Airworthiness Directive 71-08-01

one-time
AD 71-08-01 · 1971-01-01 · airframe

Airworthiness Directives; automatic deployment system, inspect the two attaching rivets for the evacuation slide lanyard attach plate and verify that the Do

Which aircraft AD 71-08-01 applies to

MakesDouglas
Part-conditional5924584-3.

Compliance is gated to verification/installation of the specific Douglas plate part number noted in the teaser — confirm applicable model from the full AD text before use.

Whether AD 71-08-01 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 71-08-01 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.