Airworthiness Directive 2003-01-01

one-time
Official AD 2003-01-01 · FR doc 03-1674 · 2003-01-27 · airframe

Airworthiness Directives; Raytheon Aircraft Company Beech Models 36, A36, A36TC, B36TC, 58, and 58A Airplanes

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2003-01-01, which was published in the Federal Register on January 8, 2003 (68 FR 997), and applies to certain Raytheon Aircraft Company (Raytheon) Beech Models 36, A36, A36TC, B36TC, 58, and 58A airplanes. We inadvertently omitted certain regulatory text to remove AD 2000-26- 16, Amendment 39-12066, from 14 CFR part 39. This action corrects the regulatory text.

Which aircraft AD 2003-01-01 applies to

MakesRaytheon
Models58, 58A, A36, A36TC, B36TC

certain

Whether AD 2003-01-01 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 2003-01-01 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 →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.