Airworthiness Directive

AD 97-03-08 62 FR 5145 Active

Federal Aviation Administration · 14 CFR part 39

FR document
97-2609
Amendment
39-9914
Published
1997-02-04
Effective
1997-03-11
Models covered
1
Last live check
2026-10-03
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AD

97-03-08

FR doc 97-2609 · 62 FR 5145

AD 97-03-08Published 1997-02-04Effective 1997-03-11

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 repetitive inspections to detect cracking of the offset lightening hole on the drag brace of the left and right main landing gear (MLG); and replacement of these braces with braces having a centralized lightening hole.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Jetstream Model 4101 airplanes, that requires repetitive inspections to detect cracking of the offset lightening hole on the drag brace of the left and right main landing gear (MLG); and replacement of these braces with braces having a centralized lightening hole. This replacement terminates the repetitive inspections This amendment is prompted by a report indicating that fatigue cracking was detected on the upper link of a drag brace. The actions specified by this AD are intended to prevent fatigue cracking of the drag braces of the MLG, which, if not corrected, could cause the MLG to fail and, consequently, result in reduced controllability of the airplane during takeoff, landing, and taxiing.

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Applies to 1 model in our index