Is AD 2006-11-14 a recurring Airworthiness Directive?

No — AD 2006-11-14 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2006-11-14 apply to?

AD 2006-11-14 applies to Sikorsky — models S-92A, S-92. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2006-11-14

one-time

Official AD 2006-11-14 · FR doc 06-4911 · 2006-05-31 · airframe

Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters

What this AD requires

This amendment adopts a new airworthiness directive (AD) for the specified Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This action requires inspecting each main transmission assembly mounting bolt (bolt) for wear or corrosion, and if wear or corrosion is found, replacing the bolt, bolt barrel nut, and cage. This amendment is prompted by a report of a failure of a bolt that was discovered during a routine maintenance inspection. The actions specified in this AD are intended to prevent failure of a bolt, which could result in loss of support of the main transmission and subsequent loss of control of the helicopter.

Which aircraft AD 2006-11-14 applies to

MakesSikorsky

ModelsS-92A, S-92

Part-conditional — SS5211-10-47.

Applies only to helicopters with main transmission mounting bolt P/N SS5211-10-47 installed. Certificated in any category.

Whether AD 2006-11-14 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 2006-11-14 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.