Airworthiness Directive 74-17-01

one-time
AD 74-17-01 · 1974-01-01 · appliance

Airworthiness Directives; Western Region. This amendment becomes effective September 16, 1974. FOOTER: The Boeing Company Lockheed Martin Corporation Sargen

Which aircraft AD 74-17-01 applies to

MakesSargent Industries, Pico Division

Inflatable Slide Regulator installed across Boeing 707-100/-100B/-200/-300 series, Douglas DC-9-81/82/83/87 (MD-80 family), and Lockheed 188A/188C Electra airframes per teaser — applicability read from the AD teaser — confirm exact model/serial/part installation from the records.

Whether AD 74-17-01 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 74-17-01 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.