Airworthiness Directives; Saab Model SAAB SF340A and SAAB 340B Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-07-16 · Effective 1998-08-20 · 63 FR 38284
Document
Document number
98-18774
Federal Register citation
63 FR 38284
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Saab Model SAAB SF340A and SAAB 340B Series
Publication date
1998-07-16
Effective date
1998-08-20
FAA docket
Docket No. 98-NM-117-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Saab Model SAAB SF340A and SAAB 340B series airplanes, that requires modification of the detachable center inlet component of the air intake system of the engine. 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 fuel and/or oil that may be present in the nacelle from entering the air intake system of the engine, which could result in a possible engine fire.