# N14938: 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: 145029
- 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 23, 1998
- Last registry action: January 29, 2015
- Mode S code: A0C701
- 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/N14938
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14938
- Page: https://openairdocs.org/deregistered/N14938-2016-03-15

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

## Service difficulty reports (87, newest 50)

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

- [SDR ASOA20140917117](https://openairdocs.org/sdr/ASOA20140917117), Sep 17, 2014: BULB. BURNED OUT. DURING MAINTENANCE INSPECTION THE LT WING AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DE
- [SDR ASOA20140807105](https://openairdocs.org/sdr/ASOA20140807105), Aug 7, 2014: LIGHT. INOPERATIVE. DURING A 3A INSPECTION, THE LT EMERGENCY LIGHT ON THE FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND TH
- [SDR ASOA20140514072](https://openairdocs.org/sdr/ASOA20140514072), May 14, 2014: ATTACH FITTING. DAMAGED. DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACI
- [SDR ASOA2014051400001](https://openairdocs.org/sdr/ASOA2014051400001), May 14, 2014: ATTACH FITTING. DAMAGED. DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACI
- [SDR ASOA20140319047](https://openairdocs.org/sdr/ASOA20140319047), Mar 19, 2014: LIGHT. INOPERATIVE. DURING PREFLIGHT, CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHT STRIP AT SEAT 4A WAS INOPERATIVE. R & R EMERGENCY LIGHT AND OPS TESTED WITH NO DEFECTS. APP
- [SDR ASOA20140311025](https://openairdocs.org/sdr/ASOA20140311025), Mar 11, 2014: SEAL. DEBONDED. EXPERIENCED CABIN DEPRESSURIZATION AT ALTITUDE AND THEN DIVERTED. MAINTENANCE FOUND CARGO DOOR RUBBER TRIM SEAL DEBONDED AND HANGING OUT IN THE AIRSTREAM. REINS
- [SDR ASOA20131216223](https://openairdocs.org/sdr/ASOA20131216223), Dec 16, 2013: SOCKET. SHORTED. THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN FRONT CABIN. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT SOCKET SHORTED AND MELTED. R & R AFFECTED 
- [SDR ASOA20130716124](https://openairdocs.org/sdr/ASOA20130716124), Jul 17, 2013: SKIN. CRACKED. DURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORME
- [SDR ASOA20130226025H](https://openairdocs.org/sdr/ASOA20130226025H), Feb 26, 2013: SKIN. CRACKED. DURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A .2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN 
- [SDR ASOA20121107123V](https://openairdocs.org/sdr/ASOA20121107123V), Nov 7, 2012: SILL. CORRODED. DURING C-CHECK, THE SERVICE DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107122V](https://openairdocs.org/sdr/ASOA20121107122V), Nov 7, 2012: HINGE FITTING. WORN. DURING C-CHECK, THE RUDDER LOWER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX OVERSIZED THE HOLES AND REPLACED THE HAT BU
- [SDR ASOA20121107121V](https://openairdocs.org/sdr/ASOA20121107121V), Nov 7, 2012: SKIN. CORRODED. DURING C-CHECK, THE CARGO DOOR LOWER INTERNAL SKIN WAS FOUND TO BE CORRODED AROUND THE BOTTOM NUT PLATES. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAI
- [SDR ASOA20121107120V](https://openairdocs.org/sdr/ASOA20121107120V), Nov 7, 2012: DOUBLER. CRACKED. DURING C-CHECK THE VERTICAL STAB DOUBLER BETWEEN FRAMES 80-81 AND STRINGERS 1L-1R WAS FOUND TO BE CRACKED. MX R & R THE DOUBLER IAW SRM 51-40-02. THE ACFT WAS A
- [SDR ASOA20121107119V](https://openairdocs.org/sdr/ASOA20121107119V), Nov 7, 2012: SHEAR TIE. CORRODED. DURING C-CHECK THE SHEAR TIE AT FRAME 19 BETWEEN STRINGERS 21L AND 21R WAS FOUND TO BE CORRODED. MX R & R THE SHEAR CLIP IAW EC5320-01713. ACFT APPROVED FOR RET
- [SDR ASOA20121107118V](https://openairdocs.org/sdr/ASOA20121107118V), Nov 7, 2012: SHEAR TIE. CRACKED. DURING C-CHECK THE CENTERLINE SHEAR TIE AT FRAME 42, 6:00 POSITION IN THE WING BOX WAS FOUND TO BE CRACKED. MX R & R THE SHEAR TIE IAW SRM 51-40-02. THE ACFT WA
