# N294SK: 2001 Embraer EMB-145LR, registration cancelled 2018-01-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 11, 2018
- Exported to: Kenya
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- 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: 145497
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 19, 2001
- Certificate issued: September 18, 2001
- Last registry action: November 9, 2017
- Mode S code: A305F0
- 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/N294SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=294SK
- Page: https://openairdocs.org/deregistered/N294SK-2018-01-11

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-145LR: https://openairdocs.org/model/embraer-emb-145lr.md

## Service difficulty reports (63, newest 50)

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

- [SDR UHLA201509130722](https://openairdocs.org/sdr/UHLA201509130722), Sep 13, 2015: SWITCH. DIRTY. THE MAIN ENTRY DOOR WAS UNABLE TO BE OPERATED WITH THE HYDRAULIC SYSTEM. MAINTENANCE FOUND AND CLEANED DEBRIS FROM THE MAIN ENTRY DOOR SWITCHES AND ALL OPS CHEC
- [SDR UHLA201507170566](https://openairdocs.org/sdr/UHLA201507170566), Jul 17, 2015: BALLAST. FAILED. THE LIGHT BALLAST OVER THE LAVATORY TOILET WAS FOUND TO BE SMOKING. MAINTENANCE DEACTIVATED THE BALLAST AND DEFERRED IT. MAINTENANCE LATER DETERMINED THE FAULT 
- [SDR UHLA201506190445](https://openairdocs.org/sdr/UHLA201506190445), Jun 19, 2015: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE DOUBLER AT LT OMEGA FRAME 20. THE DOUBLER, FILLER, AND 2 OF EACH SHIMS WERE R & R IAW SRM 53-00-10.
- [SDR UHLA201506190456](https://openairdocs.org/sdr/UHLA201506190456), Jun 15, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE CARGO DOOR CUTOUT THRESHOLD AT FRAMES 65-68. THE THRESHOLD WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506190455](https://openairdocs.org/sdr/UHLA201506190455), Jun 15, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT THE NUTPLATE HOLES AT FRAMES 59-61. THE OMEGA BEAM WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506190454](https://openairdocs.org/sdr/UHLA201506190454), Jun 15, 2015: SHEAR TIE. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR TIE AT FRAME 67 BETWEEN STRINGERS 6L AND 7L. THE SHEAR TIE AND STIFFNER WERE R & R IAW SRM 53-31-04.
- [SDR UHLA201506190453](https://openairdocs.org/sdr/UHLA201506190453), Jun 15, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND THE THE L SHAPE FRAME 65 AT THE CARGO DOOR STOP. THE DAMAGE WAS REPAIRED IAW SRM 53-31-04.
- [SDR UHLA201506190452](https://openairdocs.org/sdr/UHLA201506190452), Jun 15, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE LOWER HOLE AT THE UPRIGHT STANTION AT FRAME 20 AND THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506190451](https://openairdocs.org/sdr/UHLA201506190451), Jun 15, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE GUSSET CENTER OMEGA AT FRAMES 20, 21, 22, 23. THE CENTER OMEGA BEAM WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201506190450](https://openairdocs.org/sdr/UHLA201506190450), Jun 15, 2015: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO HAVE A CRACK AT THE AFT NUTPLATE BETWEEN FRAMES 60 AND 61. THE BEAM WAS REPAIRED IAW ETD2014-145-05099.
- [SDR UHLA201506190449](https://openairdocs.org/sdr/UHLA201506190449), Jun 15, 2015: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO HAVE CRACKS AT THE FWD AND AFT NUTPLATES AT FRAMES 59, 60, 61. NEW OMEGA BEAM INSTALLED
