Is AD E6-17828 a recurring Airworthiness Directive?

Yes — AD E6-17828 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD E6-17828 apply to?

AD E6-17828 applies to Air Tractor, Inc — models AT-602, AT-802, AT-802A. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive E6-17828

recurring

AD E6-17828 · 2006-10-27 · airframe

Airworthiness Directives; Air Tractor, Inc. Models AT-602, AT-802, and AT-802A Airplanes

What this AD requires

The FAA adopts a new airworthiness directive (AD) for all Air Tractor, Inc. Models AT-602, AT-802, and AT-802A airplanes. This AD requires you to repetitively inspect the engine mount for any cracks, repair or replace any cracked engine mount, and report any cracks found to the FAA. This AD results from reports of cracked engine mounts. We are issuing this AD to detect and correct cracks in the engine mount, which could result in failure of the engine mount. Such failure could lead to separation of the engine from the airplane.

Repetitive inspection. Re-inspect. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD E6-17828 applies to

MakesAir Tractor, Inc

ModelsAT-602, AT-802, AT-802A

applicability derived from the AD summary — confirm the model/serial from the records

Whether AD E6-17828 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 E6-17828 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.