- [SDR ASOA20121107117](https://openairdocs.org/sdr/ASOA20121107117), Nov 7, 2012: SKIN. CORRODED. DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-19 AND STRINGERS 21L-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR I
- [SDR ASOA20121001128HS](https://openairdocs.org/sdr/ASOA20121001128HS), Oct 1, 2012: WIRE HARNESS. CHAFED. DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. NARROWED DOWN TO CEILING LIGHTS 14A-18A. MX REPAIRED A CHAFED WIRE ON THE 
- [SDR ASOA20121001128](https://openairdocs.org/sdr/ASOA20121001128), Oct 1, 2012: LIGHT. ODOR. DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. FOUND TO BE CEILING LIGHTS 14A-18A. OPEN
- [SDR ASOA20120906120H](https://openairdocs.org/sdr/ASOA20120906120H), Sep 6, 2012: LIGHT. OVERHEATED. THE CREW REPORTED A STRING ELECTRICAL BURNING ODOR AROUND ROW 14. MX INSPECTED THE ACFT AND R & R THE SIDEWALL LIGHT ASSY AT ROW 15 RT, OPS TESTED WITH NO DFECT
- [SDR ASOA20120519077H](https://openairdocs.org/sdr/ASOA20120519077H), May 19, 2012: UNKNOWN. ODOR. THE CREW REPORTED THAT AFTER LANDING THERE WAS AN ELECTRICAL BURNING ODOR IN THE CABIN AND COCKPIT THAT WENT AWAY AFTER 3 MINUTES, AND SEEMED TO BE COMING FROM 
- [SDR ASOA20120404053](https://openairdocs.org/sdr/ASOA20120404053), Mar 30, 2012: TIRE. FAILED. VIBRATION FROM WHEELS ON ACFT ROTATION. TOWER FLY-BY REVEALED RT MAIN TIRE BLOWN. UPON LANDING, RT MAIN INBD WAS BLOWN. R & R NR 3 & NR 4 MWA.
- [SDR ASOA20120305032](https://openairdocs.org/sdr/ASOA20120305032), Mar 5, 2012: POWER SUPPLY. INOPERATIVE. THE CREW REPORTED EMERGENCY AISLE PATH LIGHTING NR 6, 7, & 8 TO BE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEF
- [SDR C2XA10SH178](https://openairdocs.org/sdr/C2XA10SH178), May 19, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 54. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W
- [SDR C2XA10SH177](https://openairdocs.org/sdr/C2XA10SH177), May 19, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W
- [SDR C2XA10SH176](https://openairdocs.org/sdr/C2XA10SH176), May 19, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED 
- [SDR C2XA10SH175](https://openairdocs.org/sdr/C2XA10SH175), May 19, 2010: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 
- [SDR C2XA10SH174](https://openairdocs.org/sdr/C2XA10SH174), May 18, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE LT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2L-7L. MAINTENANCE PERFORMED A BUSHING REPAIR 
- [SDR C2XA10SH173](https://openairdocs.org/sdr/C2XA10SH173), May 18, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE RT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE PERFORMED A BUSHING REPAIR 
- [SDR C2XA10SH172](https://openairdocs.org/sdr/C2XA10SH172), May 18, 2010: FRAME. CRACKED. SHV - DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L RIGHT BELOW THE LT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED F
- [SDR C2XA10SH171](https://openairdocs.org/sdr/C2XA10SH171), May 18, 2010: FRAME. CRACKED. SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R WAS FOUND TO BE CRACKED RIGHT BELOW THE RT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IA
- [SDR C2XA10SH170](https://openairdocs.org/sdr/C2XA10SH170), May 18, 2010: YOKE. CRACKED. SHV - DURING C-CHECK THE RT ENGINE FORWARD LOWER YOKE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED YOKE IAW EC 5450-01028. THE AIRCRAF
- [SDR C2XA10SH164](https://openairdocs.org/sdr/C2XA10SH164), May 2, 2010: FITTING. CRACKED. SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6R-7R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM
- [SDR C2XA10SH163](https://openairdocs.org/sdr/C2XA10SH163), May 2, 2010: FITTING. CRACKED. SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6L-7L. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 STRINGER 6L-7L IAW EMB-145 SRM 51-40-02
- [SDR C2XA10IA093](https://openairdocs.org/sdr/C2XA10IA093), Mar 11, 2010: BRAKE. MALFUNCTIONED. IAH - FLIGHT 2102, THE CREW REPORTED THAT AFTER T/O, RECEIVED A FLAP FAIL MESSAGE ON EICAS WITH THE FLAP LEVER AT 0 DEGREES AND THE FLAPS AT 9 DEGREES. THE AIRC
