Is AD 95-02-17 a recurring Airworthiness Directive?

No — AD 95-02-17 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 95-02-17 apply to?

AD 95-02-17 applies to Beech — models 1900D, 1900. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 95-02-17

one-time

Official AD 95-02-17 · FR doc 95-7784 · 1995-03-30 · airframe

Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes

What this AD requires

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-02-17, which was sent previously to known U.S. owners and operators of certain Beech Aircraft Corporation Model 1900D airplanes. This AD requires inspecting (one- time) the elevator trim tab control cables at the top of the vertical stabilizer to ensure that cables (at the left, right, and crossover pulleys) are correctly routed around the pulleys, within the cable guide pins, and are not contacting any structure; and replacing any cable that is incorrectly routed or chafed. The actions specified by this AD are intended to prevent in-flight separation of the elevator trim tab control cable caused by misrouting, which could result in loss of control of the airplane.

Which aircraft AD 95-02-17 applies to

MakesBeech

Models1900D, 1900

Applies to Model 1900D airplanes; inspect/correct elevator trim tab control cable routing per Beech 1900D Maintenance Manual P/N 129-590000-15A11 (Chapters 5-20-07, 6-40-00, 6-50-00, 27-30-04). Compliance with Beech Communique 1900D-112, dated January 1995, is considered equivalent.

Whether AD 95-02-17 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 95-02-17 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.