# N578RP: 2004 Embraer EMB-145LR, registration cancelled 2018-08-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 8, 2018 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - 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: 14500865 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 30, 2004 - Certificate issued: January 12, 2017 - Last registry action: May 8, 2018 - Mode S code: A76DA6 - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N578RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=578RP - Page: https://openairdocs.org/deregistered/N578RP-2018-08-08 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-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201505290423](https://openairdocs.org/sdr/UHLA201505290423), May 29, 2015: STRIKER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AROUND THE LOWER CARGO DOOR STRIKER PLATE ON FRAME 65. THE CORROSION WAS REPAIRED IAW ETD2015-145-045228. - [SDR UHLA201505290422](https://openairdocs.org/sdr/UHLA201505290422), May 29, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA201505290421](https://openairdocs.org/sdr/UHLA201505290421), May 29, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE SERVICE DOOR THRESHOLD BEAM. THE THRESHOLD WAS REPLACED IAW SRM 51-40-02. - [SDR UHLA201505290420](https://openairdocs.org/sdr/UHLA201505290420), May 29, 2015: SHEAR TIE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65. THE SHEAR TIE SECTION AT FRAME 65 WAS REPAIRED IAW ETD2015-145-045228. - [SDR CHQA20141018297](https://openairdocs.org/sdr/CHQA20141018297), Oct 18, 2014: BATTERY. DISCHARGED. DURING INSPECTION THE NR 2 EMER LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. THE BATTERY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130717278](https://openairdocs.org/sdr/CHQA20130717278), Jul 17, 2013: BATTERY PACK. INOPERATIVE. DURING INSPECTION, EMEREGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 BATTERY PACK. OPS CHECKED GOOD. - [SDR CHQA20130508166](https://openairdocs.org/sdr/CHQA20130508166), May 8, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM SURFACE AT THE FORWARD NUT PLATE HOLE FOR THE GUSSET AT FRAME 20. THE RIGHT OMEGA BEAM AT FRAME 2 - [SDR CHQA20130506170](https://openairdocs.org/sdr/CHQA20130506170), May 6, 2013: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 22 BETWEEN STRINGERS 15L AND 16L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-30-01 - [SDR CHQA20130506169](https://openairdocs.org/sdr/CHQA20130506169), May 6, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PREVIOUS REPAIR OF LEFT OMEGA INBOARD SIDE AT FRAME 20. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-1 - [SDR CHQA20130506168](https://openairdocs.org/sdr/CHQA20130506168), May 6, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA INBOARD SIDE AT CARBON CROSSMEMBER AT FRAME 29. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20130506167](https://openairdocs.org/sdr/CHQA20130506167), May 6, 2013: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SCREW HOLES ON THE SERVICE DOOR LOWER BEAM. THE SERVICE DOOR LOWER BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-21- - [SDR CHQA20130322088](https://openairdocs.org/sdr/CHQA20130322088), Mar 22, 2013: ENGINE. LEAKING. CREW REPORTED A LAVATORY SMOKE INDICATION DURING TAKEOFF. THE CREW REPORTED FURTHER THAT THERE WAS NO VISIBLE SMOKE OR ODOR IN THE AIRCRAFT. THE CREW