# N280SK: Embraer EMB-145LR, registration cancelled 2022-01-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 24, 2022 - Exported to: Australia - 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: 145381 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 23, 2001 - Certificate issued: February 20, 2020 - Last registry action: February 20, 2020 - Mode S code: A2CF95 - 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: LLC - 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/N280SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=280SK - Page: https://openairdocs.org/deregistered/N280SK-2022-01-24 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 (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201606030292](https://openairdocs.org/sdr/UHLA201606030292), Jun 3, 2016: SWITCH. OUT OF ADJUST. MAIN CABIN DOOR SHOWS OPEN ON THE MFD. ADJUSTED FWD LOCK BOX SWITCH ON MED IAW AMM 52-12-09. OPS CHECK GOOD. - [SDR UHLA201605250264](https://openairdocs.org/sdr/UHLA201605250264), May 25, 2016: SPRING. DAMAGED. F/A ADVISES STAIRS SLAM FLAT WHEN RAISING MCD. R & R SPRINGS ON TOP OF MCD IAW AMM 52-10-07. OPS CHECK GOOD. - [SDR UHLA201510290776](https://openairdocs.org/sdr/UHLA201510290776), Oct 29, 2015: HANDLE. UNSECURE. THE MAIN ENTRY DOOR HANDLE WAS FOUND NOT SECURE. MAINTENANCE SECURED THE HANDLE IAW AMM 52-11-06 AND ALL OPS CHECKS WERE GOOD. - [SDR UHLA2015021900146](https://openairdocs.org/sdr/UHLA2015021900146), Feb 19, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE BEAM WAS REPAIRED IAW ETD 2015-145-016197. - [SDR UHLA2015021500147](https://openairdocs.org/sdr/UHLA2015021500147), Feb 15, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM INBD FLOORBOARD FLANGE AT FRAME 25. THE FLANGE WAS REPAIRED IAW SRM 51-40-024. - [SDR UHLA2015021400144](https://openairdocs.org/sdr/UHLA2015021400144), Feb 14, 2015: SHEAR TIE. CRACKED. DURING INSPECTION, THE APU FIREWALL SHEAR CLIP WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 8L-9L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015021400143](https://openairdocs.org/sdr/UHLA2015021400143), Feb 14, 2015: SHEAR TIE. CRACKED. DURING INSPECTION, THE RT SHEAR CLIP AT FRAME 80 AND STRINGERS 5R-7R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015021300139](https://openairdocs.org/sdr/UHLA2015021300139), Feb 13, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 22. THE BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015021200142](https://openairdocs.org/sdr/UHLA2015021200142), Feb 12, 2015: DOOR FRAME. CORRODED. DURING INSPECITON, CORROSION WAS FOUND ON THE LOWER SIDE OF THE SERVICE DOOR BOTTOM FRAME. THE FRAME WAS REPAIRED IAW ETD 2015-145-016097. - [SDR UHLA2015021200140](https://openairdocs.org/sdr/UHLA2015021200140), Feb 12, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT INBD OMEGA BEAM FLOOR FLANGE. THE FLANGE WAS REPLACED IAW SRM 53-00-10. - [SDR UHLA2015021100148](https://openairdocs.org/sdr/UHLA2015021100148), Feb 11, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT OTBD SILL AT FRAME 18 THROUGH 20. THE SILL WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015021100145](https://openairdocs.org/sdr/UHLA2015021100145), Feb 11, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER ON THE CENTER SERVICE DOOR THRESHOLD SILL. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA2015021100141](https://openairdocs.org/sdr/UHLA2015021100141), Feb 11, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT THE LT OMEGA BEAM AND FRAME 20. THE ANGLE WAS REPAIRED IAW SRM 53-21-10. - [SDR UHLA2015021000149](https://openairdocs.org/sdr/UHLA2015021000149), Feb 10, 2015: FRAME. MISINSTALLED. DURING INSPECTION, THE WORKING RIVETS ON FRAME 79 BETWEEN STRINGERS 4R AND 6R WERE REPLACED IAW ETD 2015-145-017668. - [SDR CHQA20141229362](https://openairdocs.org/sdr/CHQA20141229362), Dec 29, 2014: SWITCH. FAULTY. THE CREW REPORTED THAT THEY RECEIVED A BLEED 2 VLV CLOSED MSG IN FLIGHT. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE BLEED SYS 2 PUSHBUTT - [SDR CHQA20130628251](https://openairdocs.org/sdr/CHQA20130628251), Jun 28, 2013: BATTERY. INOPERATIVE. DURING INSPECTION, THE MAIN ENTRY DOOR EMERGENCY EXIT SIGN WAS FOUND NOT TO ILLUMINATE. MX REPLACED THE EMERGENCY LIGHT INVERTER BATTERY NR 1 AFTER WHICH ALL OP - [SDR CHQA20130520173](https://openairdocs.org/sdr/CHQA20130520173), May 20, 2013: RELAY. FAILED. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE Q - [SDR CHQA20130520172](https://openairdocs.org/sdr/CHQA20130520172), May 20, 2013: RELAY. FAILED. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE Q - [SDR CHQA20130520171](https://openairdocs.org/sdr/CHQA20130520171), May 20, 2013: PRESSURE SWITCH. MALFUNCTIONED. CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE Q - [SDR CHQA20130321093](https://openairdocs.org/sdr/CHQA20130321093), Mar 21, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACKED SHEAR CLIP WAS FOUND AT FRAME 38 FROM STRINGERS 21L TO 21R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130318094](https://openairdocs.org/sdr/CHQA20130318094), Mar 18, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH 53-31-04. - [SDR CHQA20130316095](https://openairdocs.org/sdr/CHQA20130316095), Mar 16, 2013: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 38 AND 39 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-01. - [SDR CHQA20130316092](https://openairdocs.org/sdr/CHQA20130316092), Mar 16, 2013: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 37 AND 38 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-01. - [SDR CHQA20130128032](https://openairdocs.org/sdr/CHQA20130128032), Jan 28, 2013: LIGHT. DAMAGED. DURING INSPECTION, THE EMERGENCY LIGHTING STRIP THAT IS FARTHEST AFT WAS FOUND TO HAVE A BROKEN LEAD. THE EMERGENCY FLOOR LIGHT STRIP WAS REPLACED. OPERATIONAL - [SDR CHQA20120329111](https://openairdocs.org/sdr/CHQA20120329111), Mar 29, 2012: HINGE. CRACKED. DURING INSPECTION, THE LEFT AILERON DAMPER HINGE WAS FOUND TO BE CRACKED. THE LEFT AILERON DAMPER HINGE WAS REPLACED IAW SRM 51-40-08 AND 51-40-02. - [SDR CHQA20120301070](https://openairdocs.org/sdr/CHQA20120301070), Mar 1, 2012: ACM. FAILED. CREW REPORTED THAT THERE WAS SMOKE IN THE CABIN AND COCKPIT DURING TAKEOFF. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERF - [SDR CHQA201100413](https://openairdocs.org/sdr/CHQA201100413), Oct 24, 2011: INVERTER. INOPERATIVE. DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER ABOVE THE SERVI - [SDR CHQA201100256](https://openairdocs.org/sdr/CHQA201100256), Jun 28, 2011: RELAY. BURNED. CREW REPORTED THAT DURING FLIGHT RECEIVED A PITOT 3 INOPERATIVE MESSAGE ON THE EICAS FOLLOWED SHORTLY BY AN UNUSUAL ODOR IN THE FLIGHT DECK. THE CREW DIVERTED T - [SDR CHQA201100202](https://openairdocs.org/sdr/CHQA201100202), May 27, 2011: SKIN. DAMAGED. DURING INSPECTION, A PREVIOUS BLEND ON THE RIGHT CENTER FUSELAGE SKIN, SECTION I BETWEEN FRAME 16-17 AND STRINGER 19R-20R, WAS FOUND TO BE OUT OF LIMITS. THE DA - [SDR CHQA201100194](https://openairdocs.org/sdr/CHQA201100194), May 27, 2011: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65, BETWEEN STRINGERS 15L AND 17L. THREE AREAS WERE FOUND WITH THE DEEPEST DAMAGE BEING 0.022" DEEP. THE DAMAGE - [SDR CHQA201100216](https://openairdocs.org/sdr/CHQA201100216), May 21, 2011: SKIN. DENTED. DURING INSPECTION THE LOWER CONTROL SURFACE OF THE LEFT ELEVATOR WAS FOUND TO BE DENTED APPROXIMATELY AT YH-1280.00. THE DENT WAS REPAIRED IN ACCORDANCE WITH ET - [SDR CHQA201100218](https://openairdocs.org/sdr/CHQA201100218), May 20, 2011: BEAM. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE LOWER BEAM. THE CARGO FLOOR STRUCTURE LOWER BEAM WAS REPLACED; THE NEW PART WAS INSTALLED WIT - [SDR CHQA200900199](https://openairdocs.org/sdr/CHQA200900199), Sep 6, 2009: UPLOCK SWITCH. FAULTY. FLIGHT 3075, LGA TO RIC. ON TAKEOFF THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE NOSE GEAR INDICATION SHOWED YELLOW CROSS HATCHES AND A L - [SDR CHQA200900147](https://openairdocs.org/sdr/CHQA200900147), Jun 28, 2009: CONTROLLER. INOPERATIVE. THE ACFT HAD THE AUTO PRESSURIZATION MODE DEFERRED WHEN IT DEPARTED. DURING CLIMB-OUT, WHILE CLIMBING THROUGH 9,000 FT THE CABIN ALTITUDE INDICATED 8,500 FT. TH - [SDR CHQA200900127](https://openairdocs.org/sdr/CHQA200900127), May 19, 2009: INVERTER. INOPERATIVE. DURING INSPECTION THE EMERGENCY FLOOR LIGHTS NR 4, 6, 7, 8 WERE FOUND INOP. THE NR 4 FLOOR PROXIMITY LIGHT STRIP AND NR 4 INVERTER WERE REPLACED AND THE EMERGEN - [SDR CHQA200900029](https://openairdocs.org/sdr/CHQA200900029), Jan 21, 2009: PROXIMITY SENSOR. FAULTY. FLIGHT 3008, CMH TO LGA - DURING INITIAL CLIMB-OUT AFTER GEAR RETRACTION, THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS, AND WITHIN 1 MINUTE A ENG 1-2 RE - [SDR CHQA200800207](https://openairdocs.org/sdr/CHQA200800207), Oct 19, 2008: INVERTER. INOPERATIVE. FLIGHT 3084, CMH TO DCA. DURING INSPECTION THE EMERGENCY EXIT SIDEWALL LIGHT AT SEATS 12 D&F WAS INOP. MAINTENANCE FOUND THE NR 4 INVERTER INOP AND WAS REPLACED - [SDR CHQA200600060](https://openairdocs.org/sdr/CHQA200600060), May 12, 2006: CARBON SEAL. DEFECTIVE. NORMAL FLIGHT UNTIL CLIMBING THROUGH FL300, NOTICED OIL PRESSURE FOR NR 2 ENGINE WAS IN THE AMBER RANGE ON THE EICAS. CHECKED QUANTITY OF OIL ON NR 2 ENGINE, NO - [SDR CHQA20050192](https://openairdocs.org/sdr/CHQA20050192), Nov 5, 2005: WIRE. BROKEN. AFT STRIP EMERGENCY FLOOR LIGHTING HAS BROKEN WIRES. REPLACED AFT EMERGENCY LIGHTING STRIP IAW MM 33-26-06. OPS TEST GOOD. - [SDR CHQA200500139](https://openairdocs.org/sdr/CHQA200500139), Aug 9, 2005: RADIO. INOPERATIVE. FLIGHT 3143 - GSP-LGA - DURING DESCENT, AN ODOR SIMILAR TO ELECTRICAL BURNING WAS NOTICED FOLLOWED BY COM 1 FAILING. REMOVED AND REPLACED THE NR 1 INTEGRATED CO - [SDR CHQA200500126](https://openairdocs.org/sdr/CHQA200500126), Jul 12, 2005: ENGINE. UNSERVICEABLE. AFTER STARTING DESCENT OUT OF 16,000 FT, HEAT-TYPE ODOR NOTED SHORTLY AFTER MAKING INITIAL POWER REDUCTION. ODOR SUBSIDED AND ATTRIBUTED TO OCCASIONAL PACK SMEL - [SDR CHQA200500082](https://openairdocs.org/sdr/CHQA200500082), Apr 13, 2005: ENGINE. FAILED. DURING LATE STAGES OF CLIMB, AT APPROX 24500 FT., NOTICED A SPIKE IN NR 2 ITT OF 911 C. FOR 1 SEC. REDUCED THRUST ON NR 2, ITT RETURNED TO GREEN RANGE. LEVELED - [SDR CHQA200400563](https://openairdocs.org/sdr/CHQA200400563), Oct 9, 2004: ENGINE. LEAKING. DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS AB - [SDR CHQA200400562](https://openairdocs.org/sdr/CHQA200400562), Oct 6, 2004: CARBON SEAL. LEAKING. FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. THE TAKEOFF WAS ABORTED AND THE PLANE WAS E ## FAA accident and incident reports (3) 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 20050712019269I](https://openairdocs.org/incident/20050712019269I), Jul 12, 2005: Emb EMB145LR (N280SK), Syracuse, NY. (-23) On July 12, 2005, an Emb-145, chautauqua flight 3220, was cruising at 16,000 feet; on the start of descent the first officer noticed a smell or heat in… - [Incident 20041006031249I](https://openairdocs.org/incident/20041006031249I), Oct 6, 2004: Emb EMB145LR (N280SK), Rochester, NY. (-23) On October 6, 2004 at 1224 EST, chautaqua airlines flight 3115, an Emb-145, aborted take-off on runway 22 at roc due to smoke in the cabin and cockpit.… - [Incident 20021015032499I](https://openairdocs.org/incident/20021015032499I), Oct 15, 2002: Emb EMB145LR (N280SK), Richmond, VA, Minor damage. (-23) On October 15, 2002, at approximately 1208, captain jose quezada, while PIC of N280SK, an Emb-145-LR, experienced smoke in the cockpit with no warning or… --- 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.