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Federal Register / Vol. 86, No. 193 / Friday, October 8, 2021 / Proposed Rules sources, gathering and maintaining the data needed, 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.
Authority for This Rulemaking
jspears on DSK121TN23PROD with PROPOSALS1

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.
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.

16:42 Oct 07, 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:

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.

VerDate Sep<11>2014

The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

Vulcanair S.p.A.: Docket No. FAA2021
0871; Project Identifier MCAI2020
01581A.
a Comments Due Date The FAA must receive comments on this airworthiness directive AD by November 22, 2021.
b Affected ADs None.
c Applicability This AD applies to Vulcanair S.p.A.
Vulcanair Models P.68C, P.68CTC, P.68
OBSERVER, P.68 OBSERVER 2, P.68R, and P.68TC OBSERVER airplanes, serial numbers 333, 337 to 339 inclusive, 378, 379, and 383
and larger except serial numbers 387 and 398, certificated in any category, with a stabilator trim control cable part number 5.60671, 5.61611, 5.61711, 5.62312, or 5.62314 installed.
d Subject Joint Aircraft System Component JASC
Code 2740, Stabilizer Control System.
e Unsafe Condition This AD was prompted by a damaged stabilator trim control cable connected to the stabilator trim actuator assembly, mounted on fuselage frame No. 16. The FAA is issuing this AD to detect and address failure of a stabilator trim control cable, which could prevent trim surface control thereby leaving the cable remaining in the last position. The unsafe condition, if not addressed, could result in reduced control of the airplane.
f Compliance Comply with this AD within the compliance times specified, unless already done.
g Required Actions Before a stabilator trim control cable part number 5.60671, 5.61611, 5.61711, 5.62312, or 5.62314 accumulates more than 400 hours time-in-service TIS since first installation on an airplane or within 50
hours TIS after the effective date of this AD, whichever occurs later, and thereafter at intervals not to exceed 50 hours TIS, visually inspect the stabilator trim control cable for broken wires and replace the stabilator trim control cable before further flight if there is broken wire in a strand in accordance with
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steps 1 through 22 of Part 2 Work Procedure in Vulcanair S.p.A. P.68 Variants Mandatory Service Bulletin No. 263, dated October 20, 2020 MSB 263.
h Reporting Within 14 days after the initial inspection required by paragraph g of this AD or within 14 days after the effective date of this AD, whichever occurs later, report the results of the initial inspection to Vulcanair at continued.airworthiness@vulcanaair.com or at the address in paragraph k3 of this AD.
Thereafter, report the inspection results within 14 days after each inspection. Each report must include the following information:
1 Owner/operator name, mailing address, phone number, and email address;
2 Airplane model, serial number, and registration number;
3 Airplane hours TIS at the time of the inspection;
4 Stabilator trim control cable hours TIS
at the time of the inspection;
5 Date of the inspection;
6 Inspection result positive or negative;
and 7 A description of any non-conformity damage.
i Special Flight Permit Special flight permits are prohibited.
j 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 certification office, send it to the attention of the person identified in paragraph k1 of this AD or email 9-AVS-AIR-730-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.
k Related Information 1 For more information about this AD, contact Gregory Johnson, Aviation Safety Engineer, FAA, General Aviation & Rotorcraft Section, International Validation Section, 901
Locust, Room 301, Kansas City, MO 64106
2641; phone: 720 6265462; email:
gregory.johnson@faa.gov.
2 Refer to European Union Aviation Safety Agency EASA AD 20200262, dated November 30, 2020, for more information.
You may examine the EASA AD in the AD
docket at https www.regulations.gov by searching for and locating it in Docket No.
FAA20210871.
3 For service information identified in this AD, contact Vulcanair S.p.A., Fulvio Oloferni, via Giovanni Pascoli, 7, Naples, 80026, Italy; phone: +39 081 5918 135; email:
airworthiness@vulcanair.com; website:
www.vulcanair.com. You may view this referenced service information at the FAA, Airworthiness Products Section, Operational
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