# N16951: 1998 Embraer EMB-145LR, registration cancelled 2015-09-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 10, 2015
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145063
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 19, 1998
- Certificate issued: July 27, 2015
- Last registry action: July 27, 2015
- Mode S code: A1163E
- Owner when cancelled: [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC)
- Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay)
- Owner type: Corporation
- Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N16951
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16951
- Page: https://openairdocs.org/deregistered/N16951-2015-09-10

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-145LR: https://openairdocs.org/model/embraer-emb-145lr.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 ASOA20141203357](https://openairdocs.org/sdr/ASOA20141203357), Dec 3, 2014: BOWL. CORRODED. DURING C-CHECK , TOILET BOWL IS CORRODED. MAINTENANCE R & R TOILET BOWL SUPPORT ASSY IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20141203356V](https://openairdocs.org/sdr/ASOA20141203356V), Dec 3, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, RT OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2, FRAME 18. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM IAW EC5320-01991 FRAME 18. THE ACFT WAS APPR
- [SDR ASOA20141203355](https://openairdocs.org/sdr/ASOA20141203355), Dec 3, 2014: DOOR SILL. CORRODED. DURING C-CHECK BAGGAGE DOOR LOWER SILL CORRODED, LOCAL LEVEL 2, FROM FRAME 65-68. MAINTENANCE R & R BAGGAGE DOOR LOWER SILL AT FRAME 65-68 IAW SRM 51-40-02 AND 
- [SDR ASOA20141126350](https://openairdocs.org/sdr/ASOA20141126350), Dec 3, 2014: SKIN. DENTED. DURING C-CHECK 4 PROTRUDING DENTS IN SAME BAY AT FRAME 24-25, STRINGER 21R-21L. MAINTENANCE PERFORMED REPAIR OF 4 PROTRUDING DENTS BETWEEN FRAME 24-25 STRINGER 
- [SDR ASOA20141126349](https://openairdocs.org/sdr/ASOA20141126349), Dec 3, 2014: SKIN. DENTED. DURING C-CHECK 4, PROTRUDING DENTS IN SAME BAY AT FRAME 20-21, STRINGER 19L-20L. MAINTENANCE PERFORMED REPAIR OF 4 PROTRUDING DENTS BETWEEN FRAME 20-21 STRINGER
- [SDR ASOA20140717056](https://openairdocs.org/sdr/ASOA20140717056), Jul 17, 2014: POWER SUPPLY. FAULTY. DURING ROUTINE MAINTENANCE THE FWD OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHE
- [SDR ASOA20130709098](https://openairdocs.org/sdr/ASOA20130709098), Jul 9, 2013: LIGHT. INOPERATIVE. DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE LAST TWO ROWS OF AISLE PATH LIGHTING WERE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO 
- [SDR ASOA20130614088](https://openairdocs.org/sdr/ASOA20130614088), Jun 14, 2013: ACM. FAILED. THE CREW REPORTED SMOKE IN THE CABIN. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX OPERATED THE APU AND ENGINES WITH THE FLIGHT CREW, VERIFIED THE SM
- [SDR ASOA20130120004](https://openairdocs.org/sdr/ASOA20130120004), Jan 20, 2013: LAMP. INOPERATIVE. DURING ROUTINE MX THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED LAMP . OPS CHECKED GOOD.
