# N14974: 1999 Embraer EMB-145LR, registration cancelled 2021-07-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 31, 2021
- Status when cancelled: Registration expired, pending cancellation
- 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: 145161
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 1999
- Certificate issued: April 4, 2018
- Last registry action: April 4, 2018
- Mode S code: A0C789
- Owner when cancelled: [Flight Lease Holdings LLC](https://openairdocs.org/faa-owner/FLIGHT%20LEASE%20HOLDINGS%20LLC)
- Location: [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach)
- Owner type: LLC
- Owner's area on the map: 26.7158° N, 80.0668° W: Placed by OpenAirDocs at the center of ZIP code 33401, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14974
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14974
- Page: https://openairdocs.org/deregistered/N14974-2021-07-31

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 (120, newest 50)

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

- [SDR ASOA20141012128](https://openairdocs.org/sdr/ASOA20141012128), Oct 12, 2014: CONTROL MODULE. OVERHEATED. THE CREW REPORTED A BURNING ODOR COMING FROM THE CABIN LIGHT MODULE. LANDED WITHOUT INCIDENT AND MAINTENANCE R & R THE CABIN LIGHT CONTROL MODULE, OPS TESTED WI
- [SDR ASOA201400711219](https://openairdocs.org/sdr/ASOA201400711219), Jul 11, 2014: SKIN. CORRODED. DURING C-CHECK, THE FUSELAGE SKIN AT FRAME 65 AND STRINGERS 21L-21R WAS FOUND TO BE CORRODED UNDER THE RA NR 2 ANTENNA. MAINTENANCE REMOVED THE CORROSION AND PE
- [SDR ASOA201400711218V](https://openairdocs.org/sdr/ASOA201400711218V), Jul 11, 2014: FLOOR SKIN. CORRODED. DURING C-CHECK THE GALLEY FLOOR SKIN WAS FOUND TO BE CORRODED FROM FRAMES 17-19 AND STRINGERS 21R-21L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER
- [SDR ASOA201400711217](https://openairdocs.org/sdr/ASOA201400711217), Jul 11, 2014: STIFFENER. CRACKED. DURING C-CHECK THE VERTICAL STABILIZER RT AFT T/E LOWER SKIN STIFFENER WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5530-01283. THE ACF
- [SDR ASOA201400710216](https://openairdocs.org/sdr/ASOA201400710216), Jul 10, 2014: STRINGER. CORRODED. DURING C-CHECK, STRINGER 19L WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-65. MAINTENANCE R & R THE STRINGER IAW EC5330-02919. THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA201400710215](https://openairdocs.org/sdr/ASOA201400710215), Jul 10, 2014: BEAM. CORRODED. DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA201400710214V](https://openairdocs.org/sdr/ASOA201400710214V), Jul 10, 2014: SKIN. CORRODED. DURING C-CHECK, SKIN SPLICE AT FRAMES 71-72 AND STRINGERS 19-20L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW 
- [SDR ASOA20140704199](https://openairdocs.org/sdr/ASOA20140704199), Jul 4, 2014: FITTING. CORRODED. DURING C-CHECK, FRAME 75 VERTICAL FITTING IS FRETTING. REPAIRED FRAME 75 FITTING IAW EC5330-02918. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130602044](https://openairdocs.org/sdr/ASOA20130602044), Jun 2, 2013: INVERTER. INOPERATIVE. DURING MX THE GALLEY OVERHEAD AND COCKPIT STEP EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.
