# N14945: 1998 Embraer EMB-145EP, registration cancelled 2019-01-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 16, 2019 - 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: 145049 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 27, 2005 - Certificate issued: July 27, 2015 - Last registry action: July 27, 2015 - Mode S code: A0C721 - 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/N14945 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14945 - Page: https://openairdocs.org/deregistered/N14945-2019-01-16 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 (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20130921170](https://openairdocs.org/sdr/ASOA20130921170), Sep 21, 2013: SMOKE DETECTOR. INOPERATIVE. AFTER TAKEOFF, CREW REPORTED A LAVATORY SMOKE INDICATION. RAN QRH ITEMS AND MESSAGE WENT AWAY, NO SMOKE NOTED. ACFT LANDED WITHOUT INCIDENT. MX R & R LAVATORY S - [SDR ASOA20130505066](https://openairdocs.org/sdr/ASOA20130505066), May 5, 2013: SKIN. CRACKED. DURING 3A INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED NEAR FR 77 AT 1 RIVET AT STR9R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE R - [SDR ASOA20130308287](https://openairdocs.org/sdr/ASOA20130308287), Mar 8, 2013: SKIN. CORRODED. ACFT IS IN A C-CHECK POSITION WHEN INSPECTION FOUND CORROSION WAS FOUND ON A SKIN PANEL AT FRAME 13 AT STRINGERS 20R AND 19R. MX R & R THE SKIN PANEL IAW SRM 53 - [SDR ASOA20130308206](https://openairdocs.org/sdr/ASOA20130308206), Mar 8, 2013: SKIN. CORRODED. ACFT IS IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE SKIN AFT OF FRAME 18, BETWEEN STRINGERS 20L AND 19R. MX R & R THE SKIN IAW EMB 145 EC 5330-02715. THE - [SDR C2XA11TY149](https://openairdocs.org/sdr/C2XA11TY149), Sep 23, 2011: SKIN. DAMAGED. AIRCRAFT SUSTAINED GROUND DAMAGE TO THE RT REAR FUSELAGE BETWEEN FRAMES 63 AND 68. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED FILLERS AND DOU - [SDR C2XA11IA083](https://openairdocs.org/sdr/C2XA11IA083), May 6, 2011: DISPLAY. SHORTED. XNA - FLIGHT 2619 THE CREW REPORTED A SMOKE SMELL FOLLOWED BY THE CAPTAINS PFD CIRCUIT BREAKER POPPING. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED - [SDR C2XA11IA030](https://openairdocs.org/sdr/C2XA11IA030), Feb 7, 2011: UNKNOWN. ODOR. IAH - THE CREW REPORTED THAT THE COCKPIT SMELLED LIKE BURNING ELECTRICAL WIRE. MAINTENANCE INSPECTED THE AIRCRAFT POWERED UP THE AIRCRAFT WITH NO DEFECTS NOTED, - [SDR C2XA10SH315](https://openairdocs.org/sdr/C2XA10SH315), Sep 20, 2010: SKIN. DAMAGED. SHV - DURING C-CHECK 2 OBLONG HOLES IN RUDDER II SKIN, LT SIDE, ABOUT 1/2 WAY UP. MAINTENANCE PERFORMED REPAIR TO RUDDER II SKIN, LT SIDE, HALFWAY UP IAW EC5540 - [SDR C2XA10SH314](https://openairdocs.org/sdr/C2XA10SH314), Sep 20, 2010: HOUSING. DAMAGED. SHV - DURING C-CHECK VERTICAL STABILIZER RT SPERICAL BEARING HOUSING FOUND TO BE OUT OF LIMITS. MAINTENANCE PERFORMED REPAIR ON RT SPERICAL BEARING HOUSING IAW - [SDR C2XA10SH313](https://openairdocs.org/sdr/C2XA10SH313), Sep 15, 2010: BEAM. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) FRAMES 19 TO 23. MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM AT FRAME 18-24 IAW SRM 51-40-02 - [SDR C2XA10IA241](https://openairdocs.org/sdr/C2XA10IA241), Aug 31, 2010: CONNECTOR. BURNED. IAH - FLIGHT 2012, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN BEFORE BOARDING. MAINTENANCE INSPECTED THE AIRCRAFT A - [SDR C2XA10SH201](https://openairdocs.org/sdr/C2XA10SH201), Jun 11, 2010: WARNING LIGHT. FALSE ACTIVATION. FLT 2213 DIVERT - E1 BLEED LK MSG-E1 COMMANDED SHUTDOWN INFLT. MAINTENANCE DOWNLOADED DFDR AND CMC - NO FAULTS FOUND, RAN AC, NO LEAKS. PERFORMED BLEED OPERATIO - [SDR C2XA10IA107](https://openairdocs.org/sdr/C2XA10IA107), Mar 27, 2010: SKIN. CRACKED. IAH - FLIGHT 2820, DURING POST FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DO - [SDR C2XA10SH100](https://openairdocs.org/sdr/C2XA10SH100), Mar 21, 2010: LIGHT. INOPERATIVE. SHV - GALLEY EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08IA261](https://openairdocs.org/sdr/C2XA08IA261), Dec 21, 2008: UNKNOWN. ODOR. FLIGHT 2195 MOB - IAH. THE CREW REPORTED A BURNING PLASTIC SMELL AT PASSENGER SEAT ROWS 9 THROUGH 11. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENA - [SDR C2XA08IA142](https://openairdocs.org/sdr/C2XA08IA142), Jun 19, 2008: SMOKE DETECTOR. FALSE ACTIVATION. BTR - FLIGHT 2010, THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION. THE ACFT DIVERTED TO BETWEEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE A - [SDR C2XA08CL067](https://openairdocs.org/sdr/C2XA08CL067), Jun 8, 2008: BULB. FAULTY. DURING ROUTINE MAINTENANCE THE AFT OVERHEAD WHITE EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AFT OVERHEAD WHITE EMERGEN - [SDR C2XA08RI075](https://openairdocs.org/sdr/C2XA08RI075), May 16, 2008: BALLAST. DEFECTIVE. FLIGHT 2404 - EWR - FLIGHT CREW REPORTED SIDE LIGHTS AT 2A AND 3A INOPERATIVE WITH BURNING SMELL COMING FROM BALLAST. EWR MX REMOVED AND REPLACED BALLAST IAW WM - [SDR C2XA08RI074](https://openairdocs.org/sdr/C2XA08RI074), May 16, 2008: COFFEEMAKER. MALFUNCTIONED. FLIGHT 2404 - EWR - FLIGHT CREW REPORTED COFFEEMAKERS EMITTING BURNING SMELL WHEN TURNED ON. EWR MX PERFORMED OPERATIONAL CHECK OF BOTH COFFEEMAKERS IAW EMB 145 - [SDR C2XA08CL024](https://openairdocs.org/sdr/C2XA08CL024), Mar 3, 2008: PROXIMITY SWITCH. FAULTY. YQB FLIGHT 3072 - THE CREW REPORTED AFTER TAKEOFF A LOUD CLUNK ALONG WITH VIBRATION FELT IN FLIGHT CONTROLS. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR UPLOC - [SDR C2XA08IA045](https://openairdocs.org/sdr/C2XA08IA045), Feb 2, 2008: NOZZLE. DIRTY. IAH - FLIGHT 2818, THE CREW REPORTED FOG DENSE IN COCKPIT DURING TAKEOFF ROLL, NO BURNING SMELL JUST FOGGED ALL WINDOWS. TAKEOFF WAS ABORTED AND THE AIRCRAFT RE - [SDR C2XA08SH014](https://openairdocs.org/sdr/C2XA08SH014), Feb 2, 2008: FRAME. CORRODED. SHV - DURING C-CHECK FRAME 65 HAS CORROSION AT STR 17L. MX REPAIRED FR 65 STR 17 IAW EC 5310-01432. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH016](https://openairdocs.org/sdr/C2XA08SH016), Feb 2, 2008: SHEAR TIE. CORRODED. SHV - DURING C-CHECK SHEAR CLIP AT FR 65 HAS CORROSION. MX REPAIRED FR 65 SHEAR CLIP IAW EC 5330-01458. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH015](https://openairdocs.org/sdr/C2XA08SH015), Feb 2, 2008: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SECTION HAS VARIOUS ARES OF CORROSION. MX REMOVED AND REPLACED LOWER BEAM AT CARGO DOOR CUTOUT FR 65-68 IAW EMB 145 - [SDR C2XA07IA202](https://openairdocs.org/sdr/C2XA07IA202), Sep 13, 2007: CONNECTOR. BURNED. IAH FLT 2302, MX WORKING MEL 33-20-001/C PLASTIC BURNT SMELL IN AIRCRAFT. MAINTENANCE REMOVED AND REPLACED CONNECTOR TO OVERHEAD LIGHT, OPERATIONALLY CHECKED WI - [SDR C2XA07IA146](https://openairdocs.org/sdr/C2XA07IA146), Jun 19, 2007: NOZZLE. CLOGGED. FLIGHT 2553 - CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN WHEN THE AIR CONDITIONING PACKS WERE SELECTED TO MANUAL. MAINTENANCE CLEANED THE LEFT AIR C - [SDR C2XA06IA045](https://openairdocs.org/sdr/C2XA06IA045), Mar 22, 2006: WINDSHIELD. DAMAGED. IAH - FLIGHT 2537, DURING DESCENT INTO IAH, THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE MAINTENANCE REMOVED AND R - [SDR C2XA05SH131](https://openairdocs.org/sdr/C2XA05SH131), Nov 9, 2005: SUPPORT. CRACKED. SHV - DURING C-CHECK, MAINTENANCE FOUND FS 68 CARGO DOOR ROD SUPPORT BRACKET(AFT SECTION) CRACKED. MAINTENANCE REPAIRED FS 68 (AFT SECTION) OF CARGO DOOR SUPPOR - [SDR C2XA05SH130](https://openairdocs.org/sdr/C2XA05SH130), Nov 8, 2005: BUSHING. GOUGED. SHV - DURING C-CHECK, MAINTENANCE FOUND LT I/B FLAP O/B BUSHING GOUGED (ON FLAP). MAINTENANCE REMOVED AND REPLACED LT I/B FLAP O/B BUSHING (ON FLAP) IAW EMB 145 - [SDR C2XA05SH129](https://openairdocs.org/sdr/C2XA05SH129), Nov 7, 2005: FIREWALL. CHAFED. SHV-DURING C-CHECK MAINTENANCE FOUND AFT LOWER SIDE OF APU FIREWALL RIVET HEAD WITH DAMAGE. MAINTENANCE REPAIRED APU LOWER FIREWALL SKIN DAMAGE I/A/W EC 5330-01 - [SDR C2XA04IA125](https://openairdocs.org/sdr/C2XA04IA125), Sep 30, 2004: CONTROL UNIT. MALFUNCTIONED. IAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTI - [SDR C2XA04BT075](https://openairdocs.org/sdr/C2XA04BT075), Jul 8, 2004: LIGHT. DEACTIVATED. CREW REPORTED, NR 2 EMERGENCY LIGHT STRIP IN CABIN INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00, OPS CHECKED EMERGENCY LIGHTS GOO - [SDR C2XA04IA079](https://openairdocs.org/sdr/C2XA04IA079), Jun 5, 2004: CONTROL PANEL. CONTAMINATED. DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTION AT THE FLIG - [SDR C2XA03CL156](https://openairdocs.org/sdr/C2XA03CL156), Aug 30, 2003: LIGHT. MALFUNCTIONED. CLE FLIGHT NR 2115 THE CREW REPORTED TWO EMERGENCY AISLE LIGHTS OUT OF SERVICE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF AISLE PATH EMERGENCY LIG - [SDR C2XA03IA082](https://openairdocs.org/sdr/C2XA03IA082), Aug 9, 2003: LIGHT. INOPERATIVE. IAH - FLIGHT 2573 - THE FORWARD SECTION OF EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE - [SDR C2XA03BT079](https://openairdocs.org/sdr/C2XA03BT079), Aug 9, 2003: BATTERY. DISCHARGED. EWR---CO2573, CREW REPORTED DURING PREFLIGHT, EMERGENCY LIGHTS WERE INOPERATIVE......MAINTENANCE REMOVED AND REPLACED BATTERY AND REPAIRED BROKEN WIRE. (IAW EMB - [SDR C2XA03CL129](https://openairdocs.org/sdr/C2XA03CL129), Jul 27, 2003: LIGHT. MALFUNCTIONED. EWR FLIGHT NR 2568 THE CREW REPORTED THE AISLE PATH LIGHTING WAS INOPERATIVE STARTING FROM ROW 8. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND NO - [SDR C2XA03CL121](https://openairdocs.org/sdr/C2XA03CL121), Jul 8, 2003: WIRE. LOOSE. THE CREW REPORTED FLOOR EMERGENCY LIGHTS BURNED OUT IN TWO SECTIONS. MAINTENANCE RESECURED LOOSE WIRE ON EMERGENCY LIGHT STRIP. - [SDR C2XA03SH164](https://openairdocs.org/sdr/C2XA03SH164), May 29, 2003: SQUAT SWITCH. FAILED. DURING TEST FLIGHT 3160 A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. PILOT USED DOWNLOCK RELEASE BUTTON TO RAISE AND LOWER GEAR. THE AIRCRAFT COM - [SDR C2XA03SH163](https://openairdocs.org/sdr/C2XA03SH163), May 29, 2003: FLOORBEAM. CORRODED. DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED BEAM IAW EMB 145 SRM - [SDR C2XA03SH165](https://openairdocs.org/sdr/C2XA03SH165), May 28, 2003: PROXIMITY SWITCH. OUT OF ADJUST. SHV - DURING TEST FLIGHT 3160, A CAUTION MESSAGE CAME UP ON THE EICAS AND WOULD NOT CLEAR. THE PILOT USED THE DOWNLOCK RELEASE TO CYCLE THE GEAR. THE AIRCRAFT C - [SDR C2XA03SH162](https://openairdocs.org/sdr/C2XA03SH162), May 28, 2003: FLOORBEAM. CORRODED. SHV DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION AT RAMP SUPPORT ANGLE BETWEEN FRAMES 19 AND 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED - [SDR C2XA03SH161](https://openairdocs.org/sdr/C2XA03SH161), May 28, 2003: FLOORBEAM. CORRODED. SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM HAS CORROSION UNDER THE COMPOSITE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTE - [SDR C2XA03SH160](https://openairdocs.org/sdr/C2XA03SH160), May 28, 2003: STOP. CRACKED. DURING C-CHECK THE CARGO DOOR STOP LIP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED STOP IAW EMB 145 SRM 52-30-03. THE AIRCRAFT WAS APPROVED TO - [SDR C2XA03SH156](https://openairdocs.org/sdr/C2XA03SH156), May 25, 2003: BUTTSTRAP. CORRODED. DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FI - [SDR C2XA03SH155](https://openairdocs.org/sdr/C2XA03SH155), May 25, 2003: ANGLE. CRACKED. DURING C-CHECK THE LOWER ATTACH ANGLE FOR THE CARGO RAMP AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SR - [SDR C2XA03SH154](https://openairdocs.org/sdr/C2XA03SH154), May 25, 2003: SUPPORT. CORRODED. DURING C-CHECK THE AFT PASSENGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-40-02 - [SDR C2XA03SH153](https://openairdocs.org/sdr/C2XA03SH153), May 25, 2003: SUPPORT. CORRODED. DURING C-CHECK THE FORWARD PASSANGER DOOR THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB 145 SRM 51-4 - [SDR C2XA03SH152](https://openairdocs.org/sdr/C2XA03SH152), May 25, 2003: CROSSBEAM. CORRODED. DURING C-CHECK THE LOWER CROSSBEAM ANGLE FROM THE CENTER BEAM TO THE RIGHT HAND BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA03SH151](https://openairdocs.org/sdr/C2XA03SH151), May 25, 2003: FLOORBEAM. CORRODED. SHV-DURING C-CHECK THE SUPPORT RAMP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT SUPPO All 85: https://openairdocs.org/deregistered/N14945-2019-01-16/reports.md --- 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.