# N290SK: 2001 Embraer EMB-145LR, registration cancelled 2018-11-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 21, 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: 145474 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 27, 2001 - Certificate issued: May 14, 2018 - Last registry action: September 12, 2018 - Mode S code: A2F714 - 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/N290SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=290SK - Page: https://openairdocs.org/deregistered/N290SK-2018-11-21 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 (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201602120059](https://openairdocs.org/sdr/UHLA201602120059), Feb 12, 2016: HAND RAIL. MALFUNCTIONED. PAX DOOR HANDRAILS DON'T STOW WITH DOOR CLOSED. CLEANED HANDRAIL ASSY, REPLACED ASSIST SPRINGS, OPS CHECKED GOOD. - [SDR UHLA2015011400013](https://openairdocs.org/sdr/UHLA2015011400013), Jan 14, 2015: CABIN PRESSURE. MALFUNCTIONED. THE CREW REPORTED THAT THE CABIN ALTITUDE INDICATION WAS LOST ON CLIMB OUT WHILE THE AUTO PRESSURIZATION SYSTEM WAS DEFERRED. THE AIRCRAFT RETURNED TO FIELD AND - [SDR CHQA20141119337](https://openairdocs.org/sdr/CHQA20141119337), Nov 19, 2014: ELEVATOR. CRACKED. DURING INSPECTION, THE LT ELEVATOR WAS FOUND TO BE CRACKED. THE ELEVATOR WAS REPAIRED IAW ETD 2014-145-097861. - [SDR CHQA20141119334](https://openairdocs.org/sdr/CHQA20141119334), Nov 19, 2014: STRUCTURE. DENTED. DURING INSPECTION, A DENT WAS FOUND BETWEEN FRAME 19 & 20 & STRINGERS 19R & 20R. THE DENT WAS REPAIRED IAW SRM 53-21-01. - [SDR CHQA20141115335](https://openairdocs.org/sdr/CHQA20141115335), Nov 15, 2014: ANGLE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE ANGLE BRACKET IN THE RT WHEEL AREA AFT SIDE. THE PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141114341](https://openairdocs.org/sdr/CHQA20141114341), Nov 14, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59 & 61. THE BEAM WAS REPAIRED IAW ETD 2014-145-096615. - [SDR CHQA20141114339](https://openairdocs.org/sdr/CHQA20141114339), Nov 14, 2014: SKIN. CRACKED. DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BELOW STRINGER 2L. THE STRINGER WAS REPAIRED IAW ETD 2014-145-096626. - [SDR CHQA20141114338](https://openairdocs.org/sdr/CHQA20141114338), Nov 14, 2014: SKIN. CRACKED. DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 ABOVE STRINGER 2L. THE STRINGER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141114332](https://openairdocs.org/sdr/CHQA20141114332), Nov 14, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAMES 20 & 22. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141113340](https://openairdocs.org/sdr/CHQA20141113340), Nov 13, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 53. THE BEAM WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20141113336](https://openairdocs.org/sdr/CHQA20141113336), Nov 13, 2014: FLOORBEAM. CORRODED. DURING INSPECTION, THE LT FLOORBEAM WAS FOUND TO BE CORRODED ON A PREVIOUS REPAIR AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 53-00-10. - [SDR CHQA20141113333](https://openairdocs.org/sdr/CHQA20141113333), Nov 13, 2014: DOOR SILL. CORRODED. DURING INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140909248](https://openairdocs.org/sdr/CHQA20140909248), Sep 9, 2014: SWITCH. INOPERATIVE. DURING