N284SK, cancelled Jul 31, 2018

Service difficulty reports · 36

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UHLA201606040294Lens · missingRIGHT OVERWING EXIT EMERGENCY LIGHT PROTECTIVE LENS MISSING. R & R RT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10.Jun 4, 2016 · N284SK · Emb EMB145LR · Emergency LightingSDR CHQA20131025379Bleed Valve · faultyCREW 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 DEFECTOct 25, 2013 · N284SK · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20130831340Mount · damagedDURING 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.Aug 31, 2013 · N284SK · Emb EMB145LR · APU Cowling/ContainmentSDR CHQA20130424128O-Ring · leakingCREW 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.Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130424127O-Ring · leakingCREW 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.Apr 24, 2013 · N284SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20121115442Frame · damagedDURING HEAVY MAINTENANCE A PERMANENT REPAIR OF A LIGHTNING BURN AT FRAME 13 ON STRINGER 19L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-007033.Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20121115439Skin · damagedDURING 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.Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20121115441Fitting · crackedDURING 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.Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121115440Fitting · crackedDURING 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.Nov 15, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121027438Angle · damagedDURING HEAVY MAINTENANCE A PERMANENT REPAIR WAS COMPLETED ON THE RIGHT LOWER WING TRAILING EDGE IN ACCORDANCE WITH ETD 2012-145-015393B.Nov 15, 2012 · N284SK · Emb EMB145LR · Wing Miscellaneous StructureSDR CHQA20121112424Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 14. THE STRINGER WAS REPLACED.Nov 12, 2012 · N284SK · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20121111423Support Fitting · corrodedDURING 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.Nov 11, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121031420Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031419Attach Bracket · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121031418Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031417Gusset · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121031416Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031415Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031414Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031413Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031412Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031411Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121031410Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121131409Seat Track · corrodedDURING 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.Oct 31, 2012 · N284SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20120227064Battery · dischargedDURING 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.Feb 27, 2012 · N284SK · Emb EMB145LR · Emergency LightingSDR CHQA201100459Light · inoperativeDURING 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.Nov 24, 2011 · N284SK · Emb EMB145LR · Emergency LightingSDR CHQA201100398Frame · corrodedDURING 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 INOct 5, 2011 · N284SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201000181Tire · failedCREW 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 INSep 20, 2010 · N284SK · Emb EMB145LR · TireSDR CHQA201000024Unknown · malfunctionedDURING 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 ANFeb 1, 2010 · N284SK · Emb EMB145LR · Rudder Control SystemSDR CHQA200900263ATransmission · failedAFTER 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 TRANSMISSIONDec 20, 2009 · N284SK · Emb EMB145LR · Trailing Edge Flap ActuatorSDR CHQA200900037Duct · disconnectedFLIGHT 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 WENJan 28, 2009 · N284SK · Emb EMB145LR · Cabin Cooling SystemSDR CHQA200800200Filter Element · dirtyFLIGHT 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 REOct 15, 2008 · N284SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQ20080087Proximity Sensor · dirtyFLIGHT 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 SWITCHEApr 27, 2008 · N284SK · Emb EMB145LR · Drag Control SystemSDR CHQA200700095Engine · malfunctionedSTL 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 ELECTRICALDec 11, 2007 · N284SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA200600039Battery · inoperativeEMERGENCY LIGHTS AT CENTER OF AISLE INOPERATIVE. INSTALLED SERVICEABLE BATTERY IAW EMB 145 MM 33-50-04. OPS CHECK GOOD.Mar 29, 2006 · N284SK · Emb EMB145LR · Emergency LightingSDR CHQA200500178Inverter · inoperativeEMERGENCY EXIT LOCATOR ON AFT GALLEY WALL IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 30-50-11. OPS CHECK GOOD.Oct 16, 2005 · N284SK · Emb EMB145LR · Emergency Lighting
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