# N14960: 1998 Embraer EMB-145LR, registration cancelled 2015-08-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 6, 2015
- Status when cancelled: Sale reported
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145100
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 9, 1998
- Last registry action: July 20, 2015
- Mode S code: A0C762
- Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon)
- Owner type: Individual
- Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14960
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14960
- Page: https://openairdocs.org/deregistered/N14960-2015-08-06

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 (86, newest 50)

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

- [SDR ASOA20140918080](https://openairdocs.org/sdr/ASOA20140918080), Sep 18, 2014: ENGINE. LEAKING. THE CREW REPORTED BAD FUME ODOR FROM BLEED NR 1, MOST INTENSE WITH HIGH THRUST SETTING CHANGES. APU USED AS ALTERNATE BLEED SOURCE. MAINTENANCE REPLACED THE NR 
- [SDR ASOA20140913102](https://openairdocs.org/sdr/ASOA20140913102), Sep 13, 2014: SWITCH. SHORTED. CREW REPORTED PSU LIGHT AT 6D SMOKING AND FLICKERING COULD NOT TURN OFF. MAINTENANCE R & R 6D PSU LIGHT WITH NO FIX. DISCONNECTED SWITCH AND PLACED ON NEF CB02.
- [SDR ASOA20140912101](https://openairdocs.org/sdr/ASOA20140912101), Sep 12, 2014: UNKNOWN. ODOR. PILOT REPORTED ODOR OF BURNING OIL FROM NR 1 PACK WHEN IT IS POWERED BY ENGINE BLEED. MAINTENANCE PERFORMED TROUBLESHOOTING IAW AMM 21-20-00. PERFORMED ENGINE 1
- [SDR ASOA20140810093](https://openairdocs.org/sdr/ASOA20140810093), Aug 10, 2014: ACTUATOR. LOOSE. DURING FLIGHT, CREW FELT LIGHT VIBRATION IN THE FLIGHT CONTROLS DURING FLIGHT AND RETURNED TO BASE. ACFT WAS FERRIED, WHERE MAINTENANCE PERFORMED CABLE TENSIONS
- [SDR ASOA20140616088](https://openairdocs.org/sdr/ASOA20140616088), Jun 16, 2014: UNKNOWN. ODOR. ACFT WAS FERRIED FOR SMOKE IN CABIN WHEN PACKS WERE SELECTED. MAINTENANCE CHANGED OUT THE CARBON SEAL ON THE NR 1 ENGINE IAW MM 72-00-00-200. OPS AND LEAK CHECK
- [SDR ASOA20140604063](https://openairdocs.org/sdr/ASOA20140604063), Jun 4, 2014: ACM. ODOR. PILOT REPORTED A STRONG ODOR COMING FROM PACK NR 1. MX R & R THE NR 1 ACM WITH OPS CHECK GOOD AND NO ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140223027H](https://openairdocs.org/sdr/ASOA20140223027H), Feb 23, 2014: A/C PACK. MALFUNCTIONED. IT WAS REPORTED THAT THE NR 2 PACK WAS MAKING LOUD NOISE AND ODORS. R & R THE NR 2 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETU
- [SDR ASOA20131221140R](https://openairdocs.org/sdr/ASOA20131221140R), Dec 21, 2013: WIRE HARNESS. ARCED. CREW REPORTED THE CEILING LIGHT OVER ROW 1A WAS PRODUCING A BURNING ODOR. MX R & R THE ELECTRICAL HARNESS NR ROW 1A WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED
- [SDR ASOA20131013117](https://openairdocs.org/sdr/ASOA20131013117), Oct 13, 2013: INVERTER. INOPERATIVE. DURING MX INSPECTION, EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT INOPERATIVE. MX R & R INVERTER & OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130617061](https://openairdocs.org/sdr/ASOA20130617061), Jun 17, 2013: UNKNOWN. ODOR. CREW REPORTED A ODOR IN THE CABIN LIKE BURNING PLASTIC. MX PERFORMED PASSENGER CABIN LIGHT TEST WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326107](https://openairdocs.org/sdr/ASOA20130326107), Mar 28, 2013: SHEAR TIE. CORRODED. DURING C-CHECK SHEAR TIE AT FRAME 68 BETWEEN STRINGER 18L-17L IS CORRODED. MX REPAIRED SHEAR TIE IAW SRM 51-20-01 AND CPM 51-21-06. ACFT APPROVED FOR RETURN TO 
