Safety record in brief:1 NTSB incident (minor damage, Nov 2019)3 ADs may apply1 service difficulty report
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Fatigue fracture of the main rotor blade tip cap leading edge and subsequent partial separation of the tip cap, resulting in increased vibrations in the main rotor.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for ENG20IA005)
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 |
|---|---|---|---|
| 2013-03-21 | Pratt & Whitney Canada Corp. Turboshaft Engines | Mar 26, 2013 | Engine (PW206C) |
| 2009-03-05 | Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and… | Mar 27, 2009 | Engine (PW206C) |
| 2004-14-22 | Pratt & Whitney Canada PW206B, PW206C, PW206E, PW207D, and PW207E Turboshaft Engines | Aug 3, 2004 | Engine (PW206C)Only with: PW206B engines only if PWC Service Bulletin No. 28119 has been incorporated. |
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.
NUMBER 4 MAIN ROTOR TIP DETACHED DURING FLIGHT. ACFT LANDED SAFELY ON GROUND. TAIL ROTOR HUB, MAIN ROTOR HUB AND ALL FOUR MAIN ROTOR BLADES REMOVED AND SENT TO MANUFACTURER FOR FURTHER INSPECTION.
From FAA Service Difficulty Reports; matched by N-number and serial number.