# N377SK: 2002 Embraer EMB-135KL, registration cancelled 2018-03-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 30, 2018
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145579
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 29, 2002
- Certificate issued: October 5, 2016
- Last registry action: October 5, 2016
- Mode S code: A44F66
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N377SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=377SK
- Page: https://openairdocs.org/deregistered/N377SK-2018-03-30

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-135KL: https://openairdocs.org/model/embraer-emb-135kl.md

## Service difficulty reports (47)

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

- [SDR CHQA20140427125](https://openairdocs.org/sdr/CHQA20140427125), Apr 27, 2014: BATTERY. DISCHARGED. DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO 
- [SDR CHQA20130722185](https://openairdocs.org/sdr/CHQA20130722185), Jul 22, 2013: WINDSHIELD. FAILED. DURING CRUISE, HEARD A LOUD POP IN COCKPIT AND CAPTAIN'S WINDSCREEN SHATTERED. DESCENDED AND DECLARED AN EMERGENCY. DIVERTED AND LANDED WITHOUT INCIDENT. REPLAC
- [SDR CHQA20130620221](https://openairdocs.org/sdr/CHQA20130620221), Jun 20, 2013: BATTERY PACK. DISCHARGED. 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 FURTH
- [SDR CHQA20130310078](https://openairdocs.org/sdr/CHQA20130310078), Mar 10, 2013: PRESSURE SWITCH. FAULTY. 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 ALS
- [SDR CHQA20130310077](https://openairdocs.org/sdr/CHQA20130310077), Mar 10, 2013: PRESSURE SWITCH. FAULTY. 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 ALS
- [SDR CHQA201211/14431](https://openairdocs.org/sdr/CHQA201211%2F14431), Nov 14, 2012: STRINGER. CORRODED. 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), Nov 8, 2012: SUPPORT. CORRODED. 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 ACCOR
- [SDR CHQA20121108435](https://openairdocs.org/sdr/CHQA20121108435), Nov 8, 2012: SUPPORT. CORRODED. 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), Nov 8, 2012: SUPPORT BRACKET. CORRODED. DURING INSPECTION, THE COCKPIT UNDERFLOOR AILERON QUADRANT RIGHT SUPPORT BRACKET WAS FOUND TO BE CORRODED. THE SUPPORT BRACKET WAS REPLACED IN ACCORDANCE WITH S
- [SDR CHQA20121108428](https://openairdocs.org/sdr/CHQA20121108428), Nov 8, 2012: SEAT TRACK. CORRODED. 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 53-01-0
- [SDR CHQA20121108426](https://openairdocs.org/sdr/CHQA20121108426), Nov 8, 2012: DOUBLER. DAMAGED. 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
- [SDR CHQA20121108425](https://openairdocs.org/sdr/CHQA20121108425), Nov 8, 2012: DOUBLER. DAMAGED. 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 SR
- [SDR CHQA20121107433](https://openairdocs.org/sdr/CHQA20121107433), Nov 7, 2012: FLOOR SUPPORT. CORRODED. 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 OME
- [SDR CHQA20121107434](https://openairdocs.org/sdr/CHQA20121107434), Nov 7, 2012: FLOOR SUPPORT. CORRODED. 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 REPA
- [SDR CHQA20121107427](https://openairdocs.org/sdr/CHQA20121107427), Nov 7, 2012: FLOOR SUPPORT. CORRODED. 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 REPA
- [SDR CHQA20120508146](https://openairdocs.org/sdr/CHQA20120508146), May 8, 2012: CONTROL PANEL. FAULTY. CREW REPORTED THAT THE FLIGHT ATTENDANT COULD NOT CONTROL THE EMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT PANEL, THE LIGHTS WORKED PROPERLY FROM THE COCKPIT. MAI
- [SDR CHQA20120506143](https://openairdocs.org/sdr/CHQA20120506143), May 6, 2012: LIGHT. INOPERATIVE. CREW REPORTED THAT THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT THE EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR STRIP. OPERATIONAL 
- [SDR CHQA20120228065](https://openairdocs.org/sdr/CHQA20120228065), Feb 28, 2012: FUEL FILTER. CLOGGED. 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 FIE
- [SDR CHQA201200023](https://openairdocs.org/sdr/CHQA201200023), Jan 22, 2012: COMPUTER. FAULTY. CREW REPORTED THAT THE NAVIGATION 2 RADIO DASHED OUT DURING FLIGHT. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER NAVIG
- [SDR CHQA201200009](https://openairdocs.org/sdr/CHQA201200009), Dec 29, 2011: FRAME. CRACKED. 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
- [SDR CHQA201200008](https://openairdocs.org/sdr/CHQA201200008), Dec 23, 2011: BEAM. CORRODED. 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 A
- [SDR CHQA201200007](https://openairdocs.org/sdr/CHQA201200007), Dec 23, 2011: FLOOR SUPPORT. CRACKED. 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 AC
- [SDR CHQA201200002](https://openairdocs.org/sdr/CHQA201200002), Dec 23, 2011: SKIN. CRACKED. 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 
- [SDR CHQA201200010](https://openairdocs.org/sdr/CHQA201200010), Dec 22, 2011: SKIN. DENTED. 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 PERFO
- [SDR CHQA201200006](https://openairdocs.org/sdr/CHQA201200006), Dec 22, 2011: STRUCTURE. CORRODED. 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 SURRO
- [SDR CHQA201200005](https://openairdocs.org/sdr/CHQA201200005), Dec 22, 2011: FRAME. CRACKED. 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 W
- [SDR CHQA201200004](https://openairdocs.org/sdr/CHQA201200004), Dec 22, 2011: BEAM. CORRODED. 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 R
- [SDR CHQA201100425](https://openairdocs.org/sdr/CHQA201100425), Nov 8, 2011: BALLAST. DEFECTIVE. 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 
- [SDR CHQA201100229](https://openairdocs.org/sdr/CHQA201100229), Jun 21, 2011: O-RING. LEAKING. 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 BLEE
- [SDR CHQA201100184](https://openairdocs.org/sdr/CHQA201100184), May 20, 2011: ISIS. INOPERATIVE. CREW REPORTED THAT AFTER TAKEOFF THE ISIS ATTITUDE INDICATOR WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO KORD AND LANDED WITHOUT INCIDENT. MAINTENANCE R
- [SDR CHQA201100128](https://openairdocs.org/sdr/CHQA201100128), Apr 3, 2011: SKIN. DAMAGED. 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 P
- [SDR CHQA201100057](https://openairdocs.org/sdr/CHQA201100057), Mar 11, 2011: BRAKE SYS. CONTAMINATED. 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 
- [SDR CHQA201100004](https://openairdocs.org/sdr/CHQA201100004), Jan 8, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT WITH NO FURTHER DEFECTS
- [SDR CHQA201000228](https://openairdocs.org/sdr/CHQA201000228), Dec 16, 2010: PRECOOLER. CRACKED. DURING CLIMBOUT, THE FLIGHT CREW REPORTED A BLEED 1 OVERTEMP MESSAGE IN ICING CONDITIONS. THE FLIGHT CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTEN
- [SDR CHQA201000220](https://openairdocs.org/sdr/CHQA201000220), Dec 1, 2010: VALVE. INOPERATIVE. 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 CONTIN
- [SDR CHQA201000131](https://openairdocs.org/sdr/CHQA201000131), Jun 24, 2010: O-RING. LEAKING. 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 BO
- [SDR CHQA201000025](https://openairdocs.org/sdr/CHQA201000025), Feb 1, 2010: STRUT. OVERSERVICED. 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
- [SDR CHQA201000019](https://openairdocs.org/sdr/CHQA201000019), Jan 28, 2010: WIRE HARNESS. DAMAGED. 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 WIT
- [SDR CHQA201000013](https://openairdocs.org/sdr/CHQA201000013), Jan 21, 2010: ELECTRONIC UNIT. FAULTY. 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 WITHOU
- [SDR CHQA200900184](https://openairdocs.org/sdr/CHQA200900184), Aug 26, 2009: FLIGHT RECORDER. INOPERATIVE. 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
- [SDR CHQA200900169](https://openairdocs.org/sdr/CHQA200900169), Aug 2, 2009: SPLICE. DISCONNECTED. 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 OPERATE
- [SDR CHQA200900160](https://openairdocs.org/sdr/CHQA200900160), Jul 21, 2009: LIGHT. INOPERATIVE. 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 
- [SDR CHQA200800242](https://openairdocs.org/sdr/CHQA200800242), Dec 9, 2008: PROXIMITY SWITCH. FAULTY. 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 WA
- [SDR CHQA200700084](https://openairdocs.org/sdr/CHQA200700084), Dec 3, 2007: PROXIMITY SWITCH. FAULTED. 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 I
- [SDR CHQA200600127](https://openairdocs.org/sdr/CHQA200600127), Sep 25, 2006: BULB. BURNED OUT. 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), Feb 16, 2005: LAMP. BURNED OUT. LEFT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED IAW EMB 140 MM 33-50-07.
- [SDR CHQA000546](https://openairdocs.org/sdr/CHQA000546), Aug 31, 2004: BULB. INOPERATIVE. LEFT SIDE EXTERNAL EMERGENCY OVERWING LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 140 MM. OPS CHECK GOOD.

