Federal Register - December 21, 2021
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Fuente: Federal Register
Federal Register / Vol. 86, No. 242 / Tuesday, December 21, 2021 / Rules and Regulations manhole access panel attachment holes in the bottom wing skin panels 2, between rib 13 and rib 23, on airplanes with Sharklets or its structural reinforcements are installed, could lead to crack propagation, possibly resulting in reduced structural integrity of the wings. In addition, the compliance time for the required action is shorter than the time necessary for the public to comment and for publication of the final rule. Accordingly, notice and opportunity for prior public comment
are impracticable and contrary to the public interest pursuant to 5 U.S.C.
553b3B.
In addition, the FAA finds that good cause exists pursuant to 5 U.S.C. 553d for making this amendment effective in less than 30 days, for the same reasons the FAA found good cause to forgo notice and comment.
Regulatory Flexibility Act RFA
The requirements of the RFA do not apply when an agency finds good cause
72173
pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment.
Because the FAA has determined that it has good cause to adopt this rule without notice and comment, RFA
analysis is not required.
Costs of Compliance The FAA estimates that this AD
affects 1,463 airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Cost per product
Parts cost
14 work-hours $85 per hour = $1,190
$0
$1,190
Cost on U.S. operators $1,740,970 per inspection cycle.
Table does not include estimated costs for reporting inspection results.
The FAA estimates that it takes 1
work-hour per product to comply with the reporting requirement in this AD.
The average labor rate is $85 per hour.
Based on these figures, the FAA
estimates the cost of reporting the inspection results on U.S. operators to be $124,355, or $85 per product, per inspection cycle.
The FAA has received no definitive data on which to base the cost estimates for the on-condition actions specified in this AD.
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Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a currently valid OMB Control Number. The OMB
Control Number for this information collection is 21200056. Public reporting for this collection of information is estimated to take approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information.
All responses to this collection of information are mandatory. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to:
Information Collection Clearance Officer, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX 761771524.
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Authority for This Rulemaking
List of Subjects in 14 CFR Part 39
Title 49 of the United States Code specifies the FAAs 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 Agencys 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.
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
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, and 2 Will not affect intrastate aviation in Alaska.
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The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106g, 40113, 44701.
39.13
Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:
20212514 Airbus SAS: Amendment 39
21858; Docket No. FAA20211065;
Project Identifier MCAI202101264T.
a Effective Date This airworthiness directive AD is effective January 5, 2022.
b Affected ADs None.
c Applicability This AD applies to all Airbus SAS
airplanes identified in paragraphs c1
through 3 of this AD and certificated in any category.
1 Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes.
2 Model A320211, 212, 214, 216, 231, 232, and 233 airplanes.
3 Model A321111, 112, 131, 211, 212, 213, 231, and 232 airplanes.
d Subject Air Transport Association ATA of America Code 57, Wings.
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