# N14930: 1997 Embraer EMB-145EP, registration cancelled 2020-02-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 28, 2020
- 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: 145011
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: November 21, 2016
- Last registry action: November 21, 2016
- Mode S code: A0C6F9
- Owner when cancelled: [Aar Supply Chain Inc](https://openairdocs.org/faa-owner/AAR%20SUPPLY%20CHAIN%20INC)
- Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale)
- Owner type: Corporation
- Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14930
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14930
- Page: https://openairdocs.org/deregistered/N14930-2020-02-28

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-145EP: https://openairdocs.org/model/embraer-emb-145ep.md

## Service difficulty reports (142, newest 50)

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

- [SDR ASOA20140413043](https://openairdocs.org/sdr/ASOA20140413043), Apr 13, 2014: DOOR FRAME. CRACKED. CARGO DOOR AFT FRAME LOWER INSIDE CORNER HAS A CRACKED NUTPLATE. REPAIRED IAW EC5230-01326. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413042](https://openairdocs.org/sdr/ASOA20140413042), Apr 13, 2014: FIREWALL. CRACKED. DURING C-CHECK, APU FIREWALL CRACKED AT UPPER LT MOUNT. REPAIRED IAW EC5330-02578, REV B. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413041](https://openairdocs.org/sdr/ASOA20140413041), Apr 13, 2014: HOUSING. WORN. DURING C-CHECK, HORIZONTAL STAB HINGE FITTING HOUSINGS IS OUT OF LIMITS. REPAIRED IAW SRM 55-30-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413040V](https://openairdocs.org/sdr/ASOA20140413040V), Apr 13, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CENTER OMEGA BEAM CORRODED ON LOWER SIDE AT FRAME 59. MAINTENANCE PERFORMED REPAIR IAW EC5310-01473. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413039](https://openairdocs.org/sdr/ASOA20140413039), Apr 13, 2014: SHEAR TIE. CORRODED. SHEAR TIE CORRODED, AT FRAME 65, STRINGER 17L. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413038](https://openairdocs.org/sdr/ASOA20140413038), Apr 13, 2014: BEAM. CORRODED. DURING C-CHECK, CARGO LOWER BEAM FROM FRAMES 65-68 HAS CORROSION. MAINTENANCE R & R LOWER BEAM IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETU
- [SDR ASOA20130225024](https://openairdocs.org/sdr/ASOA20130225024), Feb 25, 2013: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE PASSENGER CABIN FWD EMERGENCY EXIT LOCATING SIGN ON 253CLC FAILED TO ILLUMINATE. MX R & R THE AFFECTED SIGN EMERGENCY LIGHT INVERTER, 
- [SDR ASOA20130219020](https://openairdocs.org/sdr/ASOA20130219020), Feb 19, 2013: CONNECTOR. DISCONNECTED. THE CREW REPORTED THE EXIT SIGN OVERWING EXIT WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RECONNECTED THE SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND TH
- [SDR ASOA20120122015](https://openairdocs.org/sdr/ASOA20120122015), Jan 22, 2012: FLOOR SUPPORT. CORRODED. DURING C-CHECK. CENTER OMEGA BEAM CORRODED AT FR 20. REPLACED OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120121014](https://openairdocs.org/sdr/ASOA20120121014), Jan 21, 2012: SKIN. CRACKED. DURING C-CHECK. CRACKS AROUND RIVETS ON RT FUSELAGE SKIN AT FR 75. REPAIRED SKIN CRACKS IAW EC 5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120121013](https://openairdocs.org/sdr/ASOA20120121013), Jan 21, 2012: MOUNT. CRACKED. DURING C-CHECK. RT FWD LOWER ENGINE MOUNT CRACKED. R & R RT LOWER FWD ENGINE MOUNT IAW EC 5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120117012](https://openairdocs.org/sdr/ASOA20120117012), Jan 17, 2012: FLOOR SUPPORT. CORRODED. DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 49. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120117011](https://openairdocs.org/sdr/ASOA20120117011), Jan 17, 2012: FLOOR SUPPORT. CORRODED. DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 44. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA252](https://openairdocs.org/sdr/C2XA11IA252), Nov 3, 2011: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING NR 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT
- [SDR C2XA11IA177](https://openairdocs.org/sdr/C2XA11IA177), Aug 10, 2011: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2886, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING IN THE BACK HALF OF THE AIRCRAFT WAS INOPERATIVE. MAINTENANCE RE
