Airworthiness Directive 93-24-09

one-time
AD 93-24-09 · 1993-01-01 · airframe

Airworthiness Directives; the effective date of this AD, accomplish paragraphs (b)(1) and (b)(2) of this AD. (1) Replace the currently-installed Cutler Hamm

Which aircraft AD 93-24-09 applies to

MakesBritish Aerospace
Part-conditionalSM15-CK-A6, SM15-CK-A8, HA1F.

Replaces Cutler Hammer contactor type SM15-CK-A6/A8 with Leach contactor type HA1F per British Aerospace service documentation (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 93-24-09 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 93-24-09 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.

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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.