- [SDR C2XA10IA058](https://openairdocs.org/sdr/C2XA10IA058), Feb 8, 2010: DAU. DEFECTIVE. XNA - FLIGHT 2660, THE CREW REPORTED A BLEED 1 LEAK IN FLIGHT THAT DID NOT GO AWAY. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND RETURNED TO XNA
- [SDR C2XA09IA231](https://openairdocs.org/sdr/C2XA09IA231), Sep 13, 2009: O-RING. LEAKING. IAH - FLIGHT 2264 - THE CREW REPORTED A BLEED ONE LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED
- [SDR C2XA09IA158](https://openairdocs.org/sdr/C2XA09IA158), Jun 20, 2009: SELECTOR. INOPERATIVE. IAH - FLIGHT 2967 - THE CREW REPORTED THAT THE FLAPS FAILED AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND
- [SDR C2XA09SH083](https://openairdocs.org/sdr/C2XA09SH083), Mar 17, 2009: ACCUMULATOR. FAULTY. SHV - LOUD BANGING NOISE IN WHEEL WELL FOR 30 SEC AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR HYD ACCUMULATOR IAW EMB 145 AMM 32-33-15. AIRCRAFT WAS APPROV
- [SDR C2XA08IA144](https://openairdocs.org/sdr/C2XA08IA144), Jun 19, 2008: LIGHT. INOPERATIVE. IAH - FLIGHT 2361, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE FRONT AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFEC
- [SDR C2XA07IA256](https://openairdocs.org/sdr/C2XA07IA256), Dec 30, 2007: STRUCTURE. OUT OF POSITION. IAH - DURING A-CHECK INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR WOULD NOT OPEN. THE METAL TRIM AT THE TOP OF THE DOOR WAS FOUND TO BE CATCHING ON TH
- [SDR C2XA06BT026](https://openairdocs.org/sdr/C2XA06BT026), Jun 27, 2006: SMOKE DETECTOR. FAULTY. CREW REPORTED LAV SMOKE DETECTOR WARNING ON EICAS WITH APU ON ENGINES OFF. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB145 AMM 26-14-02. O
- [SDR C2XA05CL097](https://openairdocs.org/sdr/C2XA05CL097), Dec 6, 2005: PROXIMITY SENSOR. FAILED. CLE FLIGHT NR 2235, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE PRECEEDED BY E1-2 REVERSER DISAGREE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND R
- [SDR C2XA05IA112](https://openairdocs.org/sdr/C2XA05IA112), Oct 10, 2005: LIGHT. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY 
- [SDR C2XA05SH039](https://openairdocs.org/sdr/C2XA05SH039), May 20, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AROUND NUT PLATE BETWEEN FRAMES 22 AND 23. MAINTENANCE REPAIRED LT OMEGA BEAM NUT PLATE AT FRAME 22.5 AND R
- [SDR C2XA05SH038](https://openairdocs.org/sdr/C2XA05SH038), May 20, 2005: SKIN PANEL. LIGHTNING STRIKE. DURING C-CHECK VARIOUS LIGHTNING STRIKE ON SKIN PNL 214. MAINTENANCE REPAIR SKIN PNL 214 ABOVE STR 13R AFT FR 1A IAW EC 5330-01465. THE AIRCRAFT WAS APPROVED TO
- [SDR C2XA05SH037](https://openairdocs.org/sdr/C2XA05SH037), May 17, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON I/B SIDE FROM FRAME 36 TO FRAME 38. REPAIRED LT OMEGA BEAM AT FRAME 38 IAW EMB 145 SRM 53-21-10, SECTION 2, 
- [SDR C2XA05SH036](https://openairdocs.org/sdr/C2XA05SH036), May 16, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE RT OMEGA BEAM HAS CORROSION AROUND NUT PLATE AT FRAME 23. REPAIRED CORROSION ON RT OMEGA BEAM AROUND NUT PLATE AT FRAME 23 WITH INSTALL
- [SDR C2XA05SH035](https://openairdocs.org/sdr/C2XA05SH035), May 16, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 & 24. REPAIRED CENTER OMEGA BEAM AT FRAME 24 IAW EMB 145 SRM 53-22-10 PARAGRAPH 2 FIGURE 
- [SDR C2XA05SH033](https://openairdocs.org/sdr/C2XA05SH033), May 13, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 17-24 IAW EMB 145 SRM 51-40-02.
- [SDR C2XA05SH032](https://openairdocs.org/sdr/C2XA05SH032), May 12, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 39 TO FRM 45. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FRM 44 IA

All 87: https://openairdocs.org/deregistered/N14938-2016-03-15/reports.md

## Other aircraft with N14938

- [Cancelled 1955-10-06](https://openairdocs.org/deregistered/N14938-1955-10-06): Lockheed ELECTRA 10-A, S/N 1027. Owner: [Lease Air Inc](https://openairdocs.org/faa-owner/LEASE%20AIR%20INC), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank)

---
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.