Is AD 2003-01-01 a recurring Airworthiness Directive?

No — AD 2003-01-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2003-01-01 apply to?

AD 2003-01-01 applies to Raytheon Aircraft Company. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2003-01-01

one-time

Official AD 2003-01-01 · FR doc 03-148 · 2003-01-08 · airframe

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

What this AD requires

This amendment supersedes Airworthiness Directive (AD) 2000- 26-16, which applies to certain Raytheon Aircraft Company (Raytheon) Beech Models A36, B36TC, and 58 airplanes. AD 2000-26-16 requires you to inspect for missing rivets on the right hand side of the fuselage and, if necessary, install rivets. AD 2000-26-16 resulted from Raytheon identifying several instances of missing rivets on these airplanes. AD 2000-26-16 incorporated an incorrect listing of serial numbers for the affected model airplanes and omitted certain airplane models from the applicability section of AD 2000-26-16. This AD retains the actions required in AD 2000-26-16 and corrects the applicability section. The actions specified by this AD are intended to detect and correct missing rivets in the right hand fuselage panel assembly in the area above the right wing and below the cabin door threshold. These rivets must be present for the fuselage to carry the ultimate load and prevent critical structural failure with loss of airplane control.

Which aircraft AD 2003-01-01 applies to

MakesRaytheon Aircraft Company

Specific model/serial applicability is in paragraph (a), not captured in the extracted text; action per Raytheon Mandatory SB 53-3341 Rev. 1 (May 2000) or Rev. 2 (October 2002); supersedes AD 2000-26-16, Amendment 39-12066.

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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The 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.