Airworthiness Directive 59-20-01

one-time
AD 59-20-01 · 1959-01-01 · airframe

Airworthiness Directives; VERTOL Model 44 Series Helicopters

Which aircraft AD 59-20-01 applies to

MakesVertol
Models44
Part-conditional42R1009-1.

Applies to all Model 44 Series Helicopters. Rotor blade assembly P/N 42R1009-1 in all-metal forward rotor blades to be inspected within the next twenty hours of flight in accordance with Vertol Engineering Order No. 7A (Drawing No. 42R1011).

Whether AD 59-20-01 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 59-20-01 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.