Airworthiness Directive

AD 98-21-36 63 FR 55783

Federal Aviation Administration · 14 CFR part 39

FR document
98-27760
Amendment
39-10845
Published
1998-10-19
Models covered
1
Last live check
2026-08-17
AD

98-21-36

FR doc 98-27760 · 63 FR 55783

AD 98-21-36Published 1998-10-19Effective 1998-11-23

Requires removing and replacing the cyclic control pilot's grip assembly (grip assembly) with an airworthy grip assembly.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to Robinson Helicopter Company (Robinson) Model R44 helicopters, that requires removing and replacing the cyclic control pilot's grip assembly (grip assembly) with an airworthy grip assembly. This amendment is prompted by a report of a crack in the welded corner of a grip assembly. The actions specified by this AD are intended to prevent use of a grip assembly that may crack, resulting in failure of the grip assembly and subsequent loss of control of the helicopter.

Applies to 1 model in our index