# N285SK: 2001 Embraer EMB-145LR, registration cancelled 2018-08-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 30, 2018 - Exported to: Bahamas - 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: 145435 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 24, 2001 - Certificate issued: August 28, 2018 - Last registry action: August 28, 2018 - Mode S code: A2E228 - Owner when cancelled: [Avtran LLC](https://openairdocs.org/faa-owner/AVTRAN%20LLC) - Location: [St Louis, MO](https://openairdocs.org/faa-place/MO/St%20Louis) - Owner type: Corporation - Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N285SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=285SK - Page: https://openairdocs.org/deregistered/N285SK-2018-08-30 From the FAA registry file of October 31, 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140203039](https://openairdocs.org/sdr/CHQA20140203039), Feb 3, 2014: SWITCH. FAULTY. CREW REPORTED THAT THEY RECEIVED A BLEED 1 VLV CLOSED MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD & AND LANDED WITHOUT INCIDENT. REPLACED THE BLEED 1 PUSH - [SDR CHQA20131219458](https://openairdocs.org/sdr/CHQA20131219458), Dec 20, 2013: LIGHT. ODOR. CREW REPORTED ELECTRICAL SMELL FROM ROW 7. MX TROUBLE SHOT THE ISSUES TO THE CEILING LIGHT AT ROW 7A. THE LIGHT IS CURRENTLY ON DEFERRAL & THE FINAL CORRECTIVE - [SDR CHQA20130702254](https://openairdocs.org/sdr/CHQA20130702254), Jul 2, 2013: BATTERY. INOPERATIVE. DURING INSPECTION, NR 4 AND 5 EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. MX REPLACED EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD. - [SDR CHQA20130224062](https://openairdocs.org/sdr/CHQA20130224062), Feb 24, 2013: TRANSDUCER. FAILED. CREW REPORTED A NR 1 ENGINE ANTI-ICE VALVE FAIL MESSAGE IN FLIGHT. DIVERTED TO AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ANTI-ICING PRESSURE TRANSDUCER. - [SDR CHQA20130202056](https://openairdocs.org/sdr/CHQA20130202056), Feb 2, 2013: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE THE SKIN BETWEEN FRAMES 38 AND 39 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145 - [SDR CHQA20130202055](https://openairdocs.org/sdr/CHQA20130202055), Feb 2, 2013: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 60 BETWEEN STRINGERS 19R AND 20R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130202054](https://openairdocs.org/sdr/CHQA20130202054), Feb 2, 2013: SKIN. CHAFED. DURING INSPECTION, THE PASSENGER DOOR CUTOUT INTERNAL SKIN WAS CHAFED AT THE LOWER HOLE FOR THE LEFT COCKPIT BULKHEAD. THE SKIN WAS REPAIRED IN ACCORDANCE WITH - [SDR CHQA20130201053](https://openairdocs.org/sdr/CHQA20130201053), Feb 1, 2013: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48. THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48 WAS REPLACED IN A - [SDR CHQA20130201052](https://openairdocs.org/sdr/CHQA20130201052), Feb 1, 2013: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SILL FROM FRAME 23 TO FRAME 29. THE LEFT OUTBOARD SILL AT FROM FRAME 23 TO FRAME 29 WAS REPLACED IN - [SDR CHQA20130112013](https://openairdocs.org/sdr/CHQA20130112013), Jan 12, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE AFT FLOOR PROXIMITY LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE - [SDR CHQA20130112012](https://openairdocs.org/sdr/CHQA20130112012), Jan 12, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE FLOOR PROXIMITY LIGHT STRIP FORWARD OF THE EMERGENCY EXIT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY - [SDR CHQA20120427133](https://openairdocs.org/sdr/CHQA20120427133), Apr 27, 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 CHQA20120131045](https://openairdocs.org/sdr/CHQA20120131045), Jan 31, 2012: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER BEAM ON THE CARGO DOOR SURROUND STRUCTURE. MAINTENANCE REPLACED THE LOWER BEAM ON THE CARGO DOOR SURROUND ST - [SDR CHQA20120131044](https://openairdocs.org/sdr/CHQA20120131044), Jan 31, 2012: ANGLE. CRACKED. DURING INSPECTION, THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS FOUND TO BE CRACKED AT FRAME 46. THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS REPAIRED IN ACCORDANCE WITH - [SDR CHQA201200038](https://openairdocs.org/sdr/CHQA201200038), Jan 31, 2012: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE AT FRAME 65. THE AIRCRAFT IS CURRENTLY IN C-CHECKS AND A FINAL CORRECTIVE ACTION WIL - [SDR CHQA201100453](https://openairdocs.org/sdr/CHQA201100453), Nov 17, 2011: SWITCH. FAULTY. CREW REPORTED THAT THEY RECEIVED A BLEED 1 VALVE FAIL MESSAGE DURING FLIGHT. THEY FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE VALVE WOULD NOT REOPEN. THEY RET - [SDR CHQA201100302](https://openairdocs.org/sdr/CHQA201100302), Jul 28, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER FOUR EMERGENCY BATTERY. OPERATIONAL CHEC - [SDR CHQA201100247](https://openairdocs.org/sdr/CHQA201100247), Jun 25, 2011: YAW DAMPER. MALFUNCTIONED. CREW REPORTED DURING CLIMB RECEIVED A RUDDER 1 AND 2 INOPERATIVE MESSAGE, FOLLOWED BY A YAW DAMPER AND AUTOPILOT FAIL MESSAGE ON THE EICAS. RETURNED TO KRDU AND - [SDR CHQA201100226](https://openairdocs.org/sdr/CHQA201100226), Jun 18, 2011: WINDSHIELD. UNDERTORQUED. WHILE EN ROUTE TO MSY, THE CREW REPORTED A LOUD POP FOLLOWED BY AN EXTREMELY LOUD SQUEALING NOISE. THE CREW WAS NOT COMFORTABLE WITH CONTINUING DUE TO THE NOISE - [SDR CHQA201100044](https://openairdocs.org/sdr/CHQA201100044), Feb 24, 2011: BATTERY PACK. INOPERATIVE. FLT 5045, DURING INSPECTION, BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 BATTERY POWER SUPPLY. - [SDR CHQA201100043](https://openairdocs.org/sdr/CHQA201100043), Feb 24, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXIT ROW EMERGENCY LIGHT. OPERATIONAL CHECKS W - [SDR CHQA201100039](https://openairdocs.org/sdr/CHQA201100039), Feb 18, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE NR 4 PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 PROXIMITY LIGHT STRIP AND OPERATIONAL CHECKS WERE G - [SDR CHQA201100038](https://openairdocs.org/sdr/CHQA201100038), Feb 18, 2011: CONNECTOR. BROKEN. DURING INSPECTION THE NR 1 EMERGENCY LIGHT PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE REMOVABLE SPLICE CONNECTOR ON THE NR 1 FLOOR PR - [SDR CHQA201000212](https://openairdocs.org/sdr/CHQA201000212), Nov 23, 2010: LIGHT. INOPERATIVE. DURING INSPECTION THE EMERGENCY FLOOR PROXIMITY LIGHT INOP BETWEEN ROWS 3 AND 7. MAINTENANCE REPLACED THE EMERGENCY LIGHT AND THE NR 3 STATIC