# N15941: 1997 Embraer EMB-145EP, registration cancelled 2016-03-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 15, 2016
- Status when cancelled: Valid registration
- 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: 145035
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: February 25, 1998
- Last registry action: January 27, 2015
- Mode S code: A0EE9C
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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/N15941
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15941
- Page: https://openairdocs.org/deregistered/N15941-2016-03-15

From the FAA registry file of October 31, 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 (126, newest 50)

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

- [SDR ASOA20140923120](https://openairdocs.org/sdr/ASOA20140923120), Sep 23, 2014: BATTERY PACK. DISCHARGED. DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE REPORTED TO BE INTERMITTENT WHEN TURNED ON BY THE F/A. MAINTENANCE CHARGED THE NR 4 EMERGENCY LIGHT BATTER
- [SDR ASOA20140414061](https://openairdocs.org/sdr/ASOA20140414061), Apr 14, 2014: BATTERY PACK. DISCHARGED. DURING MAINTENANCE INSPECTION, AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DE
- [SDR ASOA20140208021](https://openairdocs.org/sdr/ASOA20140208021), Feb 8, 2014: DISPLAY. FAILED. THE CREW REPORTED THE NR 2 MAIN FLIGHT DISPLAY WAS INOPERATIVE ACCOMPANIED BY AN ODOR OF AN ELECTRICAL FIRE WITH NO SMOKE DETECTED. MAINTENANCE R & R THE NR 2 M
- [SDR ASOA20131215218](https://openairdocs.org/sdr/ASOA20131215218), Dec 15, 2013: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 20A INOPERATIVE. R & R LIGHT, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130810198](https://openairdocs.org/sdr/ASOA20130810198), Aug 10, 2013: FIRE DETECTOR. DEFECTIVE. FIRE DETECTION FAIL MESSAGE ON EICAS DURING TAXI. R & R FIRE DETECTOR IAW AMM 26-11-01. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130719125](https://openairdocs.org/sdr/ASOA20130719125), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRAKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUYBLER REPAIR IAW EN
- [SDR ASOA20130719132](https://openairdocs.org/sdr/ASOA20130719132), Jul 19, 2013: SKIN. CRACKED. DURING INSPECTION, LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6L. MX PERFORMED A BUSHING REPAIR IAW ETD2013-145-019577, AND 
- [SDR ASOA20130719131](https://openairdocs.org/sdr/ASOA20130719131), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX PERFORMED A BUSHING REPAIR IAW DER APPRO
- [SDR ASOA20130719130](https://openairdocs.org/sdr/ASOA20130719130), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 4 PLACES AT A SINGLE RIVET ON FRAME 79 BELOW STRINGER 05L. MX PERFORMED A BUSHING R
- [SDR ASOA20130719129](https://openairdocs.org/sdr/ASOA20130719129), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A SINGLE RIVET ON FRAME 77 BELOW STRINGER 8L. MX PERFORMED A BUSHING RE
- [SDR ASOA20130719128](https://openairdocs.org/sdr/ASOA20130719128), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5R. MX PERFORMED A BUSHING REPAIR IAW DER APPROV
- [SDR ASOA20130719126](https://openairdocs.org/sdr/ASOA20130719126), Jul 19, 2013: SKIN. CRACKED. DURING INSPECTION, RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 BELOW STRINGER 02R. MX PERFORMED A FILLER/DOUBLER REPAIR IAW EA EC5330-02353,
- [SDR ASOA20130719127](https://openairdocs.org/sdr/ASOA20130719127), Jul 19, 2013: SKIN. CRACKED. DURING CYCLE CARD INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 3R. MX PERFORMED A BUSHING REPAIR IAW DER APPROV
- [SDR ASOA20130416055H](https://openairdocs.org/sdr/ASOA20130416055H), Apr 16, 2013: INVERTER. INOPERATIVE. DURING MX INSPECTION, THE EMERGENCY LIGHT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TES
- [SDR ASOA20130131257T](https://openairdocs.org/sdr/ASOA20130131257T), Jan 31, 2013: SKIN. CRACKED. ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 
- [SDR ASOA20121110137](https://openairdocs.org/sdr/ASOA20121110137), Nov 10, 2012: LAMP. BURNED OUT. DURING A CHECK INSPECTION, THE LT AFT OVERWRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED LAMP, OPERATIONALLY TESTED WITH NO DEFECTS NO
