This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

50881 

Vol. 76, No. 159 

Wednesday, August 17, 2011 

DEPARTMENT OF AGRICULTURE 

Grain Inspection, Packers and 

Stockyards Administration 

9 CFR Part 201 

RIN 0580–AB10 

Required Scale Tests 

AGENCY: Grain Inspection, Packers and 

Stockyards Administration, Agriculture. 

ACTION: Correcting amendment. 

SUMMARY: The Grain Inspection, Packers 

and Stockyards Administration 

published documents in the Federal 

Register on January 20, 2011, and on 

April 4, 2011, concerning required scale 

tests. Those documents defined ‘‘limited 

seasonal basis’’ incorrectly. This 

document corrects the error. 

DATES: Effective on August 17, 2011. 

FOR FURTHER INFORMATION CONTACT: S. 

Brett Offutt, Director, Policy and 

Litigation Division, P&SP, GIPSA, 1400 

Independence Ave., SW., Washington, 

DC 20250, (202) 720–7363, 

s.brett.offutt@usda.gov. 

SUPPLEMENTARY INFORMATION: 

Need for Correction 

The Grain Inspection, Packers and 

Stockyards Administration published 

two documents in the Federal Register 

on January 20, 2011 (76 FR 3485) and 

on April 4, 2011 (76 FR 18348), 

concerning required scale tests. Those 

documents incorrectly defined limited 

seasonal basis in § 201.72(a) (9 CFR 

201.72(a)). This document corrects 

§ 201.72 by revising the last sentence of 

paragraph (a). 

List of Subjects in 9 CFR Part 201 

Reporting and recordkeeping 

requirements, Measurement standards, 

Trade practices. 

Accordingly, 9 CFR part 201 is 

corrected by making the following 

correcting amendment: 

PART 201—REGULATIONS UNDER 

THE PACKERS AND STOCKYARDS 

ACT 

■ 1. The authority citation for part 201 

continues to read as follows: 

Authority: 7 U.S.C. 181–229c. 

■ 2. In § 201.72, revise the last sentence 

of paragraph (a) to read as follows: 

§ 201.72 Scales; testing of. 

(a) * * * Except that if scales are 

used on a limited seasonal basis (during 

any continuous 8-month period) for 

purposes of purchase, sale, acquisition, 

payment or settlement, the stockyard 

owner, swine contractor, market agency, 

dealer, live poultry dealer, or packer 

using such scales may use the scales 

within a 8-month period following each 

test. 

* * * * * 

J. Dudley Butler, 

Administrator, Grain Inspection, Packers and 

Stockyards Administration. 

[FR Doc. 2011–20873 Filed 8–16–11; 8:45 am] 

BILLING CODE 3410–KD–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2011–0832; Directorate 

Identifier 2011–CE–025–AD; Amendment 

39–16771; AD 2011–17–07] 

RIN 2120–AA64 

Airworthiness Directives; M7 

Aerospace LP Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

M7 Aerospace LP Models SA226–T, 

SA226–T(B), SA226–TC, and SA226– 

AT airplanes. This AD requires 

repetitive replacement and inspection of 

certain elevator, rudder, aileron, and 

aileron-to-rudder interconnect primary 

control cables, and checking and setting 

of flight control cable tension. This AD 

was prompted by a report of a failure of 

a rudder control cable. We are issuing 

this AD to correct the unsafe condition 

on these products. 

DATES: This AD is effective September 1, 

2011. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of September 1, 2011. 

We must receive comments on this 

AD by October 3, 2011. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue, SE., Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue, SE., Washington, DC 20590, 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

For service information identified in 

this AD, contact M7 Aerospace, LC, 

10823 NE. Entrance Road, San Antonio, 

Texas 78216; telephone (210) 824–9421; 

fax: 800–347–5901; e-mail: http:// 

www.m7aerospace.com/page/1/ 

contact_parts.jsp; Web site: http:// 

www.m7aerospace.com. You may 

review copies of the referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, 

call 816–329–4148. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Management Facility between 

9 a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The AD 

docket contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (phone: 800–647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 


Emcdonald on DSK2BSOYB1PROD with RULES
50882 Federal Register / Vol. 76, No. 159 / Wednesday, August 17, 2011 / Rules and Regulations 

FOR FURTHER INFORMATION CONTACT: 