- [SDR UHLA201506190448](https://openairdocs.org/sdr/UHLA201506190448), Jun 15, 2015: HINGE FITTING. WORN. DURING INSPECTION, THE RUDDER BOTTOM HINGE FITTING BUSHING BORES WERE FOUND TO BE OUT OF LIMITS. THE BOTTOM HINGE FITTING WAS REPLACED IAW SRM 55-40-02.
- [SDR UHLA201506190447](https://openairdocs.org/sdr/UHLA201506190447), Jun 15, 2015: HINGE FITTING. OUT OF LIMITS. DURING INSPECTION, THE RUDDER TOP HINGE FITTING BUSHING BORE'S WERE FOUND TO BE OUT OF LIMITS. THE TOP HINGE FITTING WAS REPLACED IAW SRM 55-40-02.
- [SDR UHLA201506190446](https://openairdocs.org/sdr/UHLA201506190446), Jun 15, 2015: TEE FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE TEE FITTING AT FRAME 65. THE TEE FITTING WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201505210380](https://openairdocs.org/sdr/UHLA201505210380), May 21, 2015: FAN. FAILED. IN FLIGHT, THE CREW NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN. NO SMOKE WAS VISIBLE. THE CREW DECLARED AN EMERGENCY AND MADE A SUCCESSFU
- [SDR CHQA20140624194](https://openairdocs.org/sdr/CHQA20140624194), Jun 24, 2014: TIRE. SEPARATED. CREW REPORTED DURING TAKEOFF THERE WAS A VIBRATION IN THE ACFT. ATC REPORTED THAT THE ACFT HAS LT TIRE DEBRIS ON THE RUNWAY. THE CREW DECLARED AN EMER & RETURNE
- [SDR CHQA20130427137](https://openairdocs.org/sdr/CHQA20130427137), Apr 27, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACKED SHEAR CLIP WAS FOUND AT FRAME 10 UNDER THE RIGHT DIRECT VISION WINDOW. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20130426136](https://openairdocs.org/sdr/CHQA20130426136), Apr 26, 2013: FITTING. DAMAGED. DURING INSPECTION, FRAME 10 WAS FOUND TO BE ELONGATED AND THE HOLES MISALIGNED ON THE UPPER ATTACH SHEAR CLIP. THE SHEAR CLIP WAS REPAIRED IN ACCORDANCE WITH SR
- [SDR CHQA20130424141](https://openairdocs.org/sdr/CHQA20130424141), Apr 24, 2013: FLOOR SUPPORT. DAMAGED. DURING INSPECTION, A MISDRILLED HOLE IN THE OMEGA BEAM SPLICE AT THE CENTER OMEGA BEAM LEFT SIDE WAS REPORTED. THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS 
- [SDR CHQA20130423132](https://openairdocs.org/sdr/CHQA20130423132), Apr 23, 2013: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE INNER SKIN AT THE POTABLE WATER NIPPLE FILL. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007598.
- [SDR CHQA20130422133](https://openairdocs.org/sdr/CHQA20130422133), Apr 22, 2013: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LATERAL L SHAPE AT THE BOTTOM OF FRAME 65. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53
- [SDR CHQA20130420131](https://openairdocs.org/sdr/CHQA20130420131), Apr 20, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RIGHT OMEGA BEAM FROM FRAME 59 TO FRAME 61 WAS FOUND TO BE CORRODED. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007501.
- [SDR CHQA20130419140](https://openairdocs.org/sdr/CHQA20130419140), Apr 19, 2013: REINFORCEMENT. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE STRINGER REINFORCEMENT FRAME 20 STRINGER 3L. THE STRINGER REINFORCEMENT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02
- [SDR CHQA20130419139](https://openairdocs.org/sdr/CHQA20130419139), Apr 19, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE LEFT OMEGA INBOARD FLOOR SUPPORT BETWEEN FRAMES 24 AND 25. THE FLOOR SUPPORT WAS REPLACED IN ACC
