[Federal Register Volume 87, Number 77 (Thursday, April 21, 2022)]
[Rules and Regulations]
[Pages 23755-23757]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-08494]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0091; Project Identifier MCAI-2021-01123-T; 
Amendment 39-22011; AD 2022-08-08]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -
113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, 
-214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -
131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted 
by reports that, during inspections accomplished as specified in 
certain airworthiness limitation items (ALIs), cracks were detected in 
the double joggle areas at frame (FR) 16 and FR20 in the nose forward 
fuselage. This AD requires repetitive special detailed inspections of 
certain areas and applicable on-condition actions, as specified in a 
European Union Aviation Safety Agency (EASA) AD, which is incorporated 
by reference. The FAA is issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective May 26, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of May 26, 
2022.

ADDRESSES: For EASA material incorporated by reference (IBR) in this 
AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
telephone +49 221 8999 000; email [email protected]; internet 
www.easa.europa.eu. You may find this IBR material on the EASA website 
at https://ad.easa.europa.eu. You may view this material at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 South 
216th St., Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195. It is also available in the AD 
docket at https://www.regulations.gov by searching for and locating 
Docket No. FAA-2022-0091.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2022-0091; 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, the 
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: Vladimir Ulyanov, Aerospace Engineer, 
Large Aircraft Section, FAA, International Validation Branch, 2200 
South 216th St., Des Moines, WA 98198; phone 206-231-3229; email 
[email protected].

SUPPLEMENTARY INFORMATION:

Background

    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2021-0227, dated October 11, 2021 
(EASA AD 2021-0227) (also referred to as the MCAI), to correct an 
unsafe condition for certain Airbus SAS Model A318 series airplanes; 
Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; 
Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and 
Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR

[[Page 23756]]

part 39 by adding an AD that would apply to certain Airbus SAS Model 
A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -
132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, 
and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -
231, and -232 airplanes. The NPRM published in the Federal Register on 
February 8, 2022 (87 FR 7062). The NPRM was prompted by reports that 
during inspections accomplished in accordance with certain ALIs, cracks 
were detected in double joggle areas at FR16 and FR20, right hand and 
left hand sides. The NPRM proposed to require repetitive special 
detailed inspections of certain areas and applicable on-condition 
actions, as specified in EASA AD 2021-0227. The NPRM also proposed an 
optional modification of the double joggle area, which terminates the 
repetitive inspections.
    The FAA is issuing this AD to address cracks in the double joggle 
areas at FR16 and FR20 in the nose forward fuselage, which, if not 
detected and corrected, could reduce the structural integrity of the 
fuselage. See the MCAI for additional background information.

Discussion of Final Airworthiness Directive

Comments

    The FAA received comments from the Air Line Pilots Association, 
International (ALPA) who supported the NPRM without change.

Conclusion

    The FAA reviewed the relevant data, considered the comment 
received, and determined that air safety and the public interest 
require adopting this final rule 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. 
Accordingly, the FAA is issuing this AD to address the unsafe condition 
on these products.

Related Service Information Under 1 CFR Part 51

    EASA AD 2021-0227 specifies procedures for repetitive special 
detailed inspections (rototest inspections) of double joggle areas at 
FR16 and FR20, right hand and left hand sides for cracking, applicable 
on-condition actions (repair) and an optional modification of the 
double joggle area, which terminates the repetitive inspections. The 
modification includes a rotating probe inspection of certain fastener 
holes for cracks, a check of the fastener holes for a minimum diameter, 
and applicable on-condition actions (repair and oversizing holes). This 
material is reasonably available because the interested parties have 
access to it through their normal course of business or by the means 
identified in the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD would affect 1,549 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
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          Labor cost                   Parts cost              Cost per product         Cost on U.S. operators
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Up to 55 work-hours x $85 per   $0......................  Up to $4,675..............  Up to $7,241,575.
 hour = $4,675.
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                  Estimated Costs for Optional Actions
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                                                             Cost per
              Labor cost                   Parts cost        product
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60 work-hours x $85 per hour = $5,100.          $1,624           $6,724
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    The FAA has received no definitive data on which to base the cost 
estimates for the on-condition repairs specified in this 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 because it addresses an unsafe condition that is likely to 
exist or develop on products identified in this rulemaking action.

Regulatory Findings

    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 adding the following new airworthiness 
directive:


[[Page 23757]]


2022-08-08 Airbus SAS: Amendment 39-22011; Docket No. FAA-2022-0091; 
Project Identifier MCAI-2021-01123-T.

(a) Effective Date

    This airworthiness directive (AD) is effective May 26, 2022.

