# N17928: 1996 Embraer EMB-145EP, registration cancelled 2016-02-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 12, 2016 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145EP](https://openairdocs.org/model/embraer-emb-145ep) (registry code 3260221) - Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145.007 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: August 19, 2015 - Last registry action: August 19, 2015 - Mode S code: A13D5B - Owner when cancelled: [Erj-145-007 LLC](https://openairdocs.org/faa-owner/ERJ-145-007%20LLC) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7965° N, 75.6128° W: Placed by OpenAirDocs at the center of ZIP code 19807, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N17928 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17928 - Page: https://openairdocs.org/deregistered/N17928-2016-02-12 From the FAA registry file of November 12, 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-145EP: https://openairdocs.org/model/embraer-emb-145ep.md ## Service difficulty reports (118, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20140710094](https://openairdocs.org/sdr/ASOA20140710094), Jul 10, 2014: INVERTER. INOPERATIVE. DURING PREFLIGHT, THE CREW REPORTED THAT 2 SECTIONS OF AISLE PATH EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT INVERTER, - [SDR ASOA20140315044](https://openairdocs.org/sdr/ASOA20140315044), Mar 15, 2014: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHT AT ROW 18 WAS FOUND TO BE INOPERATIVE. MAINTENNACE R & R BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND T - [SDR ASOA20140203018](https://openairdocs.org/sdr/ASOA20140203018), Feb 3, 2014: INVERTER. INOPERATIVE. DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE FORWARD BULKHEAD WAS NOT WORKING. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT INVERTER - [SDR ASOA20131217222](https://openairdocs.org/sdr/ASOA20131217222), Dec 17, 2013: ACM. FAILED. THE CREW REPORTED A STRONG ELECTRICAL ODOR AS NR 1 PACK WAS RUNNING, AND ODOR STOPPED WHEN NR 1 PACK TURNED OFF. ACFT LANDED WITHOUT INCIDENT. MAINTENNACE INSPE - [SDR ASOA20131125447](https://openairdocs.org/sdr/ASOA20131125447), Nov 25, 2013: BRACKET. WORN. AIRCRAFT IS IN C-CHECK WHEN INSPECTION FOUND THE RT GROUND SPOILER INBD HINGE FITTING AT THE WING SPAR AREA INBD/OTBD BUSHIONS MIGRATED AND OBLONG THE FITTING. - [SDR ASOA20130611087](https://openairdocs.org/sdr/ASOA20130611087), Jun 11, 2013: BATTERY PACK. DISCHARGED. DURING MX INSPECTION THE AISLE PATH LIGHTING AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED W - [SDR ASOA20130209009H](https://openairdocs.org/sdr/ASOA20130209009H), Feb 9, 2013: LIGHT. INOPERATIVE. DURING SCHEDULED MX, THE PASSENGER DOOR BOTTOM EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYS AND CL - [SDR ASOA20121210156](https://openairdocs.org/sdr/ASOA20121210156), Dec 10, 2012: FIREWALL. CRACKED. DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED APPROXIMATELY 1.25" TOTAL LENGTH AT THE 9 O'CLOCK POSITION WITH A RIVET IN THE MIDDLE. MA - [SDR ASOA20121208155](https://openairdocs.org/sdr/ASOA20121208155), Dec 8, 2012: SKIN. CRACKED. SUPPLEMENTAL, DURING A-CHECK INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 5 SEPARATE CRACKS AT 3 DIFFERENT RIVETS AT FRAME 75. THESE INCLUDE 2 CRACKS M - [SDR ASOA20121127143](https://openairdocs.org/sdr/ASOA20121127143), Nov 27, 2012: LIGHT. UNSECURE. DURING A-CHECK INSPECTION, THE PAX DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX RESECURED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE - [SDR ASOA20120304030H](https://openairdocs.org/sdr/ASOA20120304030H), Mar 4, 2012: RELAY. BURNED. DURING PREFLIGHT, THE CREW REPORTED A BURNING ODOR FROM THE COAT CLOSET. MX INSPECTED THE ACFT AND R & R RELAY K0454, OPERATIONALLY TESTED WITH NO DEFECTS, AND - [SDR ASOA20111202008](https://openairdocs.org/sdr/ASOA20111202008), Dec 2, 2011: ACTUATOR. WEAK. DURING CLIMB THE CREW REPORTED THAT THE RIGHT MLG WOULD NOT LOCK IN THE UP POSITION. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACE - [SDR C2XA11SH125](https://openairdocs.org/sdr/C2XA11SH125), Aug 29, 2011: DOOR FRAME. CORRODED. SHV - DURING C-CHECK THE BOTTOM FRAME OF THE MAIN CABIN DOOR WAS FOUND TO BE CORRODED AROUND THE DOOR LINING MOUNT NUT PLATES. MAINTNENANCE REMOVED THE CORROSIO - [SDR C2XA11IA159](https://openairdocs.org/sdr/C2XA11IA159), Jul 21, 2011: ELECTRONIC UNIT. INOPERATIVE. IAH - FLIGHT 2705 THE CREW REPORTED AN AIR/GRND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE - [SDR C2XA11IA158](https://openairdocs.org/sdr/C2XA11IA158), Jul 19, 2011: WIRE HARNESS. BURNED. DURING MAINTENANCE INSPECTION, AN ELECTRICAL ODOR WAS NOTICED IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIDEWALL LIGHT HARNESS AT SEAT 10BC - [SDR C2XA11IA019](https://openairdocs.org/sdr/C2XA11IA019), Jan 19, 2011: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IN THE AFFECT - [SDR C2XA10IA285](https://openairdocs.org/sdr/C2XA10IA285), Nov 8, 2010: ENGINE. ODOR. FLIGHT 2719, REPORTED A PROMINENT TURBINE CASE OIL BURNED ODOR DURING ALL PHASES OF FLT. ACFT LANDED WHERE MX INSPECTED AND PLACED NR 1 PACK ON MEL, AND AIRCRAF - [SDR C2XA10IA213](https://openairdocs.org/sdr/C2XA10IA213), Jul 28, 2010: BATTERY. OVERTEMP. IAH - FLIGHT 2163, THE CREW REPORTED A MAIN BATTERY TWO OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTER, OPERATIONALLY TESTED WITH NO DEFE - [SDR C2XA10IA165](https://openairdocs.org/sdr/C2XA10IA165), Jun 1, 2010: SKIN. CORRODED. IAH - DURING MAINTENANCE INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 72 & 73 AT STRINGER 21R. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA10IA143](https://openairdocs.org/sdr/C2XA10IA143), May 9, 2010: SKIN. CRACKED. IAH - DURING MAINTENANCE INSPECTION THE LEFT UPPER WING SKIN WAS FOUND TOP BE CRACKED AT THE SPEED BRAKE CENTER HINGE POINT CUTOUT. MAINTENANCE PLACED THE ITEM - [SDR C2XA09IA331](https://openairdocs.org/sdr/C2XA09IA331), Dec 29, 2009: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT TOP LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INV - [SDR C2XA09IA181](https://openairdocs.org/sdr/C2XA09IA181), Jul 17, 2009: LIGHT. INOPERATIVE. DURING ROUTINE INSP, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, - [SDR C2XA09CL051](https://openairdocs.org/sdr/C2XA09CL051), Apr 25, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASO - [SDR C2XA08IA152](https://openairdocs.org/sdr/C2XA08IA152), Jul 5, 2008: LIGHT. INOPERATIVE. IAH - DURING A-CK INSPECTION THE LT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSY, OPERATIONALLY TESTED W - [SDR C2XA08CL063](https://openairdocs.org/sdr/C2XA08CL063), May 29, 2008: BALLAST. FAULTY. CLE FLIGHT NR 2401, THE CREW REPORTED A STRONG BURNING SMELL COMING FROM THE LAVATORY. MAINTENANCE INSPECTED AND REPLACED THE LAV LIGHT BALLAST. - [SDR C2XA07CL074](https://openairdocs.org/sdr/C2XA07CL074), Sep 4, 2007: WIRE. LOOSE. DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED THE WIRE AT THE EXIT LIGHT. OPERATIONAL C - [SDR C2XA07CL033](https://openairdocs.org/sdr/C2XA07CL033), Mar 18, 2007: COFFEEMAKER. SMOKE. CMH FLIGHT 2930 THE CREW REPORTED THE COFFEE POT WAS SMOKING WHEN TURNED ON.THE COFFEE POT WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENA - [SDR C2XA07CL010](https://openairdocs.org/sdr/C2XA07CL010), Jan 22, 2007: CONTROLLER. BURNED. CLE FLIGHT NR 2676, THE CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN DURING ICE CONDITIONS THROUGHOUT DESCENT. MAINTENANCE INSPECTED AND FOUND THE TERM - [SDR C2XA06SH129](https://openairdocs.org/sdr/C2XA06SH129), Nov 14, 2006: FLOORBEAM. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIR - [SDR C2XA06SH130](https://openairdocs.org/sdr/C2XA06SH130), Nov 11, 2006: FRAME. CORRODED. SHV - DURING C-CHECK THE SERVICE DOOR AFT FRAME 22 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLE, BETWEEN STR 15R AND 16R. MAINTENANCE REMOVED THE DAMAGED - [SDR C2XA06CL078](https://openairdocs.org/sdr/C2XA06CL078), Sep 25, 2006: BATTERY. INOPERATIVE. DURING ROUTINE MAINTENANCE THE LT FRONT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR1 EMERGENCY BATTERY POWER SUPPLY. OPERAT - [SDR C2XA06CL074](https://openairdocs.org/sdr/C2XA06CL074), Sep 18, 2006: LIGHT. FAULTY. DURING ROUTINE