Is AD 82-04-02 a recurring Airworthiness Directive?

No — AD 82-04-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 82-04-02 apply to?

AD 82-04-02 applies to Mcdonnell Douglas — models C-9, DC-9. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 82-04-02

one-time

AD 82-04-02 · 1982-01-01 · airframe

Airworthiness Directives; year, whichever occurs first. Replacement with aluminum rudder pedal arm assemblies constitutes terminating action for this AD. C.

Which aircraft AD 82-04-02 applies to

MakesMcdonnell Douglas

ModelsC-9, DC-9

Part-conditional — 3616012, 3953505.

Inspect magnesium rudder pedal arm assemblies (P/N 3616012) for cracks at intervals not to exceed one year; if cracks are found, replace with new aluminum rudder pedal arm assemblies (P/N 3953505), which constitutes terminating action for the AD.

Whether AD 82-04-02 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 82-04-02 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.