Published 2023-06-02 · Federal Register document 2023-11705
Airworthiness Directives; Airbus SAS Airplanes
Publication summary
The FAA is removing Airworthiness Directive (AD) 92-02-14, which applied to certain Airbus SAS Model A320 series airplanes. AD 92- 02-14 required inspection for correct installation of the flexible control cables on the overwing emergency escape slides. The FAA issued AD 92-02-14 to prevent failure of the overwing emergency escape slides to deploy, which would compromise use of the exit during an emergency. Since the FAA issued AD 92-02-14, no new occurrences of incorrect cable installations have been reported, and existing maintenance activities are adequate to prevent new occurrences. Therefore, the FAA has determined that AD 92-02-14 is no longer necessary. Accordingly, AD 92- 02-14 is removed.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[149]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 92-02-14 R1
- Effective date printed in this edition
- 2023-06-02
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 7 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective June 2, 2023.
Exact source excerpt. Text positions 7118–7178, end exclusive, in the original decoded publication. SHA-256: 37ac87bb7010f2c47446cfef4f9b3375746970dcf2a1fc8b971917f3d7e481b7
Affected AD
(b) Affected AD
This AD replaces AD 92-02-14, Amendment 39-8150 (57 FR 5375,
February 14, 1992).
Exact source excerpt. Text positions 7178–7282, end exclusive, in the original decoded publication. SHA-256: f2147859037180694452aef5489ee921feaf23c88a5d86fee1146687ee0ce0ef
Applicability wording · Applicability
(c) Applicability
This action applies to Airbus Model A320-211, A320-212, and
A320-231 airplanes, certificated in any category, manufacturer
serial numbers 002 through 162 inclusive, 167, and 171 through 174
inclusive.
Exact source excerpt. Text positions 7282–7510, end exclusive, in the original decoded publication. SHA-256: b7768e9875b39487c7bb1a776f1df0d94ed57773283779e5f4000e361c9b1213
Subject
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.
Exact source excerpt. Text positions 7510–7604, end exclusive, in the original decoded publication. SHA-256: 1ffe24c6c793b9c0f0b362fce1932ad96c9dea87b917be982738f710e408a2e2
Terminating Action
(e) Terminating Action
This AD terminates all requirements of AD 92-02-14.
Exact source excerpt. Text positions 7604–7685, end exclusive, in the original decoded publication. SHA-256: a343285572e279ceefe8e2f951c5cf455301eec98b57971880bdc00ab11ddb52
Related Information
(f) Related Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, International Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; phone 206-231-3225; email
[email protected].
Exact source excerpt. Text positions 7685–7921, end exclusive, in the original decoded publication. SHA-256: 0bed9f37dbc9622a55077f99a40feb47b45c3f949318e8254772124f741fe28f
Material Incorporated by Reference
(g) Material Incorporated by Reference
None.
Exact source excerpt. Text positions 7921–7972, end exclusive, in the original decoded publication. SHA-256: c63e3dd6b9018c0d40d46d29727ed8dc72a42f9b6057adcf7d0813df4529c21a
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 92-02-14 R1 · 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: 8fb7539768e69c2688bc3090a925f6471e972c93fe8ab498e0f2799b956f2a8f. Source manifest: d5ee39636ee437c9e871f17d204a2bc1017ba122b5345388dde4ab4ddda32171.
Official source · 2023-06-02
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 88, Number 106 (Friday, June 2, 2023)]
[Rules and Regulations]
[Pages 36236-36237]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-11705]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0434; Product Identifier 91-NM-255-AD; Amendment
39-22450; AD 92-02-14 R1]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; removal.
-----------------------------------------------------------------------
SUMMARY: The FAA is removing Airworthiness Directive (AD) 92-02-14,
which applied to certain Airbus SAS Model A320 series airplanes. AD 92-
02-14 required inspection for correct installation of the flexible
control cables on the overwing emergency escape slides. The FAA issued
AD 92-02-14 to prevent failure of the overwing emergency escape slides
to deploy, which would compromise use of the exit during an emergency.
