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Airworthiness Directive

AD 2001-12-17 66 FR 33013 Active

Federal Aviation Administration · 14 CFR part 39

Requires an inspection to confirm the installation of rivets at fuselage stations 251.

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FR document
01-15211
Published
2001-06-20
Effective
2001-07-25
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2001-12-17 · 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

2001-12-17

FR doc 01-15211 · 66 FR 33013

AD 2001-12-17Published 2001-06-20Effective 2001-07-25

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 an inspection to confirm the installation of rivets at fuselage stations 251.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Raytheon Model Hawker 800XP series airplanes, that requires an inspection to confirm the installation of rivets at fuselage stations 251.975, 262.35, 272.725, and 283.10, and installation of new rivets, if necessary. The actions specified by this AD are intended to detect and correct fatigue cracking of the fuselage skin, and consequent loss of cabin pressurization. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index