Airworthiness Directive

AD 96-22-12 61 FR 55734 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting (one- time) the fuel filter assemblies to detect any bypass valve that is glued shut.

FR document
96-27756
Amendment
39-9800
Published
1996-10-29
Effective
1996-12-13
Models covered
1

Last live check: 2026-10-04

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AD

96-22-12

FR doc 96-27756 · 61 FR 55734

AD 96-22-12Published 1996-10-29Effective 1996-12-13

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires inspecting (one- time) the fuel filter assemblies to detect any bypass valve that is glued shut.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Corporation (Raytheon) Models 1900C, 1900D, and 2000 airplanes. This action requires inspecting (one- time) the fuel filter assemblies to detect any bypass valve that is glued shut. If a bypass valve is glued shut, the AD requires replacing the associated fuel filter assembly. Three in-flight occurrences in which the low fuel pressure light illuminated prompted this action. In each of the instances, a bypass valve on the affected airplane engine was glued shut with anaerobic thread lock adhesive and when the fuel filter became clogged, proper fuel flow to the engine was not obtained. The actions specified by this AD are intended to prevent lack of fuel to the engine and eventual engine shutdown caused by a clogged fuel filter and a contaminated fuel filter bypass valve.

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All Beechcraft 1900 directives

Applies to 1 model in our index