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Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-09-22 · Effective 1998-10-27 · 63 FR 50492

Document

Document number
98-25028
Federal Register citation
63 FR 50492
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-09-22
Effective date
1998-10-27
FAA docket
Docket No. 98-NM-61-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319, A320, and A321 series airplanes, that requires relocation of the engine/master 1 relay from relay box 103VU to shelf 95VU in the avionics bay. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent a simultaneous cutoff of the fuel supply to both engines, which could result in a loss of engine power and consequent reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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