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Aircraft record

N149741999 Embraer EMB-145LR

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jul 31, 2021.

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply120 service difficulty reports

Registration
Deregistered
Last based in
West Palm Beach, FL
owner city / state
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
120
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Flight Lease Holdings LLC
Owner type
LLC
City, state
West Palm Beach, FL
Certificate issued
Apr 4, 2018
Canceled
Jul 31, 2021
Airworthiness
Standard · Transport
Airworthiness date
Aug 14, 1999

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Embraer
Model
EMB-145LR
Year
1999
Serial number
145161
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
55
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A0C789

Engine

Make and model
Allison Ae 3007a
Type
Turbo-fan
Power
7,580 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2018 – 2021Flight Lease Holdings LLCWest Palm Beach, FL

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (11)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2025-08-07Flight ControlsJun 26, 2025Airframe (EMB-145LR)
2024-26-07FuselageMar 11, 2025Airframe (EMB-145LR)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-145LR)
2020-16-13Turbine Engine Compressor SectionAug 14, 2020Engine (AE 3007A)Serial numbers per Figure 1 to paragraph (c) of this AD. Only with: 3rd-stage compressor wheel P/N 23084158 installed with serial number listed in Figure 1.
2007-24-05Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan EnginesJan 2, 2008Engine (AE 3007A)
Show all 11 ADs
ADSubjectEffectiveApplies to
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-145LR)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002
2004-04-05Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan EnginesMar 9, 2004Engine (AE 3007A)
2002-14-23Empresa Brasileira de Aeronautica S.A.Aug 2, 2002Airframe (EMB-145LR)Serial numbers per EMBRAER Service Bulletin 145-27-0088, dated February 1, 2002. Only with: Equipped with horizontal stabilizer actuator (HSA) assemblies having part numbers and serial numbers listed in EMBRAER Service Bulletin 145-27-0088.
2000-09-09EMBRAER Model EMB-145 Series AirplanesJun 16, 2000Airframe (EMB-145LR)Certain serial numbers: EMB-145 145004–145047; EMB-145 145049–145051. Only with: Equipped with IC-600 #1 P/N 7017000-82402; excluding airplanes modified per EMBRAER SB 145-22-0001, SB 145-22-0004 Rev 01, or SB 145-31-0007 Rev 02.
2000-09-05Allison Engine Company AE 3007 Series Turbofan EnginesJul 5, 2000Engine (AE 3007A)Only with: Cone shafts P/Ns 23050728 and 23070729 installed.
99-03-03Allison Engine Company Model AE 3007A and AE 3007A1/1 Turbofan EnginesFeb 16, 1999Engine (AE 3007A)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (120)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Lights · control module · overheatedOct 12, 2014

    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 WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · stiffener · crackedJul 11, 2014

    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 ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor skin · corrodedJul 11, 2014

    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 REPAIR IAW EC5330-02921. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · skin · corrodedJul 11, 2014

    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 PERFORMED A DOUBLER REPAIR IAW EC5330-02922. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJul 10, 2014

    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 SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedJul 10, 2014

    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 SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · corrodedJul 10, 2014

    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 SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · corrodedJul 4, 2014

    DURING C-CHECK, FRAME 75 VERTICAL FITTING IS FRETTING. REPAIRED FRAME 75 FITTING IAW EC5330-02918. ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · inverter · inoperativeJun 2, 2013

    DURING MX THE GALLEY OVERHEAD AND COCKPIT STEP EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedAug 6, 2012

    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 SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 120 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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