# N14947: 1998 Embraer EMB-145EP, registration cancelled 2018-11-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 8, 2018
- Status when cancelled: Registration expired, pending cancellation
- 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: 145054
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: June 26, 2015
- Last registry action: June 26, 2015
- Mode S code: A0C723
- Owner when cancelled: [Aerovision Aircraft Services LLC](https://openairdocs.org/faa-owner/AEROVISION%20AIRCRAFT%20SERVICES%20LLC)
- Location: [Norton Shores, MI](https://openairdocs.org/faa-place/MI/Norton%20Shores)
- Owner type: Corporation
- 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/N14947
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14947
- Page: https://openairdocs.org/deregistered/N14947-2018-11-08

From the FAA registry file of October 29, 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 (94, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASOA20140709096](https://openairdocs.org/sdr/ASOA20140709096), Jul 9, 2014: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY, OPERATIONALLY TEST
- [SDR ASOA20130407049H](https://openairdocs.org/sdr/ASOA20130407049H), Apr 7, 2013: SKIN. CRACKED. DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STR 1R AND 2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINE
- [SDR ASOA20121107154](https://openairdocs.org/sdr/ASOA20121107154), Nov 6, 2012: SKIN. DENTED. TWO DENTS ON CARGO DOOR RIGHT ABOVE STR 12L BETWEEN X=22364.2 AND X=22640.2. RECONTOURED BACK TO ORIGINAL SHAPE AND REFINISHED.
- [SDR C2XA11IA136](https://openairdocs.org/sdr/C2XA11IA136), Jun 28, 2011: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY, OPERAT
- [SDR C2XA10IA273](https://openairdocs.org/sdr/C2XA10IA273), Oct 21, 2010: BALLAST. OVERHEATED. IAH - FLIGHT 2935, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM SEAT 1A AREA. MAINTENANCE PLACED THE CEILING BALLAST AT ROW 1A ON MEL, AND
- [SDR C2XA10IA267](https://openairdocs.org/sdr/C2XA10IA267), Oct 13, 2010: LIGHT. OVERHEATED. FLIGHT 2804, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR NEAR SEAT 1A, FOLLOWED BY AN INOP READING LIGHT. MAINTENANCE INSPECTED THE AIRCRAF
- [SDR C2XA10IA264](https://openairdocs.org/sdr/C2XA10IA264), Oct 5, 2010: VELOCITY SENSOR. INOPERATIVE. IAH - FLIGHT 2554, THE CREW REPORTED A FLAP FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REP
- [SDR C2XA10SH158](https://openairdocs.org/sdr/C2XA10SH158), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM FRAME 23 IAW EMB-145 SRM 53-21-10
- [SDR C2XA10SH157](https://openairdocs.org/sdr/C2XA10SH157), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 54. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CRO
- [SDR C2XA10SH156](https://openairdocs.org/sdr/C2XA10SH156), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 54. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CARBON CROSSBEAM A
- [SDR C2XA10SH155](https://openairdocs.org/sdr/C2XA10SH155), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 49. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CROSSBEAM AT FRAME
- [SDR C2XA10SH154](https://openairdocs.org/sdr/C2XA10SH154), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CRO
- [SDR C2XA10SH153](https://openairdocs.org/sdr/C2XA10SH153), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CARBON CROSSBEAM A
- [SDR C2XA10SH152](https://openairdocs.org/sdr/C2XA10SH152), Apr 25, 2010: FITTING. CRACKED. SHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENG YOKE FWD LWR FIT
- [SDR C2XA10SH151](https://openairdocs.org/sdr/C2XA10SH151), Apr 25, 2010: FITTING. CRACKED. SHV - DURING C-CHECK NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF CRACK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FWD LOWER PYLON
- [SDR C2XA10SH150](https://openairdocs.org/sdr/C2XA10SH150), Apr 25, 2010: BRACKET. DAMAGED. SHV - DURING C-CHECK LT AILERON PCA BRACKET I/B FLANGE HAT BUSHINGS MISSING AND HOUSING IS DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA BRACKET IAW 
