FAA airworthiness directive publication
AD 98-24-14
1998-12-02 · Final rule publication · Federal Register document 98-32045
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: 1998-12-02 · Document 98-32045. 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.
Original model and serial-number table
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Model Serial numbers
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340A................................. 215 through 1817.
414A................................. 1 through 1212.
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Rows and serial-number conditions are reproduced as written; they are not an aircraft configuration or applicability determination.
340A
414A
These observations do not determine aircraft applicability, compliance, installed configuration or current legal status.
Original legacy operative paragraph
Source publication: 1998-12-02 · Document 98-32045. 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 a new airworthiness directive (AD) to read as follows: 98-24-14 Cessna Aircraft Company: Amendment 39-10923; Docket No. 98-CE-111-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: The following airplane models and serial numbers,
certificated in any category, that are equipped with any WYE tube,
part number (P/N) 9910299-25 or P/N 9910299-26, in the engine
exhaust system:
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Model Serial numbers
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340A................................. 215 through 1817.
414A................................. 1 through 1212.
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Note 1: This AD allows the aircraft owner or pilot to check the
maintenance records to determine whether any WYE tube, P/N 9910299-
25 or P/N 9910299-26, has been installed in the engine exhaust
system between May 8, 1998, and December 21, 1998 (the effective
date of this AD). See paragraph (c) of this AD for authorization.
Note 2: Cessna is considering issuing service information
pertaining to this subject. This AD takes precedence over any
existing or future service information on this subject.
Note 3: 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 request approval for an
alternative method of compliance in accordance with paragraph (d) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Effective-date text
An effective-date observation was not extracted from this publication.
Publication context
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.