MAINTENANCE THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE G - [SDR C2XA06CL051](https://openairdocs.org/sdr/C2XA06CL051), May 18, 2006: BALLAST. BURNED. CLE FLIGHT 3156 THE CREW REPORTED A ELECTRICAL BURNING SMELL IN THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BALLAST AT ROW 18. OPERAT - [SDR C2XA06IA057](https://openairdocs.org/sdr/C2XA06IA057), Apr 13, 2006: LIGHT. INOPERATIVE. IAH - DURING 3A INSPECTION THE RIGHT HAND INTERIOR EMERGENCY EXIT LIGHT BY THE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSE - [SDR C2XA05TY013](https://openairdocs.org/sdr/C2XA05TY013), Feb 7, 2005: RIVET. LOOSE. TYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRI - [SDR C2XA05TY010](https://openairdocs.org/sdr/C2XA05TY010), Feb 3, 2005: SPAR. CRACKED. TYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRC - [SDR C2XA04CL129](https://openairdocs.org/sdr/C2XA04CL129), Dec 22, 2004: SWITCH. FAULTY. CLE - THE CREW REPORTED IN FLIGHT, IN ICING HAD A VERY HOT RUBBER SMELL AND PACK 2 AIR WAS VERY HOT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PACK DUCT OVERT - [SDR C2XA04CL122](https://openairdocs.org/sdr/C2XA04CL122), Dec 1, 2004: NOISE ATTENUATOR. RUPTURED. DURING APPROACH THE CREW REPORTED A BURNING PLASTIC SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUPTURED NR 2 RECIRCULATION FAN NOISE ATTENUATOR. - [SDR C2XA04CL114](https://openairdocs.org/sdr/C2XA04CL114), Nov 7, 2004: SMOKE. DETECTED. CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF THE APU AND ENGINES WITH THE BLEED AND PACKS ON. NO DEFECTS NOTED. - [SDR C2XA04TY142](https://openairdocs.org/sdr/C2XA04TY142), Aug 3, 2004: FLOOR SUPPORT. CORRODED. TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FL - [SDR C2XA04TY132](https://openairdocs.org/sdr/C2XA04TY132), Aug 2, 2004: SUPPORT. CORRODED. DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM - [SDR C2XA04TY134](https://openairdocs.org/sdr/C2XA04TY134), Aug 2, 2004: CHANNEL. CORRODED. DURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPLACED THE STEP UP BRACKET AND CENTER OMEGA - [SDR C2XA04TY135](https://openairdocs.org/sdr/C2XA04TY135), Aug 2, 2004: SILL. CORRODED. DURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTERSUNK FLOOR SILL ALLODINED AND INSTALL IA - [SDR C2XA04TY130](https://openairdocs.org/sdr/C2XA04TY130), Aug 2, 2004: SUPPORT BEAM. CORRODED. DURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT. REMOVED AND REPLACED ALL TOP CAPS IN T - [SDR C2XA04TY133](https://openairdocs.org/sdr/C2XA04TY133), Aug 2, 2004: FLOORBEAM. CORRODED. TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 S - [SDR C2XA04TY131](https://openairdocs.org/sdr/C2XA04TY131), Aug 2, 2004: FLOOR SUPPORT. CORRODED. TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FR 25. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FR 22 AND FR 25. ALL W - [SDR C2XA04TY128](https://openairdocs.org/sdr/C2XA04TY128), Aug 2, 2004: SILL. CORRODED. TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FLOORBOARD SILL ON THE LT SIDE AT FR 53-58. REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/14 - [SDR C2XA04TY139](https://openairdocs.org/sdr/C2XA04TY139), Jul 31, 2004: FLOOR SUPPORT. CORRODED. TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 23 TO 30. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FL - [SDR C2XA04TY138](https://openairdocs.org/sdr/C2XA04TY138), Jul 31, 2004: FLOOR SUPPORT. CORRODED. TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 61 TO FRAME 65. MAINTENANCE REMOVED AND REPLACED THE FLOOR - [SDR C2XA04TY120](https://openairdocs.org/sdr/C2XA04TY120), Jul 26, 2004: SUPPORT. CORRODED. DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM All 118: https://openairdocs.org/deregistered/N17928-2016-02-12/reports.md ## Other aircraft with N17928 - [Cancelled 1951-04-24](https://openairdocs.org/deregistered/N17928-1951-04-24): Piper J-2, S/N 1528. Owner: [Smith W A Ed Dozier & A P Dauvin](https://openairdocs.org/faa-owner/SMITH%20W%20A%20ED%20DOZIER%20%26%20A%20P%20DAUVIN), [Bessemer, AL](https://openairdocs.org/faa-place/AL/Bessemer) --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.