Safety record in brief:1 NTSB accident (substantial damage, Feb 2021)2 ADs may apply4 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 helicopter’s impact with an object on departure that could not be determined.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN21LA128)
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 |
|---|---|---|---|
| 2020-18-05 | Fuel Control/ Turbine Engines | Oct 7, 2020 | Engine (PT6B-37A)Certain serial numbers: PT6B-37A …–PCE-PU0289. Only with: Engines without an installed FCU incorporating a stainless steel air adapter per P&WC SB No. PT6B-72-39107, Revision No. 1. |
| 2019-22-03 | Turbine Engine Reduction Gear | Dec 24, 2019 | Engine (PT6B-37A)Certain serial numbers: PT6B-37A …–PCE-PU0275; PT6B-37A PCE-PU0278 |
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.
CORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN ROTOR BLADE DAMAGE. DURING CLIMB EXPERIENCED LOUD THUD PERFORMED PER-CAUTIONARY TO BASE LANDING FOUND HOLE THROUGH BLUE MAIN ROTOR BLADE AND LEADING EDGE DAMAGE. NO FLIGHT CONTROL DEFICIENCIES NOTED. HOLE AND DAMAGE IS LOCATED AT APROX 165 MM FROM ROOT OF BLADE.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND A CRACKED LT TRANSMISSION FITTING, FOUND DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0.
From FAA Service Difficulty Reports; matched by N-number and serial number.