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Airworthiness Directive 95-22-03

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Official AD 95-22-03 · FR doc 95-26106 · 1995-10-24 · airframe

Airworthiness Directives; Beech Aircraft Corporation Models 60 and A60 Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to Beech Aircraft Corporation (Beech) Models 60 and A60 airplanes. This action requires incorporating flight manual supplement revisions into the Airplane Flight Manual (AFM) that would specify a minimum airspeed for operating the affected airplanes in icing conditions. Reports of several incidents and accidents on the affected airplanes related to flight in icing conditions prompted the proposed action. The actions specified by the proposed AD are intended to prevent loss of control of the airplane because of the airplane traveling too slowly in icing conditions.

Which aircraft AD 95-22-03 applies to

MakesBeech
Part-conditional — 60-590001-17, 60-590000-5, 60-590000-11.

Extracted text begins at the standard 'preceding applicability provision' boilerplate; the AD's actual airplane model/serial list precedes this excerpt and was not captured by extraction. Requires incorporating AFM supplement 'FLIGHT IN KNOWN ICING CONDITIONS' (Revised January 1995, P/N 60-590001-17) into AFM P/N 60-590000-5 or 60-590000-11, to prevent loss of control from flying too slowly in icing conditions; oversight by the Wichita ACO.

Whether AD 95-22-03 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 95-22-03 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.