Airworthiness Directive 2013-15946

one-time
AD 2013-15946 · 2013-07-09 · airframe

Airworthiness 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

MakesArrow Falcon Exporters Inc.Ast, Inc.Bell Helicopter Textron, Inc.Global Helicopter Technology, Inc.Hagglund Helicopters, LlcJjaspp Engineering Services, LlcNorthwest Rotorcraft, LlcOverseas Aircraft Support, Inc.Richards Heavylift Helo, Inc.Robinson Air Crane, Inc.Rotorcraft Development CorporationSan Joaquin HelicoptersSouthern Helicopter, Inc.Tamarack Helicopters, Inc.Southwest Florida Aviation International, Inc.
ModelsHH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, UH-1P, HH-1, TH-1, UH-1
Part-conditional204-012-102-001, 204-012-102-005, 204-012-102-009.

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:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2013-15946 complied with on your aircraft?

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.