# N16944: 1998 Embraer EMB-145EP, registration cancelled 2015-12-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 16, 2015
- Exported to: Senegal
- 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: 145045
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2005
- Certificate issued: December 9, 2015
- Last registry action: December 9, 2015
- Mode S code: A1161E
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N16944
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16944
- Page: https://openairdocs.org/deregistered/N16944-2015-12-16

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 (99, newest 50)

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

- [SDR ASOA20140122013](https://openairdocs.org/sdr/ASOA20140122013), Jan 22, 2014: FAN. FAILED. THE CREW REPORTED A STRONG ELECTRICAL ODOR AT TURNED TO FINAL. LANDED WITHOUT INCIDENT, MAINTENANCE R & R THE NR 1 RECIRCULATION FAN, OPS TESTED WITH NO DEFECTS
- [SDR ASOA20131001182](https://openairdocs.org/sdr/ASOA20131001182), Oct 1, 2013: LIGHT. SHORTED. CREW REPORTED COCKPIT READING LIGHT CIRCUIT BREAKER TRIPPED WITH A BURNING ODOR. MX INSPECTED AND R & R F/O'S READING LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AN
- [SDR ASOA20130615089](https://openairdocs.org/sdr/ASOA20130615089), Jun 15, 2013: CONTROL MODULE. OVERHEATED. THE CREW REPORTED A PLASTIC ODOR FROM THE CABIN DOOR ENTRYWAY. MX VERIFIED THE ODOR TO BE COMING FROM THE F/A CABIN LIGHT CONTROL MODULE, DEACTIVATED THE MODULE
- [SDR ASOA20130423156](https://openairdocs.org/sdr/ASOA20130423156), May 12, 2013: SKIN. CORRODED. DURING C-CHECK, THE CENTER FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-15 AND STRINGERS 19R-20L. MX R & R THE SKIN IAW EC5330-02761. THE ACFT
- [SDR ASOA20130423153](https://openairdocs.org/sdr/ASOA20130423153), May 11, 2013: FRAME. CRACKED. DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE PILOTS DV WINDOW AT STRINGER 9L. MX R & R THE CRACKED FRAME SECTION IAW SRM 51-40-02. 
- [SDR ASOA20121017133](https://openairdocs.org/sdr/ASOA20121017133), Oct 17, 2012: SEAL. LOOSE. THE CREW REPORTED A RAPID DEPRESSURIZATION (>3000FPM) WHILE CLIMBING THROUGH 21,000' AND THAT THEY COULD NOT RECOVER PRESSURIZATION. THE CREW PERFORMED AN EMERG
- [SDR C2XA11IA254](https://openairdocs.org/sdr/C2XA11IA254), Nov 8, 2011: BATTERY PACK. LOOSE. FLIGHT 4641, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 8-12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE 
- [SDR C2XA11IA200](https://openairdocs.org/sdr/C2XA11IA200), Sep 4, 2011: UNKNOWN. ODOR. IAH - THE CREW REPORTED A BURNING SMELL IN THE LAV THAT SEEMED TO BE AROUND THE LIGHT. MAINTENANCE INSPECTED THE LAV ARE, AND COULD NOT DUPLICATE THE SMELL, AND
- [SDR C2XA11SH020](https://openairdocs.org/sdr/C2XA11SH020), Jan 13, 2011: SKIN. CRACKED. SHV - DURING C-CHECK LT WING SKIN HAS CRACK JUST FWD OF GROUND SPOILER CTR HINGE POINT. REPAIRED SKIN IAW EC5740-01276. AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA11SH021](https://openairdocs.org/sdr/C2XA11SH021), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH019](https://openairdocs.org/sdr/C2XA11SH019), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 30-35. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH018](https://openairdocs.org/sdr/C2XA11SH018), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH017](https://openairdocs.org/sdr/C2XA11SH017), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH016](https://openairdocs.org/sdr/C2XA11SH016), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH015](https://openairdocs.org/sdr/C2XA11SH015), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH014](https://openairdocs.org/sdr/C2XA11SH014), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 24-29. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH013](https://openairdocs.org/sdr/C2XA11SH013), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH012](https://openairdocs.org/sdr/C2XA11SH012), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH011](https://openairdocs.org/sdr/C2XA11SH011), Jan 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH010](https://openairdocs.org/sdr/C2XA11SH010), Jan 12, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 58. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH009](https://openairdocs.org/sdr/C2XA11SH009), Jan 11, 2011: SKIN. CRACKED. SHV - DURING C-CHECK RT SKIN CRACKED AT FR 75 STR 2R. REPAIRED SKIN IAW EC5330-02340. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH008](https://openairdocs.org/sdr/C2XA11SH008), Jan 11, 2011: SKIN. CRACKED. SHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 4R TO 7R. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED F
- [SDR C2XA11SH007](https://openairdocs.org/sdr/C2XA11SH007), Jan 11, 2011: SKIN. CRACKED. SHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 3L TO 6L. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED F
- [SDR C2XA10SH445](https://openairdocs.org/sdr/C2XA10SH445), Dec 29, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA338](https://openairdocs.org/sdr/C2XA10IA338), Dec 19, 2010: JACK. DISCONNECTED. IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOU
- [SDR C2XA10IA337](https://openairdocs.org/sdr/C2XA10IA337), Dec 19, 2010: JACK. INOPERATIVE. IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOU
- [SDR C2XA10IA335](https://openairdocs.org/sdr/C2XA10IA335), Dec 18, 2010: LIGHT. OVERHEATED. IAH - FLIGHT 2304 A BURNING SMELL WAS NOTICED IN THE CABIN AT ROW 5. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY AT ROW 5A, OPERATIONALLY TESTED WITH NO DEF
- [SDR C2XA10IA240](https://openairdocs.org/sdr/C2XA10IA240), Aug 30, 2010: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2935, DURING POST-FLIGHT INSPECTION THE CREW REPORTED SOME EXIT ROW FLOOR LIGHTING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER T
- [SDR C2XA10IA220](https://openairdocs.org/sdr/C2XA10IA220), Aug 9, 2010: DISPLAY. MALFUNCTIONED. CRP - FLIGHT 2096, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE NR 2 PFD WENT BLANK AND SMOKED. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROV
- [SDR C2XA10IA108](https://openairdocs.org/sdr/C2XA10IA108), Mar 25, 2010: SKIN. CRACKED. CRP - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. THE AIRCRAFT WAS FERRIED TO IAH WHERE MA
- [SDR C2XA10IA039](https://openairdocs.org/sdr/C2XA10IA039), Jan 25, 2010: DUCT. DEFECTIVE. IAH - FLIGHT 2569, THE CREW REPORTED THAT THE PACK TWO VALVE CLOSED ON CLIMBOUT WITH NO PRESSURIZATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INC
- [SDR C2XA10IA034](https://openairdocs.org/sdr/C2XA10IA034), Jan 22, 2010: CLAMP. LOOSE. IAH - FLIGHT 2165, THE CREW REPORTED THAT THE BLEED 1 VALVE CLOSED FROM T/O TO 10'000 FEET. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAIN
- [SDR C2XA10IA033](https://openairdocs.org/sdr/C2XA10IA033), Jan 22, 2010: CLAMP. LOOSE. IAH - FLIGHT 2165, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED TWICE DURING CLIMB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED TH
- [SDR C2XA10IA018](https://openairdocs.org/sdr/C2XA10IA018), Jan 15, 2010: PRECOOLER. LEAKING. IAH - FLIGHT 2617, THE CREW REPORTED A BLEED ONE LEAK MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND R
- [SDR C2XA10IA013](https://openairdocs.org/sdr/C2XA10IA013), Jan 11, 2010: LANDING GEAR. LOW. IAH - FLIGHT 2413, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE AFTER TAKEOFF WITH A THRUST REVERSER DISAGREE EICAS MESSAGE. THE AIRCRAFT RETURNED
