# Service difficulty reports: N376SK, cancelled Dec 8, 2017 A list on [N376SK, cancelled Dec 8, 2017](https://openairdocs.org/deregistered/N376SK-2017-12-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CHQA20121201448](https://openairdocs.org/sdr/CHQA20121201448.md): Light · inoperative · Dec 1, 2012 · N376SK · Emb EMB135KL · Emergency Lighting > CREW REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20121002366](https://openairdocs.org/sdr/CHQA20121002366.md): Switch · malfunctioned · Oct 2, 2012 · N376SK · Emb EMB135KL · Independent Instruments > CREW REPORTED THAT DURING FLIGHT, AND ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT. THE CREW DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE ISSUE TO THE FIRST OFFICER'S CHRONO BUTTON IN THE YOKE. THE ITEM WAS DEACTIVATED AND THEN DEFERR - [SDR CHQA20120927363](https://openairdocs.org/sdr/CHQA20120927363.md): Wire Harness · defective · Sep 27, 2012 · N376SK · Emb EMB135KL · Light System Wiring > CREW REPORTED THAT COCKPIT READING LIGHT WENT OUT AND AN ELECTRICAL BURNING SMELL SOON APPEARED IN THE COCKPIT. MAINTENANCE ISOLATED THE BURNING SMELL TO THE FIRST OFFICER'S CHARTHOLDER LIGHT HARNESS AND DISCONNECTED THE HARNESS. THE ITEM IS CURRENTLY ON DEF - [SDR CHQA20120915359](https://openairdocs.org/sdr/CHQA20120915359.md): Structure · bent · Sep 15, 2012 · N376SK · Emb EMB135KL · Wing Miscellaneous Structure > DURING INSPECTION, THE RIGHT OUTBOARD LEADING EDGE WAS BENT AT THE OUTBOARD FRAME. THE RIGHT OUTBOARD LEADING EDGE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013240A. - [SDR CHQA20120912358](https://openairdocs.org/sdr/CHQA20120912358.md): Floor Support · corroded · Sep 12, 2012 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER LEFT OMEGA AT FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120912357](https://openairdocs.org/sdr/CHQA20120912357.md): Floor Support · corroded · Sep 12, 2012 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT CARBON CROSSMEMBER CENTER OMEGA LEFT FLOORBOARD FLANGE BETWEEN FRAME 24 AND 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120912356](https://openairdocs.org/sdr/CHQA20120912356.md): Floor Support · corroded · Sep 12, 2012 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER LEFT OMEGA INBOARD FLOORBOARD FLANGE BETWEEN FRAMES 24 AND 25. THE OMEGA BEAN WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120912355](https://openairdocs.org/sdr/CHQA20120912355.md): Floor Support · corroded · Sep 12, 2012 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT THE CARBON CROSSMEMBER CENTER OMEGA FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120508145](https://openairdocs.org/sdr/CHQA20120508145.md): Light · inoperative · May 8, 2012 · N376SK · Emb EMB135KL · Emergency Lighting > MAINTENANCE REPORTED THAT THE ROW 12 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE FLOOR STRIP. THE DEFERRAL WAS CLEARED BY REPLACING THE FLOOR LIGHTING STRIP AT ROW 12. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECT - [SDR CHQA201100479](https://openairdocs.org/sdr/CHQA201100479.md): Skin · dented · Dec 1, 2011 · N376SK · Emb EMB135KL · Fuselage Main, Plate/Skin > DURING INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN RF II BETWEEN FRAME 76 AND 77 AND STRINGERS 16R AND 18R. MAINTENANCE REPAIRED THE DENT ON THE FUSELAGE SKIN RF II BETWEEN FRAMES 76 AND 77 AND STRINGERS 16R AND 18R IN ACCORDANCE WITH SRM 53-32-01. A H - [SDR CHQA201100482](https://openairdocs.org/sdr/CHQA201100482.md): Beam · corroded · Nov 30, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT BEAM UNDER THE OUTBOARD SEAT TRACK NUMBER 5, BETWEEN FRAME 47 TO FRAME 53 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT BEAM UNDER THE OUTBOARD SEAT TRACK NUMBER 5, BETWEEN FRAME 47 TO FRAME 53 AND INSTALLED WITH SOLID RI - [SDR CHQA201100480](https://openairdocs.org/sdr/CHQA201100480.md): Beam · corroded · Nov 30, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR CUTOUT LOWER BEAM AND INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100463](https://openairdocs.org/sdr/CHQA201100463.md): Frame · cracked · Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS FOUND ON FRAME 23 UNDER SILL NUMBER 1. MAINTENANCE REPAIRED THE RIGHT-HAND FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 2011-145-108720. - [SDR CHQA201100462](https://openairdocs.org/sdr/CHQA201100462.md): Shear Plate · corroded · Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L SHAPE. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH ETD 2011-145-108 - [SDR CHQA201100484](https://openairdocs.org/sdr/CHQA201100484.md): Angle · cracked · Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, MID WING BOX OMEGA BEAN ANGLES WERE FOUND TO BE CRACKED AT FRAME 50 (PN: 140-04214-607 AND 140-04214-609). MAINTENANCE REPLACED THE MID WING BOX OMEGA BEAM ANGLES IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA201100483](https://openairdocs.org/sdr/CHQA201100483.md): Beam · corroded · Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, AN EXISTING REPAIR ON THE LEFT INBOARD BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT INBOARD BEAM AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA201100481](https://openairdocs.org/sdr/CHQA201100481.md): Frame · cracked · Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Main, Frame > DURING INSPECTION, THE LEFT FRAME 10 WAS FOUND CRACKED INSIDE THE COCKPIT BELOW THE SIDE WINDOW. MAINTENANCE REPLACED THE LEFT FRAME 10 INSIDE THE COCKPIT BELOW THE SIDE WINDOW AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100271](https://openairdocs.org/sdr/CHQA201100271.md): Sign · inoperative · Jul 9, 2011 · N376SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, THE SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR EMERGENCY EXIT SIGN WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100176](https://openairdocs.org/sdr/CHQA201100176.md): Acm · damaged · May 14, 2011 · N376SK · Emb EMB135KL · Cabin Cooling System > AFTER TAKEOFF, THE CREW REPORTED LIGHT SMOKE IN THE COCKPIT AT ABOUT 7,000FT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KORD, LANDING WITHOUT INCIDENT. EMERGENCY PERSONNEL MET THE AIRCRAFT AND THE PLANE WAS EVACUATED. MAINTENANCE FOUND BROKEN BLADES ON - [SDR CHQA201100016](https://openairdocs.org/sdr/CHQA201100016.md): Screw · misinstalled · Jan 19, 2011 · N376SK · Emb EMB135KL · Emergency Exits > DURING INSPECTION, THE LEFT OVERWING EMERGENCY EXIT ON THE LEFT PASSENGER ESCAPE HATCH WAS FOUND TO BE BLOCKED. MAINTENANCE FOUND A SCREW THAT WAS NOT INSTALLED PROPERLY AND WAS BLOCKING THE DOOR FROM OPENING. THE SCREW WAS RE-INSTALLED AND OPERATIONAL CHECK - [SDR CHQA201000187](https://openairdocs.org/sdr/CHQA201000187.md): Rmu · malfunctioned · Sep 30, 2010 · N376SK · Emb EMB135KL · VHF Communications System > ON APPROACH INTO MKE THE FLIGHT CREW REPORTED A RMU 2 FAILURE WITH RMU, ALSO NOT WORKING PROPERLY. MKE APPROACH WAS THE ONLY FREQUENCY THAT RMU WOULD TUNE. THE CREW RECEIVED LANDING CLEARANCE FROM APPROACH AND VERIFIED THE GREEN LIGHT FROM THE TOWER AND LAND - [SDR CHQA201000154](https://openairdocs.org/sdr/CHQA201000154.md): Light · inoperative · Aug 11, 2010 · N376SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFT EXTERIOR EMERGENCY LIGHT BULB AND THE EMERGENCY LIGHTS OPERATED NORMALLY. - [SDR CHQA201000101](https://openairdocs.org/sdr/CHQA201000101.md): Light · disconnected · May 23, 2010 · N376SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT NEXT TO SEAT 1A WAS INOP. MAINTENANCE FOUND DISCONNECTED WIRES ON THE LIGHT STRIP AND RE-ATTACHED IN ACCORDANCE WITH EMB 140 MM 33-50-00, NO FURTHER DEFECTS WERE NOTED. - [SDR CHQA201000080](https://openairdocs.org/sdr/CHQA201000080.md): Brake · faulty · Apr 16, 2010 · N376SK · Emb EMB135KL · Trailing Edge Flap Control System > THE CREW REPORTED THE FLAP POSITION INDICATION WAS INOP ON APPROACH. MAINTENANCE REPLACED THE LEFT FLAP WING BRAKE DUE TO FAIL MESSAGES FOUND ON THE CMC WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000075](https://openairdocs.org/sdr/CHQA201000075.md): Battery Pack · discharged · Apr 10, 2010 · N376SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, ALL FOUR EMERGENCY LIGHT BATTERY PACKS WERE FOUND TO BE DISCHARGED. ALL FOUR EMERGENCY LIGHT BATTERIES WERE REPLACED WITH NO FURTHER DEFECTS NOTED. BATTERY NR 2: P/N: RPS1-B, S/N: 16905, TSN: 20686, CSN: 17308, TSR: 