# N375SK: 2002 Embraer EMB-135KL, registration cancelled 2017-05-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 31, 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 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: 145569
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 21, 2002
- Certificate issued: October 5, 2016
- Last registry action: October 5, 2016
- Mode S code: A447F8
- 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/N375SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=375SK
- Page: https://openairdocs.org/deregistered/N375SK-2017-05-31

From the FAA registry file of October 31, 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 (36)

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

- [SDR CHQA20130102001](https://openairdocs.org/sdr/CHQA20130102001), Jan 2, 2013: WARNING SYSTEM. FALSE ACTIVATION. ON DEPARTURE WHILE CLIMBING THROUGH 11,000FT, THE FLIGHT CREW REPORTED A BAGGAGE SMOKE MESSAGE ON EICAS AND A SMOKE ODOR. THE FLIGHT CREW DISCHARGED BOTH BAGGAG
- [SDR CHQA20120323089](https://openairdocs.org/sdr/CHQA20120323089), Mar 23, 2012: VALVE. INOPERATIVE. CREW REPORTED A BLEED 2 OVERTEMP MESSAGE DURING CLIMB. THE CREW RETURNED TO FIELD AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER 2 FA
- [SDR CHQA201100505](https://openairdocs.org/sdr/CHQA201100505), Dec 16, 2011: SKIN. DAMAGED. DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON STRINGER 20R BETWEEN FRAME 15-16. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-0
- [SDR CHQA201100504](https://openairdocs.org/sdr/CHQA201100504), Dec 16, 2011: SKIN. DAMAGED. DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON FRAME 22 BETWEEN STRINGERS 19R-20R. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21
- [SDR CHQA201100502](https://openairdocs.org/sdr/CHQA201100502), Dec 14, 2011: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM LOWER LIP AT FRAME 27. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT FRAME 27 IN ACCORDANCE WITH
- [SDR CHQA201100477](https://openairdocs.org/sdr/CHQA201100477), Dec 12, 2011: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON FRAME 23. MAINTENANCE REPAIRED THE RIGHT-HAND FUSELAGE AT FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 2011-145-1
- [SDR CHQA201100503](https://openairdocs.org/sdr/CHQA201100503), Dec 12, 2011: SKIN. CORRODED. DURING INSPECTION, A BLENDOUT ON THE LEFT SKIN BAY BORDERED BY FRAME 19-20 AND BETWEEN STRINGERS 14L-15L WAS FOUND CORRODED. MAINTENANCE REPAIRED THE BLENDOUT O
- [SDR CHQA201100501](https://openairdocs.org/sdr/CHQA201100501), Dec 10, 2011: FRAME. CRACKED. DURING INSPECTION, THE COCKPIT LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002)
- [SDR CHQA201100500](https://openairdocs.org/sdr/CHQA201100500), Dec 9, 2011: ANGLE. CRACKED. DURING INSPECTION, THE RIGHT WING BOX OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE RIGHT WING BOX OMEGA BEAM ANGLE IN ACCORDANCE WITH SRM 
- [SDR CHQA201100499](https://openairdocs.org/sdr/CHQA201100499), Dec 9, 2011: BEAM. CORRODED. DURING INSPECTION, THE LEFT OUTBOARD BEAM FROM FRAME 48 TO FRAME 53 UNDER THE SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT OUTBOARD BEAM F
- [SDR CHQA201100498](https://openairdocs.org/sdr/CHQA201100498), Dec 9, 2011: BEAM. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE I FLOOR STRUCTURE HAT BEAM AT FRAME 23 STATION WAS FOUND CORRODED. MAINTENANCE REPLACED THE CENTER FUSELAGE I FLOOR STRUC