- [SDR C2XA10SH149](https://openairdocs.org/sdr/C2XA10SH149), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CRO
- [SDR C2XA10SH148](https://openairdocs.org/sdr/C2XA10SH148), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM FRAME 38-39 IAW EMB-1
- [SDR C2XA10SH147](https://openairdocs.org/sdr/C2XA10SH147), Apr 25, 2010: INLET. CORRODED. SHV - DURING C-CHECK RT INLET HAS SEVERAL NUT PLATE HOLES THAT ARE CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT INLET NUT PLATE HOLES IAW EC5420
- [SDR C2XA10SH146](https://openairdocs.org/sdr/C2XA10SH146), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE INSTALLED DOUBLER ON CENTER OMEGA BEAM AT CARBON CR
- [SDR C2XA10SH145](https://openairdocs.org/sdr/C2XA10SH145), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAME 33 IAW EMB-
- [SDR C2XA10SH144](https://openairdocs.org/sdr/C2XA10SH144), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 29 IAW EMB-145 SRM 5
- [SDR C2XA10SH143](https://openairdocs.org/sdr/C2XA10SH143), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM CARBON CROSSBEAM CUTO
- [SDR C2XA10SH142](https://openairdocs.org/sdr/C2XA10SH142), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CRO
- [SDR C2XA10SH141](https://openairdocs.org/sdr/C2XA10SH141), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 20. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM AT FRAME 20 IAW EMB-1
- [SDR C2XA10SH140](https://openairdocs.org/sdr/C2XA10SH140), Apr 25, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 25 CARBON CR
- [SDR C2XA10SH139](https://openairdocs.org/sdr/C2XA10SH139), Apr 25, 2010: FITTING. CORRODED. SHV - DURING C-CHECK BAGGAGE DOOR CUTOUT HAS CORROSION (LEVEL 2 LOCAL) AT FWD LWR CORNER. MAINTENANCE PERFORMED REPAIR OF FRAME 65 SHEAR CLIP AT BAGGAGE DOOR CU
- [SDR C2XA10SH137](https://openairdocs.org/sdr/C2XA10SH137), Apr 17, 2010: FITTING. CRACKED. SHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT HAS VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE YOKE FWD 
- [SDR C2XA10IA078](https://openairdocs.org/sdr/C2XA10IA078), Feb 23, 2010: FCU. INOPERATIVE. IAH - FLIGHT 2481, THE CREW REPORTED BOTH FUEL QUANTITY INDICATORS WENT TO DASHES ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINT
- [SDR C2XA10IA037](https://openairdocs.org/sdr/C2XA10IA037), Jan 22, 2010: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 
- [SDR C2XA10IA031](https://openairdocs.org/sdr/C2XA10IA031), Jan 21, 2010: BALLAST. MALFUNCTIONED. DFW - FLIGHT 2324 THE CREW REPORTED A FAINT ELECTRICAL BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIR
- [SDR C2XA09IA213](https://openairdocs.org/sdr/C2XA09IA213), Aug 25, 2009: HINGE. BROKEN. IAH - FLIGHT 3040, DURING PREFLIGHT INSPECTION THE CARGO RAMP ASSY WAS FOUND TO HAVE A BROKEN HINGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ASSEMBLY
- [SDR C2XA09IA146](https://openairdocs.org/sdr/C2XA09IA146), Jun 3, 2009: UNKNOWN. MALFUNCTIONED. IAH - FLIGHT 2804 - THE CREW REPORTED THE LOSS OF GENERATORS 1, 2, & 4 IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AI
- [SDR C2XA09IA082](https://openairdocs.org/sdr/C2XA09IA082), Mar 17, 2009: CONNECTOR. DISCONNECTED. IAH - FLIGHT 2803 - DURING PREFLIGHT INSPECTION THE LEFT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-SECURED THE ELECTRICAL CONNECTION TO TH
- [SDR C2XA09IA008](https://openairdocs.org/sdr/C2XA09IA008), Jan 5, 2009: UPLOCK. INOPERATIVE. FLIGHT 4930, THE CREW REPORTED THAT THE NLG DOORS FAILED TO RETRACT. THE ACFT RETURNED TO ICT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FERRIE
- [SDR C2XA09IA007](https://openairdocs.org/sdr/C2XA09IA007), Jan 4, 2009: SOLENOID VALVE. INOPERATIVE. DURING MX INSP THE NLG DOORS WERE FOUND TO BE NOT CLOSING. MX REMOVED AND REPLACED THE NLG DOOR SOLENOID VALVE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APP
- [SDR C2XA09IA006](https://openairdocs.org/sdr/C2XA09IA006), Jan 4, 2009: PROXIMITY SWITCH. INOPERATIVE. THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON CLIMB OUT WITH THE NOSE GEAR DOWN. THE ACFT RETURNED TO ICT WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND 
