Airworthiness Directive 2013-15946
one-timeAirworthiness Directives; Various Restricted Category Helicopters
What this AD requires
We are adopting a new airworthiness directive (AD) for various restricted category Model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH- 1F, UH-1H, UH-1L, and UH-1P helicopters with certain main rotor hub inboard strap fittings (fittings) installed. This AD requires a magnetic particle inspection (MPI) of the fittings for a crack, and if there is a crack, replacing the fitting with an airworthy fitting. This AD is prompted by reports of cracked fittings on Bell model helicopters and the determination that these same part-numbered fittings may be installed on various restricted category helicopters. These actions are intended to detect a crack in a fitting, which may lead to failure of a fitting, loss of a main rotor blade, and subsequent loss of helicopter control.
Which aircraft AD 2013-15946 applies to
Applies only to helicopters with a main rotor hub inboard strap fitting bearing one of the listed part numbers and serial numbers per Table 1: P/N 204-012-102-001 (all S/Ns), P/N 204-012-102-005 (all S/Ns), or P/N 204-012-102-009 (all S/Ns except those 7500 or larger with a prefix of 'A' or 'A-FS'). Also includes Southwest Florida Aviation International, Inc. Model UH-1B (SW204 and SW204HP) and UH-1H (SW205) helicopters.
Whether AD 2013-15946 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.