Skip to content
KnownTail
Aircraft record

N165011999 Embraer EMB-135ER

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply20 service difficulty reports

Registration
Valid
expires Nov 30, 2029
Based in
Smyrna, TN
owner city / state
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
20
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Corporate Flight Management INC
Owner type
Corporation
City, state
Smyrna, TN
Certificate issued
Nov 18, 2022
Expires
Nov 30, 2029
Airworthiness
Standard · Transport
Airworthiness date
Sep 3, 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-135ER
Year
1999
Serial number
145145
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
37
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A106B3

Engine

Make and model
Allison Ae3007c Ser
Type
Turbo-jet
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. 2022 – nowCorporate Flight Management INCSmyrna, TN · current
  2. 1947 – 1949Individual ownerOverland, MO · different airframe: Waco Zqc-6 S/N 4477

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (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
2024-26-07FuselageMar 11, 2025Airframe (EMB-135ER)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-135ER)
2007-24-05Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan EnginesJan 2, 2008Engine (AE3007C SER)
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-135ER)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-135ER)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
2000-09-05Allison Engine Company AE 3007 Series Turbofan EnginesJul 5, 2000Engine (AE3007C SER)Only with: Cone shafts P/Ns 23050728 and 23070729 installed.

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

Service Difficulty Reports (20)

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 · light · malfunctionedSep 10, 2007

    FLT 2154 - EWR - CREW REPORTED EMERGENCY EXIT ROW 9A LIGHTS INOPERATIVE. EWR MX RESET ACFT ELECTRIC POWER, AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Communications · rmu · smokeOct 1, 2006

    CLE FLIGHT NR 2786, CREW REPORTED SMOKE COMING FROM THE CO-PILOTS RMU WHILE TAXIING TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE CO-PILOTS RMU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · corrodedSep 10, 2006

    SHV - DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED AT FRAME 51. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · floorbeam · corrodedSep 6, 2006

    SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 24. MAINTENANCE REMOVED THE DAMAGED AREA AND SPLICED IN A NEW BEAM SECTION IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedSep 6, 2006

    DURING C-CHECK LT OMEGA BEAM FROM FR 20 TO 24 HAS CORROSION. MAINTENANCE SPLICED IN NEW LT OMEGA BEAM AT FR 18 TO 24 IAW EC5320-01229.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin panel · corrodedSep 1, 2006

    SHV - DURING C-CHECK CENTER FUSELAGE 3 EXTERNAL SKIN HAS AREA OF CORROSION AT STR 19R FR 50 HYDRAULIC LINE PASS THROUGH. MAINTENANCE REPAIRED CENTER 3 EXTERNAL SKIN AT STR R19 FR 50 IAW EC5330-01624. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · pdu · failedJan 18, 2006

    CLE FLIGHT 2056 - THE CREW REPORTED A -FLAP FAIL- MESSAGE ON THE EICAS UPON SELECTING FLAPS -22- DEGREES. FLAPS WERE STUCK AT THE -18- DEGREE POSITION. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLAP POWER DRIVE UNIT. PERFORMED -O…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · heater · burnedMar 16, 2005

    CLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · inoperativeFeb 9, 2004

    CLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · angle · corrodedJan 10, 2004

    DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

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

Showing the 10 most recent of 20 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

Request owner name removalReport an error in this record