# N276SK: Embraer EMB-145LR, registration cancelled 2023-02-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 22, 2023 - Exported to: Mexico - 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: 145348 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 4, 2021 - Certificate issued: February 20, 2020 - Last registry action: February 21, 2023 - Mode S code: A2BE60 - Owner when cancelled: [Flight Lease Xviii LLC](https://openairdocs.org/faa-owner/FLIGHT%20LEASE%20XVIII%20LLC) - Location: [Palm Beach Gardens, FL](https://openairdocs.org/faa-place/FL/Palm%20Beach%20Gardens) - Owner type: Corporation - Owner's area on the map: 26.8457° N, 80.0874° W: Placed by OpenAirDocs at the center of ZIP code 33410, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N276SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=276SK - Page: https://openairdocs.org/deregistered/N276SK-2023-02-22 From the FAA registry file of November 4, 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 4VAA20211216003](https://openairdocs.org/sdr/4VAA20211216003), Dec 16, 2021: INVERTER. FAILED. DURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS THREE AND FOUR. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIO - [SDR 4VAA202111190002](https://openairdocs.org/sdr/4VAA202111190002), Nov 19, 2021: NONE. NONE. DURING INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INTERMITTENTLY INOPERATIVE IN THE FRONT SECTION OF THE AIRCRAFT. A LOOSE CONNECTOR WAS RESECURED AN - [SDR UHLA201607140363](https://openairdocs.org/sdr/UHLA201607140363), Jul 14, 2016: STOP. INOPERATIVE. MAIN ENTRY DOOR STEPS WILL NOT DEPLOY. R & R MAIN DOOR FOLD OUT BACK STOP IAW AMM 52-13-02. OPS TEST GOOD. - [SDR UHLA201605140239](https://openairdocs.org/sdr/UHLA201605140239), May 14, 2016: CONTROL PANEL. MALFUNCTIONED. SIDE WALL LIGHT BUTTON TURNS ON EMERGENCY LIGHTS. R & R ATTENDANT CONTROL PANEL IAW AMM 25-27-09. OPS CHECK GOOD. - [SDR UHLA2015020100068](https://openairdocs.org/sdr/UHLA2015020100068), Feb 1, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, THE INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE CAPTAINS SEAT TRACK LOCATIONS. THE FLANGES WERE REPAIRED IAW ETD 2015-145-01 - [SDR UHLA2015020100067](https://openairdocs.org/sdr/UHLA2015020100067), Feb 1, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE COCKPIT INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE F/O SEAT TRACKS. THE INBD AND OTBD FLOOR FLANGES WERE REPAIRED IAW E - [SDR UHLA2015012300070](https://openairdocs.org/sdr/UHLA2015012300070), Jan 23, 2015: ATTACH FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD PASSENGER DOOR ATTACH FITTING BELOW THE HINGE ARM. THE ATTACH FITTING WAS REPAIRED IN ACCORDANCE WITH ETD - [SDR UHLA2015012200069](https://openairdocs.org/sdr/UHLA2015012200069), Jan 22, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR BOTTOM SIDE STRUCTURE, THE STRUCTURE WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015012200066](https://openairdocs.org/sdr/UHLA2015012200066), Jan 22, 2015: ATTACH ANGLE. CRACKED. DURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5R-7R. THE ATTACH ANGLE WAS REPLAC - [SDR UHLA2015012200065](https://openairdocs.org/sdr/UHLA2015012200065), Jan 22, 2015: ATTACH ANGLE. CRACKED. DURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5L-7L. THE ATTACH ANGLE WAS REPLAC - [SDR CHQA20140705207](https://openairdocs.org/sdr/CHQA20140705207), Jul 5, 2014: PUMP. LEAKING. CREW REPORTED THAT THEY RECEIVED A HYD 1 LOW QTY MSG FOLLOWED BY A HYD SYS 1 FAIL MSG. THE CREW PERFORMED A MANUAL EXTENSION ON THE LG. THE ACFT LANDED WITHOUT - [SDR