- [SDR ASOA20120806069V](https://openairdocs.org/sdr/ASOA20120806069V), Aug 6, 2012: BUSHING. MIGRATED. DURING C-CHECK, TWO MIGRATED HAT BUSHINGS ON RT AILERON PCA FITTING. MX R & R PCA FITTING IAW EC5750-01177. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806068V](https://openairdocs.org/sdr/ASOA20120806068V), Aug 6, 2012: SUPPORT. CORRODED. DURING C-CHECK, LT UPPER SEAT TRACK SUPPORT FRM 50, LWR ATTACH FASTENERS CORRODED. MX PERFORMED REPAIR IAW SRM 51-40-02 AND EC5320-01522, REV A. WET INSTALLED F
- [SDR ASOA20120806067V](https://openairdocs.org/sdr/ASOA20120806067V), Aug 6, 2012: FRAME. DAMAGED. DURING C-CHECK, STRUCTURE AT FRM 50, STR 15R HAS 1 MISDRILLED HOLE. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806066V](https://openairdocs.org/sdr/ASOA20120806066V), Aug 6, 2012: FRAME. DAMAGED. DURING C-CHECK, STRUCTURE AT FRM 48, STR 15R HAS 2 MISDRILLED HOLES. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806065V](https://openairdocs.org/sdr/ASOA20120806065V), Aug 6, 2012: FRAME. DAMAGED. DURING C-CHECK, FRAME 48 HAS 2 MISDRILLED HOLES AT STR 15R. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120806064V](https://openairdocs.org/sdr/ASOA20120806064V), Aug 6, 2012: BEAM. CORRODED. DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT BEAM HAS CORROSION. MX R & R BAGGAGE DOOR LOWER CUTOUT BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA2011CL008](https://openairdocs.org/sdr/ASOA2011CL008), Nov 30, 2011: WIRE. LOOSE. THE CREW REPORTED THE AFT CABIN EMERGENCY LIGHT STAYS ILLUMINATED WHEN ACFT POWER WAS TURNED OFF. MX INSPECTED AND RESECURED WIRE W776-8515-20 ON CONNECTOR P810
- [SDR C2XA11IA126](https://openairdocs.org/sdr/C2XA11IA126), Jun 21, 2011: UNKNOWN. ODOR. BHM - FLIGHT 2824 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE, AND SMELLED ELECTRICAL TYPE SMOKE. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT WHERE CONTRACT M
- [SDR C2XA11IA113](https://openairdocs.org/sdr/C2XA11IA113), Jun 12, 2011: FAN. INOPERATIVE. AFTER TAKE OFF FROM DFW CREW REPORTED SMOKE IN COCKPIT. FLIGHT AIR RETURNED BACK TO DFW. LANDING WAS UNEVENTFUL. MAINTENANCE COMPLIED WITH FIM 21-20-00-810-801-
- [SDR C2XA11TY088](https://openairdocs.org/sdr/C2XA11TY088), Jun 12, 2011: CONTROL VALVE. DRAGGING. TYS - A/C WAS TAXIING FROM IAH GATE WHEN CREW FELT THE BRAKES DRAGGING. UPON FURTHER INSPECTION FOUND THE RT INBOARD BRAKE DRAGGING. MAINTENANCE REMOVED AND REP
- [SDR C2XA11TY037](https://openairdocs.org/sdr/C2XA11TY037), Mar 25, 2011: STRUCTURE. DAMAGED. TYS - A/C WAS EN ROUTE TO BNA FROM EWR WHEN LIGHTNING STRUCK THE A/C. THE A/C LANDING AT BNA WITHOUT ANY INCIDENT. MAINTENANCE COMPLIED WITH TASKCARD 6232012, W
- [SDR C2XA10SH311](https://openairdocs.org/sdr/C2XA10SH311), Sep 15, 2010: SKIN. DENTED. SHV - DURING C-CHECK SKIN DENTED BETWEEN FRAMES 65-66 STRINGER 4R-5R ON EXTERNAL FUSELAGE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 65-66 STRINGER
- [SDR C2XA10SH310](https://openairdocs.org/sdr/C2XA10SH310), Sep 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT RADIUS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BETWEEN FRAMES 18-23 I
- [SDR C2XA10SH309](https://openairdocs.org/sdr/C2XA10SH309), Sep 15, 2010: CROSSBEAM. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 29 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON
- [SDR C2XA10SH308](https://openairdocs.org/sdr/C2XA10SH308), Sep 15, 2010: CROSSBEAM. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBE
- [SDR C2XA10SH307](https://openairdocs.org/sdr/C2XA10SH307), Sep 15, 2010: FLOORBEAM. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBE
- [SDR C2XA10SH306](https://openairdocs.org/sdr/C2XA10SH306), Sep 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR TO CENTER OMEGA BEAM CARBON
- [SDR C2XA10SH305](https://openairdocs.org/sdr/C2XA10SH305), Sep 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON
- [SDR C2XA10SH304](https://openairdocs.org/sdr/C2XA10SH304), Sep 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBE
- [SDR C2XA10SH303](https://openairdocs.org/sdr/C2XA10SH303), Sep 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAMES 59-61. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 59-61 IAW EC5320-01137. THE 
- [SDR C2XA10SH302](https://openairdocs.org/sdr/C2XA10SH302), Sep 15, 2010: DOOR FRAME. CORRODED. SHV - DURING C-CHECK BAGGAGE DOOR LOWER CUTOUT FRAMES 65 TO 68 INTERIOR AND EXTERIOR HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED THE CARGO L
- [SDR C2XA10SH301](https://openairdocs.org/sdr/C2XA10SH301), Sep 15, 2010: STRINGER. DAMAGED. SHV - DURING C-CHECK STRINGER 5R DAMAGED FRAMES 65-66. MAINTENANCE PERFORMED REPAIR OF STRINGER 5R AT FRAME 65 IAW ETD 2010-145/07996. THE AIRCRAFT WAS APPROVED
- [SDR C2XA10SH300](https://openairdocs.org/sdr/C2XA10SH300), Sep 15, 2010: SUPPORT FITTING. CRACKED. SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON AT FRAME 73 STRINGER 8R. MAINTENANCE REMOVED AND INSTALLED NEW FABRICATED ANGLE SUPPORT CLIP IN PYLON A
- [SDR C2XA10SH299](https://openairdocs.org/sdr/C2XA10SH299), Sep 15, 2010: SUPPORT FITTING. CRACKED. SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON FRAME 73 STRINGER 8L. MAINTENANCE REMOVED AND FABRICATED NEW ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-73
- [SDR C2XA10SH293](https://openairdocs.org/sdr/C2XA10SH293), Sep 15, 2010: HINGE BRACKET. GOUGED. SHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE I/B ATTACHMENT BRACKET (ON WING) HAS GOUGES INSIDE & AROUND BOLT HOLE. MAINTENANCE REMOVED AND REPLACED LT SPEE
- [SDR C2XA10SH292](https://openairdocs.org/sdr/C2XA10SH292), Sep 15, 2010: FITTING. WORN. SHV - DURING C-CHECK RT AILERON PCA O/B ROD FITTING O/B HAT BUSHING ON AILERON MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA BRACKET FITTING IAW EC5
- [SDR C2XA10SH291](https://openairdocs.org/sdr/C2XA10SH291), Sep 15, 2010: HINGE BRACKET. WORN. SHV - DURING C-CHECK ON RT AILERON 2ND FROM I/B HINGE BRACKET O/B SIDE HAT BUSHING MISSING. MAINTENANCE REMOVED AND REPLACED I/B HINGE BRACKET O/B SIDE FOR RT A
- [SDR C2XA10TY096](https://openairdocs.org/sdr/C2XA10TY096), Jun 27, 2010: BATTERY. OVERTEMP. BATTERY NR 2 OVERTEMP UP TO 64C. REMOVED AND REPLACED BATTERY IAW EMB 145AMM 24-36-01, OPS CHECK GOOD.
- [SDR C2XA10IA156](https://openairdocs.org/sdr/C2XA10IA156), May 17, 2010: INVERTER. INOPERATIVE. MCI - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE RIGHT EMERGENCY DOOR EXIT LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY L
- [SDR C2XA10CL062](https://openairdocs.org/sdr/C2XA10CL062), Apr 2, 2010: O-RING. DETERIORATED. CLE FLT 2556 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED LINE GA
- [SDR C2XA10IA100](https://openairdocs.org/sdr/C2XA10IA100), Mar 21, 2010: INVERTER. INOPERATIVE. EXTERIOR EXIT MARKER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP INVERTER AND OPERATIONAL CHECKED GOOD.