- [SDR C2XA08SH165](https://openairdocs.org/sdr/C2XA08SH165), Dec 29, 2008: PROXIMITY SWITCH. DEFECTIVE. ON DEPARTURE OUT, NLG WOULD NOT RETRACT. REMOVED AND REPLACED NLG UPLOCK PROXIMITY SWITCH IAW EMB 145 32-63-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08TY058](https://openairdocs.org/sdr/C2XA08TY058), Jun 13, 2008: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN MID CEILING, AFT SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB 145 AMM 33-51-01. OPS CHECK GOOD. (S)
- [SDR C2XA08IA094](https://openairdocs.org/sdr/C2XA08IA094), Mar 30, 2008: SKIN. CRACKED. IAH - FLIGHT 2695, DURING PREFLIGHT INSPECTION, THE CREW REPORTED CRACKS AT THE SPOILER HINGE POINTS. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETERMINED THAT ON
- [SDR C2XA08TY036](https://openairdocs.org/sdr/C2XA08TY036), Mar 18, 2008: LIGHT. INOPERATIVE. EMERGENCY EXIT ROW OVERHEAD AFT EXIT LIGHT INOP. REPLACED EXIT LIGHT ASSY IAW EMB 145AMM 33-50-13. OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08RI022](https://openairdocs.org/sdr/C2XA08RI022), Feb 18, 2008: ELECTRONIC UNIT. MALFUNCTIONED. FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND
- [SDR C2XA08RI021](https://openairdocs.org/sdr/C2XA08RI021), Feb 18, 2008: CONTROL LEVER. FAULTY. FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND
- [SDR C2XA07RI094](https://openairdocs.org/sdr/C2XA07RI094), Nov 6, 2007: LANDING GEAR. MALFUNCTIONED. FLT 2581 - EWR - CREW REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT FOR ABOUT 2 MINUTES AFTER THE GEAR HANDLE WAS SELECTED UP. EWR MX PERFORME
- [SDR C2XA07SH078](https://openairdocs.org/sdr/C2XA07SH078), Sep 21, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 20 & 23. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 & 23 IAW IC 2007-145-
- [SDR C2XA07SH077](https://openairdocs.org/sdr/C2XA07SH077), Sep 21, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND RT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 18 & 19. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 18 IAW EMB 145 EC 5510-0
- [SDR C2XA07SH076](https://openairdocs.org/sdr/C2XA07SH076), Sep 21, 2007: SHROUD. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND LT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AILERON LOWER SHROUD IAW EC 5750-01315 REV 
- [SDR C2XA07SH075](https://openairdocs.org/sdr/C2XA07SH075), Sep 21, 2007: SHROUD. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AILERON SHROUD IAW EC 5750-01315 REV D. AIR
- [SDR C2XA07SH074](https://openairdocs.org/sdr/C2XA07SH074), Sep 21, 2007: SHROUD. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND RT UPPER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT UPPER AILERON SHROUD IAW EC 5750-01315 REV 
- [SDR C2XA07SH073](https://openairdocs.org/sdr/C2XA07SH073), Sep 21, 2007: SHROUD. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND RT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT LOWER AILERON SHROUD IAW EC 5750-01315 REV 

All 94: https://openairdocs.org/deregistered/N14947-2018-11-08/reports.md

## FAA accident and incident reports (2)

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 20061025022749I](https://openairdocs.org/incident/20061025022749I), Oct 25, 2006: Emb EMB145EP (N14947), Houston, TX, Minor damage. (-23) Tires in positions 1 and 2 blew out the sidewalls after aircraft N14947 turned off the runway on the high speed taxiway. The aircraft was stopped and…
- [Incident 19991121031879I](https://openairdocs.org/incident/19991121031879I), Nov 21, 1999: Emb EMB145ER (N14947), Newark, NJ. (-23) On nov. 21, 1999 at approx. 1638 hrs. Local time flight 4023 was taxiing to the active runway when the crew reported "smoke filled cabin and cockpit"…

## Other aircraft with N14947

- [Cancelled 1941-08-12](https://openairdocs.org/deregistered/N14947-1941-08-12): Lockheed ELECTRA 10-A, S/N 1034. Exported to Australia. Owner: [Babb Co](https://openairdocs.org/faa-owner/BABB%20CO), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

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