RETURNED T - [SDR CHQA20130308072](https://openairdocs.org/sdr/CHQA20130308072), Mar 8, 2013: WARNING SYSTEM. FALSE ACTIVATION. CREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE MESSAGE ON CLIMBOUT. NO SMOKE WAS DETECTED IN THE CABIN AND NO SMOKE ODORS WERE PRESENT. THE CREW DECLARED AN - [SDR CHQA20130124024](https://openairdocs.org/sdr/CHQA20130124024), Jan 24, 2013: SMOKE DETECTOR. FALSE ACTIVATION. CREW REPORTED THAT AFTER TAKEOFF WITH THE LANDING GEAR RETRACTED, THEY RECEIVED A LAVATORY SMOKE WARNING INDICATION. NO VISIBLE SMOKE, VAPOR, OR ODOR WAS NOTED. - [SDR CHQA20120212050](https://openairdocs.org/sdr/CHQA20120212050), Feb 12, 2012: BATTERY. DISCHARGED. CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHTS HAD BEEN LEFT ON OVERNIGHT. MANY OF THE LIGHTS WERE DIM AND OTHER WERE INOPERATIVE. MAINT - [SDR CHQA20120212049](https://openairdocs.org/sdr/CHQA20120212049), Feb 12, 2012: BATTERY. DISCHARGED. CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHTS HAD BEEN LEFT ON OVERNIGHT. MANY OF THE LIGHTS WERE DIM AND OTHER WERE INOPERATIVE. MAINT - [SDR CHQA20120212048](https://openairdocs.org/sdr/CHQA20120212048), Feb 12, 2012: BATTERY. DISCHARGED. CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHTS HAD BEEN LEFT ON OVERNIGHT. MANY OF THE LIGHTS WERE DIM AND OTHER WERE INOPERATIVE. MAINT - [SDR CHQA20120212047](https://openairdocs.org/sdr/CHQA20120212047), Feb 12, 2012: BATTERY. DISCHARGED. CREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHTS HAD BEEN LEFT ON OVERNIGHT. MANY OF THE LIGHTS WERE DIM AND OTHER WERE INOPERATIVE. MAINT - [SDR CHQA20120207043](https://openairdocs.org/sdr/CHQA20120207043), Feb 7, 2012: DOOR. OUT OF ADJUST. CREW REPORTED THAT DURING CLIMB AND DESCENT THERE WAS AN AUDIBLE VIBRATION COMING FROM THE NOSE LANDING GEAR AREA. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTEN - [SDR CHQA201100461](https://openairdocs.org/sdr/CHQA201100461), Nov 28, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE EMERGENCY LIGHT STRIPS AT THE AFT OF THE CABIN AND THE LEFT OVERWING AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MA - [SDR CHQA201100217](https://openairdocs.org/sdr/CHQA201100217), Jun 7, 2011: BRAKE ASSY. WORN. CREW REPORTED THAT WHEN THE LANDING GEAR WAS SELECTED DOWN, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS. FURTHER REPORTED THAT WHEN THE BRAKES WERE APPLIED B - [SDR CHQA201100188](https://openairdocs.org/sdr/CHQA201100188), May 23, 2011: ANTI-ICE VALVE. INOPERATIVE. CREW REPORTED THAT DURING FLIGHT RECEIVED AN ENGINE 2 ANTI-ICE VALVE FAIL MESSAGE AND A WING ANTI-ICE FAIL MESSAGE ON THE EICAS. THE CREW DIVERTED TO KSDF AND L - [SDR CHQA201100136](https://openairdocs.org/sdr/CHQA201100136), Apr 15, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERA - [SDR CHQA201000121](https://openairdocs.org/sdr/CHQA201000121), Jun 11, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 BATTERY WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000118](https://openairdocs.org/sdr/CHQA201000118), Jun 10, 2010: INVERTER. FAULTY. DURING INSPECTION, THE LAST 3 FLOOR PROXIMITY LIGHT STRIPS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE DC/AC INVERTER NR 6 WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000001](https://openairdocs.org/sdr/CHQA201000001), Jan 2, 2010: UNKNOWN. SMOKE. AFTER TAKEOFF THE CREW REPORTED SMOKE IN THE COCKPIT THAT