INSPECTION THE FLIGHT ATTENDANT EMER LIGHT SWITCH WAS FOUND TO BE INOPERATIVE. REPLACED THE FLIGHT ATTENDANT CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD - [SDR CHQA20140601178](https://openairdocs.org/sdr/CHQA20140601178), Jun 1, 2014: BATTERY. DISCHARGED. DURING INSPECTION, THE NR 4 EMER LIGHT BATTERY WAS REPORTED TO BE INOPERATIVE. MX REPLACED THE NR 4 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FUR - [SDR CHQA20140601177](https://openairdocs.org/sdr/CHQA20140601177), Jun 1, 2014: LIGHT. DAMAGED. DURING INSPECTION, THE RT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE DAMAGED. MX REPLACED THE RT OVERWING EMERGENCY LIGHT HOUSING ASSEMBLY. OPS CHECKED GOOD W - [SDR CHQA20140106003](https://openairdocs.org/sdr/CHQA20140106003), Jan 6, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BULB & ALL OPERATIONS CHECKED GOOD. - [SDR CHQA20140105002](https://openairdocs.org/sdr/CHQA20140105002), Jan 5, 2014: ANTI-ICE VALVE. FAULTY. CREW REPORTED THAT DURING CRUISE FLIGHT, IN ICING CONDITIONS, THEY RECEIVED A WING ANTI-ICE FAIL MESSAGE. THE CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. R - [SDR CHQA20131123428](https://openairdocs.org/sdr/CHQA20131123428), Nov 23, 2013: BATTERY. DISCHARGED. MULTIPLE EMERGENCY FLOOR STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NUMBER TWO EMERGENCY BATTERY & ALL OPERATIONS CHECKED GOOD. - [SDR CHQA20131002365](https://openairdocs.org/sdr/CHQA20131002365), Oct 2, 2013: FRAME. DAMAGED. DURING INSPECTION, A DAMAGED HOLE IN FRAME 26 BETWEEN STRINGERS 15R AND 16R WAS FOUND. THE DAMAGE WAS REPAIRED IAW ETD 2013-145-045443. - [SDR CHQA20131001366](https://openairdocs.org/sdr/CHQA20131001366), Oct 1, 2013: SHEAR TIE. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 26 BETWEEN STRINGERS 15 AND 16R. THE SHEAR TIE WAS REPLACED IAW ETD 2013-145-04543. - [SDR CHQA20131001364](https://openairdocs.org/sdr/CHQA20131001364), Oct 1, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER AT THE LT OMEGA FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10. - [SDR CHQA20131001363](https://openairdocs.org/sdr/CHQA20131001363), Oct 1, 2013: FRAME. BENT. DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN STRINGERS 15L AND 16L. THE FRAME WAS REPAIRED IAW ETD 2013-145-045154, REV B. - [SDR CHQA20130226064](https://openairdocs.org/sdr/CHQA20130226064), Feb 26, 2013: CONTROL UNIT. FAULTY. CREW REPORTED THAT ON LANDING, WITH THE BRAKES FULLY DEPRESSED, THE BRAKING WAS POOR BELOW 80 KNOTS. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENAN - [SDR CHQA20121215476](https://openairdocs.org/sdr/CHQA20121215476), Dec 15, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. THE FLOOR PROXIMITY LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FUR - [SDR CHQA20120703223](https://openairdocs.org/sdr/CHQA20120703223), Jul 3, 2012: SKIN. DAMAGED. DURING INSPECTION, THREE CREASES WERE FOUND ON CENTER FUSELAGE, BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L. THE CREASES ON CENTER FUSELAGE, BETWEEN F - [SDR CHQA20120703222](https://openairdocs.org/sdr/CHQA20120703222), Jul 3, 2012: SKIN. DAMAGED. DURING INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO BE DAMAGED AT FRAME 80 AND STRINGER 9L. THE RIGHT AFT FUSELAGE SKIN AT FRAME 80 AND STRINGER 9L WAS - [SDR CHQA201100299](https://openairdocs.org/sdr/CHQA201100299), Jul 