CHQA20140306082](https://openairdocs.org/sdr/CHQA20140306082), Mar 6, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPAIRED IAW SRM 53-0010 & SRM 51-40-02. - [SDR CHQA20140306081](https://openairdocs.org/sdr/CHQA20140306081), Mar 6, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 23. THE LT OMEGA BEAM WAS REPAIRED IAW ETD 2014-145-014567. - [SDR CHQA20140306080](https://openairdocs.org/sdr/CHQA20140306080), Mar 6, 2014: SERVICE DOOR. CORRODED. DURING INSPECTION THE SERVICE DOOR BOTTOM STRUCTURE ATTACHMENT FOR THE LINER NUT PLATE AREAS WAS FOUND TO BE CORRODED. THE SERVICE DOOR WAS REPAIRED IAW ETD 201 - [SDR CHQA20131016371](https://openairdocs.org/sdr/CHQA20131016371), Oct 16, 2013: SWITCH. FAULTY. CREW REPORTED THAT THEY RECEIVED A "BLEED 2 VALVE CLOSED" MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BL - [SDR CHQA20130706260](https://openairdocs.org/sdr/CHQA20130706260), Jul 6, 2013: WIRE HARNESS. INOPERATIVE. DURING INSPECTION, EMERGENCY LIGHT ON MAIN ENTRY DOOR HANDRAIL WAS FOUND TO BE INOPERATIVE. MX REPLACED THE CAUTION INDICATION HARNESS OPS CHECKED GOOD. - [SDR CHQA20130208046](https://openairdocs.org/sdr/CHQA20130208046), Feb 8, 2013: DISPLAY. INOPERATIVE. CREW REPORTED THE PRIMARY FLIGHT DISPLAY NUMBER 1 FAILED IN FLIGHT WITH AN ELECTRICAL ODOR PRESENT IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. - [SDR CHQA20121207475](https://openairdocs.org/sdr/CHQA20121207475), Dec 7, 2012: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD BEAM. THE THRESHOLD BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121207474](https://openairdocs.org/sdr/CHQA20121207474), Dec 7, 2012: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD BEAM AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH SRM 53- - [SDR CHQA20121207473](https://openairdocs.org/sdr/CHQA20121207473), Dec 7, 2012: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT RIGHT OMEGA FRAME 61. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 51-20-03. - [SDR CHQA20121207472](https://openairdocs.org/sdr/CHQA20121207472), Dec 7, 2012: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT LEFT OMEGA FRAME 59. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20121207471](https://openairdocs.org/sdr/CHQA20121207471), Dec 7, 2012: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SILL AT FRAME 20 TO FRAME 21. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00. - [SDR CHQA20121207470](https://openairdocs.org/sdr/CHQA20121207470), Dec 7, 2012: ANGLE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RAMP ANGLE FRAME 20 AT THE CENTER OMEGA BEAM. THE ANGLE AT FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-03. - [SDR CHQA20120801229](https://openairdocs.org/sdr/CHQA20120801229), Aug 1, 2012: PRESSURE SWITCH. FAULTY. CREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, THEY RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FUR - [SDR CHQA20120801228](https://openairdocs.org/sdr/CHQA20120801228), Aug 1, 2012: PRESSURE SWITCH. FAULTY. CREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER - [SDR CHQA201100286](https://openairdocs.org/sdr/CHQA201100286), Jul 24, 2011: CARBON SEAL. LEAKING. CREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKE-OFF AND REPORTED THAT THEY RECEIVED NO FIRE INDICATIONS AND AL - [SDR CHQA201100046](https://openairdocs.org/sdr/CHQA201100046), Feb 24, 2011: LIGHT. INOPERATIVE. DURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS - [SDR CHQA201000113](https://openairdocs.org/sdr/CHQA201000113), Jun 3, 2010: UNKNOWN. MALFUNCTIONED. AFTER TAKEOFF, CREW ATTEMPTED TO RETRACT LANDING GEAR, RECEIVED A LDG AIR/GND FAIL MESSAGE ON EICAS AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO FIE - [SDR CHQA201000081](https://openairdocs.org/sdr/CHQA201000081), Apr 16, 2010: SOLENOID VALVE. FAULTY. CREW REPORTED THAT DURING CLIMBOUT A VIBRATION AND LOW RUMBLE COULD BE HEARD AND FELT. AFTER LEVELING OFF, THE AIRCRAFT WOULD NOT ACCELERATE PAST 0.70 MACH IN C - [SDR CHQA200900261](https://openairdocs.org/sdr/CHQA200900261), Dec 11, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT AND THE NR 4 BATTERY PACK WITH NO - [SDR CHQA200900148](https://openairdocs.org/sdr/CHQA200900148), Jun 28, 2009: BATTERY PACK. DISCHARGED. DURING INSP, THE LT AND RT OVER-WING EMERGENCY EXTERIOR LIGHTS WERE FOUND TO BE INOP. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE EXTERIOR LIGHTS OPERA - [SDR CHQA200900114](https://openairdocs.org/sdr/CHQA200900114), Apr 25, 2009: WIRE. BROKEN. FLIGHT 7822, IAD TO IND - SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FT THE CREW RECEIVED A SERVICE DOOR OPEN EICAS MESSAGE. THE QRH CHECKLIST WAS COMPLETED AN - [SDR CHQA200900017](https://openairdocs.org/sdr/CHQA200900017), Jan 13, 2009: BATTERY PACK. INOPERATIVE. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE INOP ON THE LEFT AND RIGHT SIDES. THE NR 3 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYS - [SDR CHQA200700029](https://openairdocs.org/sdr/CHQA200700029), Jun 20, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 3438 - ATL-CLE - ON DESCENT WHEN FLAPS SELECTED TO 9, EICAS MESSAGES SPS ADV AND FLAP FAIL APPEARED. PERFORMED THE QRH AND DECLARED AN EMERGENCY. LANDED - [SDR CHQA200600119](https://openairdocs.org/sdr/CHQA200600119), Sep 14, 2006: INVERTER. INOPERATIVE. FLOOR PROXIMITY LIGHT NR 2 AND NR 2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW MM 33-50-00. OPS CHECK GOOD. - [SDR CHQA200600114](https://openairdocs.org/sdr/CHQA200600114), Sep 1, 2006: BULB. BURNED OUT. NR 1 EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT IAW MM 33-26-06. - [SDR CHQA200600112](https://openairdocs.org/sdr/CHQA200600112), Aug 30, 2006: BATTERY. INOPERATIVE. EMERGENCY LIGHTING PROXIMITY STRIPS 2 AND 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB 145 MM 33-50-06. OPS CHECK GOOD. - [SDR CHQA200600091](https://openairdocs.org/sdr/CHQA200600091), Jul 25, 2006: WINDSHIELD. MALFUNCTIONED. DURING DESCENT THROUGH FL200, THERE WAS A THIN CLOUD LAYER WITH ICING CONDITIONS. HEARD WHAT SOUNDED LIKE WATER DROPLETS SIZZLING. THEN SMELLED ELECTRICAL SMOKE - [SDR CHQA200500215](https://openairdocs.org/sdr/CHQA200500215), Dec 20, 2005: HUB CAP. MISSING. FLIGHT 900 - LAN-OKC - DURING INITIAL CLIMBOUT, RETRACTED GEAR DURING NORMAL SCHEDULE. RIGHT MAIN SHOWED IN TRANSITION (AMBER BOX) FOR APPROXIMATELY 10 SECONDS, - [SDR CHQA200500171](https://openairdocs.org/sdr/CHQA200500171), Oct 1, 2005: ODOR. DETECTED. FLIGHT 6320 - FLL-MCO - ON FINAL APPROACH, NOTICED SMOKE AND AN ODOR OF SMOKE. THE ELECTRIC PAGE INDICATED GEN 3 AMP 105. PERFORMED GENERAL VISUAL INSPECTION OF - [SDR CHQA200500115](https://openairdocs.org/sdr/CHQA200500115), Jun 17, 2005: LIGHT. INOPERATIVE. LEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. - [SDR CHQA200500042](https://openairdocs.org/sdr/CHQA200500042), Feb 25, 2005: LAMP. BURNED OUT. LEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REPLACED THE LEFTHAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. - [SDR 00050](https://openairdocs.org/sdr/00050), Nov 29, 2001: GASKET. LEAKING. RT ENGINE ITT 50 DEGREES HOTTER THAN LT ITT. INSPECTED AIRCRAFT NR 2 ENG, PERFORMED BORESCOPE OF COMPRESSOR TURBINE SECTION HOT SECTION WITHIN LIMITS. PERFORMED --- 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.