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Airworthiness Directive

AD 2003-13-16 68 FR 40484 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-16691
Amendment
39-13218
Published
2003-07-08
Effective
2003-08-25
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2003-13-16 · 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

2003-13-16

FR doc 03-16691 · 68 FR 40484

AD 2003-13-16Published 2003-07-08Effective 2003-08-25

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 you to inspect the forward side of the aft pressure bulkhead for scoring damage and repair, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) 90, 100, and 200 series airplanes. This AD requires you to inspect the forward side of the aft pressure bulkhead for scoring damage and repair, if necessary. This AD is the result of reports of the aft pressure bulkhead being damaged by scoring during manufacture. The actions specified by this AD are intended to detect and correct damage to the aft pressure bulkhead of the fuselage. Such damage could lead to fatigue failure of the bulkhead.

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All Beechcraft King Air 200 (Super King Air) 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