Federal Register / Vol. 80, No. 60 / Monday, March 30, 2015 / Rules and Regulations 16553 

This rule increases the quantity of 

Scotch spearmint oil that handlers may 

purchase from or handle on behalf of 

producers during the 2014–2015 

marketing year, which ends on May 31, 

2015. The 2014–2015 Scotch spearmint 

oil salable quantity was initially 

established at 1,149,030 pounds and the 

allotment percentage initially set at 55 

percent. This rule increases the Scotch 

spearmint oil salable quantity to 

1,984,423 pounds and the allotment 

percentage to 95 percent. 

The Committee reached its decision to 

recommend an increase in the salable 

quantity and allotment percentage for 

Scotch spearmint oil after careful 

consideration of all available 

information. With the increase, the 

Committee believes that the industry 

will be able to satisfactorily meet the 

current market demand for this class of 

spearmint oil. This rule amends the 

salable quantities and allotment 

percentages previously established in 

§ 985.233. Authority for this action is 

provided in §§ 985.50, 985.51, and 

985.52 of the order. 

In accordance with the Paperwork 

Reduction Act of 1995 (44 U.S.C. 

Chapter 35), the order’s information 

collection requirements have been 

previously approved by the Office of 

Management and Budget (OMB) and 

assigned OMB No. 0581–0178, 

Vegetable and Specialty Crop Marketing 

Orders. No changes in those 

requirements as a result of this action 

are necessary. Should any changes 

become necessary, they would be 

submitted to OMB for approval. 

This rule will not impose any 

additional reporting or recordkeeping 

requirements on either small or large 

spearmint oil handlers. As with all 

Federal marketing order programs, 

reports and forms are periodically 

reviewed to reduce information 

requirements and duplication by 

industry and public sector agencies. In 

addition, USDA has not identified any 

relevant Federal rules that duplicate, 

overlap, or conflict with this rule. 

Further, the Committee’s meeting was 

widely publicized throughout the 

spearmint oil industry and all interested 

persons were invited to attend the 

meeting and participate in Committee 

deliberations. Like all Committee 

meetings, the September 11, 2014, 

meeting was a public meeting and all 

entities, both large and small, were able 

to express their views on this issue. 

Comments on the interim rule were 

required to be received on or before 

December 30, 2014. No comments were 

received. Therefore, for the reasons 

given in the interim rule, we are 

adopting the interim rule as a final rule, 

without change. 

To view the interim rule, go to: 

http://www.regulations.gov/#!document

Detail;D=AMS-FV-13-0087-0003. 

This action also affirms information 

contained in the interim rule concerning 

Executive Orders 12866, 12988, 13175, 

and 13563; the Paperwork Reduction 

Act (44 U.S.C. Chapter 35); and the EGov Act (44 U.S.C. 101). 

After consideration of all relevant 

material presented, it is found that 

finalizing the interim rule, without 

change, as published in the Federal 

Register (79 FR 64657, October 31, 

2014) will tend to effectuate the 

declared policy of the Act. 

List of Subjects in 7 CFR Part 985 

Marketing agreements, Oils and fats, 

Reporting and recordkeeping 

requirements, Spearmint oil. 

Accordingly, the interim rule that 

amended 7 CFR part 985 and that was 

published at 79 FR 64657 on October 

31, 2014, is adopted as a final rule, 

without change. 

Dated: March 24, 2015. 

Rex A. Barnes, 

Associate Administrator, Agricultural 

Marketing Service. 

[FR Doc. 2015–07110 Filed 3–27–15; 8:45 am] 

BILLING CODE P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–1002; Directorate 

Identifier 2014–CE–033–AD; Amendment 

39–18127; AD 2015–06–09] 

RIN 2120–AA64 

Airworthiness Directives; Pacific 

Aerospace Limited Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for Pacific 

Aerospace Limited (PAL) Model 750XL 

airplanes. This AD results from 

mandatory continuing airworthiness 

information (MCAI) issued 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 PAL 

Model 750XL airplanes manufactured 

with only one attitude indicator. A 

second attitude indicator is required for 

flights under instrument flight rules. We 

are issuing this AD to require actions to 

address the unsafe condition on these 

products. 

