# N379SK: 2002 Embraer EMB-135KL, registration cancelled 2017-01-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 27, 2017
- 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 AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145606
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 21, 2002
- Certificate issued: October 6, 2016
- Last registry action: October 6, 2016
- Mode S code: A456D4
- 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/N379SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=379SK
- Page: https://openairdocs.org/deregistered/N379SK-2017-01-27

From the FAA registry file of November 3, 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 (41)

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

- [SDR CHQA20131107427](https://openairdocs.org/sdr/CHQA20131107427), Nov 7, 2013: SKIN. CORRODED. 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), Nov 7, 2013: SUPPORT. CORRODED. 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 51-40-0
- [SDR CHQA20131107425](https://openairdocs.org/sdr/CHQA20131107425), Nov 7, 2013: SUPPORT. CORRODED. 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 
- [SDR CHQA20131107424](https://openairdocs.org/sdr/CHQA20131107424), Nov 7, 2013: STRINGER. CORRODED. 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), Nov 7, 2013: STRINGER. CORRODED. 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), Nov 7, 2013: FITTING. CRACKED. 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), Nov 7, 2013: FITTING. CORRODED. 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), Nov 7, 2013: FITTING. CRACKED. 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), Nov 7, 2013: FITTING. CRACKED. 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), Nov 7, 2013: FITTING. CORRODED. 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), Jun 14, 2013: TRIM SWITCH. DIRTY. 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 EMER
- [SDR CHQA20130614205](https://openairdocs.org/sdr/CHQA20130614205), Jun 14, 2013: LIGHT. INOPERATIVE. 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 CHE
- [SDR CHQA20130614204](https://openairdocs.org/sdr/CHQA20130614204), Jun 14, 2013: LIGHT. INOPERATIVE. 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), Jun 2, 2013: LIGHT. INOPERATIVE. 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. O
- [SDR CHQA20120420127](https://openairdocs.org/sdr/CHQA20120420127), Apr 20, 2012: SEAL. DETACHED. 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 
- [SDR CHQA20120405116](https://openairdocs.org/sdr/CHQA20120405116), Apr 5, 2012: SKIN. DENTED. 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 EDD
- [SDR CHQA20120403123](https://openairdocs.org/sdr/CHQA20120403123), Apr 3, 2012: FLOOR SUPPORT. CRACKED. 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 ACCORD
- [SDR CHQA20120403122](https://openairdocs.org/sdr/CHQA20120403122), Apr 3, 2012: FRAME. CRACKED. 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
- [SDR CHQA20120403121](https://openairdocs.org/sdr/CHQA20120403121), Apr 3, 2012: FRAME. CRACKED. 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
- [SDR CHQA20120402120](https://openairdocs.org/sdr/CHQA20120402120), Apr 2, 2012: DOOR FRAME. CORRODED. 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), Apr 2, 2012: SHEAR PLATE. CORRODED. 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 201
- [SDR CHQA20120402118](https://openairdocs.org/sdr/CHQA20120402118), Apr 2, 2012: BEAM. CORRODED. 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 W
- [SDR CHQA20120405117](https://openairdocs.org/sdr/CHQA20120405117), Apr 2, 2012: DOOR FRAME. CRACKED. 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 2012-145-00473
- [SDR CHQA201200026](https://openairdocs.org/sdr/CHQA201200026), Jan 26, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE EXTERIOR EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY ON
- [SDR CHQA201100506](https://openairdocs.org/sdr/CHQA201100506), Dec 26, 2011: LIGHT. INOPERATIVE. DURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY EXIT LIGHT.
- [SDR CHQA201100287](https://openairdocs.org/sdr/CHQA201100287), Jul 24, 2011: PROXIMITY SWITCH. OUT OF ADJUST. 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 I
- [SDR CHQA201100133](https://openairdocs.org/sdr/CHQA201100133), Apr 13, 2011: TIRE. SEPARATED. 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 
- [SDR CHQA201100122](https://openairdocs.org/sdr/CHQA201100122), Mar 20, 2011: THERMOSTAT. INOPERATIVE. 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
- [SDR CHQA201100040](https://openairdocs.org/sdr/CHQA201100040), Feb 21, 2011: ENGINE. MALFUNCTIONED. 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 PROCEE
- [SDR CHQA201100005](https://openairdocs.org/sdr/CHQA201100005), Jan 10, 2011: PROXIMITY SWITCH. CORRODED. 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-
- [SDR CHQA201000210](https://openairdocs.org/sdr/CHQA201000210), Nov 12, 2010: TIRE. BLOWN. 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
- [SDR CHQA201000143](https://openairdocs.org/sdr/CHQA201000143), Jul 20, 2010: BATTERY PACK. DISCHARGED. 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 D
- [SDR CHQA201000140](https://openairdocs.org/sdr/CHQA201000140), Jul 12, 2010: FLEX DRIVE. DAMAGED. 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 CHEC
- [SDR CHQA200900269](https://openairdocs.org/sdr/CHQA200900269), Dec 28, 2009: LIGHT. INOPERATIVE. 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
- [SDR CHQA200900161](https://openairdocs.org/sdr/CHQA200900161), Jul 21, 2009: CONTROL VALVE. LEAKING. 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 CLE
- [SDR CHQA200900107](https://openairdocs.org/sdr/CHQA200900107), Apr 14, 2009: WIRE. BROKEN. 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
- [SDR CHQA200900025](https://openairdocs.org/sdr/CHQA200900025), Jan 19, 2009: STRUT. UNDERSERVICED. 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 FL
- [SDR CHQA200900024](https://openairdocs.org/sdr/CHQA200900024), Jan 19, 2009: CONNECTOR. CORRODED. 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
- [SDR CHQ2008F00004](https://openairdocs.org/sdr/CHQ2008F00004), Aug 30, 2008: FUEL CONTROL. FAILED. 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 WER
- [SDR CHQA200800163](https://openairdocs.org/sdr/CHQA200800163), Aug 14, 2008: CONTROL PANEL. INTERMITTENT. 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 WE
- [SDR CHQA200500086](https://openairdocs.org/sdr/CHQA200500086), Apr 22, 2005: BATTERY PACK. DISCHARGED. 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 I

## FAA accident and incident reports (1)

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 20101112052059I](https://openairdocs.org/incident/20101112052059I), Nov 12, 2010: Embraer EMB-135KL (N379SK), Flint, MI, Minor damage. Flight 5007 from fnt to ord departed fnt at 1253 EDT. Flight crew heard a loud bang and smelled rubber. The flight continued to ord and declared an emergency…

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