Federal Register / Vol. 75, No. 118 / Monday, June 21, 2010 / Proposed Rules 34953 

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 

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 § 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 


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