Safety record in brief:1 NTSB accident (Nov 2010)4 ADs may apply4 service difficulty reports
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Individual owners are shown by city and state only.
An in-flight encounter with turbulence during cruise flight, which resulted in a serious injury to a flight attendant.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN11LA085)
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) |
| 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 |
| 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. |
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.
CREW REPORTED ON TAKEOFF ABOUT 7000 FEET, “HYD1 LO QTY” MSG ILLUMINATED ON EICAS. LOOKED AT HYDRAULIC PAGE, AND QUANTITY WAS DECREASING RAPIDLY. THEN “HYD1 PUMP FAIL” MSG ILLUMINATED. HEARD THE GEAR DOOR OPEN. RETURNED TO THE FIELD. CORR ACTION MX REMOVED DAMAGED RH NOSE GEAR DOOR ACTUATOR HYD…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ACCOMPLISHMENT OF TASK CARD 53-23-00-220-C04-A00, FOUND CORROSION UNDER LAVATORY AREA FLOOR BEAM CAP, FLOOR ATTACHMENT POINTS. ORIGINAL MATERIAL THICKNESS .040", ALLOWABLE DAMAGE LIMITED TO 30% OF ORIGINAL THICKNESS, MEASURED .031" DEEP, EXCEEDING THE MAX ALLOWABLE. CONTACTED EMBRAER AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.ISSUE-CREW REPORTED ENGINE 2 ITT WENT TO RED LIMIT RIGHT AFTER V1 ON TAKEOFF ROTATION, AFTER ACCELERATION ALTITUDE REDUCED THE POWER AND DIVERTED BACK TO KBUR, AND EVEN AFTER LANDING ITT SHOWS 720 ON ENGINES IDLE. AMT'S DISCOVERED DISCHARGE TUBE ASSY BROKEN OFF. AND INBOARD INNER CORE COW…
From FAA Service Difficulty Reports; matched by N-number and serial number.DISC: ERRONEOUS FUEL INDICATION, TAKE OFF WAS 9200LBS PASSING THROUGH 4000FT “FUEL IMBALANCE” EICAS AND IT SHOWED 10200LBS TOTAL. 5500 LEFT WING 4600 RIGHT WING. CORRECTIVE ACTION: CHECKED ELECTRICAL FUEL INDICATING SYSTEM AND TRANSFERRED FUEL FROM WING TO WING. "FUEL IMBALANCE" EICAS MESSAGE CAME…
From FAA Service Difficulty Reports; matched by N-number and serial number.