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Airworthiness Directive

AD 2015-26-08 81 FR 145 Active

Federal Aviation Administration · 14 CFR part 39

Requires an inspection and, if necessary, modification of the emergency gear extension cable.

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FR document
2015-32907
Amendment
39-18356
Published
2016-01-05
Effective
2016-01-20
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2015-26-08 · 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

2015-26-08

FR doc 2015-32907 · 81 FR 145

AD 2015-26-08Published 2016-01-05Effective 2016-01-20

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 and, if necessary, modification of the emergency gear extension cable.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Model PA-44-180 and PA-44-180T airplanes. This AD requires an inspection and, if necessary, modification of the emergency gear extension cable. This AD was prompted by a report of a misrouted emergency gear extension cable. We are issuing this AD to correct the unsafe condition on these products.

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All Piper PA-44 Seminole directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index