# N279SK: 2001 Embraer EMB-145LR, registration cancelled 2019-10-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 10, 2019 - Exported to: Nigeria - 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: 145379 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 31, 2001 - Certificate issued: May 14, 2018 - Last registry action: September 12, 2018 - Mode S code: A2C985 - 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/N279SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=279SK - Page: https://openairdocs.org/deregistered/N279SK-2019-10-10 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 (53, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140323090](https://openairdocs.org/sdr/CHQA20140323090), Mar 23, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH N - [SDR CHQA20140201036](https://openairdocs.org/sdr/CHQA20140201036), Feb 1, 2014: TIRE. SEPARATED. CREW REPORTED THAT NY CENTER INFORMED THEM OF A POSSIBLE TIRE SEPARATION ON TAKEOFF. THE CREW DIVERTED TO KCMH & DID A FLY-BY ON THE CONTROL TOWER. THE TOWER CO - [SDR CHQA20140117017](https://openairdocs.org/sdr/CHQA20140117017), Jan 17, 2014: SIGN. INOPERATIVE. DURING INSPECTION, THE FWD CABIN EMERGENCY LIGHTED SIGN WAS FOUND TO BE INOPERATIVE. REPLACED THE SIGN, OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20131127441](https://openairdocs.org/sdr/CHQA20131127441), Nov 27, 2013: FITTING. CORRODED. CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 66 AT STRINGER 6L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130709265](https://openairdocs.org/sdr/CHQA20130709265), Jul 9, 2013: WIRE. BROKEN. DURING INSPECTION, EMERGENCY LIGHT AT ROW 7 FOUND TO HAVE A BROKEN WIRE. WIRE REPAIRED. OPS CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130613203](https://openairdocs.org/sdr/CHQA20130613203), Jun 13, 2013: LIGHT. INOPERATIVE. DURING INSPECTION, CREW REPORTED THAT THE SECOND EMERGENCY LIGHTING FLOOR STRIP WAS FOUND INOPERATIVE. EMERGENCY LIGHT REPLACED. OPS CHECKED GOOD. - [SDR CHQA20130501142](https://openairdocs.org/sdr/CHQA20130501142), May 1, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS - [SDR CHQA20121203468](https://openairdocs.org/sdr/CHQA20121203468), Dec 3, 2012: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 20L AND 21L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121130462](https://openairdocs.org/sdr/CHQA20121130462), Nov 30, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 53 THROUGH FRAME 58. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06 - [SDR CHQA20121129467](https://openairdocs.org/sdr/CHQA20121129467), Nov 29, 2012: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 59. THE LEFT OMEGA BEAM GUSSET AT FRAME 59 WAS REPLACED IN ACCORDANCE WITH 51-40-02. - [SDR CHQA20121129466](https://openairdocs.org/sdr/CHQA20121129466), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 30 THROUGH FRAME 36. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06. - [SDR CHQA20121129465](https://openairdocs.org/sdr/CHQA20121129465), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACORDANCE WITH AMM 53-01-06. - [SDR CHQA20121129464](https://openairdocs.org/sdr/CHQA20121129464), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 36 THROUGH FRAME 45. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06. - [SDR CHQA20121129463](https://openairdocs.org/sdr/CHQA20121129463), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 42. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06. - [SDR CHQA20121129461](https://openairdocs.org/sdr/CHQA20121129461), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 23 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-0 - [SDR CHQA20121129460](https://openairdocs.org/sdr/CHQA20121129460), Nov 29, 2012: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-0 - [SDR CHQA20121030396](https://openairdocs.org/sdr/CHQA20121030396), Oct 30, 2012: THERMOSTAT. FAULTY. CREW REPORTED THAT UPON TAKEOFF, RECEIVED A BLEED 1 OVERHEAT MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR C - [SDR CHQA20120628201](https://openairdocs.org/sdr/CHQA20120628201), Jun 28, 2012: O-RING. LEAKING. CREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O-RING AT JOINT 11. OPS AND LEAK CHECKED GOO - [SDR CHQA20120609186](https://openairdocs.org/sdr/CHQA20120609186), Jun 9, 2012: CONTROL VALVE. MALFUNCTIONED. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABI - [SDR CHQA20120609185](https://openairdocs.org/sdr/CHQA20120609185), Jun 9, 2012: SLEEVE. FAILED. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABI - [SDR CHQA20120609184](https://openairdocs.org/sdr/CHQA20120609184), Jun 9, 2012: FLAPPER VALVE. BROKEN. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABI - [SDR CHQA20120322088](https://openairdocs.org/sdr/CHQA20120322088), Mar 22, 2012: CONTROL UNIT. FAULTY. CREW REPORTED THAT AFTER LANDING, THE CAPTAIN'S LEFT BRAKE FAILED AT APPROXIMATELY 80 KNOTS. THE BRAKES BEGAN WORKING AGAIN WHEN THE AIRCRAFT SLOWED TO 20 KNOTS - [SDR CHQA201100494](https://openairdocs.org/sdr/CHQA201100494), Dec 21, 2011: TRANSDUCER. FAULTY. CREW REPORTED THAT DURING LANDING ROLLOUT, THE BRAKES FAILED AT 80 KNOTS. THE CREW SLOWED THE AIRCRAFT USING THE EMERGENCY BRAKE. THE BRAKE SYSTEM BEGAN WORKING - [SDR CHQA201100370](https://openairdocs.org/sdr/CHQA201100370), Aug 31, 2011: UNKNOWN. MALFUNCTIONED. CREW REPORTED THAT DURING DESCENT, FUEL TANK TWO'S QUANTITY INDICATIONS WERE DECREASING FUEL QUANTITY INDICATIONS WENT FROM NORMAL TO AMBER, THEN RED, THEN DASH - [SDR CHQA201100156](https://openairdocs.org/sdr/CHQA201100156), Apr 30, 2011: CONTROLLER. INOPERATIVE. CREW REPORTED THAT ON CLIMBOUT AUTO PRESSURIZATION FAILED AND ALL INDICATIONS BLANKED OUT. THEY SWITCHED TO MANUAL MODE BUT STILL WOULD NOT PRESSURIZE. THE AIRC - [SDR CHQA201100108](https://openairdocs.org/sdr/CHQA201100108), Mar 16, 2011: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE OMEGA BEAM BETWEEN FRAME 19 AND 25. MAINTENANCE REPLACED THE FLOOR STRUCTU - [SDR CHQA201100107](https://openairdocs.org/sdr/CHQA201100107), Mar 15, 2011: ANGLE. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD SIDE ANGLE. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD - [SDR CHQA201100118](https://openairdocs.org/sdr/CHQA201100118), Mar 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02. - [SDR CHQA201100117](https://openairdocs.org/sdr/CHQA201100117), Mar 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02. - [SDR CHQA201100116](https://openairdocs.org/sdr/CHQA201100116), Mar 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02. - [SDR CHQA201100115](https://openairdocs.org/sdr/CHQA201100115), Mar 11, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02. - [SDR CHQA201100106](https://openairdocs.org/sdr/CHQA201100106), Mar 11, 2011: SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I ANGLE MIDDLE SUPPORT. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER - [SDR CHQA201100105](https://openairdocs.org/sdr/CHQA201100105), Mar 11, 2011: RIB. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I AFT GALLEY RIB. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSEL - [SDR CHQA201100104](https://openairdocs.org/sdr/CHQA201100104), Mar 11, 2011: STRUCTURE. CORRODED. DURING INSPECTION THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I PASSENGER DOOR U SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CE - [SDR CHQA201100103](https://openairdocs.org/sdr/CHQA201100103), Mar 11, 2011: FLOOR SUPPORT. CORRODED. DURING INSPECTION THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM AFT ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE LEFT - [SDR CHQA201100102](https://openairdocs.org/sdr/CHQA201100102), Mar 11, 2011: BEAM. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM IAW SRM - [SDR CHQA201100101](https://openairdocs.org/sdr/CHQA201100101), Mar 11, 2011: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR ON THE LEFT OMEGA BEAM FLANGE AT FRAME 20. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE AT FRAME - [SDR CHQA201100017](https://openairdocs.org/sdr/CHQA201100017), Jan 19, 2011: RECEPTACLE. INOPERATIVE. DURING INSPECTION, THE RIGHT LOWER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT LOWER EMERGENCY LIGHT RECEPTACLE WITH NO FURTHER - [SDR CHQA201000073](https://openairdocs.org/sdr/CHQA201000073), Apr 8, 2010: INVERTER. DEFECTIVE. DURING INSPECTION THE LAST TWO ROWS OF EMERGENCY FLOOR LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE FOUND MULTIPLE FUSES IN BATTERY NR 4 BLOWN AND INVERTER NR 6 P - [SDR CHQA201000049](https://openairdocs.org/sdr/CHQA201000049), Feb 24, 2010: TRUNNION. CRACKED. DURING THE INSPECTION OF THE AFT UPPER TRUNNION ON THE RIGHT MAIN LANDING GEAR, A 20MM CRACK WAS FOUND ON THE TRUNNION FITTING ON THE FORWARD OUTBOARD FACE AND - [SDR CHQA201000005](https://openairdocs.org/sdr/CHQA201000005), Jan 17, 2010: UNKNOWN. MALFUNCTIONED. DURING CLIMBOUT OF KCLE THE CREW NOTICED THE CABIN ALTITUDE INDICATOR WAS DISPLAYING AMBER DASHES. THE AUTO PRESSURIZATION SYSTEM WAS ALREADY DEFERRED AND THE P - [SDR CHQA200900191](https://openairdocs.org/sdr/CHQA200900191), Sep 1, 2009: LIGHT. OUT OF POSITION. DURING THE WALK AROUND INSPECTION THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND TO BE UPSIDE DOWN. MAINTENANCE REPOSITIONED THE LIGHT TO THE CORRECT ORIENTA - [SDR CHQA200900151](https://openairdocs.org/sdr/CHQA200900151), Jul 3, 2009: PRESSURE SWITCH. FAULTY. DURING CLIMB OUT, AT APPROX 8,000FT, THE CREW RECEIVED AN OXY LO PRESS EICAS MESSAGE. THE CREW O2 INDICATED ZERO PSI ON THE MFD. THE ACFT LEVELED AT 10,000 FT A - [SDR CHQA200800176](https://openairdocs.org/sdr/CHQA200800176), Sep 8, 2008: LIGHT. INOPERATIVE. DURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. THE BULB FOR THE RT OVER WING EMERGENCY LIGHT WAS REPLACED IAW EMB 145 AMM 33-50-07-4. - [SDR CHQA200800172](https://openairdocs.org/sdr/CHQA200800172), Sep 1, 2008: STRUT. UNDERSERVICED. FLIGHT 3080, SDF TO LGA. WHEN THE CREW SELECTED THE LANDING GEAR DOWN THEY HEARD A THUD FROM THE NOSE AREA AND RECEIVED LG AIR/GND FAIL AND T/R DISAGREE MESSAGE - [SDR CHQA200700079](https://openairdocs.org/sdr/CHQA200700079), Nov 20, 2007: CONTROL PANEL. FAULTY. GSP TO LGA - UPON REACHING 10,000 FT DURING DESCENT, THE APU WAS STARTED DUE TO AN MEL'D NR 3 GENERATOR. SHORTLY AFTER STARTING APU, CREW RECEIVED A FIRE WARNIN - [SDR CHQA200600107](https://openairdocs.org/sdr/CHQA200600107), Aug 23, 2006: TRIM SYSTEM. MALFUNCTIONED. WHILE CLIMBING THROUGH 14000 FEET UP TO 17000 FEET, HAD RUDDER TRIM RUN AWAY TO THE LT. APPLIED THE APPROPRIATE MEMORY ITEMS AND CHECK LIST, DECLARED AN EMERGEN - [SDR CHQA200500129](https://openairdocs.org/sdr/CHQA200500129), Jul 20, 2005: BULB. BURNED OUT. REAR CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-08. OPS CHECK GOOD IAW EMB 145 J/C E33-50-0 - [SDR CHQA200500054](https://openairdocs.org/sdr/CHQA200500054), Mar 13, 2005: SMOKE. DETECTED. FLIGHT 3039 BOS-MYR - DURING INTIAL CLIMB A LAV SMOKE INDICATION APPEARED ON EICAS. THE FLIGHT ATTENDANT REPORTED THERE WAS NO EVIDENCE OF ODOR, SMOKE, OR FIRE - [SDR AE0R200400002](https://openairdocs.org/sdr/AE0R200400002), Dec 21, 2004: TURBINE BLADES. FRACTURED. ENGINE S/N CAE311220 WAS DELIVERED TO SHOP FOR REPAIR 11/03/04 DUE TO IN-FLIGHT SHUTDOWN. DURING DISASSEMBLY, DAMAGE WAS NOTED TO THE TURBINE. ONE 1ST STAGE TUR All 53: https://openairdocs.org/deregistered/N279SK-2019-10-10/reports.md ## 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 20061202029669I](https://openairdocs.org/incident/20061202029669I), Dec 2, 2006: Emb EMB145LR (N279SK), Buffalo, NY, Minor damage. (-23) This aircraft experienced extremely high gusty winds while parked on the ramp at buf. The gust lock either failed or was not engaged on this aircraft.… - [Incident 20041030027789I](https://openairdocs.org/incident/20041030027789I), Oct 30, 2004: Emb EMB145LR (N279SK), Louisville, KY, Minor damage. (-23) Chautauqua airlines flight 3103 an EMB145LR, N279SK enroute from new york, NY (lga) to Louisville, KY (sdf), declared an emergency due to an engine… --- 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.