FAA airworthiness directive publication

AD 95-25-10

1995-12-22 · Final rule publication · Federal Register document 95-31151

This page records a selected historical publication. Its current legal status, applicability to an individual aircraft and compliance have not been determined. Consult the current FAA directive and aircraft configuration and maintenance records.

Literal model wording

Source publication: 1995-12-22 · Document 95-31151. Observation edition: selected-ad-source-text-extension-2.0.0.

These are exact source labels for discovery. Manufacturer identity remains unresolved. Serial numbers, installed equipment and all other conditions have not been evaluated. The complete applicability clause below retains all conditions and notes.

441, 500, 550, 560

441, 500, 550, and 560

The source says “series”; the label has not been expanded to other models.

Source opening:

    Applicability:

These observations do not determine aircraft applicability, compliance, installed configuration or current legal status.

Original legacy operative paragraph

Source publication: 1995-12-22 · Document 95-31151. Independent observation edition: selected-ad-source-text-extension-3.0.0.

This paragraph is newly retained from the same immutable official publication. It is a legacy §39.13 amendment and the publication’s own AD header, not a newly invented Affected ADs heading. The earlier observation edition remains unchanged.

    2. Section 39.13 is amended by adding the following new 
airworthiness directive:

95-25-10 Cessna Aircraft Company: Amendment 39-9456. Docket 95-NM-
56-AD.

UNKNOWN historical relationship: adding a new entry does not establish that no earlier directives are affected. No explicit historical replacement statement was established in this bounded operative paragraph.

Applicability text in this publication

    Applicability: Model 441, 500, 550, and 560 series airplanes; 
equipped with Allied Signal outflow/safety valves; as identified in 
Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-
4056, and 103648-21-4055, all dated January 30, 1995; certificated 
in any category. 

[[Page 66485]]

    Note 1: This AD applies to each airplane identified in the 
preceding applicability provision, regardless of whether it has been 
modified, altered, or repaired in the area subject to the 
requirements of this AD. For airplanes that have been modified, 
altered, or repaired so that the performance of the requirements of 
this AD is affected, the owner/operator must use the authority 
provided in paragraph (c) of this AD to request approval from the 
FAA. This approval may address either no action, if the current 
configuration eliminates the unsafe condition; or different actions 
necessary to address the unsafe condition described in this AD. Such 
a request should include an assessment of the effect of the changed 
configuration on the unsafe condition addressed by this AD. In no 
case does the presence of any modification, alteration, or repair 
remove any airplane from the applicability of this AD.

Effective-date text

This amendment becomes effective on January 22, 1996.

Publication context

Historical effective date recorded in the publication: 1996-01-22. This date does not establish which directive controls today.

A relationship to prior directives has not been established from this publication.

Official sources

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Sources retrieved: HTML 2026-09-08; PDF 2026-09-08.

The displayed text comes from the HTML publication. Refer to the official documents for the original wording.

This selected source edition is not a complete list of current airworthiness directives. Referenced manufacturer service documents are not reproduced here.