# N14959: 1998 Embraer EMB-145LR, registration cancelled 2023-03-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 3, 2023 - Status when cancelled: Registration expired, pending cancellation - 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: 145091 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 6, 1998 - Certificate issued: September 16, 2019 - Last registry action: September 16, 2019 - Mode S code: A0C748 - Owner when cancelled: [Aerovision Aircraft Services LLC](https://openairdocs.org/faa-owner/AEROVISION%20AIRCRAFT%20SERVICES%20LLC) - Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon) - Owner type: LLC - Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14959 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14959 - Page: https://openairdocs.org/deregistered/N14959-2023-03-03 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 (109, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141202146](https://openairdocs.org/sdr/ASOA20141202146), Dec 4, 2014: RETAINER. CORRODED. THE CREW REPORTED THAT THE GALLEY DOOR SEAL SQUEELS AND SHOWS SIGNS OF LEAKING ON THE UPPER SIDE OF THE DOOR. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE - [SDR ASOA20140519086](https://openairdocs.org/sdr/ASOA20140519086), May 19, 2014: CONNECTOR. DIRTY. ACFT HAD MULTIPLE EICIAC MESSAGES THAT THE E2 FIRE DETECT FAIL. ACFT LANDED WITHOUT ISSUE AND MAINTENANCE REMOVED AND REINSTALLED FIRE DETECT PANEL TO FACILITAT - [SDR ASOA20140131016](https://openairdocs.org/sdr/ASOA20140131016), Jan 31, 2014: ACM. INOPERATIVE. DURING FLIGHT, CREW REPORTED SMOKE IN COCKPIT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R THE NR 2 ACM, OPS TESTED WITH NO DEFECTS, AND THE A - [SDR ASOA20130725196](https://openairdocs.org/sdr/ASOA20130725196), Jul 25, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS AP - [SDR ASOA20130725195V](https://openairdocs.org/sdr/ASOA20130725195V), Jul 25, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS AP - [SDR ASOA20130725194V](https://openairdocs.org/sdr/ASOA20130725194V), Jul 25, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01821. THE ACFT WAS AP - [SDR ASOA20130725193](https://openairdocs.org/sdr/ASOA20130725193), Jul 25, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE ACFT WAS AP - [SDR ASOA20130719192V](https://openairdocs.org/sdr/ASOA20130719192V), Jul 19, 2013: FIREWALL. CRACKED. DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 75A AND STRINGER 12R. MX PERFORMED A DOUBLER REPAIR IAW EC5330-02578. THE ACFT WAS APPROVED FOR - [SDR ASOA20130719191](https://openairdocs.org/sdr/ASOA20130719191), Jul 19, 2013: SKIN. CORRODED. DURING C-CHECK THE CARGO DOOR INTERNAL LOWER SKIN WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE ACFT W - [SDR ASOA20130719190](https://openairdocs.org/sdr/ASOA20130719190), Jul 19, 2013: FRAME. CORRODED. DURING C-CHECK THE LT AND RT CABIN ESCAPE HATCH DOOR BOTTOM FRAMES WERE FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5220- - [SDR ASOA20130712187](https://openairdocs.org/sdr/ASOA20130712187), Jul 12, 2013: FRAME. DAMAGED. DURING C-CHECK THE LT FRAME 10 SEGMENT BETWEEN STRINGERS 8L-12L WAS FOUND TO HAVE ELONGATED FASTENER HOLES. MX R & R