# N266SK: 2000 Embraer EMB-145LR, registration cancelled 2018-05-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 23, 2018 - Exported to: Mexico - 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: 145241 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 1, 2000 - Certificate issued: March 8, 2018 - Last registry action: March 8, 2018 - Mode S code: A296E1 - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bungay Suffolk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N266SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=266SK - Page: https://openairdocs.org/deregistered/N266SK-2018-05-23 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 (65, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201507300614](https://openairdocs.org/sdr/UHLA201507300614), Jul 30, 2015: APU. FIRE. WHILE APPROACHING THE GATE, THE CREW DISCHARGED THE APU FIRE BOTTLES AFTER A CONFIRMED APU FIRE. THE APU WAS R & R. - [SDR UHLA2015022200118](https://openairdocs.org/sdr/UHLA2015022200118), Feb 22, 2015: NONE. NONE. THE CREW REPORTED THAT THEY SUSPECTED A FUEL LEAK IN THE RT WING TANK DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECT - [SDR CHQA20141119328](https://openairdocs.org/sdr/CHQA20141119328), Nov 19, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTH - [SDR CHQA20140829255](https://openairdocs.org/sdr/CHQA20140829255), Aug 29, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE BEAM WAS REPLACED IAW ETD 2014-145-073053. - [SDR CHQA20140829253](https://openairdocs.org/sdr/CHQA20140829253), Aug 29, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140828252](https://openairdocs.org/sdr/CHQA20140828252), Aug 28, 2014: SKIN. CHAFED. DURING INSPECTION THE CARGO DOOR INNER SKIN WAS FOUND TO HAVE CHAFE MARKS ON THE LOWER AFT END. THE SKIN WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140827254](https://openairdocs.org/sdr/CHQA20140827254), Aug 27, 2014: FIREWALL. CRACKED. DURING INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER LT SUPPORT ROD. THE APU FIREWALL WAS REPAIRED IAW SRM 53-32-13. - [SDR CHQA20140826256](https://openairdocs.org/sdr/CHQA20140826256), Aug 26, 2014: DOUBLER. CORRODED. DURING INSPECTION THE LT OMEGA BEAM REPAIR DOUBLER ON THE INBD SIDE WAS FOUND TO BE CORRODED AT FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10. - [SDR CHQA20140826250](https://openairdocs.org/sdr/CHQA20140826250), Aug 26, 2014: SEAT TRACK. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SEAT TRACK FROM FRAME 25 - 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR CHQA20140826249](https://openairdocs.org/sdr/CHQA20140826249), Aug 26, 2014: SEAT TRACK. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06. - [SDR CHQA20140825251](https://openairdocs.org/sdr/CHQA20140825251), Aug 25, 2014: PROFILE. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LOWER PROFILE ON THE CARGO DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140518150](https://openairdocs.org/sdr/CHQA20140518150), May 18, 2014: FLAP. MALFUNCTIONED. DURING APPROACH, THE FLIGHT CREW RECEIVED A FLAP FAIL MSG ON THE EICAS DISPLAY. AFTER RUNNING THE CHECKLIST IN THE QRH, AN EMERGENCY WAS DECLARED & A SUCCESSFUL - [SDR CHQA20140430128](https://openairdocs.org/sdr/CHQA20140430128), Apr 30, 2014: INVERTER. INOPERATIVE. DURING INSPECTION, THE FWD CABIN COCKPIT ENTRANCE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE FWD CLOSET INVERTER. OPERATIONAL CHECKS WERE GOOD WI - [SDR CHQA20140429127](https://openairdocs.org/sdr/CHQA20140429127), Apr 29, 2014: TRANSCEIVER. FAULTY. CREW REPORTED THAT THE WEATHER RADAR WAS INOPERATIVE. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE WEATHER RADAR RECEIVER & TRANSMITTER AS - [SDR CHQA20140218062](https://openairdocs.org/sdr/CHQA20140218062), Feb 18, 2014: BATTERY. DISCHARGED. DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY BATTERY & ALL OPERATIONAL CHECKS WERE GOOD. - [SDR CHQA20140116016](https://openairdocs.org/sdr/CHQA20140116016), Jan 16, 2014: BATTERY. DISCHARGED. DURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER - [SDR CHQA20140102001](https://openairdocs.org/sdr/CHQA20140102001), Jan 2, 2014: BATTERY. DISCHARGED. DURING INSPECTION, THE RT & LT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GO - [SDR CHQA20131219457](https://openairdocs.org/sdr/CHQA20131219457), Dec 19, 2013: WARNING SYSTEM. FALSE ACTIVATION. CREW REPORTED THAT ON APPROACH THEY RECEIVED AN AURAL WARNING FOR LG. ALL THREE GEAR INDICATED DOWN & LOCKED. THE CREW DID A GO AROUND & ON THE SECOND APPROACH - [SDR CHQA20131210444](https://openairdocs.org/sdr/CHQA20131210444), Dec 10, 2013: BATTERY PACK. DISCHARGED. THE AFT EXTERIOR LT & RT FUSELAGE LIGHTS FAILED TO ILLUMINATE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK & ALL OPERATIONS CHECKED GOOD. - [SDR CHQA20131016370](https://openairdocs.org/sdr/CHQA20131016370), Oct 16, 2013: DUCT. DISCONNECTED. CREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE CABIN AROUND SEAT 9A. DECLARED AND EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE - [SDR CHQA20130822329](https://openairdocs.org/sdr/CHQA20130822329), Aug 22, 2013: FRAME. DAMAGED. DURING INSPECTION, A HOLE WAS FOUND ON THE RT SIDE OF FRAME 65 BETWEEN STRINGERS 12R AND 13R. THE FRAME WAS REPAIRED IAW ETD 2013-145-032262. - [SDR CHQA20130822328](https://openairdocs.org/sdr/CHQA20130822328), Aug 22, 2013: SUPPORT. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE RT INBD OMEGA BEAM SUPPORT AT FRAME 47 AND 48. THE OMEGA BEAM SUPPORTS WERE REPLACED IAW SRM 51-40-02. - [SDR CHQA20130822327](https://openairdocs.org/sdr/CHQA20130822327), Aug 22, 2013: CHANNEL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER OF LT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IAW SRM 53-00-10. - [SDR CHQA20130822326](https://openairdocs.org/sdr/CHQA20130822326), Aug 22, 2013: FRAME. BENT. DURING INSPECTION, FRAME 72 WAS FOUND BENT AT STRINGER 16R. FRAME REPAIRED IAW ETD 2013-145-032192-A. - [SDR CHQA20130820320](https://openairdocs.org/sdr/CHQA20130820320), Aug 20, 2013: BATTERY PACK. INOPERATIVE. DURING INSPECTION, NR 4 AND 5 EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED GOOD. - [SDR CHQA20130621226](https://openairdocs.org/sdr/CHQA20130621226), Jun 21, 2013: BATTERY PACK. INOPERATIVE. DURING INSPECTION, OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER D - [SDR CHQA20130509163](https://openairdocs.org/sdr/CHQA20130509163), May 9, 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 CHQA20130222061](https://openairdocs.org/sdr/CHQA20130222061), Feb 22, 2013: CONNECTOR. CORRODED. CREW REPORTED THAT ON TAKEOFF THEY SELECTED THE CLIMB THRUST RATING AND THE MODE AUTOMATICALLY REVERTED TO T/O THRUST MODE. THE CREW RETURNED TO FIELD AND LANDE - [SDR CHQA20130114014](https://openairdocs.org/sdr/CHQA20130114014), Jan 14, 2013: BLEED VALVE. FAULTY. CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 2 VALVE FAIL MESSAGE ALONG WITH A BLEED 2 VALVE CLOSED MESSAGE. DUE TO WEATHER RESTRICTIONS THE FLIGHT DI - [SDR CHQA20121210469](https://openairdocs.org/sdr/CHQA20121210469), Dec 10, 2012: ECU. FAULTY. CREW REPORTED, FLAP FAIL MESSAGE ON APPROACH TO KRHI. THE CREW RETURNED TO FIELD IN KMKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC C - [SDR CHQA20121209459](https://openairdocs.org/sdr/CHQA20121209459), Dec 9, 2012: ECU. FAULTY. CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE AFTER GEAR RETRACTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS AND A FLA - [SDR CHQA20120906312](https://openairdocs.org/sdr/CHQA20120906312), Sep 6, 2012: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53 - [SDR CHQA20120906311](https://openairdocs.org/sdr/CHQA20120906311), Sep 6, 2012: SKIN SPLICE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACC - [SDR CHQA20120904320](https://openairdocs.org/sdr/CHQA20120904320), Sep 4, 2012: STRINGER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R FROM FRAME 8 TO FRAME 13. THE STRINGER 21R AT FRAME 8 TO FRAME 13 WAS REPLACED IN ACCORDANCE WITH SRM 51- - [SDR CHQA20120904317](https://openairdocs.org/sdr/CHQA20120904317), Sep 4, 2012: WEB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCOR - [SDR CHQA20120904319](https://openairdocs.org/sdr/CHQA20120904319), Sep 4, 2012: STANCHION. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 11 AND 12. THE RIGHT STANCHION BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH - [SDR CHQA20120904318](https://openairdocs.org/sdr/CHQA20120904318), Sep 4, 2012: STANCHION. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 12 AND 13. THE RIGHT STANCHION BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH - [SDR CHQA20120904316](https://openairdocs.org/sdr/CHQA20120904316), Sep 4, 2012: WEB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCOR - [SDR CHQA20120828315](https://openairdocs.org/sdr/CHQA20120828315), Aug 28, 2012: SKIN SPLICE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN AC - [SDR CHQA20120828313](https://openairdocs.org/sdr/CHQA20120828313), Aug 28, 2012: FITTING. CRACKED. DURING INSPECTION, THE SHEAR FOOT AT FRAME 68 BETWEEN STRINGERS 6L AND 7L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED AND INSTALLED IN ACCORDANCE WITH - [SDR CHQA20120828310](https://openairdocs.org/sdr/CHQA20120828310), Aug 28, 2012: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLES ON THE SERVICE DOOR THRESHOLD. MAINTENANCE REPLACED THE SERVICE DOOR SILL IN ACCORDANCE WITH SRM 53-20 - [SDR CHQA20120816314](https://openairdocs.org/sdr/CHQA20120816314), Aug 16, 2012: SKIN. DENTED. DURING HEAVY MAINTENANCE A PREVIOUSLY DAMAGED SECTION OF SKIN AFT OF THE PASSENGER DOOR NEAR FRAME 19-20 AND STRINGER 12L -13L WAS REPAIRED IN ACCORDANCE WITH E - [SDR CHQA20120609187](https://openairdocs.org/sdr/CHQA20120609187), Jun 9, 2012: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH N - [SDR CHQA20120321085](https://openairdocs.org/sdr/CHQA20120321085), Mar 21, 2012: BATTERY. DISCHARGED. DURING INSPECTION, THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATI - [SDR CHQA201200027](https://openairdocs.org/sdr/CHQA201200027), Jan 27, 2012: COUPLING. DEFECTIVE. CREW REPORTED DURING CLIMB THEY RECEIVED A BLEED 1 LEAK MESSAGE. AFTER FOLLOWING THE QUICK REFERENCE HANDBOOK THE MESSAGE CLEARED. DUE TO SINGLE BLEED OPERATION - [SDR CHQA201100410](https://openairdocs.org/sdr/CHQA201100410), Oct 22, 2011: CONNECTOR. DISCONNECTED. DURING INSPECTION, THE RIGHT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR DISCONNECTED FROM THE LIGHT ASSEMBLY. THE - [SDR CHQA201100397](https://openairdocs.org/sdr/CHQA201100397), Oct 4, 2011: WARNING SYSTEM. MALFUNCTIONED. CREW REPORTED THAT ON DESCENT, RECEIVED A SPOILER FAIL MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DISCOVERED THAT THEIR LANDING DI - [SDR CHQA201100041](https://openairdocs.org/sdr/CHQA201100041), Feb 23, 2011: CONNECTOR. CORRODED. CREW REPORTED THAT AFTER TAKEOFF THE THRUST MODE WOULD NOT CHANGE FROM TAKEOFF MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND C - [SDR CHQA201100030](https://openairdocs.org/sdr/CHQA201100030), Feb 3, 2011: SHUTOFF VALVE. FAULTY. CREW RETURNED TO FIELD DUE TO A BLEED 2 VALVE FAIL MESSAGE ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE E2 PRSOV AND HIGH STAGE PRES - [SDR CHQA201100002](https://openairdocs.org/sdr/CHQA201100002), Jan 3, 2011: CONNECTOR. DIRTY. AFTER TAKEOFF THE CREW REPORTED THAT THE COMM 2 RMU WAS BLANKED OUT AND THE BACK-UP HEAD COULD NOT BE TUNED AND THAT COMM 1 WAS SWITCHING BETWEEN ACTIVE AND TUN All 65: https://openairdocs.org/deregistered/N266SK-2018-05-23/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 20131016019239I](https://openairdocs.org/incident/20131016019239I), Oct 16, 2013: Embraer EMB-145LR (N266SK), Greer, SC, No damage. Flight 6168, N266SK, returned to the departure airport (gsp) due to smoke in cabin shortly after takeoff. An evacuation was carried out through the left hand… - [Incident 20031216033239I](https://openairdocs.org/incident/20031216033239I), Dec 16, 2003: Emb EMB145LR (N266SK), Erie, PA. (-23) Chqa flight #4905, N266SK, flap failed while in transit between 0 and 9 deg on final to Erie airport. Aircraft was diverted to pittsburgh airport due to… --- 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.