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Airworthiness Directive

AD 96-17-10 61 FR 42996 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-21008
Amendment
39-9719
Published
1996-08-20
Effective
1996-09-24
Models covered
2
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/96-17-10 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

96-17-10

FR doc 96-21008 · 61 FR 42996

AD 96-17-10Published 1996-08-20Effective 1996-09-24

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 replacement of outflow/safety valves with serviceable valves.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Beech Model 400, 400A, MU-300-10, and 2000 airplanes, and Model 200, B200, 300, and B300 series airplanes, that requires replacement of outflow/safety valves with serviceable valves. This amendment is prompted by a report of cracking and subsequent failure of outflow safety valves in the pressurization system. The actions specified by this AD are intended to prevent such cracking and subsequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.

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All Beechcraft King Air 200 (Super King Air) directives

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Applies to 2 models in our index