- [SDR CHQA201100497](https://openairdocs.org/sdr/CHQA201100497), Dec 9, 2011: REPAIR. CORRODED. DURING INSPECTION, THE LEFT BEAM EXISTING REPAIR AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM AT FRAME 20 IN ACCORDANCE WITH SRM 53-
- [SDR CHQA201100365](https://openairdocs.org/sdr/CHQA201100365), Sep 9, 2011: CONTROLLER. INOPERATIVE. CREW REPORTED THAT CABIN PRESSURIZATION REACHED 10,000 FEET AT 10,500 FEET. THE CREW RECEIVED AN AURAL WARNING OF CABIN PRESSURE AND THE CABIN PRESSURE INDICATI
- [SDR CHQA201100282](https://openairdocs.org/sdr/CHQA201100282), Jul 22, 2011: SOLENOID VALVE. INOPERATIVE. CREW REPORTED THAT DURING FLIGHT THERE WAS A LOUD THUMPING NOISE FOLLOWED BY A RUSHING AIR SOUND AND VIBRATION UNDER THE COCKPIT FLOOR BOARDS. THERE WERE NO GEA
- [SDR CHQA201100259](https://openairdocs.org/sdr/CHQA201100259), Jun 30, 2011: LIGHT. INTERMITTENT. CREW REPORTED THAT UPON ENTERING THE AIRCRAFT THE MIDDLE SECTION OF EMERGENCY FLOOR PROXIMITY LIGHT STRIPS ILLUMINATED. AFTER CYCLING POWER AND PERFORMING AN OP
- [SDR CHQA201100192](https://openairdocs.org/sdr/CHQA201100192), May 25, 2011: BALLAST. BURNED. CREW REPORTED THAT DURING FLIGHT THERE WAS A STRONG BURNING SMELL FROM ROWS 6, 7, 8. MAINTENANCE FOUND THE SIDEWALL LIGHTING BALLAST AT ROW 7 TO BE BURNT. MAINT
- [SDR CHQA201100137](https://openairdocs.org/sdr/CHQA201100137), Apr 15, 2011: BATTERY. DEFECTIVE. DURING INSPECTION, MAINTENANCE FOUND THE MAIN ENTRY DOOR EMERGENCY LIGHT TO BE OPERATING INTERMITTENTLY. MAINTENANCE REPLACED THE MAIN ENTRY DOOR EMERGENCY LIGH
- [SDR CHQA201100100](https://openairdocs.org/sdr/CHQA201100100), Mar 23, 2011: CONNECTOR. CORRODED. CREW REPORTED THAT THE NOSE LANDING GEAR DOORS STAYED OPEN AFTER TAKEOFF. MAINTENANCE PLACED THE AIRCRAFT ON JACKS AND PERFORMED MULTIPLE GEAR SWINGS WITH NO DE
- [SDR CHQA201100099](https://openairdocs.org/sdr/CHQA201100099), Mar 23, 2011: UNKNOWN. NOISY. CREW REPORTED THAT DURING FLIGHT THERE WAS A LOUD NOISE COMING FROM THE NOSE OF THE PLANE. REPORTED THAT IT SOUNDED AS IF THE NOSE LANDING GEAR DOORS WERE NOT F
- [SDR CHQA201100073](https://openairdocs.org/sdr/CHQA201100073), Mar 22, 2011: UNKNOWN. NOISY. CREW REPORTED THAT AFTER RAISING THE LANDING GEAR DURING TAKEOFF, THERE WAS A LOUD WIND NOISE COMING FROM THE NOSE WHEEL COMPARTMENT. ALL GEAR INDICATIONS INDIC
- [SDR CHQA201100022](https://openairdocs.org/sdr/CHQA201100022), Jan 21, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT LEADING EDGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT LEADING EDGE EMERGENCY LIGHT BULB WITH NO 
- [SDR CHQA201100021](https://openairdocs.org/sdr/CHQA201100021), Jan 21, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT BULB WITH NO 
- [SDR CHQA201100007](https://openairdocs.org/sdr/CHQA201100007), Jan 12, 2011: UNKNOWN. VIBRATION. CREW REPORTED THAT ON CLIMBOUT, HEARD A NOISE THAT SOUNDED LIKE A PANEL WAS OPEN OR THAT THE NOSE LANDING GEAR DOORS HAD NOT CLOSED. THE VIBRATION COULD BE FELT
- [SDR CHQA201000161](https://openairdocs.org/sdr/CHQA201000161), Aug 22, 2010: UPLOCK. DAMAGED. DURING CLIMBOUT, AFTER SELECTING THE LANDING GEAR UP RECEIVED A RED CROSS HATCHED INDICATION FOR THE NOSE GEAR WHILE BOTH MAINS INDICATED UP AND LOCKED. THE QRH
- [SDR CHQA201000070](https://openairdocs.org/sdr/CHQA201000070), Apr 1, 2010: RELAY. INTERMITTENT. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE TURNING ON AND OFF INTERMITTENTLY. MAINTENANCE REPLACED RELAY K0275 PER AMM 20-10-02, OPS CHECK OF EMERGENCY LIGHTS