SMELLED LIKE CHEMICALS. BY THE TIME THE AIRCRAFT WAS PREPARED FOR LANDING THE SMOKE HAD COMPLETELY DIS - [SDR CHQA200900268](https://openairdocs.org/sdr/CHQA200900268), Dec 28, 2009: SOLENOID VALVE. DEFECTIVE. AFTER TAKEOFF AND GEAR RETRACTION THE CREW REPORTED EXCESSIVE WIND NOISE COMING FROM THE NOSE LANDING GEAR AREA. THE FLIGHT CONTINUED BELOW 250KTS AND LANDED IN - [SDR CHQA200900237](https://openairdocs.org/sdr/CHQA200900237), Nov 2, 2009: PRESSURE SWITCH. FAILED. DURING CRUISE THE CREW REPORTED A YAW DAMPER AND AUTO PILOT FAIL FOLLOWED BY RUDDER 1 AND RUDDER 2 FAIL MESSAGES. THE QRH WAS FOLLOWED AND THE YAW DAMP MESSAGE - [SDR CHQA200900236](https://openairdocs.org/sdr/CHQA200900236), Nov 2, 2009: INDICATOR. FAILED. THE FLIGHT CREW REPORTED THAT AS THE AIRCRAFT ROTATED FOR TAKEOFF, THE INTEGRATED STANDBY INSTRUMENT SYSTEM FAILED. THE AIRCRAFT RETURNED TO FIELD AND LANDED WI - [SDR CHQA200800107](https://openairdocs.org/sdr/CHQA200800107), Jun 7, 2008: PROXIMITY SENSOR. INOPERATIVE. FLIGHT 6351, BNA TO MCO. JUST AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND A LOUD NOISE AND VIBRATION CAME FROM THE NOSE OF THE ACFT. THE GEAR INDICATED 3 - [SDR CHQA200800091](https://openairdocs.org/sdr/CHQA200800091), May 1, 2008: SWITCH. DIRTY. FLIGHT 6243, HSV TO CVG, DURING CRUISE THE AUTOPILOT DISENGAGED ASSOCIATED WITH PITCH TRIM MAIN AND BACKUP INOP MESSAGES ON EICAS. THE FLIGHT CREW PERFORMED THE - [SDR CHQA200500216](https://openairdocs.org/sdr/CHQA200500216), Dec 19, 2005: SWITCH. STICKING. EMERGENCY FLOOR LIGHTING BETWEEN ROWS 8-12 PULSATES ON AND OFF WITH COCKPIT SWITCH IN ARMED POSITION. FOUND TEST SWITCH STICKY, CLEANED. OPS CHECK GOOD IAW EMB - [SDR CHQA200500214](https://openairdocs.org/sdr/CHQA200500214), Dec 19, 2005: BATTERY. INOPERATIVE. EMERGENCY LIGHT CONTROLLED BY NR 3 BATTERY FLICKERS IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NR 3 IAW EMB 145 MM 33-50-04. OPS CHE - [SDR CHQA200500157](https://openairdocs.org/sdr/CHQA200500157), Sep 3, 2005: SOLENOID. UNSERVICEABLE. FLIGHT 6360 - MCO -LIT - EN ROUTE FROM MCO TO LIT, NOSE GEAR DOORS OPENED UNCOMANDED. ALSO DOOR CMD CIRCUIT BREAKER POPPED. INITIALLY SLOWED TO 210 KTS. FOUND N - [SDR CHQA200500008](https://openairdocs.org/sdr/CHQA200500008), Jan 14, 2005: ENGINE. LEAKING. FLIGHT 6374 CHM-LGA - ON INITIAL CLIMB-OUT OF CMH AT 1000 FEET, LAV SMOKE MESSAGE APPEARED ON EICAS WITH THE ASSOCIATED TRIPLE CHIME. THE FLIGHT ATTENDANT CALLE - [SDR CHQA200500003](https://openairdocs.org/sdr/CHQA200500003), Jan 12, 2005: SMOKE DETECTOR. DIRTY. FLIGHT 6450 IND TO CVG - DURING CLIMB-OUT, A LAV SMOKE WARNING MESSAGE BRIEFLY APPEARED ON EICAS. THE FLIGHT ATTENDANT INSPECTED THE LAV AND FOUND NO EVIDENCE O - [SDR CHQA200500002](https://openairdocs.org/sdr/CHQA200500002), Jan 11, 2005: ODOR. DETECTED. AFTER TAKEOFF, A LAV SMOKE WARNING MESSAGE APPEARED ON EICAS. A SHORT TIME LATER A ODOR AND HAZE WERE NOTED IN THE COCKPIT. AFTER ACCOMP CABIN FIRE AND SMOKE PR ## 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 20100216027169I](https://openairdocs.org/incident/20100216027169I), Feb 16, 2010: Embraer EMB-145LR (N578RP), Newark, NJ, No damage. Captain stated that at approximately 50 KTS on the take-off roll, smoke started to emit from the cockpit vents and smoke alarm warnings sounded. The take-off… --- 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.