Airworthiness Directive

AD 96-23-12 61 FR 58981 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-29261
Amendment
39-9817
Published
1996-11-20
Effective
1996-12-05
Models covered
1
Last live check
2026-10-03
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AD

96-23-12

FR doc 96-29261 · 61 FR 58981

AD 96-23-12Published 1996-11-20Effective 1996-12-05

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 one-time check of the left and right main landing gear leg assemblies to determine whether certain assemblies have been installed; and the replacement of certain discrepant retaining bolts on these assemblies with…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Jetstream Model 4101 airplanes. This action requires a one-time check of the left and right main landing gear leg assemblies to determine whether certain assemblies have been installed; and the replacement of certain discrepant retaining bolts on these assemblies with correctly manufactured bolts. This amendment is prompted by a report indicating that some of these retaining bolts have failed during the assembly and installation of a main landing gear unit, due to an incorrect process that was used during the manufacture of the bolts. The actions specified in this AD are intended to prevent structural damage to the main landing gear due to failure of the retaining bolts which, if not corrected, could result in reduced controllability of the airplane during takeoff, landing, and taxiing.

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Applies to 1 model in our index