Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-01-13 · Effective 1998-02-17 · 63 FR 1903
Document
Document number
98-714
Federal Register citation
63 FR 1903
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-01-13
Effective date
1998-02-17
FAA docket
Docket No. 97-NM-45-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 737-100, -200, -300, -400, and -500 series airplanes, that requires removing the yaw damper coupler; replacing its internal rate gyroscope with a new or overhauled unit; and performing a test to verify the integrity of the yaw damper coupler, and repair, if necessary. This amendment is prompted by an FAA determination that requiring replacement of the internal rate gyroscope will significantly increase the reliability of the yaw damper coupler system. The actions specified by this AD are intended to prevent sudden uncommanded yawing of the airplane due to potential failures within the yaw damper system, and consequent injury to passengers and crewmembers.