# Service difficulty reports: N377SK, cancelled Mar 30, 2018 A list on [N377SK, cancelled Mar 30, 2018](https://openairdocs.org/deregistered/N377SK-2018-03-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CHQA20140427125](https://openairdocs.org/sdr/CHQA20140427125.md): Battery · discharged · Apr 27, 2014 · N377SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130722185](https://openairdocs.org/sdr/CHQA20130722185.md): Windshield · failed · Jul 22, 2013 · N377SK · Emb EMB135KL · Flight Compartment Windows > DURING CRUISE, HEARD A LOUD POP IN COCKPIT AND CAPTAIN'S WINDSCREEN SHATTERED. DESCENDED AND DECLARED AN EMERGENCY. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. OPS AND LEAK CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130620221](https://openairdocs.org/sdr/CHQA20130620221.md): Battery Pack · discharged · Jun 20, 2013 · N377SK · Emb EMB135KL · Emergency Lighting > DURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130310078](https://openairdocs.org/sdr/CHQA20130310078.md): Pressure Switch · faulty · Mar 10, 2013 · N377SK · Emb EMB135KL · Rudder Control System > CREW REPORTED THAT THEY RECEIVED RUDDER SYSTEM 1 AND 2 INOPERATIVE MESSAGES ON CLIMBOUT. THE ASSOCIATED MESSAGES OF YAW DAMPER FAIL AND AUTO-PILOT FAIL WERE ALSO PRESENT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDE - [SDR CHQA20130310077](https://openairdocs.org/sdr/CHQA20130310077.md): Pressure Switch · faulty · Mar 10, 2013 · N377SK · Emb EMB135KL · Rudder Control System > CREW REPORTED THAT THEY RECEIVED RUDDER SYSTEM 1 AND 2 INOPERATIVE MESSAGES ON CLIMBOUT. THE ASSOCIATED MESSAGES OF YAW DAMPER FAIL AND AUTO-PILOT FAIL WERE ALSO PRESENT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDE - [SDR CHQA201211/14431](https://openairdocs.org/sdr/CHQA201211%2F14431.md): Stringer · corroded · Nov 14, 2012 · N377SK · Emb EMB135KL · Fuselage Main, Longeron/Stringer > DURING INSPECTION, CORROSION WAS FOUND ON THE EDGE OF STRINGER 21R AT FRAME 11 THROUGH 12. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121108436](https://openairdocs.org/sdr/CHQA20121108436.md): Support · corroded · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SUPPORT AT FRAME 10 THROUGH 11 AT STRINGER 20R UNDERNEATH THE ELEVATOR QUADRANT. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-016499A. - [SDR CHQA20121108435](https://openairdocs.org/sdr/CHQA20121108435.md): Support · corroded · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SUPPORT AT FRAMES 10 THROUGH 11. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-016499A. - [SDR CHQA20121108429](https://openairdocs.org/sdr/CHQA20121108429.md): Support Bracket · corroded · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, THE COCKPIT UNDERFLOOR AILERON QUADRANT RIGHT SUPPORT BRACKET WAS FOUND TO BE CORRODED. THE SUPPORT BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121108428](https://openairdocs.org/sdr/CHQA20121108428.md): Seat Track · corroded · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 23 THROUGHT FRAME 28. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06. - [SDR CHQA20121108426](https://openairdocs.org/sdr/CHQA20121108426.md): Doubler · damaged · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE LOWER REPAIR WAS FOUND TO BE DAMAGED. THE LOWER PLATE WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00. - [SDR CHQA20121108425](https://openairdocs.org/sdr/CHQA20121108425.md): Doubler · damaged · Nov 8, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE UPPER REPAIR WAS FOUND TO BE DAMAGED. THE UPPER PLATES WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00. - [SDR CHQA20121107433](https://openairdocs.org/sdr/CHQA20121107433.md): Floor Support · corroded · Nov 7, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT CARBON CROSSMEMBER BETWEEN FRAMES 24 AND 25. THE INBOARD SIDE LEFT-HAND OMEGA BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00. - [SDR