INVERTER WITH NO F - [SDR CHQA201000203](https://openairdocs.org/sdr/CHQA201000203), Oct 22, 2010: WIRE. BROKEN. DURING INSPECTION THE AFT EMERGENCY FLOOR PROXIMITY LIGHT WAS FOUND TO HAVE A BROKEN WIRE. THE LIGHT WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000120](https://openairdocs.org/sdr/CHQA201000120), Jun 11, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE BULBS FOR BOTH LIGHTS WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900254](https://openairdocs.org/sdr/CHQA200900254), Dec 3, 2009: INVERTER. INOPERATIVE. DURING INSPECTION, MAINTENANCE FOUND THE FLIGHT ATTENDANT'S EMERGENCY EXIT LIGHT INOP. THE NR 1 INVERTER WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. - [SDR CHQA200900252](https://openairdocs.org/sdr/CHQA200900252), Nov 29, 2009: SEAL. DETACHED. AT APPROXIMATELY FL160 THE FLIGHT CREW REPORTED A SQUEAL FROM THE FIRST OFFICER'S DV WINDOW SEAL. AS THE AIRCRAFT CLIMBED THE SQUEAL BECAME WORSE AND THE FLIGHT - [SDR CHQA200900218](https://openairdocs.org/sdr/CHQA200900218), Oct 10, 2009: SOCKET. DIRTY. DURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP. THE LEFT EMERGENCY LIGHT SOCKET WAS FOUND DIRTY AND WAS CLEANED. THE LEFT OVERWING EMERGENCY - [SDR CHQA200900111](https://openairdocs.org/sdr/CHQA200900111), Apr 17, 2009: BATTERY PACK. INOPERATIVE. DURING INSPECTION BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY BATTERY PACK WAS REPLACED AND THE EMERGENCY LIGHTS - [SDR CHQA200800088](https://openairdocs.org/sdr/CHQA200800088), Apr 28, 2008: PROXIMITY SENSOR. DIRTY. FLIGHT 5809 CLE TO DCA - DURING TAKEOFF ROLL, THE FLIGHT CREW RECEIVED A MASTER WARNING FOR A SPOILER TAKEOFF CONFIGURATION MESSAGE ON THE EICAS. AT THAT TIME T - [SDR CHQA200800074](https://openairdocs.org/sdr/CHQA200800074), Apr 10, 2008: WINDSHIELD. CRACKED. FLIGHT 5801, BDL TO CLE - IN CRUISE AT FL240, WITH WINDSHIELD HEAT ON, THE CREW HEARD A LOUD POP AND NOTICED THAT THE CAPTAIN'S WINDSHIELD HAD SHATTERED (SPIDER - [SDR CHQA200700089](https://openairdocs.org/sdr/CHQA200700089), Dec 4, 2007: ENGINE. LEAKING. RDU TO CLE - AFTER TAKEOFF WHILE CLIMBING THROUGH 1,500FT, THE CREW RECEIVED A LAV SMOKE EICAS INDICATION. THE CREW PERFORMED THE CHECKLIST ITEMS FOR LAVATORY S - [SDR CHQA200700088](https://openairdocs.org/sdr/CHQA200700088), Dec 4, 2007: SMOKE DETECTOR. DIRTY. RDU TO CLE - AFTER TAKEOFF AT 1,500FT, THE CREW RECEIVED A LAV SMOKE EICAS MESSAGE. THE CREW PERFORMED THE CHECKLIST ITEMS FOR LAVATORY SMOKE AND PREPARED FOR A - [SDR CHQA200500127](https://openairdocs.org/sdr/CHQA200500127), Jul 18, 2005: BULB. BURNED OUT. RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-07-4. OPS CHECK GOOD. - [SDR CHQA200500017](https://openairdocs.org/sdr/CHQA200500017), Jan 25, 2005: SIGN. INOPERATIVE. FORWARD EMERGENCY LIGHTED EXIT SIGN IS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTED SIGN IAW EMB 145 AMM 33-50-14-4. OPS CHECK GOOD. - [SDR CHQA000528](https://openairdocs.org/sdr/CHQA000528), Jul 20, 2004: FILLER. MISSING. EMERGENCY FLOOR PROXIMITY LIGHTS STRIPS ARE MISSING FILLER STRIPS. INSTALLED FLOOR PROXIMITY FILLER STRIPS IAW AMM 33-50-12. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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