N165102000 Embraer EMB-135ER
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply30 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Corporate Flight Management INC
- Owner type
- Corporation
- City, state
- Smyrna, TN
- Certificate issued
- Jan 28, 2019
- Expires
- Jan 31, 2029
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 21, 2000
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-135ER
- Year
- 2000
- Serial number
- 145251
- 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
- A106D5
Engine
- Make and model
- Allison Ae 3007a
- Type
- Turbo-jet
- 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- 2019 – nowCorporate Flight Management INCSmyrna, TN · current
- until 1973Safair Flying Service INCTeterboro, NJ · different airframe: Piper Pa-28-180 S/N 28-7305272
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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-135ER) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-135ER) |
| 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-135ER)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-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. |
| 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.
- Lights · power supply · inoperativeFeb 2, 2007
DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT AND THE FORWARD AISLE PATH LIGHT STRIP WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Airborne auxiliary power · firewall · chafedOct 21, 2006
SHV - MAJOR - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED. MAINTENANCE CLEANED UP THE DAMAGED AREA AND INSTALLED A SHIM IAW EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · sensor · odorMay 1, 2006
CREW REPORTED, PITOT 3 INOPERATIVE CAUTION LIGHT ON EICAS AND STRONG BURNING SMELL ON CABIN AND COCKPIT. FOUND PITOT NR 3 CURRENT SENSOR MELTED. REMOVED AND REPLACED PITOT NR 3 CURRENT SENSOR K0057 IAW EMB135 AMM 30-31-00, OPS CHECKED GOOD. NO BURNING SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Windows · windshield · failedApr 21, 2006
CLE FLIGHT 2805, THE CREW REPORTED UPON ENTERING ICING CONDITIONS, WINDSHIELD HEAT SELECTED, A STRONG ELECTRICAL SMELL WAS DETECTED. THE AIRCRAFT DIVERTED INTO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedMar 13, 2004
TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · corrodedMar 12, 2004
TYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedMar 12, 2004
TYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FAB AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · channel · corrodedMar 12, 2004
TYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedMar 4, 2004
TYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOOR SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bracket · corrodedMar 4, 2004
TYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FORWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
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 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