Proposed Primary Category Airworthiness Design Standards; AutoGyro USA, LLC (AutoGyro) Model Calidus Gyroplanes, 43969-43970 [2015-18221]

Download as PDF 43969 Proposed Rules Federal Register Vol. 80, No. 142 Friday, July 24, 2015 This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules. DEPARTMENT OF AGRICULTURE Animal and Plant Health Inspection Service p.m., Monday through Friday, except holidays. To be sure someone is there to help you, please call (202) 799–7039 before coming. FOR FURTHER INFORMATION CONTACT: Dr. Carol Clarke, Research Program Manager, USDA, APHIS, Animal Care, 4700 River Road Unit 84, Riverdale, MD 20737–1234; (301) 851–3751. SUPPLEMENTARY INFORMATION: Background 9 CFR Part 3 [Docket No. APHIS–2014–0098] Petition To Develop Specific Ethologically Appropriate Standards for Nonhuman Primates in Research Animal and Plant Health Inspection Service, USDA. ACTION: Notice of petition; reopening of comment period. AGENCY: We are reopening the comment period for a petition requesting that we amend the Animal Welfare Act regulations to specify ethologically appropriate standards that researchers must adhere to in order to promote the psychological well-being of nonhuman primates used in research. This action will allow interested persons additional time to prepare and submit comments. DATES: The comment period for the notice published May 1, 2015 (80 FR 24840–24841) is reopened. We will consider all comments that we receive on or before August 31, 2015. ADDRESSES: You may submit comments by either of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov/ #!docketDetail;D=APHIS-2014-0098. • Postal Mail/Commercial Delivery: Send your comment to Docket No. APHIS–2014–0098, Regulatory Analysis and Development, PPD, APHIS, Station 3A–03.8, 4700 River Road Unit 118, Riverdale, MD 20737–1238. Supporting documents and any comments we receive on this docket may be viewed at https:// www.regulations.gov/ #!docketDetail;D=APHIS-2014-0098 or in our reading room, which is located in Room 1141 of the USDA South Building, 14th Street and Independence Avenue SW., Washington, DC. Normal reading room hours are 8 a.m. to 4:30 asabaliauskas on DSK5VPTVN1PROD with PROPOSALS SUMMARY: VerDate Sep<11>2014 16:51 Jul 23, 2015 Jkt 235001 Authority: 7 U.S.C. 2131–2159; 7 CFR 2.22, 2.80, and 371.7. Done in Washington, DC, this 20th day of July 2015. Kevin Shea, Administrator, Animal and Plant Health Inspection Service. [FR Doc. 2015–18174 Filed 7–23–15; 8:45 am] BILLING CODE 3410–34–P 1 To view the notice, supporting documents, and the comments we received, go to https:// www.regulations.gov/#!docketDetail;D=APHIS2014-0098. Frm 00001 Federal Aviation Administration 14 CFR Part 21 [Docket No. FAA–2015–3031] Proposed Primary Category Airworthiness Design Standards; AutoGyro USA, LLC (AutoGyro) Model Calidus Gyroplanes Federal Aviation Administration (FAA), DOT. ACTION: Request for comments. AGENCY: On May 1, 2015, the Animal and Plant Health Inspection Service published in the Federal Register (80 FR 24840– 24841, Docket No. APHIS–2014–0098) a notice 1 requesting comments on a petition to amend the Animal Welfare Act regulations to specify ethologically appropriate standards that researchers must adhere to in order to promote the psychological well-being of nonhuman primates used in research. Comments on the notice were required to be received on or before June 30, 2015. We are reopening the comment period on Docket No. APHIS– 2014–0098 for an additional 60 days, until August 31, 2015. We will accept all comments received between July 1, 2015 (the day after the close of the original comment period) and the date of this notice. This action will allow interested persons additional time to prepare and submit comments. We encourage the submission of scientific data, studies, or research to support your comments and position. We also invite data on the costs and benefits associated with any recommendations. We will consider all comments and recommendations received. PO 00000 DEPARTMENT OF TRANSPORTATION Fmt 4702 Sfmt 4702 This notice announces the existence of and requests comments on the proposed airworthiness design standards for acceptance of the AutoGyro Model Calidus gyroplane under the regulations for primary category aircraft. DATES: We must receive comments by September 8, 2015. ADDRESSES: Send all comments to the Federal Aviation Administration (FAA), Rotorcraft Standards Staff, Rotorcraft Directorate (ASW–110), FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177. FOR FURTHER INFORMATION CONTACT: Gary Roach, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, Texas 76177; telephone (817) 222–5110; email gary.b.roach@faa.gov. SUPPLEMENTARY INFORMATION: Any person may obtain a copy of this information by contacting the person named above under FOR FURTHER INFORMATION CONTACT. SUMMARY: Comments Invited We invite you to submit comments on the proposed airworthiness standards to the address specified above. Commenters must identify the AutoGyro Model Calidus on all submitted correspondence. The FAA will consider all communications received on or before the closing date before issuing the final acceptance. The proposed airworthiness design standards and comments received may be inspected at the FAA, Rotorcraft Directorate, Rotorcraft Standards Staff (ASW–110), FAA, 2601 Meacham Blvd., Fort Worth, TX 76137, between the hours of 7:30 a.m. and 4 p.m. weekdays, except Federal holidays. E:\FR\FM\24JYP1.SGM 24JYP1 43970 Federal Register / Vol. 80, No. 142 / Friday, July 24, 2015 / Proposed Rules Background DEPARTMENT OF TRANSPORTATION The ‘‘primary’’ category