# N14925: 1996 Embraer EMB-145EP, registration cancelled 2019-09-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 6, 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: 145004
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: April 4, 2016
- Last registry action: August 10, 2016
- Mode S code: A0C6DB
- Owner when cancelled: [Avi Sales & Leasing Services LLC](https://openairdocs.org/faa-owner/AVI%20SALES%20%26%20LEASING%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/N14925
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14925
- Page: https://openairdocs.org/deregistered/N14925-2019-09-06

From the FAA registry file of November 3, 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 (71, newest 50)

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

- [SDR ASOA20140119011](https://openairdocs.org/sdr/ASOA20140119011), Jan 19, 2014: GROUND STUD. MELTED. THE CREW REPORTED THAT THEY HAD SMOKE COMING FROM THE BASE OF WINDSHIELD NR 1, AND THAT IT STOPPED 1-2 MINUTES AFTER WINDSHIELD HEAT WAS TURNED OFF. THE ACFT LA
- [SDR ASOA20130930179](https://openairdocs.org/sdr/ASOA20130930179), Sep 30, 2013: WIRE. LOOSE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXIT SIGN ABOVE F/A`S HEAD WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RESECURRED THE WIRING ON THE 
- [SDR ASOA20130212013](https://openairdocs.org/sdr/ASOA20130212013), Feb 12, 2013: CHARGER. INOPERATIVE. DURING SCHEDULED MX, THE EMERGENCY FLOOR STIP LIGHTING AT POSITIONS 1,2,3 AND SERVICE DOOR EMERGENCY LIGHTING WERE FOUND INOPERATIVE. MX REPLACED THE EMERGENCY 
- [SDR ASOA20130130007H](https://openairdocs.org/sdr/ASOA20130130007H), Jan 30, 2013: LIGHT. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 3 TO ROW 6 WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT STRIP, OPS TESTED W
- [SDR ASOA20121217159](https://openairdocs.org/sdr/ASOA20121217159), Dec 17, 2012: SKIN. CRACKED. DURING SCHEDULED MX THE RT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.
- [SDR ASOA20121217158](https://openairdocs.org/sdr/ASOA20121217158), Dec 17, 2012: SKIN. CRACKED. DURING SCHEDULED MX THE LT UPPER FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED. THE SKIN WAS REPAIRED IAW EC 5330-02353 AND THE DISCREPANCY CLEARED.
- [SDR ASOA111227019](https://openairdocs.org/sdr/ASOA111227019), Dec 27, 2011: ACM. SMOKE. THE CREW REPORTED THAT AFTER STARTING THE NR 2 ENGINE WITH THE NR1 PACK ON THERE WAS DARK SMOKE IN THE COCKPIT AND FORWARD CABIN WITH A NOTED SULPHUR SMELL. THE
- [SDR C2XA11TY141](https://openairdocs.org/sdr/C2XA11TY141), Sep 13, 2011: SKIN. CORRODED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND VARIOUS AREAS OF CORROSION IN THE LOWER FUSELAGE BETWEEN FRAMES 13 AND 14, STRINGERS 20L TO 20R. MAINTENANC
- [SDR C2XA11TY138](https://openairdocs.org/sdr/C2XA11TY138), Sep 10, 2011: SILL. CORRODED. TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT FLOOR SILL PITTED AT FR18 THRU FR 20. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW E
- [SDR C2XA10IA274](https://openairdocs.org/sdr/C2XA10IA274), Oct 25, 2010: CONTROLLER. INOPERATIVE. IAH - FLIGHT 2873, DURING PREFLIGHT INSPECTION THE CREW REPORTED A PLASTIC BURNING SMELL. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE OVERHE
- [SDR C2XA09SH493](https://openairdocs.org/sdr/C2XA09SH493), Dec 7, 2009: WIRE HARNESS. BROKEN. SHV - DURING TAKEOFF THE AIRCREW DISCOVERED THE LANDING GEAR WOULD NOT RETRACT. PERFORMED AN AIR RETURN TO MEM AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT
- [SDR C2XA09IA304](https://openairdocs.org/sdr/C2XA09IA304), Dec 2, 2009: CHECK VALVE. INOPERATIVE. IAH - DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A PIECE OF THE LEFT NOSE LANDING GEAR TO HAVE A PIECE MISSING. THE AIRCRAFT WAS INSPECTED AND FERRIED TO I
- [SDR C2XA09IA303](https://openairdocs.org/sdr/C2XA09IA303), Dec 2, 2009: SOLENOID VALVE. DEFECTIVE. IAH - DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A PIECE OF THE LEFT NOSE LANDING GEAR TO HAVE A PIECE MISSING. THE AIRCRAFT WAS INSPECTED AND FERRIED TO I
- [SDR C2XA09IA279](https://openairdocs.org/sdr/C2XA09IA279), Nov 2, 2009: ELECTRONIC UNIT. INOPERATIVE. IAH - FLIGHT 3102, ON DEPARTURE FROM MAF, THE CREW REPORTED THAT THE NOSE GEAR RETRACTION MADE LOUD NOISES DURING STOWAGE FOLLOWED BY PERSISTENT DEEP THUMPING F
- [SDR C2XA09IA278](https://openairdocs.org/sdr/C2XA09IA278), Nov 2, 2009: UPLOCK. INOPERATIVE. IAH - FLIGHT 3102, ON DEPARTURE FROM MAF, THE CREW REPORTED THAT THE NOSE GEAR RETRACTION MADE LOUD NOISES DURING STOWAGE FOLLOWED BY PERSISTENT DEEP THUMPING F
- [SDR C2XA09IA233](https://openairdocs.org/sdr/C2XA09IA233), Sep 11, 2009: UNKNOWN. ODOR. IAH - FLIGHT 2959 - THE CREW REPORTED THAT AT FL260, SMELLED ELECTRICAL SMOKE WITH NONE VISIBLE. THE SMELL PERSISTED FOR 30-45 SECONDS AND CLEARED WITH THE F/A 
- [SDR C2XA09IA096](https://openairdocs.org/sdr/C2XA09IA096), Apr 13, 2009: SMOKE DETECTOR. MALFUNCTIONED. IAH - FLIGHT 2493, THE CREW REPORTED A LAV SMOKE INDICATION AFTER STARTING THE NUMBER ONE ENGINE. THE CREW REPORTED THAT THERE WAS NO SMOKE IN THE LAV, BUT WAS 
- [SDR C2XA09TY054](https://openairdocs.org/sdr/C2XA09TY054), Mar 21, 2009: SKIN. DAMAGED. THE LT & RT FUSELAGE SKINS HAVE 15 HOLES (7 HOLES LT AND 8 HOLES RT) THAT HAVE CRACKS RADIATING FROM THE FASTENERS. THE HOLES WERE REAMED BETWEEN .531 INCH AND 
- [SDR C2XA09TY051](https://openairdocs.org/sdr/C2XA09TY051), Mar 19, 2009: YOKE. CRACKED. TYS - DURING C-CHECK THE NR 1 ENGINE LOWER FORWARD YOKE WAS FOUND CRACKED AT ENGINE MOUNT WEBBING. THE NR 1 ENGINE LOWER FORWARD YOKE MOUNT WEBBING AFT SECTION 
- [SDR C2XA09TY050](https://openairdocs.org/sdr/C2XA09TY050), Mar 18, 2009: STIFFENER. CRACKED. AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND A STIFFENER CRACKED IN THE LEFT PYLON INSIDE PANEL 414DB CRACKED ON BOTH ENDS. MAINTENANCE REMOVED AND 
- [SDR C2XA09TY049](https://openairdocs.org/sdr/C2XA09TY049), Mar 18, 2009: STIFFENER. CRACKED. AIRCRAFT CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND A CRACK IN THE AFT PYLON STIFFENER/STRINGER INSIDE PANEL 414DB. MAINTENANCE REMOVED AND REPLACED THE PY
- [SDR C2XA09TY055](https://openairdocs.org/sdr/C2XA09TY055), Mar 17, 2009: FITTING. DAMAGED. THE FRAME 75 VERTICAL FITTING AND ADJACENT SKIN ARE SHOWING SIGNS OF FRETTING AT EDGES. REMOVED FITTING, BLENDED OUT DAMAGE, PERFORMED DYE PEN INSPECTION AND RE
- [SDR C2XA09TY019A](https://openairdocs.org/sdr/C2XA09TY019A), Jan 22, 2009: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER MAIN DOOR INOP. R&R LAMP IAW EMB 145AMM 33-50-06. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08IA056](https://openairdocs.org/sdr/C2XA08IA056), Feb 9, 2008: FUSE. BLOWN. IAH - DURING MAINTENANCE INSPECTION THE BOTH LT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE E