DATES: This AD is effective May 4, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of May 4, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1002; or in person at Document 

Management Facility, U.S. Department 

of Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590. 

For service information identified in 

this AD, contact Pacific Aerospace 

Limited, Airport Road, Private Bag 3027, 

Hamilton 3240, New Zealand; 

telephone: +64 7 843 6144; fax: +64 7 

843 6134; email: pacific@

aerospace.co.nz; Internet: http://

www.aerospace.co.nz/. You may view 

this 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. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1002. 

FOR FURTHER INFORMATION CONTACT: Karl 

Schletzbaum, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4123; fax: (816) 

329–4090; email: karl.schletzbaum@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to add an AD that would apply 

to Pacific Aerospace Limited Model 

750XL airplanes. The NPRM was 

published in the Federal Register on 

December 8, 2014 (79 FR 72564). The 

NPRM proposed to correct an unsafe 

condition for the specified products and 

was based on mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country. The MCAI states: 

This AD with effective date 10 November 

2014 is prompted by a recent determination 

that certain PAL750XL aircraft were 

inadvertently manufactured with instrument 

panels with only one Attitude Indicator (AI). 

A second AI is required for PAL750XL 

operating under Instrument Flight Rules 

(IFR). 


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16554 Federal Register / Vol. 80, No. 60 / Monday, March 30, 2015 / Rules and Regulations 

The AD mandates the installation of either 

a second AI, or the enablement of 

Reversionary Attitude mode in the Sandel 

Electronic Horizontal Situation Indicator 

(EHSI), if fitted, when operating under IFR. 

The MCAI can be found in the AD 

docket on the Internet at: http://www.

regulations.gov/#!documentDetail;D=

FAA-2014-1002-0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (79 

FR 72564, December 8, 2014) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (79 FR 

72564, December 8, 2014) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (79 FR 72564, 

December 8, 2014). 

Relative Service Information Under 1 

CFR part 51 

We reviewed Pacific Aerospace 

Limited Mandatory Service Bulletin 

PACSB/XL/074, Issue 2, dated 

November 4, 2014. The service bulletin 

describes procedures for installing a 

second attitude indicator or enabling the 

reversionary mode on a Sandel SN3500 

electronic horizontal situation indicator 

(EHSI), if installed, whichever is 

applicable. This service information is 

reasonably available; see ADDRESSES for 

ways to access this service information. 

Costs of Compliance 

We estimate that this AD will affect 

17 products of U.S. registry. We also 

estimate that it would take about 6 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts would cost about $3,500 

per product. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $68,170, or $4,010 per product. 

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 

We determined that 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 this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

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

the 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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1002; 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 the NPRM, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (telephone (800) 647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

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 AD: 

2015–06–09 Pacific Aerospace Limited: 

Amendment 39–18127; Docket No. 

FAA–2014–1002; Directorate Identifier 

2014–CE–033–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective May 4, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Pacific Aerospace 

Limited Model 750XL airplanes, all serial 

numbers, certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 34: Navigation. 

(e) Reason 

This AD was prompted by 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 Pacific 

Aerospace Limited Model 750XL airplanes 

manufactured with instrument panels with 

only one attitude indicator. A second attitude 

indicator is required to operate under 

instrument flight rules (IFR). A reversionary 

attitude indicator reduces the probability of 

a single point failure, which could result in 

loss of control. We are issuing this proposed 

AD to install a reversionary attitude indicator 

before operating in IFR conditions. 