for aircraft was created specifically for the simple, low performance personal aircraft. Section 21.17(f) provides a means for applicants to propose airworthiness standards for their particular primary category aircraft. The FAA procedure establishing appropriate airworthiness standards includes reviewing and possibly revising the applicant’s proposal, publication of the submittal in the Federal Register for public review and comment, and addressing the comments. After all necessary revisions, the standards are published as approved FAA airworthiness standards. Accordingly, the applicant, AutoGyro, has submitted a request to the FAA to include the following: Federal Aviation Administration asabaliauskas on DSK5VPTVN1PROD with PROPOSALS Proposed Airworthiness Standards for Acceptance Under the Primary Category Rule For Aircraft Certification and the Powerplant Installation: Section T Light Gyroplanes, of the British Civil Airworthiness Requirements, Issue 3, dated August 12, 2005. 14 CFR 27.853(a) and (c)(1) Amdt 27– 37 Compartment Interior; §§ 23.735(a) through (c) Amdt 23–62 Brakes except that the reference to 23.75 is replaced with Section T75 of BCAR Section T, Issue 3; §§ 27.735(a) and (c)(1) Amdt 27–21 Brakes; §§ 27.1365(b) and (c) Amdt 27–35 Electrical Cables; and § 27.1561(a) Safety Equipment, as applicable to these aircraft. For Engine Assembly Certification: ASTM F2339–06 (2009), ‘‘Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Light Sport Aircraft,’’ except paragraph A1.1.3. For Propeller Certification: Section T Light Gyroplanes, of the British Civil Airworthiness Requirements, Issue 3, dated August 12, 2005; ASTM F2506–10 (2009), ‘‘Standard Specification for Design and Testing of Fixed-Pitch or Ground Adjustable Light Sport Aircraft Propellers,’’ paragraph 5.5 Propeller Strength and Endurance and Section 6 Tests and Inspections. Issued in Fort Worth, Texas on July 16, 2015. Bruce E. Cain, Acting Directorate Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2015–18221 Filed 7–23–15; 8:45 am] BILLING CODE 4910–13–P VerDate Sep<11>2014 16:51 Jul 23, 2015 Jkt 235001 14 CFR Part 39 [Docket No. FAA–2015–2994; Directorate Identifier 2014–SW–057–AD] RIN 2120–AA64 Airworthiness Directives; Airbus Helicopters Deutschland GmbH (Formerly Eurocopter Deutschland GmbH) Helicopters Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Deutschland GmbH (Airbus) (formerly Eurocopter Deutschland GmbH) Model MBB–BK 117C–2 helicopters with an external mounted hoist system wiring harness installed. This proposed AD would require inspecting the hoist control pendant wiring harness for chafing, and if there is chafing, before the next hoist operation, replacing the wiring harness. This proposed AD would also require a installing a protection sleeve on the hoist control pendant wiring harness. This proposed AD is prompted by an uncommanded hoist release involving chafing on the wiring harness of the hoist control pendant and on the wiring. The proposed actions are intended to prevent loss of an external load or person from the hoist resulting in injury to persons being lifted and loss of control of the helicopter. DATES: We must receive comments on this proposed AD by September 22, 2015. SUMMARY: Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the European Aviation Safety Agency (EASA) AD, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (telephone 800–647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. For service information identified in this proposed AD, contact Airbus Helicopters, Inc., 2701 N. Forum Drive, Grand Prairie, TX 75052; telephone (972) 641–0000 or (800) 232–0323; fax (972) 641–3775; or at https:// www.airbushelicopters.com/techpub. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. FOR FURTHER INFORMATION CONTACT: George Schwab, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5110; email george.schwab@faa.gov. SUPPLEMENTARY INFORMATION: Examining the AD Docket Comments Invited We invite you to participate in this rulemaking by submitting written comments, data, or views. We also invite comments relating to the economic, environmental, energy, or federalism impacts that might result from adopting the proposals in this document. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. To ensure the docket does not contain duplicate comments, commenters should send only one copy of written comments, or if comments are filed electronically, commenters should submit only one time. We will file in the docket all comments that we receive, as well as a report summarizing each substantive public contact with FAA personnel concerning this proposed rulemaking. Before acting on this proposal, we will consider all comments we receive on or before the closing date for comments. We will consider comments filed after the comment period has closed if it is possible to do so without incurring expense or delay. We may change this proposal in light of the comments we receive. You may examine the AD docket on the Internet at https:// www.regulations.gov or in person at the Discussion EASA, which is the Technical Agent for the Member States of the European You may send comments by any of the following methods: • Federal eRulemaking Docket: Go to https://www.regulations.gov. Follow the online instructions for sending your comments electronically. • Fax: 202–493–2251. • Mail: Send comments to the U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590–0001. • Hand Delivery: Deliver to the ‘‘Mail’’ address between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. ADDRESSES: PO 00000 Frm 00002 Fmt 4702 Sfmt 4702 E:\FR\FM\24JYP1.SGM 24JYP1