- [SDR ASOA20130326106](https://openairdocs.org/sdr/ASOA20130326106), Mar 28, 2013: SKIN. CORRODED. DURING C-CHECK, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. ACFT APPROVED FOR RETURN TO SERVIC
- [SDR ASOA20130326104](https://openairdocs.org/sdr/ASOA20130326104), Mar 28, 2013: STRINGER. CORRODED. DURING C-CHECK, COCKPIT STRINGER 21R CORRODED. MX R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326103](https://openairdocs.org/sdr/ASOA20130326103), Mar 28, 2013: STRINGER. CORRODED. DURING C-CHECK COCKPIT STRINGER 21L CORRODED. MX REPAIRED OF STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326102](https://openairdocs.org/sdr/ASOA20130326102), Mar 28, 2013: STRINGER SPLICE. CORRODED. DURING C-CHECK, STRINGER SPLICE 21L CORRODED BETWEEN FRAMES 12-13. MX PERFORMED REPAIR ON STRINGER SPLICE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326101](https://openairdocs.org/sdr/ASOA20130326101), Mar 27, 2013: THRESHOLD. CORRODED. DURING C-CHECK CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAME 68 CORRODED AROUND NUTPLATES. MX PERFORMED REPAIR ON CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAM
- [SDR ASOA20130326100](https://openairdocs.org/sdr/ASOA20130326100), Mar 27, 2013: PLATE. CORRODED. DURING C-CHECK CARGO THRESHOLD TRIANGULAR PLATE AT FRAME 65 CORRODED. (LOCAL LEVEL 2) AROUND NUTPLATES. MX PERFORMED REPAIR ONCARGO COMP THRESHOLD TRIANGULAR PL
- [SDR ASOA20130326099](https://openairdocs.org/sdr/ASOA20130326099), Mar 27, 2013: STRUCTURE. CORRODED. DURING C-CHECK CARGO DOOR CUTOUT LWR MEMBER CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUT-OUT LWR MEMBER IAW SRM 51-20-01 AND CPM 51-21-06. THE ACFT WAS APPRO
- [SDR ASOA20130326098V](https://openairdocs.org/sdr/ASOA20130326098V), Mar 27, 2013: SHEAR ANGLE. CORRODED. DURING C-CHECK CORRODED SHEAR CLIP ON RT CROSSBEAM FRAME 65. MX PERFORMED REPAIR ON FRAME 65 RH CROSSBEAM SHEAR CLIP IAW EC5320-01494A. THE ACFT WAS APPROVED FO
- [SDR ASOA20130326097V](https://openairdocs.org/sdr/ASOA20130326097V), Mar 27, 2013: FLOOR SUPPORT. CORRODED. DURING C-CHECK LT OMEGA BEAM FLANGE CORRODED (LOCAL LEVEL 2) BETWEEN FRAMES 18-23. MX PERFORMED REPAIR FOR LT OMEGA BEAM FLANGE AT FRAME 20 IAW SRM 53-00-01. TH
- [SDR ASOA20130326096](https://openairdocs.org/sdr/ASOA20130326096), Mar 26, 2013: FRAME. GOUGED. DURING C-CHECK FRAME 60 AT STRINGER 5L GOUGED. MX PERFORMED REPAIR AT FRAME 60 STRINGER 5L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120220020](https://openairdocs.org/sdr/ASOA20120220020), Feb 20, 2012: CONTROLLER. FAULTY. THE CREW REPORTED AN 115 VOLT, AC BUSS FAILED ALONG WITH SMOKE ODOR. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD.
- [SDR C2XA11TY097](https://openairdocs.org/sdr/C2XA11TY097), Jun 29, 2011: LIGHT. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOP. REPLACED LAMP IAW EMB 145 AMM33-50-05. OPS CHECK GOOD.