- [SDR C2XA11IA149](https://openairdocs.org/sdr/C2XA11IA149), Jul 8, 2011: DAMPER PLATE. DAMAGED. IAH - DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO HAVE SEVERAL DAMAGED VIBRATION ABSORPTION PADS. MAINTENANCE REPAIRED THE VIBRATION ABSORPTION 
- [SDR C2XA10IA177](https://openairdocs.org/sdr/C2XA10IA177), Jun 18, 2010: BATTERY. OVERHEATED. IAH - FLIGHT 3121, THE CREW REPORTED A BATTERY TWO OVER-TEMP ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE 
- [SDR C2XA10IA070](https://openairdocs.org/sdr/C2XA10IA070), Feb 17, 2010: SELECTOR. MALFUNCTIONED. IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT 
- [SDR C2XA10IA069](https://openairdocs.org/sdr/C2XA10IA069), Feb 17, 2010: ELECTRONIC UNIT. DEFECTIVE. IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT 
- [SDR C2XA10IA061](https://openairdocs.org/sdr/C2XA10IA061), Feb 11, 2010: SELECTOR. INOPERATIVE. DFW - FLIGHT 2114 DURING CLIMB THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE, AND THREE RED X'S ON THE EICAS. THE AIRCRAFT RETURNED TO DFW WHERE
- [SDR C2XA09IA282](https://openairdocs.org/sdr/C2XA09IA282), Nov 3, 2009: A/C PACK. OVERHEATED. IAH - FLIGHT 2030, DURING TAXI THE CREW REPORTED THAT THE NUMBER ONE PACK OVERHEATED WITH A BURNING ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE
- [SDR C2XA09IA229](https://openairdocs.org/sdr/C2XA09IA229), Sep 12, 2009: SEAL. DEFECTIVE. IAH - DURING CLIMB THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE WINDSHIELD AREA. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTEN
- [SDR C2XA09IA208](https://openairdocs.org/sdr/C2XA09IA208), Aug 20, 2009: CONNECTOR. BURNED. FLIGHT 2526, DURING TAXI THE CREW REPORTED A STRONG ELECTRICAL PLASTIC BURNING ODOR COMING FROM THE GALLEY AREA. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTEN
- [SDR C2XA09IA168](https://openairdocs.org/sdr/C2XA09IA168), Jun 29, 2009: ELECTRONIC UNIT. INOPERATIVE. IAH - FLIGHT 2605 - THE CREW REPORTED A LANDING GEAR DISAGREE ON CLIMBOUT AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT I
- [SDR C2XA09IA164](https://openairdocs.org/sdr/C2XA09IA164), Jun 25, 2009: CONTROL HANDLE. INOPERATIVE. IAH - FLIGHT 2104 - THE CREW REPORTED WHEN COMMANDED GEAR SW TO UP, GEAR DID NOT RETRACT. TEN TO FIFTEEN SECONDS LATER CREW RECEIVED A LANDING GEAR LEVER DISAGR
- [SDR C2XA09SH164](https://openairdocs.org/sdr/C2XA09SH164), May 13, 2009: FLOOR SUPPORT. CORRODED. DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED LT OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH163](https://openairdocs.org/sdr/C2XA09SH163), May 13, 2009: SILL. CORRODED. DURING C-CHECK. BAGGAGE DOOR CUTOUT LOWER SILL HAS CORROSION. REPAIRED CARGO LOWER SILL IAW IC 2009-145/03445. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH162](https://openairdocs.org/sdr/C2XA09SH162), May 13, 2009: FLOOR SUPPORT. CORRODED. DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED RT OMEGA BEAM IAW IC2009-145/00907. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH160](https://openairdocs.org/sdr/C2XA09SH160), May 4, 2009: FITTING. CRACKED. SHV - DURING C-CHECK FRAME 80 HAS CRACKED SHEAR CLIP BETWEEN STR 6-7R. MAINTENANCE REMOVED AND REPLACED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STR 6-7R IAW EMB-
- [SDR C2XA09SH159](https://openairdocs.org/sdr/C2XA09SH159), May 4, 2009: HINGE BRACKET. WORN. SHV - DURING C-CHECK RT AILERON NR 2 HINGE FROM O/B HAS MIGRATED BUSHINGS. REMOVED AND REPLACED RT AILERON NR 2 HINGE FROM O/B SUPPORT BRACKET ASSY IAW EMB-145 
- [SDR C2XA09SH158](https://openairdocs.org/sdr/C2XA09SH158), May 4, 2009: SUPPORT BRACKET. WORN. SHV - DURING C-CHECK RT AILERON NR 1 HINGE FROM O/B HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED RT AILERON NR 1 HINGE FROM O/B SUPPORT BRACKET ASSY (
- [SDR C2XA09SH157](https://openairdocs.org/sdr/C2XA09SH157), May 4, 2009: SUPPORT BRACKET. DAMAGED. SHV - DURING C-CHECK RT AILERON MOST O/B HINGE BRACKET I/B HOUSING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON MOST O/B HINGE SUPPORT BRACKET ASSY IAW 
- [SDR C2XA09IA095](https://openairdocs.org/sdr/C2XA09IA095), Apr 6, 2009: ACTUATOR. SLOW. IAH - FLIGHT 2798, THE CREW REPORTED THE LANDING GEAR TOOK OVER 30 SECONDS TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL
- [SDR C2XA09IA067](https://openairdocs.org/sdr/C2XA09IA067), Feb 26, 2009: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, 
- [SDR C2XA09IA047](https://openairdocs.org/sdr/C2XA09IA047), Feb 13, 2009: WIRE. SHORTED. GPT - FLIGHT 2304 - THE CREW REPORTED AN ELECTRICAL BURNING SMELL BEING EMITTED FROM THE ELECTRICAL PANEL BEHIND THE CAPTAINS SEAT. THE AIRCRAFT LANDED AT GPT W
- [SDR C2XA08IA129](https://openairdocs.org/sdr/C2XA08IA129), May 14, 2008: WIRE. BROKEN. IAH - DURING MAINTENANCE INSPECTION THE 2ND AISLE PATH LIGHT STRIP ON THE FLOOR WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED L
- [SDR C2XA08TY033](https://openairdocs.org/sdr/C2XA08TY033), Mar 7, 2008: SKIN. CRACKED. A 1.26 LONG CRACK WAS DISCOVERED ON THE LT WING UPPER TRAILING EDGE SKIN ADJACENT TO THE CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01140. AIRCRAFT 
- [SDR C2XA08IA013](https://openairdocs.org/sdr/C2XA08IA013), Jan 7, 2008: SENSOR. BURNED. IAH - FLIGHT 2137, WHILE "SITTING AT THE GATE" THE CREW REPORTED A BURNT SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PITOT NUMBER ONE C
- [SDR C2XA07IA257](https://openairdocs.org/sdr/C2XA07IA257), Dec 27, 2007: SKIN. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT WING SKIN TO BE CRACKED AT THE SPOILER HINGE POINT. THE CRACK WAS INSPECTED AND PLACED ON DMI, AND 
- [SDR C2XA07SH096](https://openairdocs.org/sdr/C2XA07SH096), Nov 29, 2007: HYDRAULIC LINE. RUPTURED. SHV - FLT 2395, DURING CLIMB AND UPON MOVING THE LANDING GEAR SELECTOR TO RETRACT THE CREW OBSERVED A HYDRAULIC SYSTEM 1 ADVISORY. THE CREW MOVED THE LANDING GE
- [SDR C2XA07TY054](https://openairdocs.org/sdr/C2XA07TY054), Sep 21, 2007: BULB. INOPERATIVE. EMERGENCY LIGHT IN SERVICE DOOR AND AT SEAT 12 BC AT TOP INOP. REMOVED AND REPLACED BULBS IAW EMB 145 AMM 33-50-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURN
- [SDR C2XA06SH120](https://openairdocs.org/sdr/C2XA06SH120), Nov 4, 2006: SKIN. CORRODED. SHV - DURING C-CHECK THE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS FOUND TO BE ERRODED AND HAVE PITTING CORROSION ON THE UPPER AND LOWER SURFACES. MAINTENANCE
- [SDR C2XA06SH121](https://openairdocs.org/sdr/C2XA06SH121), Nov 1, 2006: INTAKE. CORRODED. SHV - DURING C-CHECK THE NR 2 ENGINE INTAKE FLANGE WAS FOUND TO BE CORRODED AROUND THE BOLT HOLES. MAINTENANCE REMOVED AND REPLACED THE INTAKE IAW EMB 145 AMM 7
- [SDR C2XA06SH118](https://openairdocs.org/sdr/C2XA06SH118), Oct 31, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 24 AND 29. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED SHIM FILLER REPAIRS
- [SDR C2XA06SH117](https://openairdocs.org/sdr/C2XA06SH117), Oct 31, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE CLEANED THE AREAS OF CORROSION AND FOUND THE DAMAGE TO 
- [SDR C2XA06SH116](https://openairdocs.org/sdr/C2XA06SH116), Oct 30, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLES. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A D
- [SDR C2XA06SH119](https://openairdocs.org/sdr/C2XA06SH119), Oct 30, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB
- [SDR C2XA06IA095](https://openairdocs.org/sdr/C2XA06IA095), Jun 18, 2006: BEARING. FAILED. VCT - FLIGHT 2482, THE CREW REPORTED A LAV SMOKE WARNING FOLLOWED BY A LOW OIL PRESSURE INDICATION, AND AN ENGINE 2 FIRE WARNING. THE CREW SHUTDOWN THE NUMBER T
- [SDR C2XA05IA064](https://openairdocs.org/sdr/C2XA05IA064), Apr 27, 2005: RELAY. FAILED. IAH - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL ON TAKEOFF AND A WEIGHT ON WHEEL FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. 
- [SDR C2XA05IA063](https://openairdocs.org/sdr/C2XA05IA063), Apr 26, 2005: CONTROL UNIT. INOPERATIVE. CRP - THE CREW REPORTED THAT DURING TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOV

All 142: https://openairdocs.org/deregistered/N14930-2020-02-28/reports.md

## FAA accident and incident reports (1)

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 20010825024299I](https://openairdocs.org/incident/20010825024299I), Aug 25, 2001: Emb EMB145ER (N14930), Kansas City, MO. (-23) An express jet (dba Continental express) Embraer EM-145, flight #4269, enroute from cle to mci, according to the situation report-preliminary incident…

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