Airworthiness Directive

AD 97-06-05 62 FR 11763 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-6256
Amendment
39-9962
Published
1997-03-13
Effective
1997-05-16
Models covered
1
Last live check
2026-09-30
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AD

97-06-05

FR doc 97-6256 · 62 FR 11763

AD 97-06-05Published 1997-03-13Effective 1997-05-16

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 repetitively inspecting the weld area between the strut and the lower plate of the nose landing gear leg for cracks, and replacing the strut when cracks are found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Avions Pierre Robin Model R2160 airplanes. This action requires repetitively inspecting the weld area between the strut and the lower plate of the nose landing gear leg for cracks, and replacing the strut when cracks are found. The AD is the result of several reports of cracks in the weld securing the nose wheel steering bottom bracket to the nose landing gear leg on the affected airplanes. The actions specified by this AD are intended to prevent nose landing gear failure caused by cracks in the weld area between the strut and the lower plate of the nose landing gear leg, which could result in loss of control of the airplane during landing operations.

More directives for Avions Pierre Robin

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  2. AD 2014-26-01 Airworthiness Directives; Alpha Aviation Concept Limited Airplanes 2014-12-24
  3. AD 2014-18-03 Airworthiness Directives; APEX Aircraft Airplanes 2014-09-12
  4. AD 2014-09-12 Airworthiness Directives; Alpha Aviation Concept Limited Airplanes 2014-05-09
  5. AD 2012-20-02 Airworthiness Directives; Alpha Aviation Concept Limited Airplanes 2012-10-05

All Avions Pierre Robin directives

Applies to 1 model in our index