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Airworthiness Directives; Learjet Model 23, 24, 25, 28, 29, 31, 55, and 60 Series Airplanes

airworthiness · Rule · Final rule. · Published 1999-08-02 · Effective 1999-09-07 · 64 FR 41778

Document

Document number
99-19297
Federal Register citation
64 FR 41778
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-08-02
Effective date
1999-09-07
FAA docket
Docket No. 98-NM-372-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Learjet Model 23, 24, 25, 28, 29, 31, 55, and 60 series airplanes, that requires a one-time detailed visual inspection of the electrical wire leads of the horizontal stabilizer anti-ice system to verify that the numbers on the wire leads correctly correspond to the numbers on the connected airframe wiring; installation of a wire ID strap on the left-and right-hand sides of each terminal block; and installation of a warning placard. This amendment is prompted by a report of severe flight control buffeting of a Learjet Model 55 series airplane due to a malfunction of the horizontal stabilizer anti-ice system. The actions specified by this AD are intended to prevent undetected accretion of ice on the leading edge of the horizontal stabilizer, which could result in the loss of pitch control and consequent reduced controllability of the airplane.

Source

Authoritative
Federal Register document
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