# Service difficulty reports: N379SK, cancelled Jan 27, 2017 A list on [N379SK, cancelled Jan 27, 2017](https://openairdocs.org/deregistered/N379SK-2017-01-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CHQA20131107427](https://openairdocs.org/sdr/CHQA20131107427.md): Skin · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Plate/Skin > CORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 13 & 14 BETWEEN STRINGERS 20L & 20R. THE SKIN WAS REPAIRED IAW ETD 2013-145-057134. - [SDR CHQA20131107426](https://openairdocs.org/sdr/CHQA20131107426.md): Support · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR CHQA20131107425](https://openairdocs.org/sdr/CHQA20131107425.md): Support · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > CORROSION 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. - [SDR CHQA20131107424](https://openairdocs.org/sdr/CHQA20131107424.md): Stringer · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Longeron/Stringer > DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 12 & 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131107423](https://openairdocs.org/sdr/CHQA20131107423.md): Stringer · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Main, Longeron/Stringer > DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAME 12 & FRAME 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131107422](https://openairdocs.org/sdr/CHQA20131107422.md): Fitting · cracked · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20131107421](https://openairdocs.org/sdr/CHQA20131107421.md): Fitting · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20131107420](https://openairdocs.org/sdr/CHQA20131107420.md): Fitting · cracked · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20131107419](https://openairdocs.org/sdr/CHQA20131107419.md): Fitting · cracked · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20131107418](https://openairdocs.org/sdr/CHQA20131107418.md): Fitting · corroded · Nov 7, 2013 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20130614208](https://openairdocs.org/sdr/CHQA20130614208.md): Trim Switch · dirty · Jun 14, 2013 · N379SK · Emb EMB135KL · Stabilizer Control System > DURING 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 A - [SDR CHQA20130614205](https://openairdocs.org/sdr/CHQA20130614205.md): Light · inoperative · Jun 14, 2013 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA20130614204](https://openairdocs.org/sdr/CHQA20130614204.md): Light · inoperative · Jun 14, 2013 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA20130602193](https://openairdocs.org/sdr/CHQA20130602193.md): Light · inoperative · Jun 2, 2013 · N379SK · Emb EMB135KL · Emergency Lighting > CREW 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. - [SDR CHQA20120420127](https://openairdocs.org/sdr/CHQA20120420127.md): Seal · detached · Apr 20, 2012 · N379SK · Emb EMB135KL · Service Doors > CREW 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 - [SDR CHQA20120405116](https://openairdocs.org/sdr/CHQA20120405116.md): Skin · dented · Apr 5, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Plate/Skin > DURING 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. - [SDR CHQA20120403123](https://openairdocs.org/sdr/CHQA20120403123.md): Floor Support · cracked · Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20120403122](https://openairdocs.org/sdr/CHQA20120403122.md): Frame · cracked · Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Frame > DURING 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. - [SDR CHQA20120403121](https://openairdocs.org/sdr/CHQA20120403121.md): Frame · cracked · Apr 3, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Frame > DURING 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. - [SDR CHQA20120402120](https://openairdocs.org/sdr/CHQA20120402120.md): Door Frame · corroded · Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Structure > DURING 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. - [SDR CHQA20120402119](https://openairdocs.org/sdr/CHQA20120402119.md): Shear Plate · corroded · Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20120402118](https://openairdocs.org/sdr/CHQA20120402118.md): Beam · corroded · Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20120405117](https://openairdocs.org/sdr/CHQA20120405117.md): Door Frame · cracked · Apr 2, 2012 · N379SK · Emb EMB135KL · Fuselage Main, Structure > DURING 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. - [SDR CHQA201200026](https://openairdocs.org/sdr/CHQA201200026.md): Light · inoperative · Jan 26, 2012 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA201100506](https://openairdocs.org/sdr/CHQA201100506.md): Light · inoperative · Dec 26, 2011 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA201100287](https://openairdocs.org/sdr/CHQA201100287.md): Proximity Switch · out of adjust · Jul 24, 2011 · N379SK · Emb EMB135KL · Landing Gear Position and Warning > CREW 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 LANDE - [SDR CHQA201100133](https://openairdocs.org/sdr/CHQA201100133.md): Tire · separated · Apr 13, 2011 · N379SK · Emb EMB135KL · Tire > AFTER 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 W - [SDR CHQA201100122](https://openairdocs.org/sdr/CHQA201100122.md): Thermostat · inoperative · Mar 20, 2011 · N379SK · Emb EMB135KL · Pneumatic Distribution System > CREW 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 R - [SDR CHQA201100040](https://openairdocs.org/sdr/CHQA201100040.md): Engine · malfunctioned · Feb 21, 2011 · N379SK · Emb EMB135KL · Engine (Turbine/Turboprop) > CREW 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 S - [SDR CHQA201100005](https://openairdocs.org/sdr/CHQA201100005.md): Proximity Switch · corroded · Jan 10, 2011 · N379SK · Emb EMB135KL · Landing Gear Position and Warning > WHILE 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 THA - [SDR CHQA201000210](https://openairdocs.org/sdr/CHQA201000210.md): Tire · blown · Nov 12, 2010 · N379SK · Emb EMB135KL · Tire > ON 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 INCID - [SDR CHQA201000143](https://openairdocs.org/sdr/CHQA201000143.md): Battery Pack · discharged · Jul 20, 2010 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA201000140](https://openairdocs.org/sdr/CHQA201000140.md): Flex Drive · damaged · Jul 12, 2010 · N379SK · Emb EMB135KL · Trailing Edge Flap Actuator > WHILE 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 SD - [SDR CHQA200900269](https://openairdocs.org/sdr/CHQA200900269.md): Light · inoperative · Dec 28, 2009 · N379SK · Emb EMB135KL · Emergency Lighting > DURING 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. - [SDR CHQA200900161](https://openairdocs.org/sdr/CHQA200900161.md): Control Valve · leaking · Jul 21, 2009 · N379SK · Emb EMB135KL · Pneumatic Distribution System > FLIGHT 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 TAKEOFF - [SDR CHQA200900107](https://openairdocs.org/sdr/CHQA200900107.md): Wire · broken · Apr 14, 2009 · N379SK · Emb EMB135KL · Light System Wiring > DURING 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 A - [SDR CHQA200900025](https://openairdocs.org/sdr/CHQA200900025.md): Strut · underserviced · Jan 19, 2009 · N379SK · Emb EMB135KL · Main Landing Gear Strut/Axle/Truck > FLIGHT 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 GE - [SDR CHQA200900024](https://openairdocs.org/sdr/CHQA200900024.md): Connector · corroded · Jan 19, 2009 · N379SK · Emb EMB135KL · Landing Gear System Wiring > FLIGHT 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 LA - [SDR CHQ2008F00004](https://openairdocs.org/sdr/CHQ2008F00004.md): Fuel Control · failed · Aug 30, 2008 · N379SK · Emb EMB135KL · Fuel Control/Turbine Engines > FLIGHT 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 - [SDR CHQA200800163](https://openairdocs.org/sdr/CHQA200800163.md): Control Panel · intermittent · Aug 14, 2008 · N379SK · Emb EMB135KL · Electrical Power System > FLIGHT 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. TH - [SDR CHQA200500086](https://openairdocs.org/sdr/CHQA200500086.md): Battery Pack · discharged · Apr 22, 2005 · N379SK · Emb EMB135KL · Emergency Lighting > FORWARD 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. ## 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 = 'N379SK' AND deregistration_id = 'N379SK-2017-01-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N379SK-2017-01-27/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.