- [SDR C2XA11RI097](https://openairdocs.org/sdr/C2XA11RI097), May 27, 2011: STARTER. VIBRATION. FLIGHT 2260 - EWR - FLIGHT CREW REPORTED ENGINE NR 1 HIGH VIBRATION ON TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PLACED ITEM ON DMI FOR
- [SDR C2XA11CL138](https://openairdocs.org/sdr/C2XA11CL138), May 27, 2011: STARTER. FAULTY. EWR FLT 2260 THE CREW REPORTED A NR 1 ENGINE HIGH VIBRATION ON TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 
- [SDR C2XA11SH067](https://openairdocs.org/sdr/C2XA11SH067), Mar 15, 2011: FITTING. CRACKED. SHV - DURING C-CHECK NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REMOVED AND REPLACED NR 1 ENG YOKE FITTING IAW EC5450-01028. AIRCRAFT WAS APPROVED FOR RETUR
- [SDR C2XA11SH065](https://openairdocs.org/sdr/C2XA11SH065), Mar 13, 2011: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK RT OMEGA BEAM AT FRAME 18 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18 IAW EMB-145 SRM 51-40-02 A
- [SDR C2XA11SH064](https://openairdocs.org/sdr/C2XA11SH064), Mar 13, 2011: DOUBLER. DAMAGED. SHV - DURING C-CHECK BOUBLER AT FRAME 22 IS CORRODED (LEVEL 2 LOCAL) AND BENT. MAINTENANCE PERFORMED REPAIR ON DOUBLER AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE
- [SDR C2XA10CL196](https://openairdocs.org/sdr/C2XA10CL196), Dec 10, 2010: CONTROLLER. FAULTY. CLE FLT 2690 THE CREW REPORTED THE PRESSURIZATION WAS INOPERATIVE IN BOTH MANUAL AND AUTO. THE AIRCRAFT DIVERTED INTO ORD AND LANDED WITHOUT INCIDENT. MAINTENAN
- [SDR C2XA10CL165](https://openairdocs.org/sdr/C2XA10CL165), Nov 1, 2010: BRAKE. OVERHEATED. DAY - FLT 2693 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE AFTER TAKEOFF. THE LEFT BRAKE SHOWED FULL HOT. THE BRAKES WERE COOLED PER THE QRH AND THE AIRCRAFT LAN
- [SDR C2XA10IA243](https://openairdocs.org/sdr/C2XA10IA243), Sep 6, 2010: CONNECTOR. LOOSE. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A A
- [SDR C2XA10IA242](https://openairdocs.org/sdr/C2XA10IA242), Sep 6, 2010: CONNECTOR. LOOSE. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A A
- [SDR C2XA09IA290](https://openairdocs.org/sdr/C2XA09IA290), Nov 16, 2009: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE LOWER FORWARD SERVICE DOOR EXIT IDENTIFIER AND NR 1 FLOOR PROX LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN
- [SDR C2XA09RI1137](https://openairdocs.org/sdr/C2XA09RI1137), Aug 7, 2009: FLAP. OVERSPEED. FLIGHT 2527 - EWR - FLIGHT CREW REPORTED FLAP OVER SPEED IN CRUISE (FLAP 9 AT 290 KNOTS FOR 5 MINUTES). EWR INSPECTION DEPARTMENT PERFORMED FLAP OVER SPEED INSP
- [SDR C2XA09RI115](https://openairdocs.org/sdr/C2XA09RI115), Jun 3, 2009: OUTFLOW VALVE. INOPERATIVE. FLIGHT CREW REPORTED CABIN AUTO PRESSURIZATION SYS OPERATED ABNORMALLY ON DESCENT. CREW LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTF
- [SDR C2XA09SH081](https://openairdocs.org/sdr/C2XA09SH081), Mar 16, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FR 49. MAINTENANCE REPAIRED CORRODED AREA ON LT OMEGA BEAM (CORRODED AREA
- [SDR C2XA09SH080](https://openairdocs.org/sdr/C2XA09SH080), Mar 16, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT FR 29. MAINTENANCE COMPLETED INSTALLATION OF REPAIR FOR LT OMEGA BEAM AT F
- [SDR C2XA09SH079](https://openairdocs.org/sdr/C2XA09SH079), Mar 16, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE CORRODED FRM 25 AT COMPOSITE CROSSBEAM. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00