- [SDR ASOA20130118032](https://openairdocs.org/sdr/ASOA20130118032), Jan 18, 2013: ATTACH FITTING. DAMAGED. DURING C-CHECK, FRAME 75 STR 2L-2R IS FRETTING AT BOLTS FOR VERTICAL STAB TO FUSELAGE BRACKET. MX PERFORMED REPAIR AT FRM 75 STR 2L-2R AT VERTICAL STAB TO FUSEL
- [SDR ASOA20130118031](https://openairdocs.org/sdr/ASOA20130118031), Jan 18, 2013: SKIN. DAMAGED. DURING C-CHECK SMOKING RIVETS AT FRM 77, BETWEEN STRS 3R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRM 77 BETWEEN STRS 3R-5R IAW EC5330-02673, REV ORIGINAL. T
- [SDR ASOA20130118030](https://openairdocs.org/sdr/ASOA20130118030), Jan 18, 2013: SKIN. CRACKED. DURING C-CHECK RIVET AT FRM 78, STR 5R SHOWS VISUAL INDICATION OF CRACKS. MX REPAIRED FUSELAGE SKIN AT FRM 78, STR 5R IAW EC5330-02673, REV ORIGINAL. THE AVFT W
- [SDR ASOA20130118029](https://openairdocs.org/sdr/ASOA20130118029), Jan 18, 2013: SKIN. DAMAGED. DURING C-CHECK SMOKING RIVETS AT FRM 78 STR 3R. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRM 78 STR 3R IAW EC5330-02673. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA20130118028](https://openairdocs.org/sdr/ASOA20130118028), Jan 18, 2013: DOOR FRAME. CORRODED. DURING C-CHECK, MAIN DOOR LOWER FRAME HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR ON MAIN DOOR LOWER FRAME SCREW HOLES IAW EC5210-01154, REV A. THE ACFT WAS A
- [SDR ASOA20130118027](https://openairdocs.org/sdr/ASOA20130118027), Jan 18, 2013: STRUCTURE. CORRODED. DURING C-CHECK CORROSION AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR IAW EC5210-011
- [SDR ASOA20130118026](https://openairdocs.org/sdr/ASOA20130118026), Jan 18, 2013: STRUCTURE. CORRODED. DURING C-CHECK CORROSION AROUND LOWER NUTPLATES ON SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATES ON SERVICE DOOR IAW EC5210-01154. THE ACFT WAS APPRO
- [SDR ASOA20130118025](https://openairdocs.org/sdr/ASOA20130118025), Jan 18, 2013: HINGE BRACKET. WORN. DURING C-CHECK, RT GROUND SPOILER INBD HINGE OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER INBD HINGE BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FO
- [SDR ASOA20130118024](https://openairdocs.org/sdr/ASOA20130118024), Jan 18, 2013: BUSHING. MIGRATED. DURING C-CHECK RT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAS MIGRATED HAT BUSHING. MX R & R CENTER HINGE INBD HAT BUSHING IAW EC5740-01152, REV C. T
- [SDR ASOA20130118023](https://openairdocs.org/sdr/ASOA20130118023), Jan 18, 2013: HINGE. WORN. DURING C-CHECK, LT GROUND SPOILER CENTER HINGE INBD HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS
- [SDR ASOA20130118022](https://openairdocs.org/sdr/ASOA20130118022), Jan 18, 2013: HINGE. WORN. DURING C-CHECK LT WING GROUND SPOILER INBD HINGE ATTACHMENT OTBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER INBD HINGE ATTACHMENT BRACKET IAW EC5740-
- [SDR ASOA20130118021](https://openairdocs.org/sdr/ASOA20130118021), Jan 18, 2013: HINGE. WORN. DURING C-CHECK LT WING GROUND SPOILER CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-0128
- [SDR ASOA20130118020](https://openairdocs.org/sdr/ASOA20130118020), Jan 18, 2013: HINGE. WORN. DURING C-CHECK LT WING GROUND SPOILER OTBD HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER OTBD HINGE ATTACHMENT IAW EC5740-012
- [SDR ASOA20130118019](https://openairdocs.org/sdr/ASOA20130118019), Jan 18, 2013: BUSHING. MIGRATED. DURING C-CHECK, LT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE CENTER HINGE INBD HAT BUSHING IAW EC5750-014
- [SDR ASOA20130118016](https://openairdocs.org/sdr/ASOA20130118016), Jan 18, 2013: ATTACH ANGLE. CORRODED. DURING C-CHECK, PANEL 321DR ATTACHMENT FLANGE HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR AT PANEL 321DR ATTACHMENT FLANGE SCREW HOLES IAW EC5510-01297. THE A
- [SDR ASOA20130118015](https://openairdocs.org/sdr/ASOA20130118015), Jan 18, 2013: SKIN. CRACKED. DURING C-CHECK RIVET AT FRAME 79, STRINGER 3L SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 79, STRINGER 3L IAW EC5330-02501.