368; BATTERY NR 3: P/N: - [SDR CHQA200900213](https://openairdocs.org/sdr/CHQA200900213.md): Pressure Switch · defective · Sep 30, 2009 · N376SK · Emb EMB135KL · Rudder Control System > FLIGHT 5344 STL TO RDU. IN FLIGHT AT FL330 THE FLIGHT CREW RECEIVED AN AUTO PILOT FAIL AND YAW DAMPER FAIL MESSAGE FOLLOWED SHORTLY AFTER WITH A RUDDER 1-2 INOP MESSAGE. THE CREW RAN THE QRH PROCEDURE AND DIVERTED TO SDF. MAINTENANCE CHECKED THE WIRING FROM - [SDR CHQA200900149](https://openairdocs.org/sdr/CHQA200900149.md): Inverter · inoperative · Jun 29, 2009 · N376SK · Emb EMB135KL · Emergency Lighting > DURING INSP, THE EXIT IDENTIFIER SIGN ON THE RT SIDE OF THE ACFT ABOVE SEATS 11BC WAS FOUND TO BE INOP. MX REPLACED THE NR 5 INVERTER IAW AMM 33-50-11 AND THE EMERGENCY LIGHT SYS OPERATED NORMALLY. - [SDR CHQA200800191](https://openairdocs.org/sdr/CHQA200800191.md): Hose · loose · Oct 2, 2008 · N376SK · Emb EMB135KL · Hydraulic System, Main > ON INITIAL CLIMBOUT, THE FLIGHT CREW RECEIVED A HYD SYS 1 LO QTY EICAS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP ON THE MFD AND THE HYDRAULIC SYS 1 INDICATED IN THE AMBER RANGE AND THE PRESSURE WAS FALLING. WHILE FOLLOWING THE QRH IT WAS NOTED THAT THE NOSE G - [SDR CHQ2008F00011](https://openairdocs.org/sdr/CHQ2008F00011.md): Socket · burned · Sep 13, 2008 · N376SK · Emb EMB135KL · Electrical Power System Wiring > DURING CRUISE, THE FLIGHT CREW RECEIVED A PITOT 1 INOP EICAS MESSAGE AND SMELLED SMOKE. IMMEDIATELY AFTER THEY RECEIVED AN AOA 1 HEAT INOP MESSAGE AND THE FLIGHT INSTRUMENTS ON THE CAPTAIN`S PFD BEGAN TO GIVE ERRONEOUS INDICATIONS. THE FLIGHT CONTROLS WERE TRA - [SDR CHQA200800158](https://openairdocs.org/sdr/CHQA200800158.md): Proximity Sensor · faulty · Aug 4, 2008 · N376SK · Emb EMB135KL · Landing Gear Position and Warning > FLIGHT 5360, STL TO ATL. DURING CLIMB, AFTER RETRACTING THE LANDING GEAR, THE FLIGHT CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS ALONG WITH AURAL WARNINGS FOR FLAPS AND TRIM. THE FLIGHT LEVELED OFF AND THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED. THE - [SDR CHQ2008F00000](https://openairdocs.org/sdr/CHQ2008F00000.md): Windshield · cracked · Jul 25, 2008 · N376SK · Emb EMB135KL · Flight Compartment Windows > FLIGHT 5349, MSY TO STL. DURING CRUISE THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND NOTICED THAT THE FIRST OFFICER’S WINDSHIELD HAD CRACKED. THE FLIGHT THEN DIVERTED TO CGI WHERE THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS THEN FERRIED TO STL WHERE T - [SDR CHQA200800028](https://openairdocs.org/sdr/CHQA200800028.md): Proximity Sensor · malfunctioned · Feb 12, 2008 · N376SK · Emb EMB135KL · Landing Gear Position and Warning > STL TO MSP, ON INITIAL CLIMB, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS WHEN THEY ATTEMPTED TO MOVE THE LANDING GEAR LEVER TO THE UP POSITION WITHOUT SUCCESS. WHILE PREPARING TO RETURN TO FIELD AT STL THE CREW RAN THROUGH THE QRH CHECK - [SDR CHQA20070053](https://openairdocs.org/sdr/CHQA20070053.md): Control Valve · faulted · Sep 17, 2007 · N376SK · Emb EMB135KL · Landing Gear Brake System > STL TO MSP - UPON LOWERING LANDING GEAR ON FINAL APPROACH, CREW RECEIVED "INBOARD BRAKE INOP" EICAS MESSAGE. THE CREW DID A GO-AROUND TO CONSULT THE QRH AND EVALUATE THE SITUATION. AS A PRECAUTION, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED ON THE LON - [SDR CHQA200500069](https://openairdocs.org/sdr/CHQA200500069.md): Bulb · burned out · Mar 31, 2005 · N376SK · Emb EMB135KL · Emergency Lighting > LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED LEFT HAND FORWARD EMERGENCY EXIT LIGHT IAW EMB 140 AMM 33-50-07. OPS CHECK GOOD. - [SDR CHQA000543](https://openairdocs.org/sdr/CHQA000543.md): Power Supply · inoperative · Aug 24, 2004 · N376SK · Emb EMB135KL · Emergency Lighting > OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY POWER SUPPLIES AND OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER MAINTENANCE MANUAL. ## 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 = 'N376SK' AND deregistration_id = 'N376SK-2017-12-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N376SK-2017-12-08/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.