- [SDR CHQA20130419138](https://openairdocs.org/sdr/CHQA20130419138), Apr 19, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE CENTER OMEGA LEFT FLOOR SUPPORT BETWEEN FRAMES 24 AND 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WIT
- [SDR CHQA20130419135](https://openairdocs.org/sdr/CHQA20130419135), Apr 19, 2013: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA20130419134](https://openairdocs.org/sdr/CHQA20130419134), Apr 19, 2013: DOUBLER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER AT THE LEFT OMEGA FRAME 20. THE REPAIR DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.
- [SDR CHQA20130419130](https://openairdocs.org/sdr/CHQA20130419130), Apr 19, 2013: DOUBLER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE DOUBLER AT THE POTABLE WATER FILL NIPPLE. THE DOUBLER WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007598.
- [SDR CHQA20130226066](https://openairdocs.org/sdr/CHQA20130226066), Feb 26, 2013: COMPUTER. FAULTY. CREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC
- [SDR CHQA20130226065](https://openairdocs.org/sdr/CHQA20130226065), Feb 26, 2013: DAU. FAULTY. CREW REPORTED THAT THERE WAS ELECTRICAL SMOKE SMELL AND HAZE IN THE COCKPIT IN FLIGHT. THE CREW DIVERTED TO KUNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC
- [SDR CHQA20120831304](https://openairdocs.org/sdr/CHQA20120831304), Aug 31, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CH
- [SDR CHQA20120825300](https://openairdocs.org/sdr/CHQA20120825300), Aug 25, 2012: WIRE. DAMAGED. MAINTENANCE REPORTED THAT THE AFT FLOOR PROXIMITY STRIP WIRING WAS DAMAGED AT THE PROXIMITY STRIP. THE AFT FLOOR PROXIMITY STRIP WAS REPLACED. OPERATIONAL CHECK
- [SDR CHQA201200028](https://openairdocs.org/sdr/CHQA201200028), Jan 27, 2012: CLAMP. BROKEN. CREW REPORTED THAT DURING CLIMB THERE WAS A LOUD RUSHING AIR NOISE IN THE PASSENGER CABIN. THE CREW SELECTED PACK NUMBER 1 OFF AND THE NOISE CLEARED. PACK NUMBE
- [SDR CHQA201100491](https://openairdocs.org/sdr/CHQA201100491), Dec 16, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 2 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 EME
- [SDR CHQA201100490](https://openairdocs.org/sdr/CHQA201100490), Dec 16, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 4 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EME
- [SDR CHQA201100394](https://openairdocs.org/sdr/CHQA201100394), Sep 29, 2011: MODULE. ACTIVATED. CREW REPORTED, LOST THE CABIN ALTITUDE INDICATION IN MANUAL PRESSURIZATION MODE. AUTO-PRESSURIZATION WAS ALREADY ON MEL. THE AIRCRAFT RETURNED TO KPIT AND LANDE
- [SDR CHQA201100049](https://openairdocs.org/sdr/CHQA201100049), Mar 4, 2011: WIRE. BROKEN. DURING INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH NO FUR
- [SDR CHQA201000198](https://openairdocs.org/sdr/CHQA201000198), Oct 9, 2010: WIRE. PULLED. WHILE REMOVING THE AFT CENTER FLOORBOARD, THE AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A WIRE PULLED FROM THE STRIP. THE FLOOR PROXIMITY STRIP AT ROWS 
- [SDR CHQA201000153](https://openairdocs.org/sdr/CHQA201000153), Aug 8, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS INOP WHEN TESTED. MAINTENANCE REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT STRI
- [SDR CHQA201000115](https://openairdocs.org/sdr/CHQA201000115), Jun 5, 2010: PROXIMITY SWITCH. FAULTY. CREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE GEAR WAS CYCLED SEVERAL TIMES BEFORE THE NOSE GEAR DOORS FINALLY CLOSED. THE F
