Airworthiness Directive

AD 97-18-08 62 FR 46184 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-23065
Amendment
39-10118
Published
1997-09-02
Effective
1997-09-17
Models covered
1
Last live check
2026-10-03
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AD

97-18-08

FR doc 97-23065 · 62 FR 46184

AD 97-18-08Published 1997-09-02Effective 1997-09-17

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 a visual inspection to detect wear damage of the drag brace of the main landing gear (MLG), and replacement of any worn parts with new or serviceable parts.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain British Aerospace (Jetstream) Model 4101 airplanes. This action requires a visual inspection to detect wear damage of the drag brace of the main landing gear (MLG), and replacement of any worn parts with new or serviceable parts. This action also requires an inspection to determine whether there is movement in the spherical bearing of the lower link of the drag brace, certain measurements of the drag brace, and repetitive inspections, if necessary. This amendment is prompted by reports of loose spherical bearings in the links of the drag brace of the MLG. The actions specified in this AD are intended to prevent reduced structural integrity and potential collapse of the MLG due to loose spherical bearings and subsequent wear damage of the links of the drag brace.

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All British Aerospace Jetstream 41 directives

Applies to 1 model in our index