Airworthiness Directive 2013-21578
one-timeAirworthiness Directives; Bell Helicopter Textron Canada Inc. Helicopters
What this AD requires
We are adopting a new airworthiness directive (AD) for certain Bell Helicopter Textron Canada Inc. (BHT) Model 206A, 206B, and 206L helicopters. This AD requires replacing certain part-numbered engine auto-relight kit control boxes. This AD was prompted by a design review that revealed the control box chipset did not meet the required temperature range requirements, which could cause the control box to malfunction, disabling the engine auto-relight system. The actions of this AD are intended to prevent a disabled auto-relight system, failure of the engine to relight after a flame-out, increased pilot workload during a power loss emergency, and subsequent loss of control of the helicopter.
Which aircraft AD 2013-21578 applies to
206A/206B: all S/N except S/Ns 1, 2, and 3, with engine auto-relight kit control box assembly P/N 206-375-017-101 installed. 206L: S/N 45001-45153 and 46601-46617 with control box assembly P/N 206-375-017-103 installed.
Whether AD 2013-21578 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.