- [SDR C2XA09IA185](https://openairdocs.org/sdr/C2XA09IA185), Jul 20, 2009: METERING UNIT. MALFUNCTIONED. MFE - FLIGHT 2627, THE CREW REPORTED THAT E2 WOULD NOT ADVANCE 85 PERCENT N2 OR 90 PERCENT N1 AND ITT WAS SPIKING ERRONEOUSLY BETWEEN 300-500 DEGREES, WITH AN E
- [SDR C2XA08IA225](https://openairdocs.org/sdr/C2XA08IA225), Oct 13, 2008: BATTERY. DISCHARGED. IAH DURING A CHECK INSPECTION THE AFT 3 AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED WITH NO DEFECTS AND
- [SDR C2X2008F00002](https://openairdocs.org/sdr/C2X2008F00002), Jun 8, 2008: BATTERY. DISCHARGED. EMERGENCY LIGHTING OVERHEAD AND FLOOR BY EMERGENCY EXITS ARE DIM. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. (S)
- [SDR C2XA07TY034](https://openairdocs.org/sdr/C2XA07TY034), Jul 5, 2007: SKIN. CRUSHED. TYS - AIRCRAFT SUFFERED GROUND DAMAGE FROM A BAGGAGE CART TO THE FUSELAGE UNDER WINDOWS 4 AND 5. MAINTENANCE REMOVED AND REPLACED STRINGERS 11L, 12L AND FRAME 2
- [SDR C2XA06BT048](https://openairdocs.org/sdr/C2XA06BT048), Nov 1, 2006: LAMP. FAILED. EWR LOG SQUAWK ELECTRICAL SMOKE ODOR IN THE CABIN. FOUND TO BE FORWARD SIDEWALL LIGHT ON SEAT 1A. MEL'D. LATER RE-LAMPED LIGHT AT SEAT 1A 2A IAW EMB145 AMM 33-2
- [SDR C2XA06TY011](https://openairdocs.org/sdr/C2XA06TY011), Feb 22, 2006: FLOOR SUPPORT. CORRODED. TYS - DURING A ROUTINE C-CHECK INSPECTION THE RIGHT SIDE OMEGA BEAM IN THE GALLEY WAS CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGE AREA AND FABRICATED A
- [SDR C2XA06TY010](https://openairdocs.org/sdr/C2XA06TY010), Feb 21, 2006: SHEAR PLATE. CORRODED. TYS - DURING A SCHEDULE 2C INSPECTION CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT ON LOWER SILL AT STR 16L AT FR 65. MAINTENANCE BLENDED ALL SIGNS OF CORROSION
- [SDR C2XA05TY007](https://openairdocs.org/sdr/C2XA05TY007), Jan 24, 2005: BEARING. WORN. TYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VE
- [SDR C2XA03SH474](https://openairdocs.org/sdr/C2XA03SH474), Nov 23, 2003: ANGLE. CORRODED. SHV- DURING C-CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM
- [SDR C2XA03SH473](https://openairdocs.org/sdr/C2XA03SH473), Nov 23, 2003: THRESHOLD. CORRODED. SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE A
- [SDR C2XA03SH472](https://openairdocs.org/sdr/C2XA03SH472), Nov 23, 2003: BUTTSTRAP. CORRODED. SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 
- [SDR C2XA03SH467](https://openairdocs.org/sdr/C2XA03SH467), Nov 19, 2003: STRUCTURE. GOUGED. SHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02.
- [SDR C2XA03SH466](https://openairdocs.org/sdr/C2XA03SH466), Nov 19, 2003: STRUCTURE. GOUGED. SHV-DURING C-CHECK THE RIGHT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02
- [SDR C2XA03SH465](https://openairdocs.org/sdr/C2XA03SH465), Nov 19, 2003: BUTTSTRAP. CORRODED. SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE LEFT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02
- [SDR C2XA03SH464](https://openairdocs.org/sdr/C2XA03SH464), Nov 19, 2003: 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 145 SRM 51-40-02. THE AIRCRAFT

All 99: https://openairdocs.org/deregistered/N16944-2015-12-16/reports.md

## 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 20030317016939I](https://openairdocs.org/incident/20030317016939I), Mar 17, 2003: Emb EMB145ER (N16944), Rochester, NY. (-23) On March 17, 2003, an Emb-145, flt. 2160, departed the greater Rochester international airport, Rochester, NY, 14624, air aborted for a landing gear…

## Other aircraft with N16944

- [Cancelled 1948-08-05](https://openairdocs.org/deregistered/N16944-1948-08-05): Piper J-2, S/N 810. Owner: [Finely Harley](https://openairdocs.org/faa-owner/FINELY%20HARLEY), [Marysville, CA](https://openairdocs.org/faa-place/CA/Marysville)

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