Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1999-11-30 · Effective 1999-12-15 · 64 FR 66765
Document
Document number
99-30946
Federal Register citation
64 FR 66765
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1999-11-30
Effective date
1999-12-15
FAA docket
Docket No. 99-NM-332-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to all Boeing Model 737-100, -200, -300, -400, and -500 series airplanes. This action requires a one-time inspection to verify correct installation of the fastener that connects the input rod of the spoiler mixer mechanism to the torque tube crank, and corrective actions, if necessary. For certain airplanes, this action requires replacement of the nut, bolt, and cotter pin that connects the input rod of the spoiler mixer mechanism to the torque tube crank with a new or serviceable nut, bolt, and cotter pin. This amendment is prompted by reports indicating numerous discrepancies in the installation of the fastener that connects the input rod of the spoiler mixer mechanism to the torque tube crank. The actions specified in this AD are intended to prevent the linkage between the ratio changer input rod and the aft aileron control quadrant from becoming disconnected, which could result in reduced controllability of the airplane.