# N29515: 2000 Embraer EMB-135LR, registration cancelled 2018-10-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 30, 2018 - Exported to: Angola - Status when cancelled: Valid registration - Airframe: [Embraer EMB-135LR](https://openairdocs.org/model/embraer-emb-135lr) (registry code 3260305) - 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: 145309 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 24, 2000 - Certificate issued: August 1, 2018 - Last registry action: August 1, 2018 - Mode S code: A30AA6 - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N29515 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=29515 - Page: https://openairdocs.org/deregistered/N29515-2018-10-30 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-135LR: https://openairdocs.org/model/embraer-emb-135lr.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141004122](https://openairdocs.org/sdr/ASOA20141004122), Oct 4, 2014: FAN. OVERHEATED. THE CREW REPORTED THAT THE NAV CIRCUIT BREAKER TRIPPED DURING CLIMBOUT, AND AN ELECTRICAL BURNING ODOR AT 17,000 FT. THE ACFT DIVERTED AND LANDED WITHOUT INCIDE - [SDR ASOA20140915116](https://openairdocs.org/sdr/ASOA20140915116), Sep 15, 2014: INVERTER. INOPERATIVE. DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 2 AND 3 AISLE PATH FLOOR LIGHT STRIPS WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 3 EMERGENCY LI - [SDR ASOA20140704088](https://openairdocs.org/sdr/ASOA20140704088), Jul 4, 2014: SOLENOID VALVE. MALFUNCTIONED. THE CREW REPORTED THAT THE NLG DOOR OPENED UNCOMMANDED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NLG DOOR SOLENOID VALVE, OPS TESTED WITH NO DEF - [SDR ASOA20131215221](https://openairdocs.org/sdr/ASOA20131215221), Dec 15, 2013: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, FORWARD THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND ACFT - [SDR C2XA08IA149](https://openairdocs.org/sdr/C2XA08IA149), Jul 2, 2008: DOOR. OUT OF ADJUST. IAH - FLIGHT 2975, THE CREW REPORTED THAT THE MAIN CABIN DOOR GETS HUNG UP WHEN OPENING ON THE UPPER RT. MAINTENANCE ADJUSTED THE PAX DOOR, OPERATIONALLY CHECKE - [SDR C2XA08IA141](https://openairdocs.org/sdr/C2XA08IA141), Jun 10, 2008: UNKNOWN. ODOR. IAH - FLIGHT 2386, DURING POST FLIGHT INSPECTION THE FLIGHT ATTENDANT REPORTED A BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, NR 2 PACK SYSTEM, AN - [SDR C2XA08IA117](https://openairdocs.org/sdr/C2XA08IA117), Apr 21, 2008: LIGHT. DISCONNECTED. IAH - DURING MAINTENANCE INSPECTION A FLOOR PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHT STRIP ON MEL - [SDR C2XA07IA175](https://openairdocs.org/sdr/C2XA07IA175), Jul 26, 2007: INVERTER. INOPERATIVE. IAH -FLIGHT 2487, DURING CREW INSPECTION THE RT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 5 EMERGENCY LIGHT I - [SDR C2XA07IA059](https://openairdocs.org/sdr/C2XA07IA059), Mar 8, 2007: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGE - [SDR C2XA06IA153](https://openairdocs.org/sdr/C2XA06IA153), Sep 19, 2006: CONNECTOR. LOOSE. IAH - FLIGHT 2063, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL CAUTION ON CLIMB AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE - [SDR C2XA06IA130](https://openairdocs.org/sdr/C2XA06IA130), Aug 15, 2006: LANDING GEAR. UNDERSERVICED. IAH - FLIGHT 2703, THE CREW REPORTED A AIR/GROUND FAIL MESSAGE ON GEAR RETRACTION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE IN - [SDR C2XA06IA042](https://openairdocs.org/sdr/C2XA06IA042), Mar 19, 2006: CONNECTOR. DEFECTIVE. IAH - FLIGHT 2164, THE CREW REPORTED A LANDING GEAR AIR/DRND FAILURE AFTER T/O, AND THAT THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE - [SDR C2XA04TY058](https://openairdocs.org/sdr/C2XA04TY058), Mar 28, 2004: SILL. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOOR SUPPORT FRAME WAS CORRODED AT FR 20 AND FR 21. MAINT REMOVED AND REPLACED THE LEFT FORWARD SILL IN THE AFFEC - [SDR C2XA04TY057](https://openairdocs.org/sdr/C2XA04TY057), Mar 28, 2004: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOORBEAM CAP HAD AREAS OF CORROSION AT FR 19-23. MAINT REMOVED AND REPLACED THE LEFT FLOORBEAM TOP CAP IAW EMB 13 - [SDR C2XA03TY102](https://openairdocs.org/sdr/C2XA03TY102), Jul 30, 2003: ENGINE. LACK OF LUBE. THE LT ENGINE IMPENDING OIL BYPASS INFLIGHT. AFTER APPROXIMATELY 2 MINUTES OIL PRESSURE DROPPED INTO THE RED, 32 PSI AND DROPPING. THE CREW PERFORMED PRECAUTION - [SDR C2XA02CL146](https://openairdocs.org/sdr/C2XA02CL146), Jul 10, 2002: WIRE HARNESS. FAULTY. CLE FLIGHT 3462 THE CREW REPORTED A ELECTRICAL SMELL COMING FROM SIDE WALL PANEL AT ROW 4A. MAINTENANCE INSPECTED AND FOUND A