- [SDR ASOA20130118014](https://openairdocs.org/sdr/ASOA20130118014), Jan 18, 2013: SKIN. CRACKED. DURING C-CHECK, RIVET AT FRAME 79, STRINGER 3R SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 79, STRINGER 3R IAW EC 5330-0267
- [SDR ASOA20130118013](https://openairdocs.org/sdr/ASOA20130118013), Jan 18, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK RT OMEGA BEAM CORRODED AT FRAME 23. MX R & R RT OMEGA BEAM BETWEEN FR 16-24 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118018](https://openairdocs.org/sdr/ASOA20130118018), Jan 17, 2013: STRINGER. DAMAGED. DURING C-CHECK DAMAGE, AT FRM 77, STR5R, MX PERFORMED REPAIR AT FRM 77, STR 5R IAW EMB-145 EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130118017](https://openairdocs.org/sdr/ASOA20130118017), Jan 17, 2013: HINGE. DAMAGED. DURING C-CHECK, RUDDER NR 1 AFT CENTER UPPER HINGE DAMAGE GOUGED. MX R & R RUDDER NR 1 AFT CTR UPPER HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20120808105H](https://openairdocs.org/sdr/ASOA20120808105H), Aug 8, 2012: ACM. SEIZED. AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE CABIN AND ELECTED TO RETURN TO DEPARTURE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, MX FOUND THE
- [SDR C2XA11TY159](https://openairdocs.org/sdr/C2XA11TY159), Oct 19, 2011: PUMP. OVERHEATED. HYD SYSTEM 2 OVERHEAT/FAIL IN FLIGHT. REMOVED AND REPLACED ENG NR 2 HYD PUMP AND MANIFOLD IAW EMB145 AMM 29-10-03 & 29-10-07. OPS AND LEAK CHECK GOOD. AIRCRAFT 
- [SDR C2XA11TY050](https://openairdocs.org/sdr/C2XA11TY050), Apr 28, 2011: ADC. MALFUNCTIONED. DIVERTED FOR EICAS AIRSPEED MESSAGE IN AMBER AT CRUISE. TYS R & R ADC NR1, OPS AND LEAK CHECKS GOOD. (CLOSED)
- [SDR C2XA11IA052](https://openairdocs.org/sdr/C2XA11IA052), Mar 11, 2011: PROXIMITY SENSOR. FAULTY. DURING FLIGHT THE CREW RECEIVED SPOILER FAIL AND SPOILER OPEN MESSAGES. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REPLACED A SP
- [SDR C2XA11IA050](https://openairdocs.org/sdr/C2XA11IA050), Mar 9, 2011: ACTUATOR. LEAKING. ON APPROACH INTO FAR THE CREW RECEIVED A GEAR AIR/GROUND FAIL MESSAGE. THE CREW ELECTED TO ABORT THE APPROACH AND THE MESSAGE EXTINGUISHED HOWEVER ON THE SECOND
- [SDR C2XA11SH028](https://openairdocs.org/sdr/C2XA11SH028), Jan 17, 2011: SKIN. CRACKED. SHV - DURING C-CHECK - SKIN CRACKS AROUND RIVETS BETWEEN FR 77-79 STR 4L TO 8L. REPAIRED CRACKS IAW EC5330-02342. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH027](https://openairdocs.org/sdr/C2XA11SH027), Jan 17, 2011: FITTING. DAMAGED. SHV - DURING C-CHECK - LT AILERON 2ND FROM I/B HINGE I/B HAT BUSHING MIGRATED. REPLACED FITTING IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA11SH026](https://openairdocs.org/sdr/C2XA11SH026), Jan 17, 2011: HINGE FITTING. DAMAGED. SHV - DURING C-CHECK - LT GROUND SPOILER O/B HINGE O/B HAT BUSHING MIGRATED. REPLACED HINGE FITTING BRACKET IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR 
- [SDR C2XA11SH025](https://openairdocs.org/sdr/C2XA11SH025), Jan 16, 2011: BRACKET. CRACKED. SHV - DURING C-CHECK FRAME 10 L BRACKET AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 L BRACKET AT STRINGER 10L-9L IAW EMB-145 SRM 5
- [SDR C2XA11SH024](https://openairdocs.org/sdr/C2XA11SH024), Jan 16, 2011: FRAME. CRACKED. SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 AT STRINGER 10L AND 9L IAW EMB-145 SRM 51-40-02. THE AIR