THE FRAME SEGMENT IAW SRM 51-40-02. THE ACF - [SDR ASOA20130712186](https://openairdocs.org/sdr/ASOA20130712186), Jul 12, 2013: SKIN. CORRODED. DURING C-CHECK THE INNER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-15 AND STRINGERS 19L-19R. MX R & R THE SKIN IAW EC5330-02782. THE ACFT WAS APPROVED FOR - [SDR ASOA20130706185](https://openairdocs.org/sdr/ASOA20130706185), Jul 6, 2013: STRINGER. CORRODED. DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130706184](https://openairdocs.org/sdr/ASOA20130706184), Jul 6, 2013: STRINGER. CORRODED. DURING C-CHECK, STRINGER 18R WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-23. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130520049](https://openairdocs.org/sdr/ASOA20130520049), May 20, 2013: WIRE. BROKEN. CREW REPORTED SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MX FOUND A BROKEN WIRE SPLICE AND REPLACED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SE - [SDR ASOA20130131008](https://openairdocs.org/sdr/ASOA20130131008), Jan 31, 2013: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE FLOOR PROXIMITY LIGHT STRIPS NR 4 AND NR 5, AND BOTH LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R T - [SDR ASOA20121229123](https://openairdocs.org/sdr/ASOA20121229123), Dec 29, 2012: LIGHT. INOPERATIVE. THE LT SIDE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT ASSY WITH OPS CHECK SUCCESSFUL. ACFT - [SDR ASOA20120823065](https://openairdocs.org/sdr/ASOA20120823065), Aug 23, 2012: CONTROLLER. FAULTY. CREW REPORTED CABIN ALTITUDE CLIMBED TO 8400 AT FL370 EXCESSIVE CABIN ALTITUDE CLIMB AND DECENT RATES DURING CLIMBS AND DECENTS +1500FPM -1000FPM MANUAL MODE DI - [SDR ASOA20120308026](https://openairdocs.org/sdr/ASOA20120308026), Mar 8, 2012: CHARGER. FAULTY. DURING ROUTINE MX, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND THE RT OVERWING EMERGENCY LIG - [SDR ASOA20120227021](https://openairdocs.org/sdr/ASOA20120227021), Feb 27, 2012: CHARGER. FAULTY. MX REPORTED BOTH AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MX REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD. - [SDR C2XA11CL209](https://openairdocs.org/sdr/C2XA11CL209), Sep 17, 2011: ELECTRONIC UNIT. FAULTY. ORD FLT 6137 THE CREW REPORTED AN AIR GROUND FAIL MESSAGE EVERY TIME THE GEAR WAS LOWERED FOR ABOUT 10 SECONDS. MAINTENANCE INSPECTED AND REPLACED THE LANDING G - [SDR C2XA11SH124](https://openairdocs.org/sdr/C2XA11SH124), Aug 29, 2011: SKIN. CRACKED. SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AT 2 LOCATIONS BETWEEN FRAMES 79-80 AND STRINGERS 5R-7R. MAINTENANCE REAMED OUT THE CRACKS AND PERF - [SDR C2XA11SH123](https://openairdocs.org/sdr/C2XA11SH123), Aug 29, 2011: STRINGER. CRACKED. SHV - DURING C-CHECK STRINGER 2L WAS FOUND TO BE CRACKED AT FRAME 75. MAINTENANCE REMOVED THE CRACKED SEGMENT AND PERFORMED A STRINGER SPLICE REPAIR IAW EC5310- - [SDR C2XA11SH122](https://openairdocs.org/sdr/C2XA11SH122), Aug 29, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 18-23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51- - [SDR C2XA11SH120](https://openairdocs.org/sdr/C2XA11SH120), Aug 24, 2011: SKIN. CRACKED. SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R, EMANATING