# N287SK: 2001 Embraer EMB-145LR, registration cancelled 2022-10-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 1, 2022 - Status when cancelled: Registration expired, pending cancellation - 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: 145460 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 3, 2001 - Certificate issued: June 20, 2019 - Last registry action: June 20, 2019 - Mode S code: A2E996 - Owner when cancelled: [Bai Bayview Aviation LLC](https://openairdocs.org/faa-owner/BAI%20BAYVIEW%20AVIATION%20LLC) - Location: [Mount Pleasant, SC](https://openairdocs.org/faa-place/SC/Mount%20Pleasant) - Owner type: LLC - Owner's area on the map: 32.8174° N, 79.8551° W: Placed by OpenAirDocs at the center of ZIP code 29464, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N287SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=287SK - Page: https://openairdocs.org/deregistered/N287SK-2022-10-01 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201603140109](https://openairdocs.org/sdr/UHLA201603140109), Mar 14, 2016: PIN. DAMAGED. EMERGENCY LIGHT BROKEN, LAST STRIP NEEDS CONNECTOR PIN. REPINNED LAST ROW EMERGENCY STRIP LIGHTING IAW SWPM 20-21-00. OPS CHECK GOOD. - [SDR UHLA201602090107](https://openairdocs.org/sdr/UHLA201602090107), Mar 9, 2016: STRUT. UNDERSERVICED. NLG DID NOT RETRACT, LT LEVER DISAGREE MESSAGE ON EICAS. RETURNED TO FIELD. VERIFIED NLG STRUT SERVICING AND CYCLED LANDING GEAR SEVERAL TIMES WITH NO DEFECTS N - [SDR UHLA201508270675](https://openairdocs.org/sdr/UHLA201508270675), Aug 27, 2015: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHT AT SEATS 10-16A WERE FOUND TO BE INOPERATIVE. THE LIGHTS WERE R & R IAW AMM53-50-12 AND OPS CHECKED GOOD. - [SDR UHLA2015041100247](https://openairdocs.org/sdr/UHLA2015041100247), Apr 11, 2015: UPLOCK. MALFUNCTIONED. THE CREW REPORTED RECEIVING A LANDING GEAR LEVER DISAGREE FAIL MESSAGE AND THE NOSE GEAR FAILING TO RETRACT. THE CREW MADE AN UNSCHEDULED LANDING WITHOUT INCIDE - [SDR UHLA2015041000246](https://openairdocs.org/sdr/UHLA2015041000246), Apr 10, 2015: WIRE HARNESS. DAMAGED. THE CREW REPORTED THAT THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG WIRE HARNES - [SDR UHLA2015040600238](https://openairdocs.org/sdr/UHLA2015040600238), Apr 6, 2015: WIRE HARNESS. DAMAGED. THE CREW REPORTED THAT THEY RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANC - [SDR UHLA2015022300130](https://openairdocs.org/sdr/UHLA2015022300130), Feb 23, 2015: FRAME. DENTED. DURING INSPECTION, A DENT WAS FOUND ON FRAME 62 AT STRINGER 16R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-04. - [SDR UHLA2015021900131](https://openairdocs.org/sdr/UHLA2015021900131), Feb 19, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD STRINGER BEAM. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141209351](https://openairdocs.org/sdr/CHQA20141209351), Dec 9, 2014: SEAL. DIRTY. THE CREW REPORTED THAT DURING FLIGHT THE CAPTAIN'S DIRECT VISION WINDOW WAS LEAKING. THE ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. INSPECTED THE WINDOW - [SDR CHQA20140226070](https://openairdocs.org/sdr/CHQA20140226070), Feb 26, 2014: DOWNLOCK BRACKET. BROKEN. CREW REPORTED THAT DURING CLIMB THE LG WOULD NOT RETRACT & A LG AIR & GND FAIL MSG APPEARED. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED T - [SDR CHQA20131209464](https://openairdocs.org/sdr/CHQA20131209464), Dec 9, 2013: FITTING. CORRODED. CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 & STRINGER 21R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131207465](https://openairdocs.org/sdr/CHQA20131207465), Dec 7, 2013: FRAME. DENTED. FRAME 72 WAS FOUND TO BE DENTED AT STRINGER 16R. THE FRAME WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20131207463](https://openairdocs.org/sdr/CHQA20131207463), Dec 7, 2013: THRESHOLD. CORRODED. CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT LOWER BEAM. THE THRESHOLD PLATE WAS REPAIRED IAW SRM 53-21-02. - [SDR CHQA20131207462](https://openairdocs.org/sdr/CHQA20131207462), Dec 7, 2013: FITTING. CRACKED. A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16R & 15R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131207461](https://openairdocs.org/sdr/CHQA20131207461), Dec 7, 2013: FITTING. CRACKED. A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R & 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20120909309](https://openairdocs.org/sdr/CHQA20120909309), Sep 9, 2012: INVERTER. INOPERATIVE. DURING INSPECTION, THE CENTER CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 6 DC TO AC INVERTER. OPERATIONAL CHECKS WERE - [SDR CHQA20120803231](https://openairdocs.org/sdr/CHQA20120803231), Aug 3, 2012: BATTERY. DISCHARGED. CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPED AND THE FORWARD HALF OF THE EMERGENCY LIGHTS WERE ON AND THE BA - [SDR CHQA20120729227](https://openairdocs.org/sdr/CHQA20120729227), Jul 29, 2012: SWITCH. INOPERATIVE. CREW REPORTED THAT THE EMERGENCY LIGHTS WERE TURNED ON AND WOULD NOT TURN OFF WHILE ON THE GROUND. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY LIGHT SWITCH. - [SDR CHQA20120223063](https://openairdocs.org/sdr/CHQA20120223063), Feb 23, 2012: BATTERY. FAILED. DURING INSPECTION, THE NUMBER 4 EMERGENCY BATTERY FAILED ITS OPERATIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOO - [SDR CHQA20120217053](https://openairdocs.org/sdr/CHQA20120217053), Feb 17, 2012: BATTERY. FAULTY. CREW REPORTED THAT THE EMERGENCY LIGHTS STAYED ON WHEN NOT COMMANDED TO BE ON. MAINTENANCE REPLACED THE NUMBER THREE BATTERY. OPERATIONAL CHECKS WERE GOOD WITH - [SDR CHQA201200035](https://openairdocs.org/sdr/CHQA201200035), Jan 29, 2012: CONDITIONER. FAULTY. CREW REPORTED THAT UPON LANDING, THERE WAS NO BRAKING FROM EITHER THE CAPTAIN'S OR FIRST OFFICER'S BRAKE PEDALS. THE AIRCRAFT WAS SLOWED WITH USE OF THE THRUST - [SDR CHQA201100388](https://openairdocs.org/sdr/CHQA201100388), Sep 26, 2011: ENGINE. SMOKE. AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE INDICATION ON EICAS. F/A VERIFIED SMOKE COMING FROM LAVATORY. RETURNED AND LANDED WITHOUT INCIDENT. FIRE DEPT. INFRARED - [SDR CHQA201100228](https://openairdocs.org/sdr/CHQA201100228), Jun 21, 2011: SPLICE. BROKEN. DURING INSPECTION THE AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN SPLICE. MAINTENANCE REPLACED THE SPLICE WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100127](https://openairdocs.org/sdr/CHQA201100127), Apr 3, 2011: BRAKE SYS. MALFUNCTIONED. CREW REPORTED THAT DURING THE LANDING ROLL OUT, THE BRAKES INITIALLY WORKED NORMALLY, BUT WHILE DECELERATING FROM 90KTS TO 50KTS, THE BRAKES WERE