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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

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T01:35:15.465684+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
4e68ec47f8468616021732633a1768ff5a96c6e9ad314cf8c25a5b88a039d554
Text SHA-256
8fb7539768e69c2688bc3090a925f6471e972c93fe8ab498e0f2799b956f2a8f

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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.