FROM THE FRAME 75 FITTING. MAINTENANCE PERFORMED A DOUBLE - [SDR C2XA11IA171](https://openairdocs.org/sdr/C2XA11IA171), Jul 31, 2011: FLAPPER VALVE. LEAKING. MKE - FLIGHT 2350, THE CREW REPORTED FLUID LEAKING FROM THE TOP OF THE RIGHT AILERON RIGHT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO MKE WHERE IT LANDED WITHOUT I - [SDR C2XA11060](https://openairdocs.org/sdr/C2XA11060), Apr 8, 2011: FAN. MALFUNCTIONED. FLIGHT 5817 - BUF - FLIGHT CREW REPORTED BURNING ODOR FOR ABOUT 1 MIN IN THE COCKPIT AND FA REPORTED SMOKE IN COCKPIT IN THE BACK HALF OF CABIN. EWR MX REMOVED - [SDR C2XA11CL083](https://openairdocs.org/sdr/C2XA11CL083), Mar 27, 2011: UNKNOWN. SMOKE. ORD FLT 6051 - THE CREW REPORTED WHILE SITTING ON GROUND, PACK 2 WAS SET TO MANUAL MODE TO EXPEDITE COOLING THE CABIN AND COCKPIT FILLED WITH SMOKE. THE APU BLE - [SDR C2XA11IA004](https://openairdocs.org/sdr/C2XA11IA004), Dec 30, 2010: APU. ODOR. FLIGHT 3155 THE CREW REPORTED A FUEL SMELL DURING APU START. MAINTENANCE PLACED THA APU ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/02/11 - [SDR C2XA10CL121](https://openairdocs.org/sdr/C2XA10CL121), Jul 29, 2010: BRAKE. FAULTY. CLE FLT 2243 - THE CREW REPORTED A FLAP FAILURE AFTER TAKEOFF UPON FLAP RETRACTING. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPEC - [SDR C2XA10CL089](https://openairdocs.org/sdr/C2XA10CL089), Jun 11, 2010: SOLENOID VALVE. MALFUNCTIONED. FLT 2267 CREW REPORTED LOUD NOISE FROM NOSE AREA LIKE NOSE GEAR DOORS WERE OPEN. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND - [SDR C2XA10RI062](https://openairdocs.org/sdr/C2XA10RI062), May 14, 2010: RADAR. FAILED. FLIGHT 2417 - EWR - FLIGHT CREW REPORTED WEATHER RADAR FAIL IN FLIGHT DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND R - [SDR C2XA10TY025](https://openairdocs.org/sdr/C2XA10TY025), Feb 8, 2010: VALVE. LEAKING. TYS - AIR RETURN DUE TO FUEL VENTING FROM RT WING. REPLACED RT WING VENT VALVE, LEAK CHECK GOOD. - [SDR C2XA10RI021](https://openairdocs.org/sdr/C2XA10RI021), Feb 4, 2010: CHARGER. INOPERATIVE. FLIGHT 2521 - EWR - FLIGHT CREW REPORTED BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED NR 4 EMERGENCY BATTERY CHARGER ASSY AND PERFORM - [SDR C2XA09SH300](https://openairdocs.org/sdr/C2XA09SH300), Sep 27, 2009: CONTROLLER. MALFUNCTIONED. AUTO PRESSURIZATION FAILED IN FLIGHT. REMOVED AND REPLACED DIGITAL PRESSURE CONTROLLER IAW EMB 145 AMM 21-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09RI103](https://openairdocs.org/sdr/C2XA09RI103), May 16, 2009: MODULE. FAILED. FLIGHT 2345, FLIGHT CREW REPORTED EMERGENCY LIGHTS STAY ON IN OFF POSITION. MX REMOVED AND REPLACED EMERGENCY LIGHT MODULE AND PERFORMED OPS CHECK SUCCESSFULLY. - [SDR C2XA09IA085](https://openairdocs.org/sdr/C2XA09IA085), Mar 21, 2009: CONTROL MODULE. OVERHEATED. IAH - FLIGHT 2057 - DURING TAXI THE CREW REPORTED A BURNING SMELL IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL - [SDR C2XA08RI149](https://openairdocs.org/sdr/C2XA08RI149), Sep 24, 2008: BALLAST. FAULTY. FLT 2325 - EWR - FLT CREW REPORTED BURNING SMELL IN CABIN. EWR MX R&R LIGHT BALLAST AT 5A AND 16A SEAT AREAS. PERFORMED OPS CHECK SUCCESSFULLY. AC