# N274SK: 2000 Embraer EMB-145LR, registration cancelled 2020-02-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 13, 2020 - 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: 145344 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 3, 2000 - Certificate issued: April 16, 2018 - Last registry action: September 12, 2018 - Mode S code: A2B6F2 - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bungay Norfolk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N274SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=274SK - Page: https://openairdocs.org/deregistered/N274SK-2020-02-13 From the FAA registry file of November 7, 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201607170368](https://openairdocs.org/sdr/UHLA201607170368), Jul 17, 2016: SWITCH. OUT OF ADJUST. MAIN ENTRY DOOR SHOWS OPEN ON MFD WHEN DOOR IS CLOSED. ADJUSTED MAIN ENTRY DOOR SWITCHES IAW AMM 52-73-00. OPS CHECKED GOOD. - [SDR UHLA201607120361](https://openairdocs.org/sdr/UHLA201607120361), Jul 12, 2016: SWITCH. OUT OF ADJUST. MAIN ENTRY DOOR SHOWS OPEN WHEN CLOSED. ADJUSTED THE SWITCHES IAW AMM 52-12-09. OPS CHECKED GOOD. - [SDR UHLA201606200331](https://openairdocs.org/sdr/UHLA201606200331), Jun 20, 2016: SWITCH. DIRTY. MED INDICATES OPEN WHEN VERIFIED CLOSED. CLEANED AND LUBED MED INDICATION MICROSWITCHES AS REQUIRED. PERFORMED OPS CHECK IAW 52-73-00 ON MED WARNING SYSTEM, OPS - [SDR UHLA201606140326](https://openairdocs.org/sdr/UHLA201606140326), Jun 14, 2016: CLAMP. LOOSE. BLEED 1 LEAK AFTER TAKEOFF. AFTER RUNNING QRH, MESSAGE WENT AWAY. ON AFTER LANDING WHILE USING THE APU BLEED, BLEED 1 LEAK MESSAGE RETURNED. DECLARED EMERGENCY, - [SDR UHLA201606120324](https://openairdocs.org/sdr/UHLA201606120324), Jun 12, 2016: SWITCH. LACK OF LUBE. MED INDICATES OPEN WHEN VERIFIED CLOSED. CHECKED HISTORY AND INSPECTED THE DOOR WIRING. LUBRICATED THE SWITCH LOCKING MECHANISM, CHECKED THE SWITCHES FOR PROPER - [SDR UHLA201504290351](https://openairdocs.org/sdr/UHLA201504290351), Apr 29, 2015: SKIN. CRACKED. DURING INSPECTION, THE SKIN AT LT FRAME 75, BETWEEN STRINGERS 1L AND 2L WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW ETD2015-145-040536. - [SDR UHLA201504290350](https://openairdocs.org/sdr/UHLA201504290350), Apr 29, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT OTBD SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA201504280358](https://openairdocs.org/sdr/UHLA201504280358), Apr 28, 2015: STRUCTURE. CRACKED. DURING INSPECTION, THE RT WING ZONE 651, RIB 21 WAS FOUND TO BE CRACKED AT YA 8598.0. THE AREA WAS REPAIRED IAW ETD 2015-145-041608. - [SDR UHLA201504210359](https://openairdocs.org/sdr/UHLA201504210359), Apr 21, 2015: RIB. CRACKED. DURING INSPECTION, THE RT WING ZONE 651, RIB 22 WAS FOUND TO BE CRACKED AT YA 9031.0. THE AREA WAS REPAIRED IAW ETD 2015-145-041608. - [SDR UHLA201504200349](https://openairdocs.org/sdr/UHLA201504200349), Apr 20, 2015: FRAME. BENT. DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT AT STRINGERS 16R. THE FRAME WAS REPLACED IAW SRM 53-00-04. - [SDR UHLA201504190352](https://openairdocs.org/sdr/UHLA201504190352), Apr 19, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA201504180357](https://openairdocs.org/sdr/UHLA201504180357), Apr 18, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT THE RIVET AROUND FRAME 78 BETWEEN STRINGERS 5R AND 6R. THE RIVET WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-037397. - [SDR UHLA201504180356](https://openairdocs.org/sdr/UHLA201504180356), Apr 18, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT THE RIVET AROUND FRAME 77 BETWEEN STRINGER 8R AND 9R. THE RIVET WAS REPAIRED IAW ETD 2015-145-037397. - [SDR UHLA201504180355](https://openairdocs.org/sdr/UHLA201504180355), Apr 18, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT THE RIVET AROUND FRAME 79 BETWEEN STRINGER 6L. THE RIVET WAS REPAIRED IAW ETD 2015-145-037397. - [SDR UHLA201504180354](https://openairdocs.org/sdr/UHLA201504180354), Apr 18, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT THE RIVET AROUND FRAME 77 BETWEEN STRINGERS 7L AND 8L. THE RIVET WAS REPAIRED IAW ETD 2015-145-037397. - [SDR CHQA20141103312](https://openairdocs.org/sdr/CHQA20141103312), Nov 3, 2014: LIGHT. INOPERATIVE. DURING INSPECTION THE FLOOR EMER PROXIMITY LIGHT STRIP AT ROW 7 WAS FOUND TO BE INOPERATIVE. REPLACED THE EMER LIGHT FLOOR STRIP AT ROW 7. OPERATIONAL CHECKS GO - [SDR CHQA20140722235](https://openairdocs.org/sdr/CHQA20140722235), Jul 22, 2014: TIRE. SEPARATED. THE LT INBD TIRE SEPARATED ON TAKEOFF. DECLARED AN EMER & DIVERTED THE ACFT FROM ITS INTENDED FLIGHT PLAN. THE ACFT LANDED WITHOUT FURTHER INCIDENT. PERFORMED T - [SDR CHQA20140701204](https://openairdocs.org/sdr/CHQA20140701204), Jul 1, 2014: LAMP SOCKET. DEFECTIVE. CREW REPORTED THAT THE BALLAST LIGHT BULB ABOVE ROW 6A BURNT OUT DURING FLIGHT & CAUSED A MINOR HAZE IN THE CABIN. THE ACFT LANDED AT ITS INTENDED DESTINATION W - [SDR CHQA20140701203](https://openairdocs.org/sdr/CHQA20140701203), Jul 1, 2014: LIGHT. BURNED OUT. CREW REPORTED THAT THE BALLAST LIGHT BULB ABOVE ROW 6A BURNT OUT DURING FLIGHT & CAUSED A MINOR HAZE IN THE CABIN. THE ACFT LANDED AT ITS INTENDED DESTINATION W - [SDR CHQA20140308076](https://openairdocs.org/sdr/CHQA20140308076), Mar 8, 2014: RELAY. FAILED. CREW REPORTED THAT THEY RECEIVED A TAT 2 HEAT INOPERATIVE MSG DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED CURRENT SENSOR RE - [SDR CHQA20131223466](https://openairdocs.org/sdr/CHQA20131223466), Dec 23, 2013: ANTI-ICE VALVE. INOPERATIVE. IN FLIGHT, CREW REPORTED RECEIVING AN ENG 1 ANTI-ICE VLV FAIL MESSAGE. WHILE FOLLOWING PROCEDURES, THE CREW DECIDED TO RETURN TO THE DEPARTURE FIELD FOR AN UNEV - [SDR CHQA20131212446](https://openairdocs.org/sdr/CHQA20131212446), Dec 12, 2013: LIGHT. INOPERATIVE. THE LT FWD EMERGENCY LIGHT PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. THE LT FWD EMERGENCY PROXIMITY STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO - [SDR CHQA20130907339](https://openairdocs.org/sdr/CHQA20130907339), Sep 7, 2013: WIRE. BROKEN. DURING INSPECTION, THE NR 3 EMERGENCY LIGHT WAS FOUND TO HAVE A BROKEN WIRE. MX REPAIRED WIRE AND OPS CHECKED GOOD. - [SDR CHQA20130407119](https://openairdocs.org/sdr/CHQA20130407119), Apr 7, 2013: CROSSBEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND UNDER THE CARBON FLOOR CROSS BEAM ON THE LEFT OF FRAME 18. THE CARBON FLOOR CROSS BEAM LEFT SIDE WAS REPAIRED IN ACCORDAN - [SDR CHQA20130405121](https://openairdocs.org/sdr/CHQA20130405121), Apr 5, 2013: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON FRAME 72 BETWEEN STRINGERS 11R AND 12R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130403120](https://openairdocs.org/sdr/CHQA20130403120), Apr 3, 2013: FRAME. CRACKED. DURING INSPECTION, A DENT WAS FOUND ON FRAME 72 ON THE LEFT SIDE ABOVE STRINGER 14L. A HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND THE FRAME TO BE CRACKED. THE - [SDR CHQA20130402123](https://openairdocs.org/sdr/CHQA20130402123), Apr 2, 2013: RAIL. CORRODED. DURING INSPECTION, THE PASSENGER DOOR STEP RAILS WERE FOUND TO BE CORRODED. THE PASSENGER DOOR STEP RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130402122](https://openairdocs.org/sdr/CHQA20130402122), Apr 2, 2013: RAIL. CORRODED. DURING INSPECTION, THE PASSENGER DOOR STEP RAILS WERE FOUND TO BE CORRODED. THE PASSENGER DOOR STEP RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130401118](https://openairdocs.org/sdr/CHQA20130401118), Apr 1, 2013: FRAME. CHAFED. DURING INSPECTION, A CHAFE WAS FOUND AT FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04. - [SDR CHQA20130109009](https://openairdocs.org/sdr/CHQA20130109009), Jan 9, 2013: O-RING. LEAKING. CREW REPORTED THAT THEY RECEIVED A BLEED 1 LEAK MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RINGS - [SDR CHQA20121023387](https://openairdocs.org/sdr/CHQA20121023387), Oct 23, 2012: O-RING. LEAKING. CREW REPORTED THAT DURING FLIGHT THEY RECEVED A BLEED 1 LEAK MESSAGE ON THE EICAS. THE FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. THE ENGINE GROUND STA - [SDR CHQA20121023386](https://openairdocs.org/sdr/CHQA20121023386), Oct 23, 2012: COUPLING. LEAKING. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 LEAK MESSAGE ON THE EICAS. THE FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. THE ENGINE GROUND ST - [SDR CHQA20120907308](https://openairdocs.org/sdr/CHQA20120907308), Sep 7, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY FLOOR LIGHTING STRIP AT THE OVERWING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTING STRIP. - [SDR CHQA20120510147](https://openairdocs.org/sdr/CHQA20120510147), May 10, 2012: HYDRAULIC SYSTEM. LOW. CREW REPORTED THAT THEY RECEIVED A HYDRAULIC 1 LOW QUANTITY MESSAGE IN FLIGHT. AFTER RECEIVING THE MESSAGE THEY RECEIVED A HYDRAULIC SYSTEM 1 FAIL MESSAGE. THE - [SDR CHQA201100421](https://openairdocs.org/sdr/CHQA201100421), Oct 29, 2011: CONTROL UNIT. INOPERATIVE. CREW REPORTED THAT DURING DESCENT RECEIVED AN AUTOPILOT FAIL MESSAGE. WHILE REFERENCING THE QUICK REFERENCE HANDBOOK, CREW THEN RECEIVED PITCH TRIM MAIN AND PIT - [SDR CHQA201100400](https://openairdocs.org/sdr/CHQA201100400), Oct 7, 2011: CONTROL PANEL. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHTS WOULD NOT TURN ON FROM THE FLIGHT ATTENDANT CONTROL PANEL. MAINTENANCE REPLACED THE FLIGHT ATTENDANT CONTROL PANEL ASSEM - [SDR CHQA201100380](https://openairdocs.org/sdr/CHQA201100380), Sep 22, 2011: WIRE. DAMAGED. CREW REPORTED THAT THE REAR EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE ON THE FLOOR LIGHT STRIP. THE WIRE WAS REPAIRED. OPERATIONAL - [SDR CHQA201100058](https://openairdocs.org/sdr/CHQA201100058), Mar 11, 2011: UNKNOWN. ODOR. CREW REPORTED THAT ON DESCENT, AFTER ANTI-ICE SYSTEM WAS ACTIVATED, THAT THERE WAS A BURNING SMELL IN THE COCKPIT. ON CALL MAINTENANCE INSPECTED THE ELECTRICAL - [SDR CHQA201100029](https://openairdocs.org/sdr/CHQA201100029), Feb 3, 2011: ALTIMETER. STICKS. CREW RETURNED TO FIELD FOR AN ERRATIC STANDBY ALTITUDE INDICATOR. THE STANDBY ALTIMETER WOULD STICK AT 900FT EVERY TIME AROUND. THE AIRCRAFT LANDED WITHOUT INCI - [SDR CHQA200900244](https://openairdocs.org/sdr/CHQA200900244), Nov 11, 2009: ACCUMULATOR. LEAKING. CREW REPORTED A HYDRAULIC SYSTEM LOW QUANTITY EICAS MESSAGE AFTER GEAR RETRACTION. THE CREW CONTINUED THE FLIGHT AND DURING CRUISE THE SYSTEM 1 QUANTITY DROPPED - [SDR CHQA200900224](https://openairdocs.org/sdr/CHQA200900224), Oct 22, 2009: LIGHT. INOPERATIVE. DURING INSPECTION THE NR 4 EMERGENCY FLOOR LIGHT STRIP WAS INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY FLOOR LIGHT STRIP IAW EMB-145 AMM 33-50-12. THE EMERGEN - [SDR CHQA200600108](https://openairdocs.org/sdr/CHQA200600108), Aug 26, 2006: SMOKE. DETECTED. FLIGHT 6334 - ATL-LEX - SMOKE IN CABIN DURING TAKEOFF CLIMB JUST AFTER ROTATION. FLIGHT ATTENDANT OBSERVED SMOKE IN CABIN AND CREW NOTED WHAT THEY THOUGHT TO BE - [SDR CHQA200600050](https://openairdocs.org/sdr/CHQA200600050), Apr 20, 2006: BULB. BURNED OUT. CEILING CABIN EMERGENCY LIGHTS AT SEATS 17 ARE INOPERATIVE. REMOVED AND REPLACED THE CEILING AFT EMERGENCY LIGHT BULBS AT SEATS 12 AND 17 IAW EMB 145 MM 33-50-0 ## 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 20040919025229I](https://openairdocs.org/incident/20040919025229I), Sep 19, 2004: Emb EMB145LR (N274SK), Madison, WI. (-23) Flight crew reported that enroute from msp to cvg passing through flight level 240, noticed smell of burned rubber/oil followed shortly thereafter with… - [Incident 20020307008449I](https://openairdocs.org/incident/20020307008449I), Mar 7, 2002: Emb EMB145LR (N274SK), Lincoln, NE. (-23) N274SK operated by chautauqua airlines as American airlines flight 5787 departed Lincoln, NE enroute to st. louis, MO, and returned to Lincoln due to a… --- 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.