Is AD 05-6757 a recurring Airworthiness Directive?

No — AD 05-6757 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 05-6757 apply to?

AD 05-6757 applies to Mcdonnell Douglas — models DC-9-10, DC-9-20, DC-9-30, DC-9-40, DC-9-50. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 05-6757

one-time

AD 05-6757 · 2005-04-06 · airframe

Airworthiness Directives; McDonnell Douglas Model DC-9-15F Airplanes Modified In Accordance With Supplemental Type Certificate (STC) SA1993SO; and Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes in All-Cargo Configuration, Equipped With a Main-Deck Cargo Door

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for the airplanes listed above. For certain airplanes, this AD requires inspecting to determine the airplane's cargo configuration, and reporting findings to the FAA. For airplanes modified in accordance with a certain STC or with a cargo configuration that deviates from the as-delivered configuration, this AD requires revising certain manuals and manual supplements to specify certain cargo limitations. This AD also requires relocating all cargo restraints on the main cargo deck. This AD is prompted by reports that deficiencies related to the cargo loading system may exist on all McDonnell Douglas Model DC-9-15F airplanes modified in accordance with STC SA1993SO. We are issuing this AD to ensure that cargo in the main cabin is adequately restrained and to prevent failure of components of the cargo loading system, failure of the floor structure, or shifting of cargo. Any of these conditions could cause cargo to exceed load distribution limits or cause damage to the fuselage or control cables, which could result in reduced controllability of the airplane.

Which aircraft AD 05-6757 applies to

MakesMcdonnell Douglas

ModelsDC-9-10, DC-9-20, DC-9-30, DC-9-40, DC-9-50

Modified

Whether AD 05-6757 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 05-6757 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.