- [SDR C2XA11SH023](https://openairdocs.org/sdr/C2XA11SH023), Jan 16, 2011: STRINGER. CORRODED. SHV - DURING C-CHECK STRINGER 21R BETWEEN FRAMES 12 AND 13 IS CORRODED. MAINTENANCE PERFORMED REPAIR OF STRINGER 21R BETWEEN FRAMES 12 AND 13 BY INSTALLING STRI
- [SDR C2XA10CL199](https://openairdocs.org/sdr/C2XA10CL199), Dec 15, 2010: CONTROLLER. MALFUNCTIONED. CLE FLT 2629 THE CREW REPORTED A STRONG ELECTRICAL SMELL AND A WINDSHIELD HEAT NR 2 FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 WINDSHIE
- [SDR C2XA10IA327](https://openairdocs.org/sdr/C2XA10IA327), Dec 13, 2010: ACM. SEIZED. IAH - FLIGHT 2380, THE CREW REPORTED NOISE AND A SMOKE SMELL COMING FROM THE NUMBER ONE PACK. MAINTENANCE FOUND THE NR 1 ACM TO BE SEIZED, AND PLACED THE LEFT C
- [SDR C2XA10IA122](https://openairdocs.org/sdr/C2XA10IA122), Apr 15, 2010: BALLAST. OVERHEATED. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL AT ROW 4. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED CEILING LIGHT BALLAST,
- [SDR C2XA09IA225A](https://openairdocs.org/sdr/C2XA09IA225A), Sep 9, 2009: VALVE. LEAKING. MEM - FLIGHT 2291, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON CLIMB. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVE
- [SDR C2XA09RI116](https://openairdocs.org/sdr/C2XA09RI116), Jun 4, 2009: LIGHT. MALFUNCTIONED. FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WERE INOPERATIVE. MX PERFORMED SYS RESET SUCCESSFULLY AND ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI076](https://openairdocs.org/sdr/C2XA09RI076), Apr 27, 2009: UNKNOWN. MALFUNCTIONED. FLIGHT 3134 - EWR - FLIGHT CREW REPORTED NOSE EXCESSIVELY HEAVY ON TAKE OFF AND LANDING AND CREW HAD TO USE FULL NOSE UP TRIM ON LANDING. CREW DECLARED EMERGENC
- [SDR C2XA09TY062](https://openairdocs.org/sdr/C2XA09TY062), Apr 14, 2009: STOP FITTING. DEFECTIVE. MAIN CABIN DOOR WILL NOT CLOSE. REMOVED AND REPLACED FWD AND AFT DOOR STOP HARDWARE, REPOSITIONED DOOR SEAL AND RIGGED DOOR. REMOVED AND REPLACED FWD AND AFT UP
- [SDR C2XA09IA061](https://openairdocs.org/sdr/C2XA09IA061), Feb 22, 2009: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING BETWEEN ROWS 6-8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND R
- [SDR C2XA09IA038](https://openairdocs.org/sdr/C2XA09IA038), Feb 9, 2009: INVERTER. INOPERATIVE. IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE SLOW TO CHARGE, AND SOME BLINK ON AND OFF. MX R&R THE NR 3 EMERGENCY LIGHT 
- [SDR C2XA09IA039](https://openairdocs.org/sdr/C2XA09IA039), Feb 8, 2009: BATTERY PACK. DISCHARGED. IAH - FLIGHT 3097, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX CHARGED THE NR 3 EMERGENCY LIGHT

All 126: https://openairdocs.org/deregistered/N16951-2015-09-10/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 20120808016309I](https://openairdocs.org/incident/20120808016309I), Aug 8, 2012: Embraer EMB-145LR (N16951), Omaha, NE, No damage. Shortly after take off from Eppley Airfield, Omaha, NE. The crew experienced smoke in the cabin. Aircraft returned to airport and completed an emergency…

## Other aircraft with N16951

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N16951-undated): Bell 206L, S/N 45152. Triennial form not returned

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