Andrew McAnaul, Aerospace Engineer, 

FAA, ASW–150 (c/o San Antonio MIDO 

(SW–MIDO–43)), 10100 Reunion Place, 

Suite 650, San Antonio, Texas 78216; 

phone: (210) 308–3365; fax: (210) 308– 

3370; e-mail: andrew.mcanaul@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We received a report of an M7 

Aerospace LP Model SA226–T airplane 

experiencing loss of rudder control 

during single-engine occurrence training 

requiring applied full rudder to 

compensate for yaw effect. The airplane 

made an uneventful landing. A visual 

inspection found the left-hand primary 

rudder control cable had failed where 

the cable makes a 30 degree angle over 

a small pulley to accommodate rerouting of the control cable alongside 

the camera system installed in the 

center of the cabin. 

AD 87–02–02 (52 FR 2511, January 

23, 1987) requires periodic inspection or 

replacement of all flight control cables 

on Models SA226 and SA227 airplanes. 

This new AD action requires repetitive 

replacement of specific flight control 

cables on affected serial number Model 

SA226 airplanes that have been 

modified by installation of a camera 

system requiring rerouting of the 

affected flight control cables. 

This condition, if not corrected, could 

result in loss of controlled flight due to 

failure of a rudder, aileron and/or 

elevator control cable. 

Relevant Service Information 

We reviewed M7 Aerospace LP 

Service Bulletin 226–27–072, dated June 

27, 2011. The service information 

describes procedures for repetitive 

inspection and replacement of all 

elevator, rudder, aileron, and aileron-torudder interconnect primary control 

cables. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of these same 

type designs. 

AD Requirements 

This AD requires accomplishing the 

actions specified in the service 

information described previously. 

FAA’s Justification and Determination 

of the Effective Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because if an elevator cable or 

another cable in certain situations 

breaks, the outcome can be catastrophic. 

Therefore, we find that notice and 

opportunity for prior public comment 

are impracticable and that good cause 

exists for making this amendment 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety and 

was not preceded by notice and an 

opportunity for public comment. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2011–0832; Directorate Identifier 2011– 

CE–025–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this AD. We will consider all 

comments received by the closing date 

and may amend this AD because of 

those comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD affects 4 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. 

operators 

Logbook check ............................. 1 work-hour × $85 per hour = $85 Not Applicable ............ $85 ............................. $340. 

Inspection of all elevator, rudder, 

aileron, and aileron-to-rudder 

interconnect primary control cables.

80 to 100 work-hours × $85 per 

hour = $6,800 to $8,500.

Not Applicable ............ $6,800 to $8,500 ........ $27,200 to $34,000. 

Replacement of all elevator, rudder, aileron, and aileron-to-rudder interconnect primary control 

cables.

120 to 180 work-hours × $85 per 

hour = $10,200 to $15,300.

$18,800 ...................... $29,000 to $34,100 .... $116,000 to $136,400. 

Check (set) flight control cable 

tension.

20 to 25 work-hours × $85 per 

hour = $1,700 to $2,125.

Not Applicable ............ $1,700 to $2,125 ........ $6,800 to $8,500. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s 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 Agency’s 

authority. 

We are 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: 


Emcdonald on DSK2BSOYB1PROD with RULES
Federal Register / Vol. 76, No. 159 / Wednesday, August 17, 2011 / Rules and Regulations 50883 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) 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. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2011–17–07 M7 Aerospace LP: Amendment 

39–16771; Docket No. FAA–2011–0832; 

Directorate Identifier 2011–CE–025–AD. 

(a) Effective Date 

This AD is effective September 1, 2011. 

(b) Affected ADs 

AD 87–02–02 (52 FR 2511, January 23, 

1987) requires repetitive inspection or 

replacement of all flight control cables on 

Models SA226 and SA227 airplanes. This 

new action requires repetitive replacement of 

specific flight control cables on affected 

serial number Model SA226 airplanes that 

have been modified by installation of a 

camera system requiring rerouting of the 

affected flight control cables. 

(c) Applicability 

This AD applies to the following M7 

Aerospace LP airplanes, certificated in any 

category, as identified in Table 1 of this AD: 

TABLE 1—APPLICABILITY

Model— Serial Nos.— 

SA226–T ................ T265, T267. 

SA226–T(B) ........... T(B)348. 