Since the FAA issued AD 92-02-14, no new occurrences of incorrect cable
installations have been reported, and existing maintenance activities
are adequate to prevent new occurrences. Therefore, the FAA has
determined that AD 92-02-14 is no longer necessary. Accordingly, AD 92-
02-14 is removed.
DATES: This AD becomes effective June 2, 2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-0434; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Validation Branch, FAA, 2200 South 216th St., Des Moines,
WA 98198; phone 206-231-3225; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by removing AD 92-02-14, Amendment 39-8150 (57 FR 5375,
February 14, 1992) (AD 92-02-14). AD 92-02-14 applied to certain Airbus
SAS Model A320 series airplanes. The NPRM was published in the Federal
Register on March 24, 2023 (88 FR 17751). The NPRM was prompted by the
determination that AD 92-02-14 is no longer necessary. AD 92-02-14
required inspection for correct installation of the flexible control
cables on the overwing emergency escape slides. The FAA issued AD 92-
02-14 to prevent failure of the overwing emergency escape slides to
deploy, which would compromise use of the exit during an emergency.
Since the FAA issued AD 92-02-14, no new occurrences of incorrect cable
installations have been reported, and existing maintenance activities
are adequate to prevent new occurrences. The NPRM proposed to remove AD
92-02-14. The FAA is issuing this AD to remove AD 92-02-14.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from The Air Line Pilots Association,
International (ALPA), in support of the NPRM without change.
[[Page 36237]]
Justification for Determination of the Effective Date
Section 553(d) of the Administrative Procedure Act (APA) (5 U.S.C.
551 et seq.) authorizes agencies to make rules effective in less than
thirty days, upon a finding of ``good cause.'' Since the FAA issued AD
92-02-14, no new occurrences of incorrect cable installations have been
reported, and existing maintenance activities are adequate to prevent
new occurrences. Therefore, the FAA is issuing this AD to remove AD 92-
02-14, and the FAA did not receive any adverse comments or useful
information about this AD from U.S. operators that necessitates waiting
30 days for relief from this requirement. Accordingly, the FAA finds
that good cause exists pursuant to 5 U.S.C. 553(d) for making this
amendment effective in less than 30 days.
Conclusion
The FAA reviewed the relevant data, considered the comment
received, and determined that air safety requires adopting this AD as
proposed. Except for minor editorial changes, this AD is adopted as
proposed in the NPRM. None of the changes will increase the economic
burden on any operator.
This AD removes all actions of AD 92-02-14. Therefore, the
requirements of AD 92-02-14 are terminated.
Related Costs of Compliance
This AD adds no costs. This AD removes AD 92-02-14 from 14 CFR part
39; therefore, operators are no longer required to show compliance with
that AD.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority.
Regulatory Findings
The FAA determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by:
0
a. Removing Airworthiness Directive (AD) 92-02-14, Amendment 39-8150
(57 FR 5375, February 14, 1992), and
0
b. Adding the following new AD:
92-02-14 R1 Airbus SAS: Amendment 39-22450; Docket No. FAA-2023-
0434; Product Identifier 92-NM-155-AD.
(a) Effective Date
This AD is effective June 2, 2023.
(b) Affected AD
This AD replaces AD 92-02-14, Amendment 39-8150 (57 FR 5375,
February 14, 1992).
(c) Applicability
This action applies to Airbus Model A320-211, A320-212, and
A320-231 airplanes, certificated in any category, manufacturer
serial numbers 002 through 162 inclusive, 167, and 171 through 174
inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.
(e) Terminating Action
This AD terminates all requirements of AD 92-02-14.
(f) Related Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, International Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; phone 206-231-3225; email
[email protected].
(g) Material Incorporated by Reference
None.
Issued on May 26, 2023.
Ross Landes,
Deputy Director for Regulatory Operations, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023-11705 Filed 6-1-23; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
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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.