CHQA20121107434](https://openairdocs.org/sdr/CHQA20121107434.md): Floor Support · corroded · Nov 7, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE OF THE CENTER OMEGA BEAM AT CARBON CROSSMEMBER FRAME 24. THE LEFT CENTER OMEGA BEAM AT FRAME 24 WAS REPAIRED IN ACCORDANCE WITH SRM53-00-10. - [SDR CHQA20121107427](https://openairdocs.org/sdr/CHQA20121107427.md): Floor Support · corroded · Nov 7, 2012 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE OF THE CENTER OMEGA BEAM AT CARBON CROSSMEMBER FRAME 28. THE LEFT CENTER OMEGA BEAM AT FRAME 28 WAS REPAIRED IN ACCORDANCE WITH SRM 51-20-03. - [SDR CHQA20120508146](https://openairdocs.org/sdr/CHQA20120508146.md): Control Panel · faulty · May 8, 2012 · N377SK · Emb EMB135KL · Emergency Lighting > CREW REPORTED THAT THE FLIGHT ATTENDANT COULD NOT CONTROL THE EMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT PANEL, THE LIGHTS WORKED PROPERLY FROM THE COCKPIT. MAINTENANCE REPLACED THE PASSENGER LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER - [SDR CHQA20120506143](https://openairdocs.org/sdr/CHQA20120506143.md): Light · inoperative · May 6, 2012 · N377SK · Emb EMB135KL · Emergency Lighting > CREW REPORTED THAT THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT THE EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120228065](https://openairdocs.org/sdr/CHQA20120228065.md): Fuel Filter · clogged · Feb 28, 2012 · N377SK · Emb EMB135KL · Engine Fuel Distribution > CREW REPORTED THAT THEY RECEIVED AN ENGINE 1 FUEL IMPENDING BYPASS MESSAGE AND AN ENGINE 2 FUEL IMPENDING BYPASS MESSAGE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH THE ENGINE 1 AND ENGINE 2 FUEL FILTERS. - [SDR CHQA201200023](https://openairdocs.org/sdr/CHQA201200023.md): Computer · faulty · Jan 22, 2012 · N377SK · Emb EMB135KL · Navigation System > CREW REPORTED THAT THE NAVIGATION 2 RADIO DASHED OUT DURING FLIGHT. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER NAVIGATION COMPUTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201200009](https://openairdocs.org/sdr/CHQA201200009.md): Frame · cracked · Dec 29, 2011 · N377SK · Emb EMB135KL · Fuselage Main, Frame > DURING INSPECTION, THE COCKPIT LEFT FRAME 10, JUST BELOW THE SIDE WINDOW WAS FOUND CRACKED. THE COCKPIT LEFTD FRAME 10, JUST BELOW THE SIDE WINDOW, WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201200008](https://openairdocs.org/sdr/CHQA201200008.md): Beam · corroded · Dec 23, 2011 · N377SK · 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 CHQA201200007](https://openairdocs.org/sdr/CHQA201200007.md): Floor Support · cracked · Dec 23, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, THE CENTER FUSELAGE 3 RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CENTER FUSELAGE 3 RIGHT OMEGA BEAM ANGLE IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA201200002](https://openairdocs.org/sdr/CHQA201200002.md): Skin · cracked · Dec 23, 2011 · N377SK · Emb EMB135KL · Wing, Plate/Skin > DURING INSPECTION, THE LEFT WING LOWER SKIN, AT WING STATION YA-2360.17 WAS FOUND TO BE CRACKED. THE LEFT WING LOWER SKIN AT STATION YA-2360.17 WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-109980. - [SDR CHQA201200010](https://openairdocs.org/sdr/CHQA201200010.md): Skin · dented · Dec 22, 2011 · N377SK · Emb EMB135KL · Wing, Plate/Skin > DURING INSPECTION, MAINTENANCE COMPLIED WITH DMI 750741/1, BY REPAIRING DENT IN THE LOWER WING RIGHT NEAR THE MAIN LANDING GEAR WHEEL WELL. THE REPAIR WAS PERFORMED IN ACCORDANCE WITH ETD 2011-145-109800. - [SDR CHQA201200006](https://openairdocs.org/sdr/CHQA201200006.md): Structure · corroded · Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE FORWARD (PN: 145-25175-001) AND AFT (PN:145-25369-003) L SHAPE. THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L SHAPE WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-110089. - [SDR CHQA201200005](https://openairdocs.org/sdr/CHQA201200005.md): Frame · cracked · Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT FRAME 23, JUST UNDER SILL NUMBER 1. THE RIGHT FRAME 23, JUST UNDER SILL NUMBER 1, WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-109968 AND SRM 53-00-04. - [SDR CHQA201200004](https://openairdocs.org/sdr/CHQA201200004.md): Beam · corroded · Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE REAR FUSELAGE 1 FLOOR STRUCTURE. THE CARGO DOOR LOWER BEAM WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100425](https://openairdocs.org/sdr/CHQA201100425.md): Ballast · defective · Nov 8, 2011 · N377SK · Emb EMB135KL · Passenger Compartment Lighting > CREW REPORTED THAT ON DESCENT THERE WAS AN ELECTRICAL ODOR IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LIGHTING BALLAST AT ROW 3 AND ROW 5. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100229](https://openairdocs.org/sdr/CHQA201100229.md): O-Ring · leaking · Jun 21, 2011 · N377SK · Emb EMB135KL · Pneumatic Distribution System > CREW REPORTED A BLEED 1 LEAK MESSAGE WHILE CLIMBING OUT OF KORD. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 BLEED SYSTEM AND FOUND THE O-RINGS AT JOINTS 5 AND 13 LEAKING. THE O-RINGS WERE REPLACED WITH NO FURT - [SDR CHQA201100184](https://openairdocs.org/sdr/CHQA201100184.md): Isis · inoperative · May 20, 2011 · N377SK · Emb EMB135KL · Integrated Flight System > CREW REPORTED THAT AFTER TAKEOFF THE ISIS ATTITUDE INDICATOR WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO KORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ISIS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100128](https://openairdocs.org/sdr/CHQA201100128.md): Skin · damaged · Apr 3, 2011 · N377SK · Emb EMB135KL · Fuselage Main, Plate/Skin > WHILE MOVING THE JET BRIDGE FROM THE AIRCRAFT, THE JET BRIDGE MADE CONTACT AIRCRAFT DAMAGING THE FORWARD FUSELAGE, AOA VANE, TAT SENSOR, ICE DETECTOR, AND THE PITOT PROBE. AOA VANE, TAT SENSOR, ICE DETECTOR AND PITOT PROBE WERE REPLACED AND A TEMPORARY REPAIR - [SDR CHQA201100057](https://openairdocs.org/sdr/CHQA201100057.md): Brake Sys · contaminated · Mar 11, 2011 · N377SK · Emb EMB135KL · Landing Gear Brake System > CREW REPORTED THAT AFTER LANDING THE BRAKES WERE SLUGGISH AND THAT THE PEDALS HAD TO BE PUSHED ALL THE WAY TO THE FLOOR BEFORE THEY WERE EFFECTIVE. MAINTENANCE BLED ALL 4 BRAKE SYSTEMS. AIR WAS FOUND TO BE PRESENT IN THE INBOARD AND OUTBOARD BRAKE SYSTEMS. - [SDR CHQA201100004](https://openairdocs.org/sdr/CHQA201100004.md): Light · inoperative · Jan 8, 2011 · N377SK · Emb EMB135KL · Antenna/Radome Anti-Ice/De-Ice System > DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000228](https://openairdocs.org/sdr/CHQA201000228.md): Precooler · cracked · Dec 16, 2010 · N377SK · Emb EMB135KL · Pneumatic Distribution System > DURING CLIMBOUT, THE FLIGHT CREW REPORTED A BLEED 1 OVERTEMP MESSAGE IN ICING CONDITIONS. THE FLIGHT CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE THERMOSTAT BUT THE SYSTEM WOULD NOT PASS OPS CHECKS. UPON FURTHER VISUAL INSPEC - [SDR CHQA201000220](https://openairdocs.org/sdr/CHQA201000220.md): Valve · inoperative · Dec 1, 2010 · N377SK · Emb EMB135KL · Pneumatic Distribution System > DURING CLIMB OUT OF GRR, THE FLIGHT CREW REPORTED A BLD 1 OVERTEMP MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE BLEED 1 VALVE WAS CLOSED AND THE FLIGHT CONTINUED ON TO ORD. ON APPROACH INTO ORD, REPORTED AN ICE CONDITION-ANTI ICE INOP WARNING. DUE TO THE - [SDR CHQA201000131](https://openairdocs.org/sdr/CHQA201000131.md): O-Ring · leaking · Jun 24, 2010 · N377SK · Emb EMB135KL · Pneumatic Distribution System > AFTER TAKEOFF THE CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS AND RETURNED TO FIELD. MAINTENANCE FOUND LEAKS AT JOINTS 9 AND 11 AND REPLACED THE O-RINGS AT BOTH JOINTS AND THE BLEED SYSTEM WAS CHECKING GOOD. - [SDR CHQA201000025](https://openairdocs.org/sdr/CHQA201000025.md): Strut · overserviced · Feb 1, 2010 · N377SK · Emb EMB135KL · Nose/Tail Landing Gear Strut/Axle > WHILE GETTING VECTORS FOR APPROACH THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS WHEN THE GEAR WAS EXTENDED. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR STRUT FULLY EXTENDED UPON INSPECTION. - [SDR CHQA201000019](https://openairdocs.org/sdr/CHQA201000019.md): Wire Harness · damaged · Jan 28, 2010 · N377SK · Emb EMB135KL · Landing Gear System Wiring > THE FLIGHT CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF ALONG WITH A TAKEOFF CONFIG WARNING. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DOWNLOADED THE CMC AND FOUND MESSAGES FOR LGEU FAIL 1X, NOSE LG PROX SW - [SDR CHQA201000013](https://openairdocs.org/sdr/CHQA201000013.md): Electronic Unit · faulty · Jan 21, 2010 · N377SK · Emb EMB135KL · Landing Gear Position and Warning > AFTER TAKEOFF FROM EWR, THE LANDING GEAR WOULD NOT RETRACT AND CREW RECEIVED AN LG AIR/GND FAIL MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LGEU DUE TO LGEU FAIL MESSAGE ON CMC. THE AIRCRAFT WAS THEN - [SDR CHQA200900184](https://openairdocs.org/sdr/CHQA200900184.md): Flight Recorder · inoperative · Aug 26, 2009 · N377SK · Emb EMB135KL · Data Recorders (Flight/Maintenance) > DURING TAKEOFF ROLL IN STL ON RW 12L, EICAS MESSAGE "DFDR FAIL" APPEARED AT 60 KNOTS. THE TAKEOFF WAS ABORTED. WHEN THE FLIGHT RETURNED TO THE GATE, MAINTENANCE DEFERRED THE ITEM AND THE FLIGHT THEN CONTINUED AS NORMAL. ON THE NEXT DAY IN STL, MAINTENANCE C - [SDR CHQA200900169](https://openairdocs.org/sdr/CHQA200900169.md): Splice · disconnected · Aug 2, 2009 · N377SK · Emb EMB135KL · Light System Wiring > DURING INSPECTION, THE NR 3 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOP. THE REMOVABLE SPLICE WAS RECONNECTED AT THE PROXIMITY STRIP AND THE LIGHTS OPERATED NORMALLY. - [SDR CHQA200900160](https://openairdocs.org/sdr/CHQA200900160.md): Light · inoperative · Jul 21, 2009 · N377SK · Emb EMB135KL · Emergency Lighting > THE EMERGENCY LIGHTS WERE ON WITH THE AIRCRAFT POWERED DOWN, BUT SOME WERE NOT ILLUMINATED. AFTER CYCLING THE EMERGENCY LIGHTS ALL BUT THE LIGHTS OVER THE WING EXITS OPERATED NORMALLY. MAINTENANCE RE-LAMPED THE LIGHTS AT THE OVERWING EXITS AND CLEANED AND RE - [SDR CHQA200800242](https://openairdocs.org/sdr/CHQA200800242.md): Proximity Switch · faulty · Dec 9, 2008 · N377SK · Emb EMB135KL · Landing Gear Position and Warning > FLIGHT 5315, MSP TO STL - AFTER TAKEOFF THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT BACK AT MSP. THE MESSAGE DISAPPEARED AFTER LAN - [SDR CHQA200700084](https://openairdocs.org/sdr/CHQA200700084.md): Proximity Switch · faulted · Dec 3, 2007 · N377SK · Emb EMB135KL · Landing Gear Position and Warning > BWI TO STL - ON APPROACH TO STL, WHEN THE GEAR WAS SELECTED DOWN, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE. THE AIRCRAFT DID A GO AROUND IN ORDER TO RUN THE QRH AND AS A PRECAUTION THE LANDING GEAR WAS LEFT DOWN. ON THE SECOND APPROACH - [SDR CHQA200600127](https://openairdocs.org/sdr/CHQA200600127.md): Bulb · burned out · Sep 25, 2006 · N377SK · Emb EMB135KL · Emergency Lighting > RT OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW MM 33-50-07. OPS CHECK GOOD. - [SDR CHQA200500033](https://openairdocs.org/sdr/CHQA200500033.md): Lamp · burned out · Feb 16, 2005 · N377SK · Emb EMB135KL · Emergency Lighting > LEFT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED IAW EMB 140 MM 33-50-07. - [SDR CHQA000546](https://openairdocs.org/sdr/CHQA000546.md): Bulb · inoperative · Aug 31, 2004 · N377SK · Emb EMB135KL · Emergency Lighting > LEFT SIDE EXTERNAL EMERGENCY OVERWING LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 140 MM. 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 = 'N377SK' AND deregistration_id = 'N377SK-2018-03-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N377SK-2018-03-30/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.