- [SDR C2XA08IA022](https://openairdocs.org/sdr/C2XA08IA022), Jan 9, 2008: POWER SUPPLY. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION NUMEROUS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTER
- [SDR C2XA08IA012](https://openairdocs.org/sdr/C2XA08IA012), Jan 4, 2008: SKIN. CRACKED. IAH, FLIGHT 2472, DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE LEFT WING UPPER SKIN ADJACENT TO THE LEFT SPOILER INBOARD HINGE POINT. THE SKIN W
- [SDR C2XA07RI083](https://openairdocs.org/sdr/C2XA07RI083), Sep 24, 2007: WIRE. BROKEN. EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT PATH STRIP NOT WORKING. MX FOUND STRIP WIRE BROKEN. MX REPAIRED THE WIRING AND PERFORMED OPERATIONAL 
- [SDR C2XA07RI079](https://openairdocs.org/sdr/C2XA07RI079), Sep 12, 2007: LIGHT. INOPERATIVE. FLT 2297 - EWR - CREW REPORTED EMERGENCY FLOOR LIGHTING WIRE IS VISIBLE OUTSIDE PLASTIC MOLDING AND STRIP IS INOPERATIVE BY SEAT 12A. EWR MX REMOVED AND REPLACE
- [SDR C2XA06IA184](https://openairdocs.org/sdr/C2XA06IA184), Nov 22, 2006: BALLAST. BURNED. IAH - FLIGHT 2648, THE CREW REPORTED A SMOKE ODOR COMING FROM THE CABIN. MAINTENANCE REMOVED AND REPLACED THE SIDEWALL/CEILING LIGHT BALLAST, OPERATIONALLY CHEC
- [SDR C2XA06IA176](https://openairdocs.org/sdr/C2XA06IA176), Nov 9, 2006: BALLAST. INOPERATIVE. IAH - FLIGHT 2555, DURING POST FLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE
- [SDR C2XA06IA175](https://openairdocs.org/sdr/C2XA06IA175), Nov 9, 2006: UNKNOWN. ODOR. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND WAS UNABLE TO DUPLICATE THE DISCREPANCY,
- [SDR C2XA06RI004](https://openairdocs.org/sdr/C2XA06RI004), Aug 29, 2006: BEVEL GEAR. FRACTURED. DURING CLIMB, ENG NR 1 IN FLT SHUTDOWN. ACFT DIVERTED TO IAD. MX FOUND METAL DEBRIS ON CHIP DETECTOR. MX R & R ENGINE. OPS CHECKS PERFORMED SUCCESSFULLY. ACFT A
- [SDR C2XA06SD012](https://openairdocs.org/sdr/C2XA06SD012), Jul 22, 2006: WARNING SYSTEM. FALSE ACTIVATION. HEARD (LANDING GEAR) AURAL WARNING TWICE AT 13000 FT, IN MOD TURB AND PRECIP LANDING GEAR WAS UP AND NO INDICATIONS WERE SEEN ON EICAS. RESET RA CB'S TESTED RA'
- [SDR C2XA06CL067](https://openairdocs.org/sdr/C2XA06CL067), Jul 21, 2006: LIGHT. INOPERATIVE. CLE FLIGHT NR 2221 THE CREW REPORTED THE EMERGENCY LIGHTS BY THE EXIT ROW WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. OPERATIO
- [SDR C2XA06CL011](https://openairdocs.org/sdr/C2XA06CL011), Jan 25, 2006: CONNECTOR. LOOSE. DURING ROUTINE MAINTENANCE THE RT EMERGENCY EXIT IDENTIFIER SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR BEHIND THE EXIT SIGN. OPERAT
- [SDR C2XA06CL010](https://openairdocs.org/sdr/C2XA06CL010), Jan 25, 2006: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE SEVERAL EMERGENCY LIGHTS WERE FOUND NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT BATTERIES. OPER
- [SDR C2XA06BT003](https://openairdocs.org/sdr/C2XA06BT003), Jan 24, 2006: CHARGER. FAULTY. CREW REPORTED, THE RIGHT WING EMERGENCY LIGHT IS NOT WORKING. REMOVED AND REPLACED NR 2 BATTERY CHARGER IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETU
- [SDR C2XA06IA009](https://openairdocs.org/sdr/C2XA06IA009), Jan 13, 2006: HYDRAULIC SYSTEM. LEAKING. IAH - FLIGHT 2966, THE CREW REPORTED THAT THE HYDRAULIC SYSTEM ONE QUANTITY INDICATION WENT TO ZERO DURING FLIGHT. THE CREW DEACTIVATED THE SYSTEM 1 HYDRAULICS,
