Emb EMB145LR · Emergency Lighting
  > DURING INSPECTION, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
- [SDR CHQA201100398](https://openairdocs.org/sdr/CHQA201100398.md): Frame · corroded · Oct 5, 2011 · N284SK · Emb EMB145LR · Fuselage Main, Frame
  > DURING INSPECTION, MAINTENANCE FOUND CORROSION ON FRAME 65 BETWEEN STRINGERS 16L AND 17L. MAINTENANCE REPAIRED FRAME 65 BETWEEN STRINGERS 16L AND 17L IN ACCORDANCE WITH ETD 2011-145-10626 REVISION A. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT IN
- [SDR CHQA201000181](https://openairdocs.org/sdr/CHQA201000181.md): Tire · failed · Sep 20, 2010 · N284SK · Emb EMB145LR · Tire
  > CREW REPORTED THAT THE LEFT INBOARD TIRE BLEW ON TAKEOFF. REPORTED HEARING A NOISE ON TAKEOFF BUT DID NOT RECEIVE AN INDICATIONS UNTIL MLG EXTENSION ON APPROACH FOR LANDING. THE ACFT LANDED WITHOUT INCIDENT. ACFT IS CURRENTLY OUT OF SERVICE. MAINTENANCE IN
- [SDR CHQA201000024](https://openairdocs.org/sdr/CHQA201000024.md): Unknown · malfunctioned · Feb 1, 2010 · N284SK · Emb EMB145LR · Rudder Control System
  > DURING CLIMBOUT, THE CREW RECEIVED A RUDDER SYS 1-2 INOP MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSAGE CLEARED AND AS A RESULT THE CREW RECEIVED AUTO-PILOT AND YAW DAMPER FAIL MESSAGES ON EICAS. THE CREW REDUCED ALTITUDE DUE TO NOW BEING NON-RVSM AN
- [SDR CHQA200900263A](https://openairdocs.org/sdr/CHQA200900263A.md): Transmission · failed · Dec 20, 2009 · N284SK · Emb EMB145LR · Trailing Edge Flap Actuator
  > AFTER TAKEOFF THE CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. RAN THROUGH THE APPROPRIATE CHECK LISTS AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR MESSAGES AND FOUND A RT TRANSMISSION FAIL CMC. THE RIGHT FLAP TRANSMISSION
- [SDR CHQA200900037](https://openairdocs.org/sdr/CHQA200900037.md): Duct · disconnected · Jan 28, 2009 · N284SK · Emb EMB145LR · Cabin Cooling System
  > FLIGHT 2897, CLE TO ATL - DURING CLIMB AT APPROXIMATELY 6,000 FT, THE FLIGHT ATTENDANT REPORTED A BURNING SMELL COMING FROM THE FORWARD PART OF THE AIRCRAFT. THE AIRCRAFT WAS LEVELED OFF AND THE FLIGHT CREW CYCLED THROUGH EACH BLEED AND PACK AND THE SMELL WEN
- [SDR CHQA200800200](https://openairdocs.org/sdr/CHQA200800200.md): Filter Element · dirty · Oct 15, 2008 · N284SK · Emb EMB145LR · Pneumatic Distribution System
  > FLIGHT 5941, CLE TO ORD. WHILE CLIMBING THROUGH FL190, THE FLIGHT CREW RECEIVED A BLD 1 OVERTEMP MESSAGE ON EICAS. THE QRH PROCEDURES WERE FOLLOWED AND BLEED 1 WAS DESELECTED AND CROSS BLEED WAS TURNED TO OPEN. THE FLIGHT ENCOUNTERED ICING CONDITIONS AND RE
- [SDR CHQ20080087](https://openairdocs.org/sdr/CHQ20080087.md): Proximity Sensor · dirty · Apr 27, 2008 · N284SK · Emb EMB145LR · Drag Control System
  > FLIGHT 5906 ORD TO CLE - DURING TAKEOFF ROLE, THE FLIGHT CREW RECEIVED A SPOILER TAKEOFF CONFIGURATION MESSAGE ON THE EICAS. AT THAT POINT THE CREW DECIDED TO ABORT TAKEOFF AND RETURN TO THE GATE WITH NO INCIDENT. MAINTENANCE FOUND NUMEROUS PROXIMITY SWITCHE
- [SDR CHQA200700095](https://openairdocs.org/sdr/CHQA200700095.md): Engine · malfunctioned · Dec 11, 2007 · N284SK · Emb EMB145LR · Engine (Turbine/Turboprop)
  > STL TO IAH - AFTER TAKEOFF FROM STL FLIGHT CREW RECEIVED A LAV SMOKE EICAS MESSAGE. AT THE SAME TIME THE FLIGHT ATTENDANT CALLED THE COCKPIT TO REPORT SMOKE IN THE CABIN COMING FROM THE LAV TO ABOUT MID CABIN. THE FLIGHT CREW ALSO DETECTED A FAINT ELECTRICAL
- [SDR CHQA200600039](https://openairdocs.org/sdr/CHQA200600039.md): Battery · inoperative · Mar 29, 2006 · N284SK · Emb EMB145LR · Emergency Lighting
  > EMERGENCY LIGHTS AT CENTER OF AISLE INOPERATIVE. INSTALLED SERVICEABLE BATTERY IAW EMB 145 MM 33-50-04. OPS CHECK GOOD.
- [SDR CHQA200500178](https://openairdocs.org/sdr/CHQA200500178.md): Inverter · inoperative · Oct 16, 2005 · N284SK · Emb EMB145LR · Emergency Lighting
  > EMERGENCY EXIT LOCATOR ON AFT GALLEY WALL IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 30-50-11. OPS CHECK GOOD.

## 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 = 'N284SK' AND deregistration_id = 'N284SK-2018-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N284SK-2018-07-31/reports

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