# N13958: 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: 145085 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 11, 1998 - Last registry action: July 17, 2015 - Mode S code: A09FC8 - Location: [Norton Shores, MI](https://openairdocs.org/faa-place/MI/Norton%20Shores) - 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/N13958 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13958 - Page: https://openairdocs.org/deregistered/N13958-2015-08-06 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 (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C2XA11IA241](https://openairdocs.org/sdr/C2XA11IA241), Oct 20, 2011: SOLENOID VALVE. INOPERATIVE. DFW - FLIGHT 4416 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON APPROACH. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL - [SDR C2XA11IA239](https://openairdocs.org/sdr/C2XA11IA239), Oct 20, 2011: CONTROL LEVER. INOPERATIVE. DFW - FLIGHT 4416 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON APPROACH. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL - [SDR C2XA11TY133](https://openairdocs.org/sdr/C2XA11TY133), Aug 22, 2011: DOOR FRAME. CORRODED. TYS - A/C IN FOR A C-CHECK WHEN INSPECTION FOUND THE LOWER AFT CORNER OF THE SERVICE DOOR CUTOUT CORRODED. MAINTENANCE REPAIRED THE LOWER AFT CORNER OF THE SERV - [SDR C2XA11TY130](https://openairdocs.org/sdr/C2XA11TY130), Aug 21, 2011: SKIN. DAMAGED. GALLEY AREA SKIN PITTED ON FRAME 19 BETWEEN STRINGERS 21L AND 21R. CUT OUT DAMAGE. FABRICATED FILLER AND DOUBLER, ALODINED, PRIMED AND PAINTED IAW EC 5330-02467 - [SDR C2XA11TY098](https://openairdocs.org/sdr/C2XA11TY098), Jul 1, 2011: PRESSURE SWITCH. LEAKING. HYDRAULIC SYSTEM 1 WENT TO AMBER ON THE EICAS DURING FLIGHT. AIRCRAFT DIVERTED INTO TYS FROM RIC. MAINTENANCE REMOVED AND REPLACED THE LT RUDDER ACTUATOR PRESSU - [SDR C2XA11CL139](https://openairdocs.org/sdr/C2XA11CL139), Jun 1, 2011: ENGINE. LEAKING. IND FLT 2586 THE CREW REPORTED A NR 1 ENGINE OIL LEAK AND HIGH OIL TEMPERATURE. THE AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED - [SDR C2XA11RI095](https://openairdocs.org/sdr/C2XA11RI095), May 25, 2011: SENSOR. DEFECTIVE. FLIGHT 2236 - EWR - FLIGHT CREW REPORTED ENG NR 1 OIL TEMP RISING RAPIDLY. CREW PERFORMED ENG NR 1 PRECAUTIONARY ENGINE SHUT DOWN PER QHR. CREW PERFORMED AIR RE - [SDR C2XA11RI079](https://openairdocs.org/sdr/C2XA11RI079), May 13, 2011: PRECOOLER. DEFECTIVE. FLIGHT 2169 - FLIGHT CREW REPORTED BLEED 1 OVERTEMP ON ICE TEST. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED PRE-COOLER NR 1 - [SDR C2XA11TY049](https://openairdocs.org/sdr/C2XA11TY049), Apr 25, 2011: LIGHT. INOPERATIVE. ACFT WAS IN FOR AN OVERNIGHT SERVICE WHEN MX FOUND THE EMERGENCY LIGHT IN THE CABIN INOP. MX R & R THE FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-00. OPS CHECK A - [SDR C2XA11CL101](https://openairdocs.org/sdr/C2XA11CL101), Apr 23, 2011: HOSE. LEAKING. CREW REPORTED ERRATIC AIRSPEED AND ALTIMETER INDICATIONS ON THE F/O PFD ALONG WITH ASSOCIATED AIR SPEED AND ALTMETER ALERTS ON THE PFD IN STORMY WX AT FL370. TH - [SDR C2XA11RI026](https://openairdocs.org/sdr/C2XA11RI026), Feb 