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Airworthiness Directive

AD 96-13-10 61 FR 33646 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-15956
Amendment
39-9678
Published
1996-06-28
Effective
1996-08-02
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/96-13-10 · 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

96-13-10

FR doc 96-15956 · 61 FR 33646

AD 96-13-10Published 1996-06-28Effective 1996-08-02

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 modification of the existing diaphragms on the surround structure of the Type II emergency exit.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Jetstream Model 4101 airplanes, that requires modification of the existing diaphragms on the surround structure of the Type II emergency exit. This amendment is prompted by a report indicating that, during fatigue tests on a Model 4101 test article, fatigue-related cracking was found in the surround structure of a Type II emergency exit. The actions specified by this AD are intended to prevent such cracking in the surround structure, which could result in reduced structural integrity of the fuselage pressure vessel.

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All British Aerospace Jetstream 41 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index