Airworthiness Directive 2019-03641
recurringAirworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines
What this AD requires
We are adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran Helicopter Engines), ASTAZOU XIV B and H model engines with certain 3rd-stage turbine wheels installed. This AD requires initial and repetitive inspections of the 3rd-stage turbine wheels. This AD was prompted by a report that six 3rd-stage turbine wheels were returned to service after a repair that could result in exceedance of the allowable vibration threshold during operation. We are issuing this AD to address the unsafe condition on these products.
Which aircraft AD 2019-03641 applies to
Applies to engines with 3rd-stage turbine wheel P/N 0 265 25 706 0 (S/N AD78691AD, AD78703AD, AD93845AD, CC52860, RD39596) or P/N 0 265 25 705 0 (S/N L232AD) installed, per Figure 1 to paragraph (c) of this AD.
Whether AD 2019-03641 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.