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Airworthiness Directive

AD 98-13-11 63 FR 34563 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-16166
Amendment
39-10599
Published
1998-06-25
Effective
1998-08-03
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/98-13-11 · 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

98-13-11

FR doc 98-16166 · 63 FR 34563

AD 98-13-11Published 1998-06-25Effective 1998-08-03

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 modifying the airplane by incorporating Raytheon Kit No.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Model 1900D airplanes. This action requires modifying the airplane by incorporating Raytheon Kit No. 129-5200-1, ``Ground Fine Switch Installation Kit''. This action is the result of design analysis during certification of 5.5 degree approach landings of the Model 1900D airplanes. The actions specified by this AD are intended to prevent a loose or misrigged ground fine switch, which could result in very hard landings causing structural damage to the airplane and possible passenger injury.

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All Beechcraft 1900 directives

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Applies to 1 model in our index