Airworthiness Directive

AD 97-23-05 62 FR 60161 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacing the attachment bolt between the pitch control cables and control column lever with a bolt of improved design.

FR document
97-29232
Amendment
39-10193
Published
1997-11-07
Effective
1997-12-01
Models covered
1

Last live check: 2026-08-19

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AD

97-23-05

FR doc 97-29232 · 62 FR 60161

AD 97-23-05Published 1997-11-07Effective 1997-12-01

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires replacing the attachment bolt between the pitch control cables and control column lever with a bolt of improved design.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin Model R3000 airplanes. This AD requires replacing the attachment bolt between the pitch control cables and control column lever with a bolt of improved design. This AD is the result of mandatory continued airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to prevent the pitch control cables on the control column from becoming jammed due to failure of the attachment bolt, which could result in a reduction in the directional controllability of the airplane.

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All Avions Pierre Robin directives

Applies to 1 model in our index