(b) Affected ADs

    This AD affects AD 2020-20-05, Amendment 39-21261 (85 FR 65197, 
October 15, 2020) (AD 2020-20-05).

(c) Applicability

    This AD applies to Airbus SAS Model airplanes specified in 
paragraphs (c)(1) through (4) of this AD, certificated in any 
category, as identified in European Union Aviation Safety Agency 
(EASA) AD 2021-0227, dated October 11, 2021 (EASA AD 2021-0227).
    (1) Model A318-111, -112, -121, and -122 airplanes.
    (2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 
airplanes.
    (3) Model A320-211, -212, -214, -216, -231, -232, and -233 
airplanes.
    (4) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 
airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Unsafe Condition

    This AD was prompted by reports that, during inspections 
accomplished as specified in certain airworthiness limitation items 
(ALIs), cracks were detected in the double joggle areas at frame 
(FR) 16 and FR20 in the nose forward fuselage. The FAA is issuing 
this AD to address cracks in these areas, which, if not detected and 
corrected, could reduce the structural integrity of the fuselage.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, EASA AD 2021-0227.

(h) Exceptions to EASA AD 2021-0227

    (1) Where EASA AD 2021-0227 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2021-0227 does not apply 
to this AD.
    (3) Where paragraph (2) of EASA AD 2021-0227 specifies to 
``contact Airbus for approved repair instructions and, within the 
compliance time specified therein, accomplish those instructions 
accordingly'' if any cracks are detected, for this AD if any 
cracking is detected, the cracking must be repaired before further 
flight using a method approved by Airbus SAS's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.
    (4) Where paragraphs (3) and (4) of EASA AD 2021-0227 specify 
``Airbus approved repair instructions,'' or ``post-repair inspection 
instructions approved by Airbus,'' for this AD, to be acceptable for 
credit, the repair instructions must be approved by Airbus SAS's 
EASA DOA. If approved by the DOA, the approval must include the DOA 
authorized signature.

(i) No Reporting Requirement

    Although the service information referenced in EASA AD 2021-0227 
specifies to submit certain information to the manufacturer, this AD 
does not include that requirement.

(j) Terminating Action for Certain Requirements in AD 2020-20-05

    Accomplishing the initial inspections required by this AD 
terminates ALI Tasks 531153-02-1, 531153-02-2, 531155-02-1 and 
531155-02-2, as required by paragraph (i) of AD 2020-20-05 only for 
the airplanes identified in paragraph (c) of this AD.

(k) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Large Aircraft Section, International Validation Branch, FAA, has 
the authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, 
send your request to your principal inspector or responsible Flight 
Standards Office, as appropriate. If sending information directly to 
the Large Aircraft Section, International Validation Branch, send it 
to the attention of the person identified in paragraph (l) of this 
AD. Information may be emailed to: [email protected]. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
responsible Flight Standards Office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, Large Aircraft 
Section, International Validation Branch, FAA; or EASA; or Airbus 
SAS's EASA DOA. If approved by the DOA, the approval must include 
the DOA-authorized signature.
    (3) Required for Compliance (RC): Except as required by 
paragraphs (h)(3), (i), and (k)(2) of this AD, if any service 
information contains procedures or tests that are identified as RC, 
those procedures and tests must be done to comply with this AD; any 
procedures or tests that are not identified as RC are recommended. 
Those procedures and tests that are not identified as RC may be 
deviated from using accepted methods in accordance with the 
operator's maintenance or inspection program without obtaining 
approval of an AMOC, provided the procedures and tests identified as 
RC can be done and the airplane can be put back in an airworthy 
condition. Any substitutions or changes to procedures or tests 
identified as RC require approval of an AMOC.

(l) Related Information

    For more information about this AD, contact Vladimir Ulyanov, 
Aerospace Engineer, Large Aircraft Section, FAA, International 
Validation Branch, 2200 South 216th St., Des Moines, WA 98198; phone 
206-231-3229; email [email protected].

(m) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference of the service information listed in this 
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (i) European Union Aviation Safety Agency (EASA) AD 2021-0227, 
dated October 11, 2021.
    (ii) [Reserved]
    (3) For EASA AD 2021-0227, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; telephone +49 221 8999 000; email 
[email protected]; internet www.easa.europa.eu. You may find this 
EASA AD on the EASA website at https://ad.easa.europa.eu.
    (4) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th St., 
Des Moines, WA. For information on the availability of this material 
at the FAA, call 206-231-3195.
    (5) You may view this material that is incorporated by reference 
at the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, email 
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on April 4, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2022-08494 Filed 4-20-22; 8:45 am]
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