- [SDR C2XA09SH078](https://openairdocs.org/sdr/C2XA09SH078), Mar 16, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 44. MAINTENANCE REPAIRED LT OMEGA BEAM IAW IC2009-145/00816. THE AIRCRAFT 
- [SDR C2XA09SH077](https://openairdocs.org/sdr/C2XA09SH077), Mar 16, 2009: STRINGER. CORRODED. SHV - DURING C-CHECK STR 17R FRMS 16-24 HAS CORROSION. MAINTENANCE REMOVED AND COMPLETED INSTALLATION OF STR 17R AT FRMS 16-24 BY INSTALLING HI-LOKS AT STRINGER
- [SDR C2XA09SH076](https://openairdocs.org/sdr/C2XA09SH076), Mar 16, 2009: SMOKE DETECTOR. INOPERATIVE. SHV - DURING C-CHECK LAV SMOKE DETECTOR TEST PANEL HAS NO POWER. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB-145 AMM 26-14-01. OPS CHECK GO
- [SDR C2XA09SH074](https://openairdocs.org/sdr/C2XA09SH074), Mar 10, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW IC 2009-145/00816. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH071](https://openairdocs.org/sdr/C2XA09SH071), Mar 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 33. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM AT FRM 33 IAW EMB-1
- [SDR C2XA09SH069](https://openairdocs.org/sdr/C2XA09SH069), Mar 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM FRM 25, CORRODED AT COMPOSITE CROSSBEAM. MAINTENANCE REPAIRED CENTER OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00-10. THE AIRC
- [SDR C2XA08TY031](https://openairdocs.org/sdr/C2XA08TY031), Feb 25, 2008: CONNECTOR. LOOSE. THE AFT FACING PORTION OF THE CEILING EMERGENCY EXIT SIGN AT SEAT 12 IS INOP. RESECURED THE CONNECTOR, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE
- [SDR C2XA07SH033](https://openairdocs.org/sdr/C2XA07SH033), Jun 10, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM FROM FRAME 18 TO 23 WITH CORROSION. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRAME 18 TO 23 IAW SRM 51-40-
- [SDR C2XA07SH032](https://openairdocs.org/sdr/C2XA07SH032), Jun 10, 2007: PANEL. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND OVER THE WING TO FUSELAGE PNL 195 WITH CORRODED BONDING STRAPS. MAINTENANCE REPAIRED PNL 195 IAW EC 5750-01315, AIRCRAFT 
- [SDR C2XA07CL020](https://openairdocs.org/sdr/C2XA07CL020), Feb 7, 2007: SWITCH. LEAKING. EWR FLIGHT 2996 THE CREW REPORTED HYDRAULIC SYSTEM NR 2 FAILURE. TOTAL LOSS OF SYSTEM NR 2 FLUID. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCI
- [SDR C2XA06IA197](https://openairdocs.org/sdr/C2XA06IA197), Dec 21, 2006: PROXIMITY SWITCH. FAULTY. BNA - FLT 2278 THE CREW REPORTED THAT THE NOSE GEAR DOORS DID NOT CLOSE UNTIL REACHING AN ALTITUDE OF 11,000 FT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK
- [SDR C2XA05IA141](https://openairdocs.org/sdr/C2XA05IA141), Dec 12, 2005: BATTERY PACK. DISCHARGED. IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMER

All 86: https://openairdocs.org/deregistered/N14960-2015-08-06/reports.md

## Other aircraft with N14960

- [Cancelled 1943-05-06](https://openairdocs.org/deregistered/N14960-1943-05-06): Lockheed ELECTRA 10-B, S/N 1038. Owner: [Defense Supplies Corp](https://openairdocs.org/faa-owner/DEFENSE%20SUPPLIES%20CORP), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington)

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