# N272SK: 2000 Embraer EMB-145LR, registration cancelled 2018-09-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 19, 2018 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145306 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 28, 2000 - Certificate issued: April 17, 2018 - Last registry action: September 12, 2018 - Mode S code: A2AF84 - 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/N272SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=272SK - Page: https://openairdocs.org/deregistered/N272SK-2018-09-19 From the FAA registry file of November 5, 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 (51, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201606140329](https://openairdocs.org/sdr/UHLA201606140329), Jun 14, 2016: BRACKET. BENT. MED STEPS WILL NOT DEPLOY. R & R BENT ROLLER BRACKET AND OPS CHECK GOOD IAW 52-13-02. - [SDR UHLA201602260084](https://openairdocs.org/sdr/UHLA201602260084), Feb 26, 2016: STOP. DAMAGED. AIR STAIRS DO NOT DEPLOY. R & R MAIN DOOR STEP FOLD-OUT BACKSTOP IAW AMM 52-13-02. OPS CHECKED GOOD. - [SDR UHLA201602260075](https://openairdocs.org/sdr/UHLA201602260075), Feb 26, 2016: STOP. DAMAGED. AIR START DOES NOT DEPLOY. R & R MAIN DOOR STEP FOLD-OUT BACKSTOP IAW AMM 52-13-02. OPS CHECK GOOD. - [SDR UHLA201512040896](https://openairdocs.org/sdr/UHLA201512040896), Dec 4, 2015: FITTING. CRACKED. LEFT ENGINE LOWER FWD YOKE LINKAGE FITTING CRACKED. R & R LT ENGINE LOWER FWD YOKE LINKAGE FITTING IAW ETD2015-145-112035, REV A. - [SDR UHLA201510060759](https://openairdocs.org/sdr/UHLA201510060759), Oct 6, 2015: ROD. NOT REPORTED. THE MAIN ENTRY DOOR AIRSTAIRS WOULD NOT RETRACT WHEN THE DOOR WAS CLOSED. MAINTENANCE R & R THE DOOR STEP ACTUATING ROD IAW AMM 52-10-03 AND ALL OPS CHECKS WERE - [SDR UHLA201509100696](https://openairdocs.org/sdr/UHLA201509100696), Sep 10, 2015: INVERTER. INOPERATIVE. DURING INSPECTION, THE EMERGENCY EXIT SIGNS OVER THE LT OVERWING EMERGENCY EXIT, FORWARD BULKHEAD, AND SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE R - [SDR UHLA201505040343](https://openairdocs.org/sdr/UHLA201505040343), May 4, 2015: WINDSHIELD. FAULTY. THE CREW REPORTED A BURNING ODOR IN FLIGHT WHEN THE WINDSHIELD 1 HEAT WAS IN OPERATION. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MA - [SDR UHLA201505030339](https://openairdocs.org/sdr/UHLA201505030339), May 3, 2015: UNKNOWN. ODOR. THE CREW REPORTED THAT THEIR WAS A BURNING ODOR IN THE COCKPIT AND CABIN DURING FLIGHT. THE ACFT LANDED UNEVENTFULLY AT ITS INTENDED DESTINATION. MAINTENANCE IN - [SDR UHLA2015011400051](https://openairdocs.org/sdr/UHLA2015011400051), Jan 14, 2015: FRAME. GOUGED. DURING INSPECTION, A GOUGE WAS FOUND ON FRAME 15 BETWEEN STRINGERS 1R AND 2R. THE FRAME REPAIRED IAW SRM 53-00-04, SRM 51-40-02, AND CPM 51-21-04. - [SDR UHLA2015011300054](https://openairdocs.org/sdr/UHLA2015011300054), Jan 13, 2015: FRAME. CRACKED. DURING INSPECTION, FRAME 10 ON THE FIRST OFFICERS SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011300049](https://openairdocs.org/sdr/UHLA2015011300049), Jan 13, 2015: FRAME. CRACKED. DURING INSPECTION, FRAME 10 ON THE CAPTAIN`S SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011200056](https://openairdocs.org/sdr/UHLA2015011200056), Jan 12, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015011200055](https://openairdocs.org/sdr/UHLA2015011200055), Jan 12, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM SILL AT FRAME 24. THE SILL WAS REPAIRED IAW ETD 2015-145-004502. - [SDR UHLA2015011200052](https://openairdocs.org/sdr/UHLA2015011200052), Jan 12, 2015: STEP. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER NUTPLATE FOR THE PASSENGER DOOR LOWER STEP. THE CENTER NUTPLATE STRIP FITTING WAS REPLACED IAW SRM 51-40-02 - [SDR UHLA2015011200050](https://openairdocs.org/sdr/UHLA2015011200050), Jan 12, 2015: FRAME. CRACKED. DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2R. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-00367 - [SDR UHLA201501110053](https://openairdocs.org/sdr/UHLA201501110053), Jan 11, 2015: SKIN. DAMAGED. DURING HEAVY, FOUND A LIGHTNING BURN. A REPAIR DOUBLER WAS INSTALLED AT FRAME 14 AND STRINGER 1R IAW ETD 2014-145-081088. - [SDR CHQA20140925283](https://openairdocs.org/sdr/CHQA20140925283), Sep 27, 2014: ANGLE. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. THE RAM ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140925285](https://openairdocs.org/sdr/CHQA20140925285), Sep 25, 2014: SUPPORT. CORRODED. DURING INSPECTION THE RT RAMP SUPPORT WAS FOUND TO BE CORRODED. THE RT RAMP ANGLE WAS REPLACED IAW SRM 51-40-02 & ETD 2014-145-08-1412. - [SDR CHQA20140925284](https://openairdocs.org/sdr/CHQA20140925284), Sep 25, 2014: PROFILE. CORRODED. DURING INSPECTION THE PROFILE FWD OF THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE PROFILE WAS REPAIRED IAW SRM 53-21-10. - [SDR CHQA20140705206](https://openairdocs.org/sdr/CHQA20140705206), Jul 5, 2014: SWITCH. FAULTY. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VLV FAIL MSG. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED SYS 1 PUSH - [SDR CHQA20140608187](https://openairdocs.org/sdr/CHQA20140608187), Jun 8, 2014: FLAPPER VALVE. BROKEN. CREW REPORTED THAT THE AUTO PRESSURIZATION SYS WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND THE MANUAL PRESSURI - [SDR CHQA20140521152](https://openairdocs.org/sdr/CHQA20140521152), May 21, 2014: BATTERY. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH N - [SDR CHQA20140213053](https://openairdocs.org/sdr/CHQA20140213053), Feb 13, 2014: UNKNOWN. ODOR. CREW REPORTED THAT DURING FLIGHT, PACK 1 HAS AN ODOR WHEN SELECTED ON. INSPECTED THE PACK AREA WITH NO DEFECTS. OPERATIONS CHECKED GOOD WITH NO DEFECTS OR ODORS - [SDR CHQA20131121437](https://openairdocs.org/sdr/CHQA20131121437), Nov 21, 2013: CONTROLLER. ERRATIC. CREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN THE AUTO PRESSURIZATION MODE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE AUTO P - [SDR CHQA20131114410](https://openairdocs.org/sdr/CHQA20131114410), Nov 14, 2013: ICU. FAULTY. CREW REPORTED THAT AFTER TAKEOFF BOTH RADIO MANAGEMENT UNITS SHOWED DASHES IN THE TRANSPONDER AND TCAS FIELDS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT I - [SDR CHQA20131104381](https://openairdocs.org/sdr/CHQA20131104381), Nov 4, 2013: BATTERY. INOPERATIVE. DURING INSPECTION, FORWARD WING TO FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND OPS CHECKED G - [SDR CHQA20131104380](https://openairdocs.org/sdr/CHQA20131104380), Nov 4, 2013: BATTERY. INOPERATIVE. DURING INSPECTION, OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND ALL OPERATIONAL CHECKS WERE G - [SDR CHQA20130724188](https://openairdocs.org/sdr/CHQA20130724188), Jul 24, 2013: WIRE. DAMAGED. MX REPORTED THAT THE MAIN ENTRY DOOR HANDRAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE W737-0034-20. OPS CHECKED GOOD WITH NO FURTHER DEFECTS - [SDR CHQA20130213051](https://openairdocs.org/sdr/CHQA20130213051), Feb 13, 2013: WIRE HARNESS. FAULTY. CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER ROTATION AND REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WI - [SDR CHQA20130127031](https://openairdocs.org/sdr/CHQA20130127031), Jan 27, 2013: CONTROL UNIT. FAULTY. CREW REPORTED THAT ON LANDING THE CAPTAIN'S BRAKES SEEMED TO LOSE PRESSURE FOR APPROXIMATELY ONE SECOND AND THEN WOULD GRAB. THE AIRCRAFT TAXIED TO THE GATE WIT - [SDR CHQA20120929364](https://openairdocs.org/sdr/CHQA20120929364), Sep 29, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND - [SDR CHQA20120919361](https://openairdocs.org/sdr/CHQA20120919361), Sep 19, 2012: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN - [SDR CHQA20120919360](https://openairdocs.org/sdr/CHQA20120919360), Sep 19, 2012: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN - [SDR CHQA20120918362](https://openairdocs.org/sdr/CHQA20120918362), Sep 18, 2012: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK SUPPORT AT FRAME 50 WAS REPLACED IN ACCORDANCE WITH - [SDR CHQA20120609183](https://openairdocs.org/sdr/CHQA20120609183), Jun 8, 2012: BALLAST. FAILED. CREW REPORTED AN ELECTRICAL ODOR FROM THE CEILING LIGHT AT SEAT 1A. REMOVED AND REPLACED CEILING LIGHT BALLAST. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20120218054](https://openairdocs.org/sdr/CHQA20120218054), Feb 18, 2012: SMOKE DETECTOR. FALSE INDICATION. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A LAVATORY SMOKE WARNING MESSAGE. FLIGHT ATTENDANT VERIFIED THAT THERE WAS NO SMOKE OR ODOR IN THE CABIN. DECLA - [SDR CHQA201100395](https://openairdocs.org/sdr/CHQA201100395), Sep 30, 2011: ENGINE. LEAKING. CREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPL - [SDR CHQA201100391](https://openairdocs.org/sdr/CHQA201100391), Sep 28, 2011: UNKNOWN. SMOKE. CREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO KDTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT EL - [SDR CHQA201100182](https://openairdocs.org/sdr/CHQA201100182), May 20, 2011: INVERTER. INOPERATIVE. DURING INSPECTION, THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 5 DC TO AC INV - [SDR CHQA201000145](https://openairdocs.org/sdr/CHQA201000145), Jul 23, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT SEAT 6A WAS INOP. MAINTENANCE REPLACED THE LIGHT STRIP. - [SDR CHQA200900255](https://openairdocs.org/sdr/CHQA200900255), Dec 3, 2009: FIXTURE. INOPERATIVE. DURING INSPECTION, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOP. THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY WAS REPLACED WITH NO FURTHER DE - [SDR CHQA200900154](https://openairdocs.org/sdr/CHQA200900154), Jul 9, 2009: BLEED VALVE. CLOSED. FLIGHT 6030 FROM CMH TO JFK. THE FLIGHT CREW RECEIVED A BLEED 2 VALVE CLOSED MESSAGE DURING FLIGHT. THE CREW CYCLED THE VALVE BUT THE MESSAGE REMAINED. THE AIRC - [SDR CHQA200900103](https://openairdocs.org/sdr/CHQA200900103), Apr 8, 2009: CONNECTOR. UNSECURE. FLIGHT 6033, CVG TO MSY. AFTER TAKE-OFF THE CREW RECEIVED A CABIN SERVICE DOOR WARNING ON EICAS AND RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE DEF - [SDR CHQA200900082](https://openairdocs.org/sdr/CHQA200900082), Mar 14, 2009: WINDSHIELD. CRACKED. FLIGHT 6042, CVG TO JAX - THE FLIGHT CREW REPORTED THAT DURING CLIMB AT FL230 THEY HEARD A POP FROM THE CAPTAIN'S WINDSCREEN AND THE OUTSIDE PANE WAS CRACKED. T - [SDR CHQA200800118](https://openairdocs.org/sdr/CHQA200800118), Jun 19, 2008: CONTACTOR. FAULTY. FLIGHT 6312, CVG TO FWA. WHILE CLIMBING THROUGH 1,000 FT, AN EMERGENCY LIGHTS NOT ARMED WAS DISPLAYED. THE EMERGENCY LIGHTS WERE RESET AND LIGHTS CAME BACK ON A - [SDR CHQA200800048](https://openairdocs.org/sdr/CHQA200800048), Mar 9, 2008: ACTUATOR. OUT OF ADJUST. CMH TO CMH - DURING CLIMB-OUT FROM CMH, THE CREW RECEIVED AN E1 REVERSER DISAGREE MESSAGE ON EICAS. THE CREW LEVELED OFF, FOLLOWED THE APPROPRIATE QRH CHECKLIST - [SDR CHQA200600133](https://openairdocs.org/sdr/CHQA200600133), Oct 8, 2006: BATTERY PACK. DISCHARGED. FOUND OVERWING EMERGENCY LIGHT ON RIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 30-50-04-4. - [SDR CHQA200600129](https://openairdocs.org/sdr/CHQA200600129), Oct 3, 2006: LIGHT. INOPERATIVE. AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT BULB IAW MM 33-50-00. OPS CHECK GOOD. - [SDR CHQA200500160](https://openairdocs.org/sdr/CHQA200500160), Sep 9, 2005: STARTER. SMOKE. ON PUSHBACK & ENG START, NORMAL UNTIL START OF NR 1 ENG, WHEN START/STOP SELECTOR ENGAGED RECEIVED NO INDICATION OF NORMAL START. NO ROTATION, NO OIL PRESSURE, - [SDR CHQA200500100](https://openairdocs.org/sdr/CHQA200500100), May 17, 2005: BATTERY PACK. UNSERVICEABLE. ON INITIAL WALK OUT TO THE AIRCRAFT THE EMERGENCY LIGHTS WERE ALL ON. FOUND THE SWITCH IN THE COCKPIT TO BE IN THE OFF POSITION. INSPECTED AIRCRAFT AND FOUND IT All 51: https://openairdocs.org/deregistered/N272SK-2018-09-19/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 DCA08IA019](https://openairdocs.org/ntsb/DCA08IA019), Dec 17, 2007: Embraer 145 (N272SK), Jamaica, NY, incident, minor damage. Probable cause: the failure of the elevator control rods due to exposure to high winds while the aircraft was parked overnight. Contributing to this incident was the failure of the existing airworthiness directive… ## 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 20071217831309I](https://openairdocs.org/incident/20071217831309I), Dec 17, 2007: Emb EMB145LR (N272SK), New York, NY, Minor damage. (-23) This aircraft sustained high gust winds for a period of twenty hours prior to takeoff while parked with gust locks reported to be engaged while ron at… --- 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.