Existence of Proposed Airworthiness Design Standards for Acceptance Under the Primary Category Rule; Orlando Helicopter Airways (OHA), Inc., Models Cessna 172I, 172K, 172L, and 172M, 34953 [2010-14975]

Download as PDF Federal Register / Vol. 75, No. 118 / Monday, June 21, 2010 / Proposed Rules certified. For purposes of this section, end product shall be defined as walnut pieces equal to or larger than eight sixtyfourths of an inch in diameter. Walnut meal shall be defined as walnut pieces smaller than eight sixty-fourths of an inch in diameter. (1) End product. End product must be sized, inspected and certified, and the size must be noted on the inspection certificate. The end product quality must be equal to or better than the minimum requirements of U.S. Commercial grade as defined in the United States Standards for Shelled Walnuts (Juglans regia). (2) Walnut meal. Walnut meal that is accumulated during the cutting or dicing of shelled walnuts to create end product must be presented with the smallest end product from that manufacturing run that is inspected and certified. If the end product meets the applicable U.S. Commercial grade requirements, the walnut meal accumulated during the manufacture of that end product shall be identified and referenced on a separate meal certificate as ‘‘meal derived from walnut pieces that meet U.S. Commercial grade requirements.’’ The certificate number of the smallest end product will be referenced on the meal certificate. (3) Failed lots. If the end product fails to meet applicable U.S. Commercial grade requirements, the end product may be reconditioned, re-sampled, inspected again, and certified. However, the walnut meal accumulated during the manufacture of that end product shall be rejected and disposed of pursuant to the requirements of § 984.64. Dated: June 11, 2010. Rayne Pegg, Administrator, Agricultural Marketing Service. [FR Doc. 2010–14845 Filed 6–18–10; 8:45 am] BILLING CODE P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration sroberts on DSKD5P82C1PROD with PROPOSALS 14 CFR Part 21 Existence of Proposed Airworthiness Design Standards for Acceptance Under the Primary Category Rule; Orlando Helicopter Airways (OHA), Inc., Models Cessna 172I, 172K, 172L, and 172M AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Request for comments. SUMMARY: This notice announces the existence of and requests comments on VerDate Mar<15>2010 15:44 Jun 18, 2010 Jkt 220001 the proposed airworthiness design standards for acceptance of the OHA, Inc., Models Cessna 172I, 172K, 172L, and 172M airplanes under the regulations for primary category aircraft. DATES: Comments must be received on or before July 21, 2010. ADDRESSES: Send all comments to the Federal Aviation Administration (FAA), Standards Office, Small Airplane Directorate (ACE–111), Aircraft Certification Service, 901 Locust Street, Room 301, Kansas City, MO 64106. FOR FURTHER INFORMATION CONTACT: Mr. Leslie B. Taylor, Aerospace Engineer, Standards Office (ACE–111), Small Airplane Directorate, Aircraft Certification Service, FAA; telephone number (816) 329–4134, fax number (816) 329–4090, e-mail at leslie.b.taylor@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 interested parties to submit comments on the proposed airworthiness standards to the address specified above. Commenters must identify the OHA Models Cessna 172I, 172K, 172L, and 172M and submit comments to the address specified above. 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, Small Airplane Directorate, Aircraft Certification Service, Standards Office (ACE–110), 901 Locust Street, Room 301, Kansas City, MO 64106, between the hours of 7:30 a.m. and 4 p.m. weekdays, except Federal holidays. 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, OHA, Inc., has submitted a request to the FAA to include the following: PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 34953 Proposed Airworthiness Standards for Acceptance Under the Primary Category Rule For All Airplane Modifications and the Powerplant Installation Part 3 of the Civil Air regulations (CAR 3), effective November 1, 1949, as amended by 3–1 through 3–12, except for § 3.415, Engines and § 3.416(a), Propellers; and 14 CFR part 23, §§ 23.603, 23.863, 23.907, 23.961, 23.1322 and 23.1359 (latest amendments through Amendment 23– 59) as applicable to these airplanes. For Engine Assembly Certification Joint Aviation Requirements 22 (JAR 22), ‘‘Sailplanes and Powered Sailplanes,’’ Change 5, dated October 28, 1995, Subpart H only. For Propeller Certification 14 CFR part 35 as amended through 35–8 except § 35.1 (or a propeller with an FAA type certificate may be used). For Noise Standards 14 CFR part 36, Amendment 36–28, Appendix G. Issued in Kansas City, Missouri, on June 14, 2010. Sandra J. Campbell, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010–14975 Filed 6–18–10; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2010–0463; Directorate Identifier 2010–CE–021–AD] RIN 2120–AA64 Airworthiness Directives; GA 8 Airvan (Pty) Ltd Models GA8 and GA8–TC320 Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: We propose to adopt a new airworthiness directive (AD) for the products listed above that would revise an existing AD. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Inspection of a high time E:\FR\FM\21JNP1.SGM 21JNP1

