Voglio sapere a riguardo di…

10495

Federal Register / Vol. 86, No. 33 / Monday, February 22, 2021 / Proposed Rules will be available on the internet at https www.regulations.gov by searching for and locating Docket No.
FAA20201178 after the FAA final rule is published.

not limited to the section titled Required Actions and Compliance Times in the EASA AD. Service information specified in EASA AD
20200203 that is required for compliance with EASA AD 20200203

Costs of Compliance The FAA estimates that this proposed AD affects 15 airplanes of U.S. registry.
The FAA estimates the following costs to comply with this proposed AD:

ESTIMATED COSTS FOR REQUIRED ACTIONS
Cost per product
Parts cost
Cost on U.S.
operators
Action
Labor cost
Retained AFM revision from AD 202009
14.
Retained installation from AD 20200914
New proposed actions

1 work-hour $85 per hour = $85

$0

$85

$1,105.

2 work-hours $85 per hour = $170
Up to 42 work-hours $85 per hour = Up to $3,570.

$170
Up to $3,570

$2,210.
Up to $53,550.

The FAA has received no definitive data regarding cost estimates for these parts.

The FAA has received no definitive data on which to base the cost estimates for the on-condition actions specified in this proposed AD.
According to the manufacturer, some or all of the costs of this proposed AD
may be covered under warranty, thereby reducing the cost impact on affected individuals. The FAA does not control warranty coverage for affected individuals. As a result, the FAA has included all known costs in the cost estimate.

tkelley on DSKBCP9HB2PROD with PROPOSALS

Authority for This Rulemaking 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.
Regulatory Findings The FAA determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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.

VerDate Sep<11>2014

18:29 Feb 19, 2021

Jkt 253001

For the reasons discussed above, I
certify this proposed regulation:
1 Is not a significant regulatory action under Executive Order 12866, 2 Would not affect intrastate aviation in Alaska, and 3 Would 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 Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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:
a. Removing Airworthiness Directive 20200914, Amendment 3919910 85
FR 30601, May 20, 2020; and b. Adding the following new AD:

Airbus SAS: Docket No. FAA20201178;
Project Identifier MCAI202001325T.
a Comments Due Date The FAA must receive comments for this airworthiness directive AD action by April 8, 2021.
b Affected ADs This AD replaces AD 20200914, Amendment 3919910 85 FR 30601, May 20, 2020 AD 20200914.
c Applicability This AD applies to Airbus SAS Model A350941 and 1041 airplanes, certificated
PO 00000

Frm 00037

Fmt 4702

Sfmt 4702

in any category, as identified in European Union Aviation Safety Agency EASA AD
20200203, dated September 23, 2020 EASA
AD 20200203.
d Subject Air Transport Association ATA of America Code 31, Instruments.
e Reason This AD was prompted by two reports of abnormal operation of the components of the ENG START panel or Electronic Centralized Aircraft Monitoring ECAM Control Panel ECP due to liquid spillage in the system, and the subsequent uncommanded engine inflight shutdown IFSD of one engine in each case. This AD was also prompted by the development of a new, water-resistant integrated control panel ICP that will address this unsafe condition. The FAA is issuing this AD to address the potential for dual-engine IFSD, possibly resulting in a forced landing with consequent damage to the airplane and injury to occupants.
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 20200203.
h Exceptions to EASA AD 20200203
1 Where EASA AD 20200203 refers to its effective date, this AD requires using the effective date of this AD.
2 Where EASA AD 20200203 refers to the effective date of EASA AD 20200020E, this AD requires using February 14, 2020 the effective date of AD 20200312.
3 Where EASA AD 20200203 refers to the effective date of EASA AD 20200090, this AD requires using June 4, 2020 the effective date of AD 20200914.
4 Where paragraph 7 of EASA AD 2020
0203 specifies removing the AFM airplane flight manual changes as required by paragraph 2 or 4 of the MCAI, as applicable, this AD requires removing the AFM changes required by paragraph 1, 2, 4, or 5, as applicable, from the AFM.

E:FRFM22FEP1.SGM

22FEP1