INEFFECTIVE. R - [SDR CHQA201000227](https://openairdocs.org/sdr/CHQA201000227), Dec 12, 2010: PRESSURE SWITCH. INOPERATIVE. DURING CLIMBOUT, THE CREW REPORTED AN E2 ANTI-ICE VALVE FAIL MESSAGE ON EICAS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE E2 A - [SDR CHQA200900208](https://openairdocs.org/sdr/CHQA200900208), Sep 24, 2009: O-RING. DAMAGED. FLIGHT 5516, ATL TO CLE. AIRCRAFT RETURNED TO FIELD DUE TO A BLEED 1 LEAK MESSAGE ON EICAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A DAMAGED O-RING IN TH - [SDR CHQA200900139](https://openairdocs.org/sdr/CHQA200900139), Jun 11, 2009: RELAY. FAULTY. FLIGHT 5876, CLE TO LGA. DURING CLIMBOUT THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. NO VISIBLE SMOKE WAS REPORTED. THE AIRCRAFT RETURNE - [SDR CHQA200900039](https://openairdocs.org/sdr/CHQA200900039), Jan 30, 2009: BALLAST. INOPERATIVE. DURING INSPECTION THE MAIN DOOR EXIT SIGN WAS FOUND TO BE INOP. THE NR 1 EMERGENCY LIGHT BALLAST WAS REPLACED AND THE LIGHT OPERATED NORMALLY. - [SDR CHQA200900021](https://openairdocs.org/sdr/CHQA200900021), Jan 17, 2009: BATTERY PACK. INOPERATIVE. DURING INSPECTION THE FORWARD EMERGENCY LIGHT ON THE OVERWING EXIT CEILING PANEL WAS FOUND TO BE INOPERATIVE ALONG WITH THE EMERGENCY LIGHTS AT THE LEFT AND RIG - [SDR CHQA200800241](https://openairdocs.org/sdr/CHQA200800241), Dec 8, 2008: INVERTER. INOPERATIVE. EMERGENCY FLOOR STRIP LIGHTS 2 AND 3 WERE INOPERATIVE DURING TEST. THE NR 3 INVERTER WAS REPLACED IAW EMB 145 AMM 33-50-11 AND THE SYSTEMS CHECKED OPERATIONAL. - [SDR CHQA200800150](https://openairdocs.org/sdr/CHQA200800150), Jul 17, 2008: HOSE. CHAFED. FLIGHT 5923, GSO TO CLE. ON DESCENT INTO CLE, THE FLIGHT CREW RECEIVED AN E1 HYD PUMP FAIL MESSAGE. THE QRH WAS FOLLOWED AND IT WAS DETERMINED THAT THERE WAS NO - [SDR CHQA200800080](https://openairdocs.org/sdr/CHQA200800080), Apr 19, 2008: PUMP. OVERHEATED. FLIGHT 5901, CLE TO MSY - WHILE CRUISING AT FL360 THE FLIGHT CREW RECEIVED A MASTER CAUTION AND EICAS MESSAGE FOR HYD SYS 1 OVHT. THE CREW RAN THROUGH THE APPRO - [SDR CHQA200600101](https://openairdocs.org/sdr/CHQA200600101), Aug 18, 2006: BATTERY. INOPERATIVE. NR 2 AND NR 3 EMERGENCY STRIP AND AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB 145 MM 33-50-04. OPS CHECK GOOD A - [SDR CHQA200600102](https://openairdocs.org/sdr/CHQA200600102), Aug 18, 2006: BATTERY. INOPERATIVE. LEFT HAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY IAW EMB 145 MM 33-50-04. - [SDR CHQA200600019](https://openairdocs.org/sdr/CHQA200600019), Jan 28, 2006: SIGN. INOPERATIVE. FOUND FORWARD CABIN EXIT SIGN SERVICE DOOR OVERHEAD INOPERATIVE. REMOVED AND REPLACED SIGN IAW EMB 145 MM 33-50-15. - [SDR CHQA200400551](https://openairdocs.org/sdr/CHQA200400551), Sep 4, 2004: BATTERY PACK. DISCHARGED. BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. ## 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 20110926021309I](https://openairdocs.org/incident/20110926021309I), Sep 26, 2011: Embraer EMB-145LR (N287SK), Windsor Locks, CT, No damage. After takeoff from bdl at an altitude of 200 feet, several passengers in the aft cabin area yelled "smoke; smoke". The flight attendant noted a concentration… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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