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS11IA819](https://openairdocs.org/ntsb/OPS11IA819), Aug 8, 2011: Embraer EMB-135KL (N377SK), Chicago, IL, incident, no damage. Probable cause: The improper air traffic control takeoff clearance issued by the local controller because of his lack of monitoring and lack of awareness of the conflicting arrival airplane.
- [NTSB CEN11IA270](https://openairdocs.org/ntsb/CEN11IA270), Apr 3, 2011: Embraer EMB-135KL (N377SK), Dubuque, IA, incident, minor damage. Probable cause: The airport authorities' improper decision to deactivate the jet bridge braking system which created an unsafe condition by the gate agents not being able to stop the bridge from impacting the…

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110403011519I](https://openairdocs.org/incident/20110403011519I), Apr 3, 2011: Embraer EMB-135KL (N377SK), Dubuque, IA, Substantial damage. With the wheels facing forward, the jet bridge was retracted away from the aircraft to its normal retracted length. The wheels were then turned 90 degrees to…
- [Incident 20030520009259I](https://openairdocs.org/incident/20030520009259I), May 20, 2003: Emb EMB135KL (N377SK), St Louis, MO. (-23) Chqa flight 5896 enroute to stl had an unruly passenger who tried to enter the cockpit. Passenger was subdued by other passengers and strapped into his…

---
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.