Airworthiness Directive

AD 98-10-02 Amendment 39-10513

Federal Aviation Administration · 14 CFR part 39

FR document
98-11809
Amendment
39-10513
Published
1998-05-06
Models covered
1
Last live check
Not yet re-verified
AD

98-10-02

FR doc 98-11809

AD 98-10-02Published 1998-05-06Effective 1998-06-10

Requires replacement of certain wheel tie bolts with new bolts; and placing a life limit on these wheel tie bolts.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain British Aerospace (Jetstream) Model 4101 airplanes, that requires replacement of certain wheel tie bolts with new bolts; and placing a life limit on these wheel tie bolts. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent metal fatigue failure of the wheel tie bolts, which could result in a tire burst or loss of the main wheel/tire assembly, and consequent reduced controllability of the airplane.

Applies to 1 model in our index