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Federal Register / Vol. 86, No. 225 / Friday, November 26, 2021 / Rules and Regulations
67311

ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
Replace screws, cables, fuses, supports, and protective tape; reroute harnesses.
Apply protective tape
Replace cables, fuses and protective tape

5 work-hours $85 per hour = $425

$600

$1.025

1 work-hour $85 per hour = $85
1 work-hour $85 per hour = $85

50
600

135
685

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 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.

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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:

VerDate Sep<11>2014

16:31 Nov 24, 2021

Jkt 256001

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:

20212202 Leonardo S.p.a.: Amendment 3921775; Docket No. FAA20210461;
Project Identifier MCAI202100156R.
a Effective Date This airworthiness directive AD is effective January 3, 2022.
b Affected ADs None.
c Applicability This AD applies to all Leonardo S.p.a.
Model AB139 and AW139 helicopters, certificated in any category.
d Subject Joint Aircraft System Component JASC
Code 2400, Electrical Power System.
e Unsafe Condition This AD was prompted by a report of a short circuit caused by chafing of the electrical wiring in the overhead panel. The FAA is issuing this AD to address a short circuit caused by chafing of the electrical wiring in the overhead panel, which could cause damaged electrical wiring, possible fire in the overhead panel, and loss of control of the helicopter.
f Compliance Comply with this AD within the compliance times specified, unless already done.

Parts cost
Cost per product
Action
4 Where paragraphs 3 and 5 of EASA
AD 20210044 refer to any discrepancy, for this AD, discrepancies include chafing of the cable harnesses or incorrect clearance between the anchor nuts/screws and the cable harnesses, incorrect length of the screws, inadequately bonded supports, and poor condition of the white protective tape.
i No Reporting Requirement Although EASA AD 20210044 and the service information referenced in EASA AD
20210044 specify to submit certain information to the manufacturer, this AD
does not include that requirement.
j Special Flight Permit Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199
to operate the helicopter to a location where the helicopter can be modified if the operator elects to do so, provided the flight is straight, level, and avoids areas of known turbulence.
k Alternative Methods of Compliance AMOCs 1 The Manager, 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph l of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
2 Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.
l Related Information
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, European Union Aviation Safety Agency EASA AD 20210044, dated February 5, 2021 EASA AD 20210044.

For more information about this AD, contact Jacob Fitch, Aerospace Engineer, COS
Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; phone: 817 2224130;
email: jacob.fitch@faa.gov.

h Exceptions to EASA AD 20210044
1 Where EASA AD 20210044 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20210044 does not apply to this AD.
3 Where EASA AD 20210044 refers to flight hours FH, this AD requires using hours time-in-service.

m Material Incorporated by Reference
PO 00000

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Fmt 4700

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1 The Director of the Federal Register approved the incorporation by reference IBR of the service information listed in this paragraph under 5 U.S.C. 552a 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.

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