25, 2011: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE LEFT CHANNEL FRAME AT FRAME - [SDR CHQA201100300](https://openairdocs.org/sdr/CHQA201100300), Jul 25, 2011: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE CHANNEL OF THE CARGO FRAME AT FRAME 66 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE CHANNEL CARGO FRAME AT - [SDR CHQA201100306](https://openairdocs.org/sdr/CHQA201100306), Jul 25, 2011: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR LOWER CUTOUT BEAM IN ACCORDANCE WITH SRM 51-40-0 - [SDR CHQA201100305](https://openairdocs.org/sdr/CHQA201100305), Jul 25, 2011: ANGLE. CORRODED. DURING INSPECTION, THE CARGO DOOR CUT-OUT FORWARD LATERAL L-SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE CARGO DOOR CUTOUT FORWARD LATERAL L-SHAPE I - [SDR CHQA201000209](https://openairdocs.org/sdr/CHQA201000209), Nov 11, 2010: CONTROLLER. INOPERATIVE. DURING CLIMB, CREW REPORTED CABIN ALTITUDE CLIMBING ABNORMALLY IN AUTO MODE. CREW DECLARED AN EMERGENCY & DESCENDED TO FL100, DIVERTED & LANDED WITHOUT INCIDENT - [SDR CHQA201000194](https://openairdocs.org/sdr/CHQA201000194), Oct 6, 2010: CONNECTOR. CORRODED. DURING CLIMB THE CREW REPORTED AN E1 ANTI-ICE FAIL MESSAGE AND THE E1 ANTI-ICE CIRCUIT BREAKER HAD TRIPPED. THE FLIGHT DIVERTED TO CLE AND LANDED WITHOUT INCIDE - [SDR CHQA201000190](https://openairdocs.org/sdr/CHQA201000190), Oct 3, 2010: FLAP. MALFUNCTIONED. ON DESCENT INTO MKE, WHEN THE CREW EXTENDED FLAPS, THE RECEIVED A FLAP FAIL MSG WITH THE FLAPS STUCK AT ZERO DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTE - [SDR CHQA200600097](https://openairdocs.org/sdr/CHQA200600097), Aug 13, 2006: BULB. BURNED OUT. EMERGENCY LIGHT NR 5 FLOOR STRIP AND LT WING FWD LIGHT INOPERATIVE. REMOVED AND REPLACED NR 5 FLOOR STRIP AND LT WING FWD BULB IAW MM 33-26-07. OPS CHECK GOOD. - [SDR CHQA200600036](https://openairdocs.org/sdr/CHQA200600036), Mar 10, 2006: ENGINE. DAMAGED. FLIGHT 7796 - ORD-BUF - SHORTLY AFTER SELECTING CLIMB THRUST, NR 2 ENGINE INDICATED AN ABNORMALLY HIGH ITT AND THE FUEL FLOW WAS SIGNIFICANTLY HIGHER THAN ENGIN - [SDR CHQA200600006](https://openairdocs.org/sdr/CHQA200600006), Jan 10, 2006: BULB. BURNED OUT. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-09. OPS CHECK GOOD. - [SDR CHQA000570](https://openairdocs.org/sdr/CHQA000570), Oct 19, 2004: BULB. BURNED OUT. LT SIDE ADT EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. - [SDR CHQ00046](https://openairdocs.org/sdr/CHQ00046), Nov 27, 2001: SMOKE DETECTOR. ACTIVATED. LAV SMOKE DETECTOR WENT OFF WHEN DOING A/I TEST, THEN ON CLIMBOUT. ## 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 NYC02IA076](https://openairdocs.org/ntsb/NYC02IA076), Mar 27, 2002: Embraer EMB-145LR (N290SK), Jefferson, NY, incident, minor damage. Probable cause: An in-flight encounter with lightning, which severed two of the four elevator cables. ## 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 20020326007409I](https://openairdocs.org/incident/20020326007409I), Mar 26, 2002: Emb EMB145LR (N290SK), Windsor Locks, CT, Minor damage. (-23) Aircraft was on an approach into the bradley international airport when it was struck by lightning. Aircraft damage included two severed elevator cables,… --- 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.