Back to publication catalog

Published 1996-12-10 · Federal Register document 96-31264

Airworthiness Directives; Aerospace Technologies of Australia Pty Ltd. (Formerly Government Aircraft Factory) Models N22B, N24A, and N22S Airplanes; Correction

Publication summary

This action makes a correction to an airworthiness directive (AD) that was published in the Federal Register on November 12, 1996 (61 FR 57993), and concerns Aerospace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N24A, and N22S airplanes. The AD number for that action should be AD 96-23-18, but was referenced as AD 96-23-03. The AD currently requires replacing the existing fuselage stub fin plate with one of improved design. This action corrects the AD to reflect the correct AD number.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:47.711690+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_1996-de90a15e77992e3a
Source row
results[116]
Raw source SHA-256
de90a15e77992e3af396b1c6f02ea423ac0c6519413e915acf4d797175e81157

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
96-23-18
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 96-23-18 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: a1c41244014b75513669d89991ff753247dde8f25ec3e92516d629c88658e460. Source manifest: 906de173931a2bd8aaa6bce1ed2af3db657a89afc1d889745cbb8a7e3e911d63.

Official source · 1996-12-10

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 61, Number 238 (Tuesday, December 10, 1996)]
[Rules and Regulations]
[Page 64985]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-31264]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 95-CE-103-AD; Amendment 39-9808; AD 96-23-18]
RIN 2120-AA64


Airworthiness Directives; Aerospace Technologies of Australia Pty 
Ltd. (Formerly Government Aircraft Factory) Models N22B, N24A, and N22S 
Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This action makes a correction to an airworthiness directive 
(AD) that was published in the Federal Register on November 12, 1996 
(61 FR 57993), and concerns Aerospace Technologies of Australia Pty 
Ltd. (ASTA) Models N22B, N24A, and N22S airplanes. The AD number for 
that action should be AD 96-23-18, but was referenced as AD 96-23-03. 
The AD currently requires replacing the existing fuselage stub fin 
plate with one of improved design. This action corrects the AD to 
reflect the correct AD number.

EFFECTIVE DATE: December 23, 1996.

FOR FURTHER INFORMATION CONTACT: Mr. Ron Atmur, Aerospace Engineer, 
FAA, Los Angeles Aircraft Certification Office, 3960 Paramount 
Boulevard., Lakewood, California 90712; telephone (310) 627-5224; 
facsimile (310) 627-5210.

SUPPLEMENTARY INFORMATION: On October 28, 1996, the FAA issued an 
airworthiness directive (AD), Amendment 39-9808 (61 FR 57993, November 
12, 1996), to require replacing the existing fuselage stub fin plate 
with one of improved design on ASTA Models N22B, N24A, and N22S 
airplanes.

Need for the Correction

    The AD number for that action should be AD 96-23-18, but was 
referenced as AD 96-23-03. As written, operators of the ASTA Models 
N22B, N24A, and N22S airplanes would be referencing the wrong AD in 
their logbook, thus creating confusion as to whether the operator had 
complied with the AD.
    Action is taken herein to correct this reference in Amendment 39-
9808 and to add this AD correction to Sec. 39.13 of the Federal 
Aviation Regulations (14 CFR 39.13).
    The effective date remains December 23, 1996.

Correction of Publication

    Accordingly, the publication of November 12, 1996 (61 FR 57993), of 
Amendment 39-9808; AD 96-23-03, which was the subject of FR Doc. 96-
28164, is corrected as follows:
    On page 57993, in the first column, in the fifth line of the 
heading of the document, replace AD 96-23-03 with AD 96-23-18.


Sec. 39.13  [Corrected]

    On page 57994, in the first column, Sec. 39.13, the first line of 
the AD, replace 96-23-03 with 96-23-18.

    Issued in Kansas City, Missouri on December 2, 1996.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 96-31264 Filed 12-9-96; 8:45 am]
BILLING CODE 4910-13-U


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T05:13:29.809696+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
f746496fa1040779523edff8968b8dfd7c19a9c3c6651d427a4a81396884d5f5
Text SHA-256
a1c41244014b75513669d89991ff753247dde8f25ec3e92516d629c88658e460

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.