- [SDR CHQA201000111](https://openairdocs.org/sdr/CHQA201000111), Jun 2, 2010: LEVER. FAILED. AFTER TAKEOFF, CREW RETRACTED MLG & AFTER RETRACTION, NLG DOORS REMAINED OPEN. ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND A GROUND AT PIN X2 ON 
- [SDR CHQA201000109](https://openairdocs.org/sdr/CHQA201000109), Jun 1, 2010: CONNECTOR. SHORTED. AFTER TAKEOFF, GEAR SELECTED UP, CREW REPORTED NORMAL RETRACTION & EICAS INDICATIONS, BUT A LOUD NOISE HEARD FROM NLG AREA. ACFT RETURNED TO FIELD & LANDED WITH
- [SDR CHQA201000107](https://openairdocs.org/sdr/CHQA201000107), May 29, 2010: PROXIMITY SENSOR. FAULTY. AFTER TAKEOFF, WHEN THE LANDING GEAR WAS UP AND LOCKED, THE CREW NOTICED A LOUD RUSHING AIR NOISE FROM THE NOSE. THERE WERE NO UNUSUAL INDICATIONS ON EICAS AND 
- [SDR CHQA201000103](https://openairdocs.org/sdr/CHQA201000103), May 27, 2010: UNKNOWN. MALFUNCTIONED. CREW REPORTED THAT AFTER SELECTING THE LANDING GEAR UP, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW VERIFIED WITH TOWER THAT THE NOSE GEAR DOORS WERE 
- [SDR CHQA201000093](https://openairdocs.org/sdr/CHQA201000093), May 4, 2010: CONNECTOR. DAMAGED. DURING INSPECTION A FLOOR PROXIMITY LIGHT STRIP WAS FOUND WITH DAMAGED CONNECTORS. THE FLOOR LIGHT STRIP WAS REPLACED BY MAINTENANCE IAW AMM 33-50-12.
- [SDR CHQA201000082](https://openairdocs.org/sdr/CHQA201000082), Apr 17, 2010: CONTROL LEVER. FAULTY. CREW REPORTED THAT THE AIRCRAFT WOULD NOT ACCELERATE AND A RUMBLE COULD BE HEARD AND FELT. THE CREW INSPECTED THE WINGS DURING FLIGHT AND FOUND THE FLAPS SLIGHT
- [SDR CHQA201000079](https://openairdocs.org/sdr/CHQA201000079), Apr 15, 2010: SOLENOID VALVE. FAULTY. CREW RETURNED TO FIELD DUE TO A RUMBLING NOISE FROM THE NOSE LANDING GEAR AREA AFTER GEAR RETRACTION. THE AIRCRAFT WAS FERRIED TO SDF FOR FURTHER TROUBLESHOOTIN
- [SDR CHQA201000078](https://openairdocs.org/sdr/CHQA201000078), Apr 14, 2010: LANDING GEAR. MALFUNCTIONED. ON DEPARTURE THE CREW REPORTED THAT IT TOOK THE NOSE LANDING GEAR ALMOST 1 MINUTE TO RETRACT AFTER SELECTING THE GEAR UP. A LANDING GEAR DISAGREE MESSAGE WAS AL
- [SDR CHQA201000034](https://openairdocs.org/sdr/CHQA201000034), Feb 11, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND LAMP WITH NO FURTHER
- [SDR CHQA201000033](https://openairdocs.org/sdr/CHQA201000033), Feb 10, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP DURING TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10, OPS

All 63: https://openairdocs.org/deregistered/N294SK-2018-01-11/reports.md

## NTSB investigations (1)

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 MIA03LA127](https://openairdocs.org/ntsb/MIA03LA127), Jun 18, 2003: Embraer EMB-145LR (N294SK), Taylor, FL, no damage. Probable cause: The in-flight encounter with turbulence during normal descent resulting in a serious injury to a passenger. A finding in the investigation was the seatbelt sign had been on for approximately 2…

## 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.

- [Accident 20030618022019A](https://openairdocs.org/incident/20030618022019A), Jun 18, 2003: Emb EMB145LR (N294SK), Orlando, FL. (-23) On June 18, 2003 approximately 1456 EDT, an Embraer Emb-145LR, N294SK operated by chautauqua airlines dba delta connection flight 6355 enroute from…

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