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Airworthiness Directives; Boeing Model 737 Series Airplanes

airworthiness · Rule · Final rule; correction. · Published 1999-12-13 · Effective 1999-06-28 · 64 FR 69392

Document

Document number
99-32193
Federal Register citation
64 FR 69392
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Boeing Model 737 Series
Publication date
1999-12-13
Effective date
1999-06-28
FAA docket
Docket No. 98-NM-383-AD

Abstract

This document corrects and clarifies information in an existing airworthiness directive (AD) that applies to all Boeing Model 737 series airplanes. That AD currently requires repetitive displacement tests of the secondary slide in the dual concentric servo valve of the power control unit (PCU) for the rudder, and replacement of the valve assembly with a modified valve assembly, if necessary. This document corrects certain PCU part and serial numbers and clarifies that PCU's with certain other serial numbers are not required to comply with the requirements of this AD. This correction is necessary to prevent failure of the secondary slide and consequent rudder hardover and reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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