Airworthiness Directive

AD 99-05-13 64 FR 10560

Federal Aviation Administration · 14 CFR part 39

FR document
99-5148
Amendment
39-11061
Published
1999-03-05
Effective
1999-04-19
Status
Withdrawn by the FAA
Last live check
2026-09-30
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.
AD

99-05-13

FR doc 99-5148 · 64 FR 10560

AD 99-05-13Published 1999-03-05Effective 1999-04-19

Rescinded

Rescinded Rescinded or withdrawn. This directive was rescinded or withdrawn by the FAA (see the Federal Register document below). It is no longer in force and nothing on this page is an applicable requirement. See the official FAA record (opens in a new tab).

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 series airplanes. This AD requires installing a placard on the fuel tank selector to warn of the no-flow condition that exists between the fuel tank detents. This AD is the result of reports of engine stoppage on the affected airplanes where the cause was considered to be incorrect positioning of the fuel selector. The actions specified by this AD are intended to help prevent a lack of fuel flow to the engine caused by incorrect positioning of the fuel selector, which could result in loss of engine power.

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