This N-number isn't registered right now. Below is its last known registration, canceled Sep 6, 2019.
Safety record in brief:1 NTSB accident (Aug 2001)9 ADs may apply36 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Inadequate company procedures/directives, which resulted in the flight attendant leaving her seat prematurely, while the airplane was still in an area of turbulence.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for IAD01LA102)
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 |
| 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.
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.
DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 3 & 4 FAILED OPERATIONAL CHECK. MAINTENANCE INSPECTED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT ROW 3 & 4. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW REPORTED, THE AFT SECTION OF EMERGENCY FLOOR AISLE PATH LIGHTING WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NR 3 AND NR 4 EMERGENCY LIGHT BATTERIES IAW EMB135 AMM NR 33-50-04, OPS CHECKED SYSTEM GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.SHV DURING C-CHECK CRACK WERE IDENTIFIED ON THE PAX AND SERVICE DOOR. PAX DOOR CRACK LOCATED AT LOWER INBOARD HOLE ON FORWARD FRAME AT STRINGER 14L IN THE 7 O'CLOCK POSITION. SERVICE DOOR HAS CRACK LOCATED ON AFT FRAME FORWARD SIDE AT STRINGER 7R IN THE 3 O’CLOCK POSITION. MAINTENANCE REPAIRED THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.CLE - THE CREW REPORTED RIGHT GEAR NO INTRANSIT INDICATION WHEN GEAR WAS RETRACTED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR UPLOCK PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.CLE FLIGHT 2944, THE CREW REPORTED A VERY STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT ANYTIME ANT-ICE WAS ON. MAINTENANCE INSPECTED AND FOUND THE -P- TERMINAL ON THE RIGHT WINDSHIELD BURNT. THE RIGHT WINDSHIELD WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.CLE FLIGHT 2578 - THE CREW REPORTED A BURNING RUBBER SMELL FROM THE NR 2 PACK. MAINTENANCE INSPECTED AND REINSTALLED DUCT UNDER FLOORBOARD ON THE NR 2 PACK. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.TYS - ON CLIMB THE CREW GOT A ICAS MESSAGE THAT THE WING ANTI-ICE FAIL, CREW RETURN TO BLOCK AND MAINTENANCE FOUND A PUSH PIN ON A CONNECTOR LOOSE. MAINTENANCE REINSERTED THE PIN AND OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING C-CHECK THE NR 1 EMERGENCY AISLE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB 135 AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A NEW SECTION IAW EMB 135 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 36 reports.