Safety record in brief:1 NTSB accident (substantial damage, Dec 2020)No ADs since 1998 matched4 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.
The pilot’s decision to attempt takeoff with frost covering the airplane and rotating below the published rotation speed, which led to exceedance of the airplane’s critical angle of attack and an aerodynamic stall.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN21LA101)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
ALTERNATOR IN THE NR 1 POSITION FAILED IN FLIGHT. THE MAIN POWER STUD IS ATTACHED TO A PORTION OF THE RECTIFIER PLATE JUST AFTER A 90 DEGREE BEND, BROKE OFF AND CAUSED SIGNIFICANT ARCING AND BURNING IN THE ALTERNATOR. RIGHT NEXT TO THE BEND IN THE RECTIFIER PLATE THERE IS A STICKER THAT SAYS "MADE…
From FAA Service Difficulty Reports; matched by N-number and serial number.EXHAUST VALVE BROKEN IN HALF.
From FAA Service Difficulty Reports; matched by N-number and serial number.SOMETHING WITHIN THE 90 DEGREE DRIVE ASSY FAILED WHICH MADE THE FLAP FAIL TO EXTEND OR RETRACT. THE ACTUATOR WAS OH 20.6 HRS AGO.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE INSPECTING THE LEFT MLG AREA DURING A ROUTINE INSPECTION, NOTED UPPER TORQUE KNEE WAS CRACKED IN TWO PLACES. SUBMITTER STATED IF GONE UNNOTICED, IT COULD HAVE RESULTED IN THE LOSS OF THE LOWER STRUT ASSY AND SERIOUS DAMAGE TO AIRCRAFT. TOTAL TIME ON PART APPROXIMATELY 7,509 HOURS. A POSSIBLE…
From FAA Service Difficulty Reports; matched by N-number and serial number.