← FAA Federal Register actions

Airworthiness Directives; Allison Engine Company 250-B and 250-C Series Turboshaft and Turboprop Engines

airworthiness · Rule · Final rule. · Published 1998-12-03 · Effective 1999-01-07 · 63 FR 66735

Document

Document number
98-31702
Federal Register citation
63 FR 66735
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Allison
Publication date
1998-12-03
Effective date
1999-01-07
FAA docket
Docket No. 98-ANE-23-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Allison Engine Company 250-B and 250-C series turboshaft and turboprop engines, that requires replacing existing beryllium copper main fuel control (MFC) bellows assemblies with Inconel 718 stainless steel welded MFC bellows assemblies. This amendment is prompted by reports of leaking MFC bellows assemblies resulting in an uncommanded minimum fuel flow condition, loss of engine fuel flow control and subsequent forced landing. The actions specified by this AD are intended to prevent MFC bellows assembly leakage, which can result in an uncommanded minimum fuel flow condition and subsequent loss of engine fuel flow control.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown