This N-number isn't registered right now. Below is its last known registration, canceled May 7, 2022.
Safety record in brief:1 NTSB accident (destroyed damage, Jun 2019)2 ADs may apply1 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 non-instrument-rated pilot’s decision to initiate the flight into marginal visual flight rules and instrument meteorological conditions, which resulted in spatial disorientation and a subsequent loss of control.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for ERA19FA191)
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 |
|---|---|---|---|
| 2009-03-05 | Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and… | Mar 27, 2009 | Engine (PW206A) |
| 2004-17-03 | Pratt & Whitney Canada PW206A and PW206E Turboshaft Engines | Sep 24, 2004 | Engine (PW206A) |
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.
PILOT FELT VIBRATION IN TAIL ROTOR PEDALS DURING APPROACH. POST FLIGHT INSPECTION REVEALED THAT 1 TAIL ROTOR BLADE HAD A CHORD WISE CRACK BEGINNING AFT OF THE SPAR AND EXTENDING THROUGH THE TRAILING EDGE OF THE BLADE. THE CRACK WAS THROUGH BOTH SKINS AND THE HONEYCOMB CORE. SB109EP-30 REV B AND AD…
From FAA Service Difficulty Reports; matched by N-number and serial number.