Is AD 77-14-01 a recurring Airworthiness Directive?

No — AD 77-14-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 77-14-01 apply to?

AD 77-14-01 applies to Agusta. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 77-14-01

one-time

AD 77-14-01 · 1977-01-01 · appliance

Airworthiness Directives; this AD, replace the main rotor hub flap hinge bearings P/N SJ7355/IR7355 in accordance with Part I of Agusta Technical Bulletin N

Which aircraft AD 77-14-01 applies to

MakesAgusta

Part-conditional — SJ7355, IR7355.

Main rotor hub flap hinge bearings, P/N SJ7355/IR7355; replace per Part I of Agusta Technical Bulletin No. 109-3, dated May 4, 1977, or FAA-approved equivalent; inspect and replace bearings if abnormal oil leaks occur from flap hinges per Part II of the same bulletin.

Whether AD 77-14-01 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 77-14-01 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 →

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.