Safety record in brief:1 NTSB accident (substantial damage, Oct 2006)No ADs since 1998 matched3 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-in-command's improper remedial action, which resulted in a loss of helicopter control. Contributing factors were the retardant tank and snorkel designs.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX07TA001)
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.
NR 1 ENGINE REMOVED FROM ACFT, DUE TO 5 INCH AXIAL BULGE AT OUTER TURBINE CASE, 2-3 OCLOCK POSITION WITH APPROX .5625 INCH HORIZONTAL CRACK RUNNING THROUGH CENTER MOST PORTION OF THE BULGED AREA. UPON REMOVAL OF ENGINE HOT SECTION, TURBINE OUTLET DUCT FOUND TO HAVE APPROX A 8.5 INCH SECTION OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE BLADE WAS REMOVED FROM THE AIRCRAFT FOR BIM INDICATION. A 10-DAY LEAK CHECK WAS PERFORMED AND A CRACK WAS FOUND IN THE SPAR 117.75 INCHES FROM THE TIP END AND 4.50 INCHES FROM THE LEADING EDGE ON THE BOTTOM SIDE OF THE BLADE. CAUSE: UNKNOWN
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN GEARBOX PN 643520400063, SN A6032 WAS REMOVED FROM SERVICE WITH A TOTAL TIME OF 3683.8 AND A TIME SINCE OVERHAUL OF 1172.0 FOR AN OVER TEMP CONDITION. DURING OVERHAUL INSPECTION, THIRTEEN CRACKS WERE DETECTED BY FLUORESCENT PENETRANT INSPECTION, EXTENDING FROM LIGHTENING HOLES AND IN WEBBING…
From FAA Service Difficulty Reports; matched by N-number and serial number.