- [SDR ASOA20120711047V](https://openairdocs.org/sdr/ASOA20120711047V), Jul 11, 2012: YOKE. CRACKED. DURING C CHECK. RT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED RT ENGINE FWD LOWER YOKE IAW EC5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120711046](https://openairdocs.org/sdr/ASOA20120711046), Jul 11, 2012: YOKE. CRACKED. DURING C CHECK. LEFT FWD LOWER ENGINE YOKE IS CRACKED. REPAIRED LT FWD LOWER ENGINE YOKE IAW EC5450-01052. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11TY157](https://openairdocs.org/sdr/C2XA11TY157), Oct 14, 2011: SKIN PANEL. CRACKED. TYS - A/C WAS IN MOB WHEN A BELTLOADER HIT THE 191 BELLY PANEL AND CRACKED THE PANEL AFT OF THE PORTABLE WATER DOOR. A/C WAS FERRIED TO TYS WHERE THE COMPOSITE 
- [SDR C2XA11SH111](https://openairdocs.org/sdr/C2XA11SH111), Aug 1, 2011: COMPUTER. MALFUNCTIONED. AIRCRAFT 15941 FLIGHT 2734 AHRS 2 FAIL IAH-XNA DIVERTED TO SHV. SHV MAINTENANCE REMOVED AND REPLACED NUMBER 2 AHRS COMPUTER IAW 34-21-01, OPERATIONAL CHECK GOOD
- [SDR C2XA11IA165](https://openairdocs.org/sdr/C2XA11IA165), Jul 29, 2011: WARNING SYSTEM. FALSE ACTIVATION. IAH - FLIGHT 2734, DURING PREFLIGHT INSPECTION THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL INDICATION. MAINTENANCE RESET THE AIRCRAFT, AND THE INDICATION DID
- [SDR C2XA11IA147](https://openairdocs.org/sdr/C2XA11IA147), Jul 10, 2011: PROXIMITY SENSOR. INOPERATIVE. IAH - FLIGHT 2318, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT.
- [SDR C2XA11IA134](https://openairdocs.org/sdr/C2XA11IA134), Jun 28, 2011: WARNING SYSTEM. FALSE ACTIVATION. MEM - FLIGHT 2998, THE CREW REPORTED A LANDING GEAR AIR/GND FAIL MESSAGE WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE AIRCR
- [SDR C2XA11IA118](https://openairdocs.org/sdr/C2XA11IA118), Jun 15, 2011: CONTROL LEVER. FAULTY. IAH - CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. COULD NOT RAISE LANDING GEAR. AIRCRAFT AIR RETURNED AND LANDED UNEVENTFULLY. IC 1-2 WOW
- [SDR C2XA11IA090](https://openairdocs.org/sdr/C2XA11IA090), May 7, 2011: CONNECTOR. BURNED. IAH - POST FLIGHT 2812, THE CREW REPORTED ELECTRICAL SMOKE IN THE CABIN AND COCKPIT, AND SEEMED TO BE STRONGEST AROUND ROWS 8 & 9. IAH MAINTENANCE INSPECTED THE
- [SDR C2XA10IA261](https://openairdocs.org/sdr/C2XA10IA261), Sep 24, 2010: SKIN PANEL. CRACKED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO
- [SDR C2XA10IA127](https://openairdocs.org/sdr/C2XA10IA127), Apr 23, 2010: BALLAST. MALFUNCTIONED. MEM - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL BY ROWS 16-19. MAINTENANCE INSPECTED THE AIRCRAFT AND IDENTIFIED A BAD BALLAST
- [SDR C2XA10IA025](https://openairdocs.org/sdr/C2XA10IA025), Jan 17, 2010: FITTING. LEAKING. IAH - FLIGHT 2895, DURING CLIMB THE CREW REPORTED HYDRAULIC FLUID COMING FROM THE RT WING LOWER WEEP HOLE WHEN THE SPOILERS WERE ACTUATED. THE AIRCRAFT RETURNED
- [SDR C2XA09TY273](https://openairdocs.org/sdr/C2XA09TY273), Dec 14, 2009: TRUNNION. DAMAGED. RIGHT MLG AFT TRUNNION PITTED. REWORKED TRUNNION WITH BORE MACHINE IAW EC5750-01398.
- [SDR C2XA09IA187](https://openairdocs.org/sdr/C2XA09IA187), Jul 24, 2009: DUCT. LEAKING. IAH - FLIGHT 2834, THE CREW REPORTED A BLEED 1 LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED TH
- [SDR C2XA09TY109](https://openairdocs.org/sdr/C2XA09TY109), Jun 12, 2009: MODULE. DEFECTIVE. TYS FOR IAH - THERE WAS INTERMITTENT OPERATION OF THE EMERGENCY LIGHTS IN ASSOCIATION WITH THE ECIAS SHOWING NOT ARMED. MAINTENANCE REMOVED AND REPLACED THE LIG
- [SDR C2XA09IA155](https://openairdocs.org/sdr/C2XA09IA155), Jun 11, 2009: CONTROL MODULE. INOPERATIVE. DAL - FLIGHT 2149, DURING PREFLIGHT INSPECTION THE GALLEY, EMERGENCY, AND LAV LIGHTS WERE FOUND TO BE INTERMITTENT, AND NOT OPERATING WITH THEIR RESPECTIVE SWIT
- [SDR C2XA09IA127A](https://openairdocs.org/sdr/C2XA09IA127A), May 15, 2009: LIGHT. INOPERATIVE. IAH - FLIGHT 2046, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS DO NOT ALWAYS ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND RE
- [SDR C2XA09IA070](https://openairdocs.org/sdr/C2XA09IA070), Mar 5, 2009: STRUT. LOW. IAH - FLIGHT 2003 THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE NOSE
- [SDR C2XA08TY086](https://openairdocs.org/sdr/C2XA08TY086), Aug 19, 2008: BATTERY. DISCHARGED. NR 1 EMERGENCY LIGHT BATTERY NOT CHARGING. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S)
- [SDR C2XA08IA008](https://openairdocs.org/sdr/C2XA08IA008), Jan 2, 2008: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION EMERGENCY FLOOR LIGHT STRIP NR 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPE
- [SDR C2XA07IA189](https://openairdocs.org/sdr/C2XA07IA189), Sep 3, 2007: UNKNOWN. ODOR. LFT - FLIGHT 2734, DURING PREFLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND THE ODOR TO BE C
- [SDR C2XA07IA173](https://openairdocs.org/sdr/C2XA07IA173), Jul 24, 2007: INVERTER. INOPERATIVE. IAH - FLIGHT 2533, DURING POSTFLIGHT INSPECTION THE RIGHT HAND EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIV
- [SDR C2XA07TY029](https://openairdocs.org/sdr/C2XA07TY029), Jun 12, 2007: SKIN. DENTED. DENT ON FUSELAGE SKIN AFT OF PAX DOOR. CUT OUT DAMAGE, FABRICATED FILLER & DOUBLER AND INSTALLED IAW EMB 134/145 SRM 51-20-03, 51-40-06, 51-40-02, 53-21-01 & CP
- [SDR C2XA07TY028](https://openairdocs.org/sdr/C2XA07TY028), Jun 10, 2007: RIB. DENTED. LEFT LWR COWL DENTED. REMOVED AND REPLACED DAMAGED RIB IN CENTER SECTION OF COWL, RECON TOURED DENTS AT OIL SERVICE DOOR, FABRICATED AND INSTALLED EXTERNAL DOUB
- [SDR C2XA07TY027](https://openairdocs.org/sdr/C2XA07TY027), Jun 8, 2007: DOOR FRAME. CRACKED. FRAME 68 CRACKED UNDERNEATH CARGO DOOR -HOLD OPEN- HANDLE RETAINING CUP. CUT OUT AFFECTED FRAME, FABRICATED THE FRAME REPAIR SEGMENT FROM A SECTION OF A NEW FRA
- [SDR C2XA05TY031](https://openairdocs.org/sdr/C2XA05TY031), Mar 24, 2005: FLOOR SUPPORT. CORRODED. TYS DURING A C-CHECK INSPECTION THE CENTER AISLE SUPPORT STRUCTURE ON THE LEFT SIDE WAS FOUND WITH CORROSION FROM FRAME 20 TO 60. MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA05TY030](https://openairdocs.org/sdr/C2XA05TY030), Mar 23, 2005: FITTING. LOOSE. DURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE D
- [SDR C2XA05TY029](https://openairdocs.org/sdr/C2XA05TY029), Mar 20, 2005: FRAME. DAMAGED. TYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INT
- [SDR C2XA05TY028](https://openairdocs.org/sdr/C2XA05TY028), Mar 20, 2005: FITTING. CORRODED. TYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, D
- [SDR C2XA04CL125](https://openairdocs.org/sdr/C2XA04CL125), Dec 8, 2004: WIRE. BROKEN. CLE FLIGHT 2481 THE CREW REPORTED THE EMERGENCY LIGHTS AT THE CENTER OF THE AIRCRAFT WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES IN THE CE
- [SDR C2XA04BT115](https://openairdocs.org/sdr/C2XA04BT115), Oct 30, 2004: INVERTER. FAULTY. CREW REPORTED, EMERGENCY EXIT LIGHT INVERTER INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS CHECKED GOOD. 
- [SDR C2XA04SD009](https://openairdocs.org/sdr/C2XA04SD009), Oct 19, 2004: BULB. INOPERATIVE. DURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CHECK GOOD.
- [SDR C2XA04SH459](https://openairdocs.org/sdr/C2XA04SH459), Jul 9, 2004: CONTROL VALVE. INOPERATIVE. SHV - DURING TAXI TO THE GATE BRK OUTBD INOP WAS OBSERVED ON THE EICAS. CREW RESET THE CIRCUIT BREAKERS AND THE MESSAGE WENT AWAY. DURING TAXI TO THE HANGER THE
- [SDR C2XA03CL206](https://openairdocs.org/sdr/C2XA03CL206), Dec 20, 2003: CONTROL PANEL. FAULTY. CLE FLIGHT 3253 THE CREW REPORTED THE EMERGENCY LIGHT AISLE PATH LIGHTING STAYED ON. MAINTENANCE REPLACED THE FLIGHT ATTENDANT'S CONTROL PANEL. OPERATIONAL CHEC

All 126: https://openairdocs.org/deregistered/N15941-2016-03-15/reports.md

## Other aircraft with N15941

- [Cancelled 1991-01-30](https://openairdocs.org/deregistered/N15941-1991-01-30): Grumman E-2C, S/N 158641. Administratively canceled. Owner: [US Customs Service](https://openairdocs.org/faa-owner/US%20CUSTOMS%20SERVICE), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington)

---
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.