# N14508: 2000 Embraer EMB-135ER, 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-135ER](https://openairdocs.org/model/embraer-emb-135er) (registry code 3260307) - 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: 145220 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 5, 2000 - Certificate issued: May 3, 2016 - Last registry action: May 3, 2016 - Mode S code: A0B7BC - Owner when cancelled: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC) - Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago) - Owner type: Corporation - Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14508 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14508 - Page: https://openairdocs.org/deregistered/N14508-2019-09-06 From the FAA registry file of November 7, 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-135ER: https://openairdocs.org/model/embraer-emb-135er.md ## Service difficulty reports (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C2XA08CL071](https://openairdocs.org/sdr/C2XA08CL071), Jun 15, 2008: CARBON SEAL. LEAKING. CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDIN - [SDR C2XA08RI037](https://openairdocs.org/sdr/C2XA08RI037), Mar 19, 2008: CONTROL UNIT. DEFECTIVE. FLIGHT 2424 - EWR - CREW REPORTED BRAKES INEFFECTIVE AT HIGH SPEED AFTER LANDING. BRAKE DEGRADE MESSAGE ON EICAS APPEARED MOMENTARILY, AND THEN DISAPPEARED, BUT - [SDR C2XA07TY089](https://openairdocs.org/sdr/C2XA07TY089), Dec 26, 2007: FLASHLIGHT. INOPERATIVE. NR 3 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT LAMP IAW EMB 135 VCMM 25-60-02. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA07TY085](https://openairdocs.org/sdr/C2XA07TY085), Dec 18, 2007: BATTERY. DISCHARGED. FA FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IAW EMB 135 AMM 33-50-16. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA07RI063](https://openairdocs.org/sdr/C2XA07RI063), Jul 26, 2007: HYDRAULIC LINE. LEAKING. FLT 4923 - EWR - AT MLG RETRACTION, CREW REPORTED THAT RT MLG RETRACTED FASTER THAN LF MLG CAUSING YAW MOTION TO THE RIGHT. EWR MX REMOVED AND REPLACED MLG ACTU - [SDR C2XA06SH101](https://openairdocs.org/sdr/C2XA06SH101), Oct 9, 2006: SKIN PANEL. DAMAGED. SHV - MAJOR - DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CREASED FORWARD OF FR 9 AND BELOW STR 15R. AFTER INITIAL REWORK THE AREA WAS STILL CRE - [SDR C2XA06SH100](https://openairdocs.org/sdr/C2XA06SH100), Oct 7, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR - [SDR C2XA06CL024](https://openairdocs.org/sdr/C2XA06CL024), Feb 14, 2006: LAMP. INOPERATIVE. DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA05CL077](https://openairdocs.org/sdr/C2XA05CL077), Sep 6, 2005: ACM. DEFECTIVE. CLE FLIGHT NR 2268, CREW REPORTED, SAW AND SMELLED SMOKE IN THE AIRCRAFT WITH PACK NR 1 ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AIR CYCLE MACHIN - [SDR C2XA04TY091](https://openairdocs.org/sdr/C2XA04TY091), Jun 17, 2004: BULB. BURNED OUT. DURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR - [SDR C2XA04CL041](https://openairdocs.org/sdr/C2XA04CL041), Apr 24, 2004: ENGINE. FAILED. CLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND - [SDR C2XA04SH113](https://openairdocs.org/sdr/C2XA04SH113), Feb 27, 2004: CONTROL PANEL. INOPERATIVE. SHV- DURING C-CHECK THE EMERGENCY LIGHT PUSH BUTTON ON THE FLIGHT ATTENDANTS CONTROL PANEL WOULD NOT OPERATE THE EMERGENCY LIGHTING TEST. MAINTENANCE REMOVED AN - [SDR C2XA04SH108](https://openairdocs.org/sdr/C2XA04SH108), Feb 26, 2004: SUPPORT. CORRODED. DURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED - [SDR C2XA04SH107](https://openairdocs.org/sdr/C2XA04SH107), Feb 26, 2004: STRINGER. CORRODED. SHV- DURING C-CHECK THE CENTER OMEGA BEAM STRINGER FROM FRAMES 22 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB - [SDR C2XA04SH106](https://openairdocs.org/sdr/C2XA04SH106), Feb 26, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 - [SDR C2XA04SH105](https://openairdocs.org/sdr/C2XA04SH105), Feb 26, 2004: HINGE BRACKET. CORRODED. SHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC - [SDR C2XA04SH104](https://openairdocs.org/sdr/C2XA04SH104), Feb 26, 2004: CROSSBEAM. CORRODED. SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL - [SDR C2XA04SH103](https://openairdocs.org/sdr/C2XA04SH103), Feb 26, 2004: SKIN. CHAFED. SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMA - [SDR C2XA04SH102](https://openairdocs.org/sdr/C2XA04SH102), Feb 26, 2004: STIFFENER. CHAFED. SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW - [SDR C2XA04SH088](https://openairdocs.org/sdr/C2XA04SH088), Feb 20, 2004: STRUCTURE. CHAFED. SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 135 SRM 5 - [SDR C2XA04SH087](https://openairdocs.org/sdr/C2XA04SH087), Feb 20, 2004: STRUCTURE. CHAFED. SHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW E - [SDR C2XA04SH086](https://openairdocs.org/sdr/C2XA04SH086), Feb 