N165252001 Embraer EMB-135LR
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply30 service difficulty reports
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- Corporate Flight Management DBA
- Owner type
- Corporation
- City, state
- Smyrna, TN
- Certificate issued
- Jul 30, 2020
- Expires
- Jul 31, 2027
- Airworthiness
- Standard · Transport
- Airworthiness date
- Mar 24, 2001
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 dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-135LR
- Year
- 2001
- Serial number
- 145403
- 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
- A106FD
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- 2020 – nowCorporate Flight Management DBASmyrna, TN · current
- 1970 – 1973Co-ownersElsinore, CA · different airframe: Lockheed Electra 10-A S/N 1110
- 1942 – 1943Woodley AirwaysAnchorage, AK · different airframe: Waco Dqc-6 S/N 4480
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (9)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-135LR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-135LR) |
| 2020-16-13 | Turbine Engine Compressor Section | Aug 14, 2020 | Engine (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. |
| 2007-24-05 | Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan Engines | Jan 2, 2008 | Engine (AE 3007A) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-135LR)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002 |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-04-05 | Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan Engines | Mar 9, 2004 | Engine (AE 3007A) |
| 2002-14-23 | Empresa Brasileira de Aeronautica S.A. | Aug 2, 2002 | Airframe (EMB-135LR)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. |
| 2000-09-05 | Allison Engine Company AE 3007 Series Turbofan Engines | Jul 5, 2000 | Engine (AE 3007A)Only with: Cone shafts P/Ns 23050728 and 23070729 installed. |
| 99-03-03 | Allison Engine Company Model AE 3007A and AE 3007A1/1 Turbofan Engines | Feb 16, 1999 | Engine (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 (30)
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.
- Windows · windshield · crackedJun 4, 2026
ON JUNE 4, 2026 OUR FLIGHT VTE 3304 (N16252, PHX - PGA, PHX) RETURNED TO PHX AFTER THE CAPTAINS SIDE WINDSHIELD OUTER PANE CRACKED WHILE IN A DESCENT FROM FL260 TO FL250. THE FO DECLARED AN EMERGENCY AND BEGAN A DESCENT TO 10,000 FT AS A PRECAUTION. CREW COMPLETED QRH AND ELECTED TO RETURN TO PHX.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · dischargedMay 12, 2015
DURING A-CHECK INSPECTION, THE LT LOWER EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · dischargedMay 12, 2015
DURING A-CHECK INSPECTION NUMEROUS EMERGENCY LIGHTS IN THE CABIN FAILED TO ILLUMINATE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY 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.
Show all 10 reportsShow fewer reports
- Lights · ballast · overheatedJan 4, 2014
THE CREW REPORTED A BURNING ODOR FROM LIGHT BALLAST APPROXIMATELY ROW 1-3. LANDED WITHOUT INCIDENT. MAINTENANCE R & R LIGHT ASSY, OPS TESTED WITH NO DEFECTS. ACFT APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · gougedApr 9, 2013
FOUND SKIN GOUGED FRAME 19 TO 20. A DOUBLER REPAIR PERFORMED IAW SRM 53-21-01, AND ACFT APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedSep 13, 2007
LT SILL CORROSION AROUND FASTENERS AT FRM 22. REMOVED AND REPLACED SILL IAW SRM 51-40-22, AIRCRAFT STILL IN C CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedSep 13, 2007
SERVICE DOOR AFT LOWER CORNER BRACKET HAS CORROSION. REMOVED AND REPLACED AFT SILL IAW SRM 51-40-02. AIRCRAFT STILL IN C CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedSep 12, 2007
TYS - DURING THE CURRENT C-CHECK INSPECTION THE RIGHT OMEGA BEAM WAS FOUND TO HAVE CORROSION AROUND A NUT PLATE THAT WAS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM IAW EMB 135/145 SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedSep 12, 2007
TYS - DURING A CURRENT C-CHECK INSPECTION THE FWD DIGITAL WAS FOUND WITH CORROSION. MAINTENANCE REMOVED THE CORRODED SECTION, INSTALL A NEW SECTION WITH A DOUBLER. ALL WORK WAS IAW EMB EC 5320-01059. A/C WILL BE RELEASED AT THE END OF THE CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedSep 12, 2007
TYS - DURING A CURRENT C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED FROM FR 18 TO FR 22. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 30 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026