Is AD E7-2512 a recurring Airworthiness Directive?

No — AD E7-2512 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD E7-2512 apply to?

AD E7-2512 applies to Airbus — models B4. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive E7-2512

one-time

AD E7-2512 · 2007-02-27 · airframe

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes

What this AD requires

The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B2, B4-100, and B4-200 series airplanes. That AD currently requires supplemental structural inspections to detect fatigue cracking, and repair of cracked structure. This new AD requires revising the maintenance program by incorporating new and revised supplemental structural inspections, inspection intervals, and repairs; and repair of any damaged, cracked, or corroded structure; which would end the existing supplement structural inspections. This AD results from a review of service history and reports received from the current supplemental structural inspection document program. We are issuing this AD to prevent reduced structural integrity of these airplanes due to fatigue cracking.

Which aircraft AD E7-2512 applies to

MakesAirbus

ModelsB4

incorporating

Whether AD E7-2512 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 E7-2512 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.