- [SDR C2XA04CL099](https://openairdocs.org/sdr/C2XA04CL099), Sep 25, 2004: SPLINE. STRIPPED. THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND REPLACED THE INSIDE DOOR HANDLE. OPS CHECKED GOOD.
- [SDR C2XA04CL091](https://openairdocs.org/sdr/C2XA04CL091), Sep 10, 2004: CONTROL LEVER. MALFUNCTIONED. AFTER TAKEOFF FROM CLE FLIGHT CREW HAD TO CYCLE THE LANDING GEAR HANDLE TWICE TO GET THE LANDING GEAR TO RETRACT. AIRCRAFT RETURNED TO CLE LANDED WITH OUT INCID
- [SDR C2XA04SH488](https://openairdocs.org/sdr/C2XA04SH488), Aug 28, 2004: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER RE
- [SDR C2XA04SH489](https://openairdocs.org/sdr/C2XA04SH489), Aug 28, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 
- [SDR C2XA04SH485](https://openairdocs.org/sdr/C2XA04SH485), Aug 10, 2004: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 
- [SDR C2XA04CL059](https://openairdocs.org/sdr/C2XA04CL059), Jun 1, 2004: INVERTER. INOPERATIVE. THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE 
- [SDR C2XA04BT044](https://openairdocs.org/sdr/C2XA04BT044), Apr 1, 2004: BATTERY. FAULTY. CREW REPORTED, THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER PACK IAW EMB145 MM 33-50-11, OPS C
- [SDR C2XA03CL161](https://openairdocs.org/sdr/C2XA03CL161), Sep 6, 2003: SHROUD. LOOSE. WHILE PERFORMING A 1A INSPECTION MAINTENANCE REPORTED THAT THE RIGHT HAND EMERGENCY EXIT WOULD NOT OPEN IT WAS BLOCKED AT THE TOP BY A SIDEWALL PANEL. MAINTENAN
- [SDR C2XA03BT085](https://openairdocs.org/sdr/C2XA03BT085), Aug 27, 2003: POWER SUPPLY. DISCHARGED. EWR LOG BOOK SQUAWK AISLE PATH LIGHTING STRIPS SEGMENTS 2 AND 3 INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECK
- [SDR C2XA03BT063](https://openairdocs.org/sdr/C2XA03BT063), May 29, 2003: SMOKE DETECTOR. MALFUNCTIONED. CREW REPORTED, DECLARED EMERGENCY FOR BAGGAGE AREA SMOKE WARNING IN FLIGHT, DIVERTED TO RDU, FIRE EXTINGUISHER BLOWN. MAINTENANCE DISPATCHED TO AIRCRAFT, INSPEC
- [SDR C2XA03CL029](https://openairdocs.org/sdr/C2XA03CL029), Feb 3, 2003: BALLAST. FAULTY. CLE FLIGHT#2267 THE CREW REPORTED A ELECTRICAL BURNING SMELL COMING FROM ABOVE THE FLIGHT ATTENDANT CALL PANEL.MAINTENANCE INSPECTED AND REPLACED THE DIMMING BA
- [SDR C2XA03BT010](https://openairdocs.org/sdr/C2XA03BT010), Jan 17, 2003: UPLOCK SWITCH. FAULTY. SYR---CO2576, CREW REPORTED, LANDING GEAR LEVER DISAGREEMENT AFTER TAKEOFF. LEFT MAIN GEAR WOULD NOT RETRACT. AIRCRAFT AIR RETURNED TO SYR AND LANDED UNEVENTFUL

All 71: https://openairdocs.org/deregistered/N14925-2019-09-06/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 19980907038119I](https://openairdocs.org/incident/19980907038119I), Sep 7, 1998: Emb EMB145 (N14925), Newark, NJ. (-5)The captain stated that they had deviated around thunderstorms. The main cell was thirty miles away although the radar showed extensions from the cell.…
- [Incident 19971022041739I](https://openairdocs.org/incident/19971022041739I), Oct 22, 1997: Emb EMB145 (N14925), Cleveland, OH. Narrative: crew received a #1 engine control "a-b" fail message and visual and aural warning. (Eng shut down?) Aircraft landed at Cleveland without incident.…

## Other aircraft with N14925

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N14925-undated): Douglas DC2, S/N 1411, built 1935. Owner: [Douglas Aircraft Co Inc](https://openairdocs.org/faa-owner/DOUGLAS%20AIRCRAFT%20CO%20INC), [Santa Monica, CA](https://openairdocs.org/faa-place/CA/Santa%20Monica)

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