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FAA airworthiness directive publication

AD 99-18-15

1999-08-31 · Final rule publication · Federal Register document 99-22534

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.

Scoped source model wording

Source publication: 1999-08-31 · Document 99-22534. Independent observation edition: selected-ad-source-text-extension-3.0.0.

These are exact source model cells or numbered groups. Every original condition remains in the full clause below. A cell can remain readable while its model tokenization is UNKNOWN. Manufacturer identity remains unresolved; installation, aircraft applicability, compliance and current legal status have not been determined.

C90A

Complete literal source labels in this observation: C90A.

B200

Complete literal source labels in this observation: B200.

B300

Complete literal source labels in this observation: B300.

1900D

Complete literal source labels in this observation: 1900D.

C90A

Complete literal source labels in this observation: C90A.

B200

Complete literal source labels in this observation: B200.

B300

Complete literal source labels in this observation: B300.

1900D

Complete literal source labels in this observation: 1900D.

No source observation establishes aircraft applicability or compliance. See the complete original applicability clause and official source links below.

Original legacy operative paragraph

Source publication: 1999-08-31 · Document 99-22534. 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:

99-18-15  Raytheon Aircraft Company (All type certificates of the 
affected airplanes previously held by the Beech Aircraft 
Corporation): Amendment 39-11281; Docket No. 99-CE-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: The following Raytheon Beech airplane models and 
serial numbers, certificated in any category:

          Replacement Requirements of Paragraph (a) of this AD
------------------------------------------------------------------------
              Model                            Serial numbers
------------------------------------------------------------------------
C90A.............................  LJ-1526 through LJ-1550.
B200.............................  BB-1628 through BB-1659.
B300.............................  FL-213 through FL-237.
1900D............................  UE-346 through UE-356, UE-358, and UE-
                                    367.
------------------------------------------------------------------------


          Installation Requirements of Paragraph (b) of this AD
------------------------------------------------------------------------
              Model                            Serial numbers
------------------------------------------------------------------------
C90A.............................  All serial numbers.
B200.............................  All serial numbers.
B300.............................  All serial numbers.
1900D............................  All serial numbers.
------------------------------------------------------------------------

    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 request approval for an 
alternative method of compliance in accordance with paragraph (e) 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

This amendment becomes effective on September 27, 1999.

Publication context

Historical effective date recorded in the publication: 1999-09-27. 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.

Related sources

Explore all recorded source editions of this AD identifier · Find selected publications with this AD number. Matching numbers are discovery links; source identity, current legal status and aircraft applicability remain separate.

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