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Aircraft record

N159321997 Embraer EMB-145EP

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Dec 31, 2022.

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply115 service difficulty reports

Registration
Deregistered
Last based in
Austin, TX
owner city / state
Engine
AE3007 SER · 6,442 lb thrust
Rolls-Royc
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
115
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Spectre Air Capital LLC
Owner type
LLC
City, state
Austin, TX
Certificate issued
Sep 12, 2019
Canceled
Dec 31, 2022
Airworthiness
Standard · Transport
Airworthiness date
Jun 27, 2005

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-145EP
Year
1997
Serial number
145.015
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
A0EE7A

Engine

Make and model
Rolls-Royc Ae3007 Ser
Type
Turbo-fan
Power
6,442 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. 2019 – 2022Spectre Air Capital LLCAustin, TX
  2. 1973Individual ownerLock Haven, PA · different airframe: Piper Pa-34-200 S/N 34-7350110

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

ADs published since 1998 that may apply (6)

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-145EP)
2024-26-07FuselageMar 11, 2025Airframe (EMB-145EP)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-145EP)
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-145EP)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002
2002-14-23Empresa Brasileira de Aeronautica S.A.Aug 2, 2002Airframe (EMB-145EP)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.
Show all 6 ADs
ADSubjectEffectiveApplies to
2000-09-09EMBRAER Model EMB-145 Series AirplanesJun 16, 2000Airframe (EMB-145EP)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.

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

Service Difficulty Reports (115)

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.

  • Fuselage · sill · corrodedDec 18, 2013

    DURING C-CHECK, SERVICE DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-02. ACFT APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · support · corrodedDec 18, 2013

    DURING C-CHECK, LAVATORY WASTE DRAIN SUPPORT ASSY WAS FOUND TO BE CORRODED. R & R SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedDec 18, 2013

    DURING C-CHECK, RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · stringer · crackedDec 18, 2013

    DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 14. R & R STRINGER SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedDec 18, 2013

    DURING C-CHECK, LEFT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. R & R FRAME SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · hinge fitting · wornDec 18, 2013

    DURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · hinge fitting · wornDec 18, 2013

    DURING C-CHECK, THE RUDDER II UPPER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING 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 · skin · crackedDec 18, 2013

    DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-80 AND STRINGERS 3-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02840. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · hinge fitting · wornDec 18, 2013

    DURING C-CHECK, HORIZONTAL STAB HINGE PIN FITTING NR 1 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · hinge fitting · wornDec 18, 2013

    DURING C-CHECK, THE HORIZONTAL STAB HINGE PIN FITTING NR 2 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. 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 115 reports.

Related aircraft

Show all 8 related aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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