Agencies

[Federal Register Volume 80, Number 142 (Friday, July 24, 2015)]
[Proposed Rules]
[Pages 43969-43970]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-18221]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 21

[Docket No. FAA-2015-3031]


Proposed Primary Category Airworthiness Design Standards; 
AutoGyro USA, LLC (AutoGyro) Model Calidus Gyroplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Request for comments.

-----------------------------------------------------------------------

SUMMARY: This notice announces the existence of and requests comments 
on the proposed airworthiness design standards for acceptance of the 
AutoGyro Model Calidus gyroplane under the regulations for primary 
category aircraft.

DATES: We must receive comments by September 8, 2015.

ADDRESSES: Send all comments to the Federal Aviation Administration 
(FAA), Rotorcraft Standards Staff, Rotorcraft Directorate (ASW-110), 
FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177.

FOR FURTHER INFORMATION CONTACT: Gary Roach, Aviation Safety Engineer, 
Regulations and Policy Group, Rotorcraft Directorate, FAA, 10101 
Hillwood Pkwy., Fort Worth, Texas 76177; telephone (817) 222-5110; 
email gary.b.roach@faa.gov.

SUPPLEMENTARY INFORMATION: Any person may obtain a copy of this 
information by contacting the person named above under FOR FURTHER 
INFORMATION CONTACT.

Comments Invited

    We invite you to submit comments on the proposed airworthiness 
standards to the address specified above. Commenters must identify the 
AutoGyro Model Calidus on all submitted correspondence. The FAA will 
consider all communications received on or before the closing date 
before issuing the final acceptance. The proposed airworthiness design 
standards and comments received may be inspected at the FAA, Rotorcraft 
Directorate, Rotorcraft Standards Staff (ASW-110), FAA, 2601 Meacham 
Blvd., Fort Worth, TX 76137, between the hours of 7:30 a.m. and 4 p.m. 
weekdays, except Federal holidays.

[[Page 43970]]

Background

    The ``primary'' category for aircraft was created specifically for 
the simple, low performance personal aircraft. Section 21.17(f) 
provides a means for applicants to propose airworthiness standards for 
their particular primary category aircraft. The FAA procedure 
establishing appropriate airworthiness standards includes reviewing and 
possibly revising the applicant's proposal, publication of the 
submittal in the Federal Register for public review and comment, and 
addressing the comments. After all necessary revisions, the standards 
are published as approved FAA airworthiness standards.
    Accordingly, the applicant, AutoGyro, has submitted a request to 
the FAA to include the following:

Proposed Airworthiness Standards for Acceptance Under the Primary 
Category Rule

    For Aircraft Certification and the Powerplant Installation:
    Section T Light Gyroplanes, of the British Civil Airworthiness 
Requirements, Issue 3, dated August 12, 2005.
    14 CFR 27.853(a) and (c)(1) Amdt 27-37 Compartment Interior; 
Sec. Sec.  23.735(a) through (c) Amdt 23-62 Brakes except that the 
reference to 23.75 is replaced with Section T75 of BCAR Section T, 
Issue 3; Sec. Sec.  27.735(a) and (c)(1) Amdt 27-21 Brakes; Sec. Sec.  
27.1365(b) and (c) Amdt 27-35 Electrical Cables; and Sec.  27.1561(a) 
Safety Equipment, as applicable to these aircraft.
    For Engine Assembly Certification:
    ASTM F2339-06 (2009), ``Standard Practice for Design and 
Manufacture of Reciprocating Spark Ignition Engines for Light Sport 
Aircraft,'' except paragraph A1.1.3.
    For Propeller Certification:
    Section T Light Gyroplanes, of the British Civil Airworthiness 
Requirements, Issue 3, dated August 12, 2005; ASTM F2506-10 (2009), 
``Standard Specification for Design and Testing of Fixed-Pitch or 
Ground Adjustable Light Sport Aircraft Propellers,'' paragraph 5.5 
Propeller Strength and Endurance and Section 6 Tests and Inspections.

    Issued in Fort Worth, Texas on July 16, 2015.
Bruce E. Cain,
Acting Directorate Manager, Rotorcraft Directorate, Aircraft 
Certification Service.
[FR Doc. 2015-18221 Filed 7-23-15; 8:45 am]
BILLING CODE 4910-13-P

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