N379SK, cancelled Jan 27, 2017

Service difficulty reports · 41

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 = 'N379SK' AND deregistration_id = 'N379SK-2017-01-27'
  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 CHQA20131107427Skin · corrodedCORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 13 & 14 BETWEEN STRINGERS 20L & 20R. THE SKIN WAS REPAIRED IAW ETD 2013-145-057134.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20131107426Support · corrodedCORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET BETWEEN STRINGER 20R & 21R AT FRAMES 12 & 13 13. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107425Support · corrodedCORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET BETWEEN STRINGER 20L & 21L AT FRAME 12. THE AILERON TORQUE TUBE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107424Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 12 & 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR CHQA20131107423Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAME 12 & FRAME 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR CHQA20131107422Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L & 8L. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107421Fitting · corrodedDURING INSPECTION, THE SHEAR CLIP AT FRAME 23 BETWEEN STINGERS 16R & 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107420Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 BETWEEN STINGERS 15R & 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107419Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R & 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20131107418Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21R & 20R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20130614208Trim Switch · dirtyDURING CLIMBOUT, THE FLIGHT CREW RECEIVED AN AURAL "TRIM" WARNING MESSAGE AND FOUND THE MAIN AND BACK-UP PITCH TRIM TO BE INOPERATIVE. THE CREW DECLARED AN EMERGENCY, RETURNED TO THE FIELD, AND MADE AN UNEVENTFUL LANDING. MX CLEANED THE BACK UP TRIM SWITCH AJun 14, 2013 · N379SK · Emb EMB135KL · Stabilizer Control SystemSDR CHQA20130614205Light · inoperativeDURING INSPECTION, CREW REPORTED THE CABIN CEILING EMERGENCY EXIT LIGHTS AFT OF THE EMERGENCY EXIT DOORS DID NOT ILLUMINATE. EMERGENCY EXIT LIGHT R & R. OPS CHECKED SUCCESSFUL.Jun 14, 2013 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA20130614204Light · inoperativeDURING INSPECTION, CREW REPORTED THE EXIT LIGHT IN THE FORWARD GALLEY OVER THE SERVICE DOOR DID NOT ILLUMINATE. EXIT LIGHTS WERE R & R. OPS CHECKED SUCCESSFUL.Jun 14, 2013 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA20130602193Light · inoperativeCREW REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT BULB WAS FOUND TO BE INOPERATIVE DURING PRE-FLIGHT INSPECTION. MX REPLACED THE FLIGHT DECK EMERGENCY LIGHT. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS. NOTED.Jun 2, 2013 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA20120420127Seal · detachedCREW REPORTED, DURING FLIGHT THAT THERE WAS A LOUD BANGING NOISE FROM THE GALLEY SERVICE DOOR. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE GALLEY SERVICE DOOR LOWER TRIM STRIP TO BE UNSECURED. THE GALLEY SERVICE DOOR TRIM STRIP WAS Apr 20, 2012 · N379SK · Emb EMB135KL · Service DoorsSDR CHQA20120405116Skin · dentedDURING INSPECTION, AN EXISTING REPAIR WAS FOUND ON THE LOWER SKIN BETWEEN FRAME 7 AND FRAME 8 AND BETWEEN THE CENTER LINE AND STRINGER 20L. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT AND AFTER INVESTIGATION 2 DENTS WERE FOUND UNDER THE REPAIR. Apr 5, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA20120403123Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20120403122Frame · crackedDURING INSPECTION, THE LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. THE LEFT AND RIGHT FRAME 10 WERE REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120403121Frame · crackedDURING INSPECTION, THE LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. THE LEFT AND RIGHT FRAME 10 WERE REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA20120402120Door Frame · corrodedDURING INSPECTION, THE CARGO DOOR FORWARD FRAME 65 WAS FOUND TO BE CORRODED. THE CARGO DOOR FORWARD FRAME 65 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004743.Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA20120402119Shear Plate · corrodedDURING INSPECTION, THE CARGO DOOR CUTOUT FORWARD L-SHAPE WAS FOUND TO BE CORRODED. THE CARGO DOOR CUTOUT FORWARD L-SHAPE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004748.Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20120402118Beam · corrodedDURING INSPECTION, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20120405117Door Frame · crackedDURING INSPECTION, FRAME 23 AFT OF THE SERVICE DOOR WAS FOUND TO BE CRACKED. FRAME 23 AFT OF THE SERVICE DOOR WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004737.Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA201200026Light · inoperativeDURING INSPECTION, THE EXTERIOR EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 26, 2012 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA201100506Light · inoperativeDURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 26, 2011 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA201100287Proximity Switch · out of adjustCREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR LEVER WOULD NOT MOVE UP. AT 400 FEET AGL THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ALONG WITH IC WOW 1/2 INOP MESSAGE. ALL OTHER INDICATION APPEARED NORMAL. THE CREW RETURNED TO KSDF AND LANDEJul 24, 2011 · N379SK · Emb EMB135KL · Landing Gear Position and WarningSDR CHQA201100133Tire · separatedAFTER TAKEOFF, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG. AFTER FOLLOWING THE QRH, IT WAS DECIDED TO RETURN TO ORD WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. DURING POST FLIGHT INSPECTION, THE RIGHT INBOARD TIRE WAS FOUND TO HAVE LOST ITS TREAD WApr 13, 2011 · N379SK · Emb EMB135KL · TireSDR CHQA201100122Thermostat · inoperativeCREW REPORTED THAT DURING FLIGHT RECEIVED A BLEED 2 OVERTEMP MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND BLEED 2 WAS DESELECTED, AND RETURNED TO A NORMAL TEMPERATURE. ADDITIONAL WARNING MESSAGES FOR WING ANTI-ICE AND STAB ANTI-ICE FAIL WERE RMar 20, 2011 · N379SK · Emb EMB135KL · Pneumatic Distribution SystemSDR CHQA201100040Engine · malfunctionedCREW REPORTED THAT AFTER LEVELING OFF AT 23,000FT, REPORTED SMELLING A BURNING OIL/ELECTRICAL ODOR. THE CAPTAIN AND FIRST OFFICER DONNED OXYGEN MASKS AND PROCEEDED TO DIVERT TO IND. THE ODOR WAS CONTAINED MAINLY TO COCKPIT BUT FLIGHT ATTENDANT DID REPORT A SFeb 21, 2011 · N379SK · Emb EMB135KL · Engine (Turbine/Turboprop)SDR CHQA201100005Proximity Switch · corrodedWHILE ON APPROACH AFTER SELECTING THE GEAR DOWN, THE RIGHT MAIN LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED. THE APPROACH WAS ABORTED AND THE AIRCRAFT OVER-FLEW THE AIRPORT FOR VISUAL CONFIRMATION THAT THE RIGHT GEAR HAD EXTENDED. THE TOWER CONFIRMED THAJan 10, 2011 · N379SK · Emb EMB135KL · Landing Gear Position and WarningSDR CHQA201000210Tire · blownON ROTATION, CREW REPORTED A LOUD BANG & COULD SMELL ODOR OF