Airworthiness Directive 2005-16-04

one-time
Official AD 2005-16-04 · FR doc 05-15581 · 2005-08-08 · airframe

Airworthiness Directives; Bell Helicopter Textron Model 206A and 206B Helicopters

What this AD requires

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron (Bell) Model 206A and 206B helicopters modified by Aeronautical Accessories, Inc. Supplemental Type Certificate (STC) SH1392SO with certain part-numbered high crosstubes. This amendment requires inspecting at specified time intervals and replacing any cracked crosstubes. This amendment is prompted by the discovery of a cracked high forward crosstube. The actions specified by this AD are intended to detect a crack in the crosstube which could lead to failure of the crosstube, collapse of the landing gear, and subsequent loss of control of the helicopter.

Which aircraft AD 2005-16-04 applies to

MakesBell
Models206A, 206B, 206
Part-conditional206-321-001, 206-321-002.

Applies only to helicopters modified by Aeronautical Accessories, Inc. STC SH1392SO, with high forward crosstube P/N 206-321-001, S/N 1001 through 1152, and high aft crosstube P/N 206-321-002, S/N 2001 through 2152, installed. Certificated in any category.

Whether AD 2005-16-04 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 2005-16-04 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.