This N-number isn't registered right now. Below is its last known registration, canceled Nov 21, 2020.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jul 2007)No ADs since 1998 matched1 service difficulty report
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 loss of engine power due to a clogged fuel tube. A contributing factor was the lack of suitable terrain for the forced landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DFW07LA162)
THE HELICOPTER WAS BEING USED IN A LONG LINE DEMONSTRATION WHEN THE CABLE CONTACTED A MAN ON THE GROUND AND INJURED HIM.ACCORDING TO THE PILOT, AFTER THE ACFT WAS LANDED AT THE STAGING AREA, THE FIELD WAS BRIEFED ON HELICOPTER OPERATIONS FOR APRX 45 MIN. WHEN THE HELICOPTER TOOK OFF SEVERAL DISTRATIONS CAUSED THE GROUND CREWMEN TO FORGET TO DISCONNECT THE LONG LINE. NO ONE NOTICED THE LINE…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN83LA095)
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.
DURING POST-FLIGHT INSPECTION, A 2.50 INCH CHORDWISE CRACK WAS FOUND APPROXIMATELY .50 INCH INBOARD FROM THE TRAILING EDGE AND 14 INCHES FROM THE TIP OF THE BLADE. CORROSIVE OPERATING CONDITIONS. SUSPECT INTERGRANULAR CORROSION EMANATING FROM THE INTERIOR OF THE BLADE. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.