20, 2011: UNKNOWN. ODOR. FLIGHT 2315 - EWR - FLIGHT CREW REPORTED ELECTRICAL BURN SMELL WHEN GALLEY LIGHT IS TURNED ON. EWR MX COULD NOT DUPLICATE ELECTRICAL SMELL AND PERFORMED OPERATI - [SDR C2XA10RI157](https://openairdocs.org/sdr/C2XA10RI157), Dec 11, 2010: FLAP. STUCK. FLIGHT 2251 - IND - FLIGHT CREW REPORTED FLAP STUCK AT 9 DEGREES ON CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. FLAPS SYSTEM RESET AND OPERATIONAL - [SDR C2XA09CL136](https://openairdocs.org/sdr/C2XA09CL136), Oct 15, 2009: WIRE. SHORTED. CLE - FLT 2333 - THE CREW REPORTED NR 2 BLEED VALVE FAIL MESSAGE ON THE ECIAS DURING CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANC - [SDR C2XA09CL098](https://openairdocs.org/sdr/C2XA09CL098), Jul 18, 2009: SIGN. INOPERATIVE. DURING ROUTINE MX LT EMERGENCY EXIT SIDEWALL SIGN WAS FOUND INOPERATIVE. MX REPLACED EXIT SIGN AND OPS CHECKS WERE GOOD . - [SDR C2XA09TY148](https://openairdocs.org/sdr/C2XA09TY148), Jul 9, 2009: BUSHING. DAMAGED. IAW ENGINEERING REQUEST THE RT ELEVATOR REAR QUANDRANT ATTACH BRACKET WAS REMOVED. MX REMOVED THE HAT BUSHING, REAM HSG AND INSTALL A NEW FABRICATED BUSHING IAW - [SDR C2XA09SH184](https://openairdocs.org/sdr/C2XA09SH184), Jul 6, 2009: BUSHING. MIGRATED. SHV - DURING C-CHECK LT AILERON O/B HINGE FITTING (ON AILERON) HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE FITTING IAW EMB-14 - [SDR C2XA09SH191](https://openairdocs.org/sdr/C2XA09SH191), Jul 5, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM WAS CORRODED AT FR 20 ON UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FR 18-23 IAW EMB-145 SRM 51-40 - [SDR C2XA09SH190](https://openairdocs.org/sdr/C2XA09SH190), Jul 5, 2009: ATTACH FITTING. LOOSE. SHV - DURING C-CHECK VERTICAL STABILIZER ATTACHMENT AT FR 75 HAS WORKING HARDWARE AND FASTENERS. MAINTENANCE REMOVED AND INSTALLED NEW VERTICAL STABILIZER ATTAC - [SDR C2XA09SH189](https://openairdocs.org/sdr/C2XA09SH189), Jul 5, 2009: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM CORRODED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APP - [SDR C2XA09SH188](https://openairdocs.org/sdr/C2XA09SH188), Jul 5, 2009: HINGE. WORN. SHV - DURING C-CHECK RUDDER 1 CENTER, UPPER AND LOWER HINGES HAD PLAY. MAINTENANCE REMOVED AND REPLACED RUDDER 1 CENTER, UPPER AND LOWER HINGES IAW AMM 55-31-01 - [SDR C2XA09SH187](https://openairdocs.org/sdr/C2XA09SH187), Jul 5, 2009: BUSHING. WORN. SHV - DURING C-CHECK RT AILERON PCA TO AILERON ATTACHMENT HINGE HAS WORN HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED PCA ATTACHMENT FITTING ON AILERON SIDE I - [SDR C2XA09SH186](https://openairdocs.org/sdr/C2XA09SH186), Jul 5, 2009: BUSHING. MIGRATED. SHV - DURING C-CHECK LT AILERON O/B ATTACHMENT BRACKET ON AILERON SPAR, O/B & I/B HAT BUSHINGS WERE MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HI - [SDR C2XA09SH185](https://openairdocs.org/sdr/C2XA09SH185), Jul 5, 2009: HINGE FITTING. DAMAGED. SHV - DURING C-CHECK LT AILERON O/B HINGE FITTING (ON AILERON) I/B HAT BUSHING HOUSING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE - [SDR C2XA08RI152](https://openairdocs.org/sdr/C2XA08RI152), Oct 2, 2008: ADC. MALFUNCTIONED. FLT 2199 - BNA - FLT CREW REPORTED AIR DATA COMPUTER NR 1 FAILURE AND TOTAL FUEL DASHING OUT. FLT CREW PERFORMED AIR RETURN ANEVENTFULLY. FLT CREW PROCEEDED WIT - [SDR C2XA08RI002](https://openairdocs.org/sdr/C2XA08RI002), Jan 2, 2008: ANTI-ICE VALVE. INOPERATIVE. FLT 2708 - EWR - CREW REPORTED WING ANTI ICE FAIL MESSAGE ON EICAS AND PERFORMED AIR RETURN. ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 WING ANT - [SDR C2XA08RI003](https://openairdocs.org/sdr/C2XA08RI003), Jan 1, 2008: INVERTER. INOPERATIVE. EWR - DURING ROUTINE INSPECTION, MX FOUND EMERGENCY LIGHT FLOOR STRIP NR 1 INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT AC/DC INVERTER IAW EMB145 AMM 33 - [SDR C2XA07CL089](https://openairdocs.org/sdr/C2XA07CL089), Oct 23, 2007: INVERTER. INOPERATIVE. DURING ROUTINE MAINTENANCE THE RIGHT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND INOPERATIVE ALONG WITH THE AFT GALLEY EMERGENCY LIGHT. MAINTENANCE INSPECTED AND RE - [SDR C2XA07IA164](https://openairdocs.org/sdr/C2XA07IA164), Jul 11, 2007: BATTERY PACK. DISCHARGED. DAY - FLIGHT 2770, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERWING INTERIOR EXIT LIGHT AND AISLE PATH LIGHTING TO BE INOP. CONTRACT MAINTENANCE CHARG - [SDR C2XA07RI005](https://openairdocs.org/sdr/C2XA07RI005), Feb 19, 2007: POWER SUPPLY. INOPERATIVE. RIC - MX DURING ROUTINE MAINTENANCE, MX FOUND LT & RT OVERWING EMERGENCY LIGHTS INOP. MX TROUBLESHOT THE PROBLEM AND FOUND EMERGENCY POWER SUPPLY NR 4 INOP. MX - [SDR C2XA07IA020](https://openairdocs.org/sdr/C2XA07IA020), Jan 22, 2007: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION, THE NUMBER 4 AND 5 AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE - [SDR C2XA06BT046](https://openairdocs.org/sdr/C2XA06BT046), Oct 27, 2006: CONTACTOR. SHORTED. IN BTV LOG SQUAWK STRONG ELECTRICAL SMOKE SMELL IN FLIGHT DECK AND LANDING LIGHT ON WITH SWITCH SELECTED OFF. MEL'D. LATER IN EWR REMOVED AND REPLACED NOSE LAND - [SDR C2XA06IA125](https://openairdocs.org/sdr/C2XA06IA125), Aug 5, 2006: O-RING. FAILED. IAH - FLIGHT 2278, THE CREW REPORTED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANC - [SDR C2XA06TY036](https://openairdocs.org/sdr/C2XA06TY036), Jun 14, 2006: UPLOCK. MALFUNCTIONED. TYS, LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS, LOG PAGE 2077577, ORIGINAL FLIGHT GSP TO CLE, FLIGHT 2948, DIVERTED TO TYS. MAINTENANCE REMOVED AND REPLACED - [SDR C2XA06IA080](https://openairdocs.org/sdr/C2XA06IA080), May 26, 2006: LIGHT. MALFUNCTIONED. IAH - FLIGHT 2455, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE AISLE PATH LIGHTING TO BE INOPERATIVE BY ROWS 8 & 9. MAINTENANCE INSPECTED THE AIRCRAFT, - [SDR C2XA05SH99](https://openairdocs.org/sdr/C2XA05SH99), Aug 11, 2005: FLOORBEAM. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 61. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT FR 61 IAW EC 5320-01255. THE AIRCRAFT WAS APPROVED - [SDR C2XA05SH095](https://openairdocs.org/sdr/C2XA05SH095), Aug 7, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON LT OMEGA BEAM AT FRAME 25- FRAME 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 IAW EMB 145 SRM 53-00-10 - [SDR C2XA05SH094](https://openairdocs.org/sdr/C2XA05SH094), Aug 7, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON THE CENTER OMEGA BEAM AT FRAME 25-29. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 29 IAW EMB 145 SRM 53- - [SDR C2XA05SH100](https://openairdocs.org/sdr/C2XA05SH100), May 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 22-23. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FR 22-23 IAW EMB 145 SRM 53-21-10 SECTION 8 FIGURE - [SDR C2XA04IA132](https://openairdocs.org/sdr/C2XA04IA132), Oct 17, 2004: CONTROL LEVER. INOPERATIVE. CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND NORMALLY. AIRCRAFT LANDED AT OKC WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRIED TO IAH AND LANDING WITHOUT INCID - [SDR C2XA03SH379](https://openairdocs.org/sdr/C2XA03SH379), Oct 9, 2003: LIGHT. INOPERATIVE. DURING C-CHECK THE AFT EMERGENCY LIGHT PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT STRIP IAW EMB 145 AMM 33-50-12 - [SDR C2XA03SH369](https://openairdocs.org/sdr/C2XA03SH369), Oct 3, 2003: BUTTSTRAP. CORRODED. SHV-DURING C CHECK THE FWD DIGITAL BUTTSTRAP AT FR 14 TO FR 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB - [SDR C2XA03SH368](https://openairdocs.org/sdr/C2XA03SH368), Oct 3, 2003: STRUCTURE. GOUGED. SHV- DURING C-CHECK THE RIGHT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 - [SDR C2XA03SH367](https://openairdocs.org/sdr/C2XA03SH367), Oct 3, 2003: BUTTSTRAP. CORRODED. DURING C CHECK THE RT CENTER BUTT STRAP FROM FR 20 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 53-10-02. - [SDR C2XA03SH366](https://openairdocs.org/sdr/C2XA03SH366), Oct 2, 2003: STRUCTURE. CHAFED. DURING C-CHECK THE LT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO CHAFED THRU. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40- - [SDR C2XA03SH365](https://openairdocs.org/sdr/C2XA03SH365), Oct 2, 2003: ANGLE. CORRODED. SHV- DURING C-CHECK THE RAMP ANGLE AT FR 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIR - [SDR C2XA03SH364](https://openairdocs.org/sdr/C2XA03SH364), Oct 2, 2003: FLOORBEAM. CORRODED. DURING C-CHECK THE RIGHT CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WA - [SDR C2XA03SH362](https://openairdocs.org/sdr/C2XA03SH362), Sep 30, 2003: BUTTSTRAP. CORRODED. DURING C CHECK THE LT BUTTSTRAP IN THE CARGO COMPARTMENT AT FR 65-68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SR - [SDR C2XA03SH360](https://openairdocs.org/sdr/C2XA03SH360), Sep 30, 2003: SILL. CORRODED. DURING C CHECK THE AFT SERVICE DOOR SILL AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE - [SDR C2XA03SH359](https://openairdocs.org/sdr/C2XA03SH359), Sep 30, 2003: BUTTSTRAP. CORRODED. DURING C CHECK THE LEFT BUTTSTRAP BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51- - [SDR C2XA03SH358](https://openairdocs.org/sdr/C2XA03SH358), Sep 30, 2003: BUTTSTRAP. CORRODED. DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 5 All 72: https://openairdocs.org/deregistered/N13958-2015-08-06/reports.md --- 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.