- [SDR CHQA201000069](https://openairdocs.org/sdr/CHQA201000069), Apr 1, 2010: LIGHT. MALFUNCTIONED. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE FLASHING ON AND OFF INTERMITTENTLY. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB AMM 35-50-00.
- [SDR CHQA201000045](https://openairdocs.org/sdr/CHQA201000045), Feb 22, 2010: BLEED VALVE. FAILED. DURING CLIMB, CREW REPORTED A BLEED 1 VALVE FAIL MESSAGE IN ICING CONDITIONS. IT WAS DECIDED TO RETURN TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED 
- [SDR CHQA201000004](https://openairdocs.org/sdr/CHQA201000004), Jan 16, 2010: CONNECTOR. CONTAMINATED. JUST AFTER TAKEOFF FROM KSTL THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE AND AN ENG 1/2 REVERSER DISAGREE MESSAGE. THE FLIGHT RETURNED TO THE FIELD AND LANDED U
- [SDR CHQA200800238](https://openairdocs.org/sdr/CHQA200800238), Dec 3, 2008: GENERATOR. FAILED. AFTER LANDING THE FLIGHT CREW RECEIVED A GENERATOR NR 4 BEARING FAIL MESSAGE ON EICAS. THE MESSAGE WAS DEFERRED PER MEL 24-31-02-1 CAT A. THE NR 4 GENERATOR WAS
- [SDR CHQ2008F00006](https://openairdocs.org/sdr/CHQ2008F00006), Sep 9, 2008: UNKNOWN. SMOKE. WHILE CLIMBING THROUGH 8,000 FT THE FLIGHT CREW WAS INFORMED OF SMOKE OR STEAM COMING FROM THE FLOOR OF THE CABIN BY THE F/A. THE QRH CHECKLISTS WERE COMPLIED W
- [SDR CHQA20070050](https://openairdocs.org/sdr/CHQA20070050), Sep 15, 2007: CARBON SEAL. LEAKING. STL TO MSP - AFTER TAKEOFF AT AROUND 1700FT, THE LAV SMOKE ALARM WENT OFF. THE FLIGHT ATTENDANT CONFIRMED THAT THE LAV SMOKE DETECTOR WAS GOING OFF. THERE WAS N
- [SDR CHQA200600104](https://openairdocs.org/sdr/CHQA200600104), Aug 23, 2006: CONTROLLER. MALFUNCTIONED. FLIGHT 9891 - SDF-STL - DURING CLIMBOUT WHILE LEVEL AT FL180 AND WAITING FOR FURTHER CLIMB CLEARANCE, THE CABIN ALTITUDE ALERT WENT OFF. THE ALTITUDE AT THE TIM
- [SDR CHQA200600022](https://openairdocs.org/sdr/CHQA200600022), Jan 30, 2006: WINDSHIELD. MELTED. FLIGHT 5342 - STL-MSP - WHEN WINDOW HEAT IS ON AND AIRCRAFT ENTERS ICING CONDITIONS, BOTH SHIELDS BEGIN TO SMOKE NEAR THE SENSOR BOX ONLY WHEN AIRCRAFT ANTI ICE
- [SDR CHQA200500150](https://openairdocs.org/sdr/CHQA200500150), Aug 27, 2005: LAMP. BURNED OUT. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW EMB 140 MM 33-50-07.
- [SDR CHQA200500137](https://openairdocs.org/sdr/CHQA200500137), Aug 7, 2005: REGULATOR VALVE. BURNED. FLIGHT 5282 - STL - ATL - ON CLIMB-OUT, RECEIVED BLEED 1 CLOSED MESSAGE AND A BURNING SMELL AROUND ROW 5A. FOUND THE PACK VALVE CIRCUIT BREAKER POPPED AND FOUND
- [SDR CHQA000567](https://openairdocs.org/sdr/CHQA000567), Oct 16, 2004: LAMP. BURNED OUT. LT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED INOPERATIVE LIGHT. OPS CHECK GOOD IAW MM 33-51-00.

## 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 20130102000109I](https://openairdocs.org/incident/20130102000109I), Jan 2, 2013: Embraer EMB-135KL (N375SK), Cedar Rapids, IA, No damage. Following departure from the Eastern Iowa Airport, Cedar Rapids, Iowa, the captain noticed an intermittent smell and assumed it to be deice fluid. While…
- [Incident 20080909846979I](https://openairdocs.org/incident/20080909846979I), Sep 9, 2008: Emb EMB135KL (N375SK), Raleigh/Durham, NC, No damage. (-23) Chautauqua flight 5331 operating on September 9, 2008 from Raleigh, north carolina to st. louis, Missouri experienced smoke in cabin during initial…

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