Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-05-02 · Effective 1997-06-06 · 62 FR 24008
Document
Document number
97-11200
Federal Register citation
62 FR 24008
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1997-05-02
Effective date
1997-06-06
FAA docket
Docket No. 96-NM-150-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 an inspection of reworked aileron/ elevator power control units (PCU's) and rudder PCU's to determine if reworked PCU manifold cylinder bores containing chrome plating are installed, and replacement of the cylinder bores with bores that have been reworked using the oversize method or the steel sleeve method, if necessary. This amendment is prompted by a review of the design of the flight control systems on Model 737 series airplanes. The actions specified by this AD are intended to prevent a reduced rate of movement of the elevator, aileron, or rudder due to contamination of hydraulic fluid from chrome plating chips; such reduced rate of movement, if not corrected, could result in reduced controllability of the airplane.