N145082000 Embraer EMB-135ER
This N-number isn't registered right now. Below is its last known registration, canceled Sep 6, 2019.
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply45 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- United Airlines INC
- Owner type
- Corporation
- City, state
- Chicago, IL
- Certificate issued
- May 3, 2016
- Canceled
- Sep 6, 2019
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 5, 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
- 145220
- 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
- A0B7BC
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- 2016 – 2019United Airlines INCChicago, IL
- 1977 – 1978Individual ownerBrownsville, TX · different airframe: Cessna Tu206f S/N U206-03110
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (45)
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.
- Engine · carbon seal · leakingJun 15, 2008
CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDING. MAINTENANCE INSPECTED AND FOUND MAJOR OIL LEAK AT THE REAR OF THE ENG. THE NR 2 ENG WAS REPLACED. THE TEAR DOWN REPORT FROM ROLLS ROYCE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · control unit · defectiveMar 19, 2008
FLIGHT 2424 - EWR - CREW REPORTED BRAKES INEFFECTIVE AT HIGH SPEED AFTER LANDING. BRAKE DEGRADE MESSAGE ON EICAS APPEARED MOMENTARILY, AND THEN DISAPPEARED, BUT BRAKE OPERATED NORMAL AT LOW SPEED. EWR MX REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. AIRCRAFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Equipment and furnishings · flashlight · inoperativeDec 26, 2007
NR 3 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT LAMP IAW EMB 135 VCMM 25-60-02. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery · dischargedDec 18, 2007
FA FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IAW EMB 135 AMM 33-50-16. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · hydraulic line · leakingJul 26, 2007
FLT 4923 - EWR - AT MLG RETRACTION, CREW REPORTED THAT RT MLG RETRACTED FASTER THAN LF MLG CAUSING YAW MOTION TO THE RIGHT. EWR MX REMOVED AND REPLACED MLG ACTUATOR EXTENSION LINE AND BLEED THE SYSTEM. MX PERFORMED LG OPERATIONAL CHECK SUCCESSFULLY. ACFT PERFORMED FLIGHT TEST SUCCESSFULLY. ACFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin panel · damagedOct 9, 2006
SHV - MAJOR - DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CREASED FORWARD OF FR 9 AND BELOW STR 15R. AFTER INITIAL REWORK THE AREA WAS STILL CREASED, HAD MINOR OIL CANNING AND MINOR WAVINESS OUT OF SRM LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedOct 7, 2006
SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10, FIG 206 DET B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · lamp · inoperativeFeb 14, 2006
DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · bulb · burned outJun 17, 2004
DURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · engine · failedApr 24, 2004
CLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 45 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