Agencies

[Federal Register Volume 75, Number 118 (Monday, June 21, 2010)]
[Proposed Rules]
[Page 34953]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-14975]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 21


Existence of Proposed Airworthiness Design Standards for 
Acceptance Under the Primary Category Rule; Orlando Helicopter Airways 
(OHA), Inc., Models Cessna 172I, 172K, 172L, and 172M

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 
OHA, Inc., Models Cessna 172I, 172K, 172L, and 172M airplanes under the 
regulations for primary category aircraft.

DATES: Comments must be received on or before July 21, 2010.

ADDRESSES: Send all comments to the Federal Aviation Administration 
(FAA), Standards Office, Small Airplane Directorate (ACE-111), Aircraft 
Certification Service, 901 Locust Street, Room 301, Kansas City, MO 
64106.

FOR FURTHER INFORMATION CONTACT: Mr. Leslie B. Taylor, Aerospace 
Engineer, Standards Office (ACE-111), Small Airplane Directorate, 
Aircraft Certification Service, FAA; telephone number (816) 329-4134, 
fax number (816) 329-4090, e-mail at leslie.b.taylor@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 interested parties to submit comments on the proposed 
airworthiness standards to the address specified above. Commenters must 
identify the OHA Models Cessna 172I, 172K, 172L, and 172M and submit 
comments to the address specified above. 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, Small Airplane 
Directorate, Aircraft Certification Service, Standards Office (ACE-
110), 901 Locust Street, Room 301, Kansas City, MO 64106, between the 
hours of 7:30 a.m. and 4 p.m. weekdays, except Federal holidays.

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, OHA, Inc., has submitted a request to 
the FAA to include the following:

Proposed Airworthiness Standards for Acceptance Under the Primary 
Category Rule

For All Airplane Modifications and the Powerplant Installation
    Part 3 of the Civil Air regulations (CAR 3), effective November 1, 
1949, as amended by 3-1 through 3-12, except for Sec.  3.415, Engines 
and Sec.  3.416(a), Propellers; and 14 CFR part 23, Sec. Sec.  23.603, 
23.863, 23.907, 23.961, 23.1322 and 23.1359 (latest amendments through 
Amendment 23-59) as applicable to these airplanes.
For Engine Assembly Certification
    Joint Aviation Requirements 22 (JAR 22), ``Sailplanes and Powered 
Sailplanes,'' Change 5, dated October 28, 1995, Subpart H only.
For Propeller Certification
    14 CFR part 35 as amended through 35-8 except Sec.  35.1 (or a 
propeller with an FAA type certificate may be used).
For Noise Standards
    14 CFR part 36, Amendment 36-28, Appendix G.

    Issued in Kansas City, Missouri, on June 14, 2010.
Sandra J. Campbell,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-14975 Filed 6-18-10; 8:45 am]
BILLING CODE 4910-13-P
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