- [SDR C2XA09CL166](https://openairdocs.org/sdr/C2XA09CL166), Dec 21, 2009: CONTROL UNIT. FAULTY. CLE FLT 2841 THE CREW REPORTED A INBOARD BRAKE INOP MESSAGE WHEN THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL C
- [SDR C2XA09IA267](https://openairdocs.org/sdr/C2XA09IA267), Oct 22, 2009: LIGHT. MALFUNCTIONED. IAH - FLIGHT 2117, THE CREW REPORTED AN ELECTRIC SMELL IN THE COCKPIT ON DESCENT INTO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED
- [SDR C2XA09IA206](https://openairdocs.org/sdr/C2XA09IA206), Aug 13, 2009: ACTUATOR. MALFUNCTIONED. OMA - FLIGHT 2593, ON DESCENT THE CREW REPORTED THAT THE SPOILER FAILED TO CLOSE SYMMETRICALLY, AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT OMA WITHOUT IN
- [SDR C2XA09IA116](https://openairdocs.org/sdr/C2XA09IA116), May 2, 2009: MAGNETIC SEAL. LEAKING. IAH - FLIGHT 3108, THE CREW REPORTED THAT APPROXIMATELY ONE HOUR INTO FLIGHT THEY STARTED LOSING OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE. THE CREW SHUT DO
- [SDR C2XA08CL096](https://openairdocs.org/sdr/C2XA08CL096), Aug 8, 2008: BATTERY. INOPERATIVE. CLE FLIGHT 2522, THE CREW REPORTED THE CAPTAIN` S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN`S FLASHLIGHT BATTERY. OPERATIONAL
- [SDR C2XA08SH082](https://openairdocs.org/sdr/C2XA08SH082), Jun 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK IT WAS FOUND THAT THE RT OMEGA BEAM HAT SECTION WAS CORRODED AROUND NUT PLATE HOLES AT FRAME 18. MAINTENANCE REMOVED THE CORROSION AND PERF
- [SDR C2XA08SH083](https://openairdocs.org/sdr/C2XA08SH083), Jun 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK IT WAS FOUND THAT THE LT OMEGA SHAPE WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145
- [SDR C2XA08SH084](https://openairdocs.org/sdr/C2XA08SH084), Jun 11, 2008: SKIN. DENTED. SHV - DURING C-CHECK IT WAS FOUND THAT THE LT REAR FUSELAGE SKIN WAS DENTED AT FRAME 65/STRINGER 16L, DIRECTLY BELOW THE FORWARD LOWER CORNER OF THE CARGO DOOR 
- [SDR C2XA07RI084](https://openairdocs.org/sdr/C2XA07RI084), Sep 24, 2007: INVERTER. INOPERATIVE. EWR - DURING ROUTINE MAINTENANCE, MX FOUND FIRST EMERGENCY LIGHT STRIP INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND
- [SDR C2XA07RI085](https://openairdocs.org/sdr/C2XA07RI085), Sep 19, 2007: INVERTER. INOPERATIVE. EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIPS 6, 7 AND 8 INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 

All 120: https://openairdocs.org/deregistered/N14974-2021-07-31/reports.md

## FAA accident and incident reports (2)

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 20090813014379I](https://openairdocs.org/incident/20090813014379I), Aug 13, 2009: Emb EMB145LR (N14974), Omaha, NE, No damage. (-23) N14974, Emb-145LR, being operated by express jet as Continental express flight 2593 landed at Omaha, NE, with asymmetrical spoilers. The crew reported to…
- [Incident 20070714014419I](https://openairdocs.org/incident/20070714014419I), Jul 14, 2007: Emb EMB145LR (N14974), Manchester, NH, No damage. (-23) This office notified by new england area operations center that Continental express 2853, E145, reported a hydraulic problem prior to landing Manchester,…

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