SA226–TC ............. TC277. 

SA226–AT ............. AT071, AT072, AT073. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code: 27, Flight Controls. 

(e) Unsafe Condition 

This AD was prompted by a report of a 

failure of a rudder control cable. We are 

issuing this AD to correct the unsafe 

condition on these products. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done, following M7 Aerospace LP Service 

Bulletin 226–27–072, dated June 27, 2011. If 

the hours time-in-service (TIS) of the control 

cables can not be positively determined by 

the logbook, then you must use hours TIS of 

the airplane to comply with the requirements 

of this AD. 

(g) Inspection 

(1) For cables with more than 6,000 hours 

TIS: Inspect cables for deficiencies within 10 

hours TIS after September 1, 2011 (the 

effective date of this AD). 

(2) If any deficiencies are found during the 

inspection required in paragraph (g)(1) of this 

AD, before further flight replace cables. 

(h) Replacement 

(1) Replace primary control cables within 

the initial compliance times as listed below 

and repetitively thereafter at intervals not to 

exceed 3,500 hours time-in-service (TIS): 

(i) For cables with less than or equal to 

3,500 hours TIS: Replace cables when the 

control cables reach a total of 3,500 hours TIS 

or 150 hours TIS after September 1, 2011 (the 

effective date of this AD), whichever occurs 

later. 

(ii) For cables with less than or equal to 

5,000 hours TIS but greater than 3,500 hours 

TIS: Replace cables within 150 hours TIS 

after September 1, 2011 (the effective date of 

this AD). 

(iii) For cables with more than 5,000 hours 

TIS: Replace cables within 50 hours TIS after 

September 1, 2011 (the effective date of this 

AD). 

(2) Between 50 hours TIS and 200 hours 

TIS after installing any new control cable as 

required in paragraphs (g)(2) or (h)(1) of this 

AD, check (set) flight control cable tension. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Fort Worth Airplane 

Certification Office, 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 ACO, send it to the 

attention of the person identified in the 

Related Information section of this AD. 

(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. 

(j) Related Information 

For more information about this AD, 

contact Andrew McAnaul, Aerospace 

Engineer, FAA, ASW–150 (c/o San Antonio 

MIDO (SW–MIDO–43)), 10100 Reunion 

Place, Suite 650, San Antonio, Texas 78216; 

phone: (210) 308–3365; fax: (210) 308–3370; 

e-mail: andrew.mcanaul@faa.gov. 

(k) Material Incorporated by Reference 

You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) under 5 U.S.C. 552(a) and 1 CFR part 

51 of M7 Aerospace LP Service Bulletin 226– 

27–072, dated June 27, 2011, on September 

1, 2011. 

(2) For service information identified in 

this AD, contact M7 Aerospace, LC, 10823 

NE. Entrance Road, San Antonio, Texas 

78216; telephone (210) 824–9421; fax: 800– 

347–5901; e-mail: http:// 

www.m7aerospace.com/page/1/ 

contact_parts.jsp; Web site: http:// 

www.m7aerospace.com. 

(3) You may review copies of the 

referenced service information at the FAA, 

Small Airplane Directorate, 901 Locust, 

Kansas City, Missouri 64106. For information 

on the availability of this material at the 

FAA, call 816–329–4148. 

(4) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at an NARA facility, call 202–741– 

6030, or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Kansas City, Missouri, on August 

2, 2011. 

John R. Colomy, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2011–20127 Filed 8–16–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOMELAND 

SECURITY 

U.S. Customs and Border Protection 

DEPARTMENT OF THE TREASURY 

19 CFR Part 159 

[USCBP–2010–0008; BP Dec. 11–17] 

RIN 1515–AD67 (formerly RIN 1505–AC21) 

Courtesy Notice of Liquidation 

AGENCY: Customs and Border Protection, 

Department of Homeland Security; 

Department of the Treasury. 

ACTION: Final rule. 

SUMMARY: This document amends title 

19 of the Code of Federal Regulations 

(‘‘CFR’’) pertaining to the method by 

which U.S. Customs and Border 

Protection (‘‘CBP’’) issues courtesy 

notices of liquidation to importers of 

record whose entry summaries are filed 

in the Automated Broker Interface 

(‘‘ABI’’). Courtesy notices of liquidation 


Emcdonald on DSK2BSOYB1PROD with RULES