MELTED PLASTIC CONNECTOR FOR THE C - [SDR C2XA02BT031](https://openairdocs.org/sdr/C2XA02BT031), Jul 10, 2002: HARNESS. FAULTY. DSM/EWR---CO3463, CREW REPORTED "BURNING SMELL COMING FROM SIDEWALL PANEL IN ROW 4 SEAT A....MAINTENANCE IN DSM RELEASED AIRCRAFT IAW MEL #33-20-00 CATEGORY "C" - [SDR C2XA02CL068](https://openairdocs.org/sdr/C2XA02CL068), Mar 8, 2002: LIGHT. INOPERATIVE. CLE FLIGHT 3237 THE CREW REPORTED 1 SECTION OF EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHTING SECTION. OP - [SDR C2XA02TY045](https://openairdocs.org/sdr/C2XA02TY045), Feb 22, 2002: WIRE. BROKEN. TYS, DURING A SCHEDULED 1C INSPECTION A BROKEN WIRE WAS FOUND ON EMERGENCY LIGHT STRIP ON PANEL 251DE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRI - [SDR C2XA02TY044](https://openairdocs.org/sdr/C2XA02TY044), Feb 21, 2002: SKIN. DENTED. TYS, DURING A SCHEDULED 1C INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF FR24, BELOW STR 10R. MAINTENANCE RE CONTOURED DENT, PERFORMED DYE-PENATRENT - [SDR C2XA02TY043](https://openairdocs.org/sdr/C2XA02TY043), Feb 21, 2002: PLATE. CORRODED. TYS, During a scheduled 1C inspection, corrosion was found on the forward digital plate aft of cockpit door. Maintenance removed the corrosion by cutting out th - [SDR C2XA02TY042](https://openairdocs.org/sdr/C2XA02TY042), Feb 21, 2002: BEAM. CORRODED. TYS, During a scheduled 1C inspection, corrosion was found on the left omega beam ar FR20 under the carbon fiber beam. Maintenance cut out the damage, fabricate - [SDR C2XA02TY041](https://openairdocs.org/sdr/C2XA02TY041), Feb 21, 2002: SUPPORT. CORRODED. TYS, During a scheduled 1C inspection, corrosion was found on the center omega beam ramp support between FR19-20. Maintenance removed and replaced the ramp supp - [SDR C2XA02TY040](https://openairdocs.org/sdr/C2XA02TY040), Feb 21, 2002: ANGLE. CORRODED. TYS, During a scheduled 1C inspection, corrosion was found on the support angle at main door entrance below the threshold strip. Maintenance removed and replace - [SDR C2XA02TY039](https://openairdocs.org/sdr/C2XA02TY039), Feb 21, 2002: FLOORBEAM. CORRODED. TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE AFT OF COCKPIT DOOR. MAINTENANCE REMOVED CORROSION BY CUTTING OUT THE CE - [SDR C2XA02TY038](https://openairdocs.org/sdr/C2XA02TY038), Feb 21, 2002: BEAM. CORRODED. TYS, During a scheduled 1C inspection, corrosion was found on the forward center omega beam galley area. Maintenance removed corrosion and replaced affected riv - [SDR C2XA02TY037](https://openairdocs.org/sdr/C2XA02TY037), Feb 20, 2002: FLOORBEAM. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION THE FORWARD DIGITAL PLATE AFT OF THE COCKPIT DOOR WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION BY CUTTING OUT THE - [SDR C2XA02TY035](https://openairdocs.org/sdr/C2XA02TY035), Feb 20, 2002: ANGLE. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE SUPPORT ANGLE AT THE MAIN DOOR ENTRANCE BELOW THE THRESHOLD. MAINTENANCE REMOVED AND REPLACED T - [SDR C2XA02TY034](https://openairdocs.org/sdr/C2XA02TY034), Feb 19, 2002: LEVER. GOUGED. TYS DURING A SCHEDULED 1-C INSPECTION THE RT SERVO TAB DOG BONE WAS FOUND WEARING INTO THE ELEVATOR SUPPORT BRACKET WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLIS - [SDR C2XA02TY033](https://openairdocs.org/sdr/C2XA02TY033), Feb 19, 2002: LEVER. GOUGED. TYS DURING A SCHEDULED 1-C INSPECTION THE LT SERVO TAB DOG BONE WAS FOUND WEARING AGAINST THE ELEVATOR SUPPORT BRACKET, WHICH REQUIRED A GST. ALL WORK WAS ACCOM - [SDR C2XA02TY032](https://openairdocs.org/sdr/C2XA02TY032), Feb 18, 2002: WIRE. BROKEN. TYS DURING A SCHEDULED 1-C INSPECTION A BROKEN WIRE WAS FOUND ON THE PROXIMITY LIGHT STRIP ON PANEL 251DF. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW - [SDR C2XA02TY031](https://openairdocs.org/sdr/C2XA02TY031), Feb 18, 2002: DUCT. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND BETWEEN THE OUTER BYPASS AND THE FAN CASE ON NR 2 ENGINE. MAINTENANCE CLEANED THE AFFECTED AREA, APPLI - [SDR C2XA02TY030](https://openairdocs.org/sdr/C2XA02TY030), Feb 18, 2002: SUPPORT. CORRODED. TYS DURING A SCHEDULED 1-C INSPECTION THE RAMP SUPPORT ON THE CENTER OMEGA BEAM BETWEEN FR'S 19 AND 20 HAS A AREA OF CORROSION. MAINTENANCE REMOVED AND REPLACED ## Other aircraft with N29515 - [Cancelled 1995-01-30](https://openairdocs.org/deregistered/N29515-1995-01-30): Cessna 177, S/N 17700937. Triennial form not returned. Owner: [Gasperich Rudolph](https://openairdocs.org/faa-owner/GASPERICH%20RUDOLPH), [Broadview, IL](https://openairdocs.org/faa-place/IL/Broadview) --- 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.