WAS APPROVED - [SDR C2XA08CL079](https://openairdocs.org/sdr/C2XA08CL079), Jul 5, 2008: WIRE. LOOSE. DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED WIRE W734-0001-20. OPERATIONAL CHECKS WERE G - [SDR C2XA08CL055](https://openairdocs.org/sdr/C2XA08CL055), May 5, 2008: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA08RI014](https://openairdocs.org/sdr/C2XA08RI014), Jan 8, 2008: LIGHT. INOPERATIVE. RIC - DURING ROUTINE MAINTENANCE, MX FOUND AFT EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL - [SDR C2XA07CL095](https://openairdocs.org/sdr/C2XA07CL095), Nov 7, 2007: SOLENOID VALVE. FAULTY. CLE FLIGHT 3023 - THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE NOSE WHEEL COMPARTMENT. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANC - [SDR C2XA07CL091](https://openairdocs.org/sdr/C2XA07CL091), Oct 25, 2007: TERMINAL BLOCK. SHORTED. CLE FLIGHT 2477 - THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED AND FOUND THE TERMINAL BLOCK MELTED ON THE CAPTAINS WINDSHIELD. - [SDR C2XA07RI092](https://openairdocs.org/sdr/C2XA07RI092), Oct 22, 2007: BALLAST. DEFECTIVE. FLT 2322 - EWR - DURING TAXIING OUT OF THE GATE, CREW REPORTED A BURNING ODOR IN CABIN AND GALLEY AREA. CREW RETURNED TO GATE AND EWR MX FOUND BALLAST IN GALLEY - [SDR C2XA07TY044](https://openairdocs.org/sdr/C2XA07TY044), Aug 17, 2007: ATTACH FITTING. CORRODED. TYS - DURING A CURRENT C-CHECK INSPECTION, THE VERTICAL STAB ATTACH FITTING AT FRAME 75 WAS FOUND FRETTING. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STAB F - [SDR C2XA07IA080](https://openairdocs.org/sdr/C2XA07IA080), Apr 6, 2007: SMOKE DETECTOR. FALSE ACTIVATION. HRL - FLIGHT 3124, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS. THE CREW INSPECTED THE AIRCRAFT AND PLACED THE BAGGAGE SMOKE DETECTOR ON MEL 26-15-00 - [SDR C2XA07RI012](https://openairdocs.org/sdr/C2XA07RI012), Apr 1, 2007: UNKNOWN. ODOR. FLT 2335 - CREW REPORTED BURNING SMELL WHEN ANTI-ICE SYSTEM WAS ON IN ICING. MX RAN BOTH ENGINES, WITH ANTI ICE SYSTEM ON AND COULD NOT DUPLICATE THE SMELL. AC - [SDR C2XA06IA044](https://openairdocs.org/sdr/C2XA06IA044), Mar 21, 2006: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION, THE RIGHT EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INV - [SDR C2XA06IA023](https://openairdocs.org/sdr/C2XA06IA023), Feb 18, 2006: PCU. MALFUNCTIONED. IAH - FLIGHT 2840, THE CREW REPORTED A RUDDER TRIM RUN-AWAY AT 50-100 FEET ABOVE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. M - [SDR C2XA06CL023](https://openairdocs.org/sdr/C2XA06CL023), Feb 9, 2006: INVERTER. FAULTY. DURING ROUTINE MAINTENANCE 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT THE MAIN CABIN DOOR. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL C All 109: https://openairdocs.org/deregistered/N14959-2023-03-03/reports.md ## Other aircraft with N14959 - [Cancelled 1952-02-27](https://openairdocs.org/deregistered/N14959-1952-02-27): Douglas DC3C-S4C4G, S/N 11654, built 1952. Owner: [Pacific Southwest Airlines](https://openairdocs.org/faa-owner/PACIFIC%20SOUTHWEST%20AIRLINES), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego) --- 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.