20, 2004: FLOORBEAM. CORRODED. SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1S - [SDR C2XA04SH085](https://openairdocs.org/sdr/C2XA04SH085), Feb 20, 2004: FLOORBEAM. CORRODED. SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAF - [SDR C2XA04SH084](https://openairdocs.org/sdr/C2XA04SH084), Feb 20, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT W - [SDR C2XA04SH083](https://openairdocs.org/sdr/C2XA04SH083), Feb 20, 2004: SPLICE. GOUGED. SHV- DURING C-CHECK STRINGER 19 LEFT INTERNAL SPLICE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 135 SRM 51-40-02. THE - [SDR C2XA04SH082](https://openairdocs.org/sdr/C2XA04SH082), Feb 20, 2004: ANGLE. CORRODED. SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCR - [SDR C2XA04SH081](https://openairdocs.org/sdr/C2XA04SH081), Feb 20, 2004: BRACKET. CORRODED. SHV- DURING C-CHECK THE PASSENGER DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. T - [SDR C2XA04SH080](https://openairdocs.org/sdr/C2XA04SH080), Feb 20, 2004: SILL. CORRODED. SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB 135 SRM 51-40-02. THE AIRC - [SDR C2XA04SH079](https://openairdocs.org/sdr/C2XA04SH079), Feb 20, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAF - [SDR C2XA04SH078](https://openairdocs.org/sdr/C2XA04SH078), Feb 20, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW E - [SDR C2XA04SH077](https://openairdocs.org/sdr/C2XA04SH077), Feb 20, 2004: STRINGER. GOUGED. SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02 AND EC 532 - [SDR C2XA04SH069](https://openairdocs.org/sdr/C2XA04SH069), Feb 16, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB1 - [SDR C2XA04SH068](https://openairdocs.org/sdr/C2XA04SH068), Feb 16, 2004: DOUBLER. CORRODED. SHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM - [SDR C2XA04SH067](https://openairdocs.org/sdr/C2XA04SH067), Feb 16, 2004: DOUBLER. CORRODED. SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM - [SDR C2XA04SH070](https://openairdocs.org/sdr/C2XA04SH070), Feb 16, 2004: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFEC - [SDR C2XA04SH060](https://openairdocs.org/sdr/C2XA04SH060), Feb 12, 2004: SILL. CORRODED. SHV-DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-4 - [SDR C2XA02CL145](https://openairdocs.org/sdr/C2XA02CL145), Jul 5, 2002: ODOR. DETECTED. CLE FLIGHT 3149 THE CREW REPORTED A BURNT RUBBER SMELL WITH THE PACK SYSTEM ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM. NO DE - [SDR C2XA02CL031](https://openairdocs.org/sdr/C2XA02CL031), Feb 3, 2002: FIREWALL. CRACKED. DURING ROUTINE MAINTENANCE THE APU FIREWALL WAS FOUND CRACKED AT UPPER RIGHT CORNER OF FIREWALL.THE FIREWALL WAS REPAIRED I/A/W EMBRAER GST-0401/02.THE AIRCRAFT - [SDR C2XA01CL232](https://openairdocs.org/sdr/C2XA01CL232), Nov 25, 2001: SMOKE WARNING. MALFUNCTIONED. CLE FLIGHT 3207 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSP - [SDR C2XA01TY160](https://openairdocs.org/sdr/C2XA01TY160), Oct 17, 2001: BULB. BURNED OUT. TYS During a scheduled inspection the overhead emergency light on right side was found out. Maintenance removed and replaced the bulb, operational checks good I - [SDR C2XA01CL197](https://openairdocs.org/sdr/C2XA01CL197), Aug 23, 2001: CONNECTOR. BURNED. CLE FLIGHT 3692 THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE GALLEY HOT JUG RECEPTACLE TO BE BURNT. THE RECEPTACLE CONNEC - [SDR C2XA01CL175](https://openairdocs.org/sdr/C2XA01CL175), Jul 25, 2001: ENGINE. FAILED. CLE FLIGHT 3722 THE CREW REPORTED THE NR 1 ENGINE FAILED AT 2800 FT WITH NO ABNORMAL INDICATIONS PRIOR TO FAILURE. THE AIRCRAFT DIVERTED TO CMH AND LANDED WITHO - [SDR C2XA01TY099](https://openairdocs.org/sdr/C2XA01TY099), Jul 19, 2001: STRINGER. CHAFED. TYS DURING A SCHEDULED INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 2412/ - [SDR C2XA01TY098](https://openairdocs.org/sdr/C2XA01TY098), Jul 19, 2001: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE, LOCATED JUST AFT OF COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCO - [SDR C2XA01CL089](https://openairdocs.org/sdr/C2XA01CL089), Apr 24, 2001: RECEPTACLE. BURNED. YYZ FLIGHT 3898 THE CREW REPORTED A BURNING SMELL FROM THE LEFT COFFEE JUG. MAINTENANCE REPLACED THE LEFT COFFEE JUG RECEPTACLE CONNECTOR. OPERATIONAL CHECKS WE - [SDR C2XA01TY061](https://openairdocs.org/sdr/C2XA01TY061), Mar 30, 2001: SKIN. DAMAGED. TYS DURING A SCHEDULED INSPECTION, THE LEFT HAND AFT FUSELAGE SKIN AT FRAME 74 BETWEEN STRINGERS 15L AND 17L WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE D ## Other aircraft with N14508 - [Cancelled 1978-11-15](https://openairdocs.org/deregistered/N14508-1978-11-15): Cessna TU206F, S/N U206-03110. Exported to Mexico. Owner: [Ray Bennie E](https://openairdocs.org/faa-owner/RAY%20BENNIE%20E), [Brownsville, TX](https://openairdocs.org/faa-place/TX/Brownsville) --- 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.