RUBBER. ACFT CONTINUED TO CLIMBOUT WITH NO ISSUES & ALL INDICATIONS NORMAL. FLT CONTINUED. PRIOR TO LANDING, ACFT PERFORMED A FLY-BY OF TOWER & NO DEFECTS WERE REPORTED. ACFT LANDED WITHOUT INCIDNov 12, 2010 · N379SK · Emb EMB135KL · TireSDR CHQA201000143Battery Pack · dischargedDURING INSPECTION, THE EMERGENCY LIGHT FLOOR STRIPS NR 4 AND NR 5 WERE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOTED.Jul 20, 2010 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA201000140Flex Drive · damagedWHILE ON APPROACH TO CID, WHEN THE CREW SELECTED THE FLAPS TO 9 DEGREES, THE FLAPS STAYED AT ZERO AND FLAP FAIL WAS DISPLAYED ON EICAS. THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO SDJul 12, 2010 · N379SK · Emb EMB135KL · Trailing Edge Flap ActuatorSDR CHQA200900269Light · inoperativeDURING THE OPS CHECK OF THE EMERGENCY LIGHTS DUE TO A TIME REQUIRED CHANGE OF THE NR 3 BATTERY, THE FLOOR PROXIMITY LIGHT STRIP AT SEAT 7A WAS INOP. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT STRIP AND OPS CHECK NORMAL PER EMB AMM 33-50-12.Dec 28, 2009 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA200900161Control Valve · leakingFLIGHT 5365, PHL TO STL. AFTER PUSHBACK AFTER STARTING E2 THE CREW RECEIVED A BLEED 2 LEAK INDICATION ON EICAS. THE QRH WAS FOLLOWED AND THE LEAK INDICATION CLEARED. E1 WAS STARTED AND BOTH BLEEDS WERE OPENED WITH NO FURTHER LEAK INDICATIONS. AFTER TAKEOFFJul 21, 2009 · N379SK · Emb EMB135KL · Pneumatic Distribution SystemSDR CHQA200900107Wire · brokenDURING INSPECTION THE ROW NR 16 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. UPON FURTHER INSPECTION, IT WAS FOUND THAT THE WIRING FOR THE STRIP HAD BROKEN WIRES. THE LIGHT STRIP WAS THEN PLACED ON DEFERRAL. CORRECTIVE ACTION WILL BE SUBMITTED AApr 14, 2009 · N379SK · Emb EMB135KL · Light System WiringSDR CHQA200900025Strut · underservicedFLIGHT 5298, STL TO PHL - THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER GEAR RETRACTION ALONG WITH AN E1 AND E2 REVERSE DISAGREE. THE FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING THE RIGHT MAIN LANDING GEJan 19, 2009 · N379SK · Emb EMB135KL · Main Landing Gear Strut/Axle/TruckSDR CHQA200900024Connector · corrodedFLIGHT 5306, STL TO EWR - THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND E1 AND E2 REVERSER DISAGREE MESSAGE DURING CLIMB-OUT. THE AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. THE CMC WAS DOWNLOADED AND HAD MESSAGES FOR RIGHT LAJan 19, 2009 · N379SK · Emb EMB135KL · Landing Gear System WiringSDR CHQ2008F00004Fuel Control · failedFLIGHT 5346, STL TO MSY. WHILE ON DESCENT INTO MSY, AT APPROXIMATELY FL285 THE FLIGHT CREW NOTICED ABNORMAL INDICATIONS ON EICAS FROM E2. THE N1 INDICATIONS WERE INCREASE AND DECREASING RAPIDLY BUT WERE STAYING WITHIN LIMITS AS WELL AT THE ITT. IT WAS ALSO Aug 30, 2008 · N379SK · Emb EMB135KL · Fuel Control/Turbine EnginesSDR CHQA200800163Control Panel · intermittentFLIGHT 5302, STL TO AUS - DURING CRUISE THE CREW RECEIVED AN ELECTRICAL ABNORMAL MESSAGE. THE ELECTRICAL STATUS PAGE WAS CHECKED AND FOUND THAT THE BATTERIES WERE NOT CHARGING. THE CREW FOLLOWED THE QRH AND STARTED THE APU BUT THE MESSAGES DID NOT CLEAR. THAug 14, 2008 · N379SK · Emb EMB135KL · Electrical Power SystemSDR CHQA200500086Battery Pack · dischargedFORWARD EMERGENCY LIGHTING EGRESS LIGHT STRIPS AND RIGHT WING EGRESS LIGHT ARE INOP. REMOVED AND REPLACED THE NR 2 FORWARD GALLEY EMERGENCY LIGHT BATTERY PACK IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD.Apr 22, 2005 · N379SK · Emb EMB135KL · Emergency Lighting
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