(f) Actions and Compliance 

Unless already done, before the next flight 

requiring instrument flight rules (IFR) after 

the effective date of this AD, install a second 

attitude indicator into the right hand 

instrument panel or enable the reversionary 

mode on a Sandel SN3500 electronic 

horizontal situation indicator (EHSI), if 

installed, whichever is applicable, following 

the ACCOMPLISHMENT INSTRUCTIONS in 

Pacific Aerospace Limited Mandatory Service 

Bulletin PACSB/XL/074, Issue 2, dated 

November 4, 2014. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Karl Schletzbaum, Aerospace 

Engineer, 901 Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329–4123; 

fax: (816) 329–4090; email: 


asabaliauskas on DSK5VPTVN1PROD with RULES
Federal Register / Vol. 80, No. 60 / Monday, March 30, 2015 / Rules and Regulations 16555 

karl.schletzbaum@faa.gov. Before using any 

approved AMOC on any airplane to which 

the AMOC applies, notify your appropriate 

principal inspector (PI) in the FAA Flight 

Standards District Office (FSDO), or lacking 

a PI, your local FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(h) Related Information 

Refer to MCAI in Civil Aviation Authority 

(CAA) AD DCA/750XL/17A, dated November 

6, 2014, for related information. The MCAI 

can be found in the AD docket on the 

Internet at http://www.regulations.gov/#

!documentDetail;D=FAA-2014-1002-0002. 

(i) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

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

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Pacific Aerospace Limited Mandatory 

Service Bulletin PACSB/XL/074, Issue 2, 

dated November 4, 2014. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Pacific Aerospace Limited, 

Airport Road, Private Bag 3027, Hamilton 

3240, New Zealand; telephone: +64 7 843 

6144; fax: +64 7 843 6134; email: pacific@

aerospace.co.nz; Internet: http://

www.aerospace.co.nz/. 

(4) You may view this 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. In 

addition, you can access this service 

information on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2014–1002. 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http://www.archives.

gov/federal-register/cfr/ibr-locations.html. 

Issued in Kansas City, Missouri, on March 

19, 2015. 

Pat Mullen, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–07104 Filed 3–27–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0619; Directorate 

Identifier 2014–NM–029–AD; Amendment 

39–18124; AD 2015–06–06] 

RIN 2120–AA64 

Airworthiness Directives; BAE 

Systems (Operations) Limited 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all BAE 

Systems (Operations) Limited Model 

4101 airplanes. This AD was prompted 

by a report of the failure, due to 

overheat, of a bracket on which the 

earth post (EP) for the generator and 

propeller de-ice systems is located. This 

AD requires an inspection of the 

affected EPs and attachment structure 

for damage, an inspection of the earth 

cables of the generator and propeller deice system for signs of overheating and 

arcing damage, a torque check of the 

affected EP stiff nuts, an electrical high 

current bonding check of the bracket, 

and corrective actions if necessary. We 

are issuing this AD to detect and correct 

an overheat failure of the EPs for the 

generator and propeller de-ice system, 

and possible degradation of the wing 

front spar cap and/or web, which could 

affect the structural integrity of the 

wing. 

DATES: This AD becomes effective May 

4, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of May 4, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://www.

regulations.gov/#!docketDetail;D=FAA2014-0619 or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC. 

For service information identified in 

this AD, contact BAE Systems 

(Operations) Limited, Customer 

Information Department, Prestwick 

International Airport, Ayrshire, KA9 

2RW, Scotland, United Kingdom; 

telephone +44 1292 675207; fax +44 

1292 675704; email RApublications@

baesystems.com; Internet http://www.

baesystems.com/Businesses/Regional

Aircraft/index.htm. You may view this 

referenced service information at the 

FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. 

For information on the availability of 

this material at the FAA, call 425–227– 

1221. It is also available on the Internet 

at http://www.regulations.gov by 

searching for and locating Docket No. 

FAA 2014–0619. 

FOR FURTHER INFORMATION CONTACT: 

Todd Thompson, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone 425–227–1175; 

fax 425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to all BAE Systems (Operations) 

Limited Model 4101 airplanes. The 

NPRM published in the Federal 

Register on September 3, 2014 (79 FR 

52270). The NPRM was prompted by a 

report of the failure, due to overheat, of 

a bracket on which the EP for the 

generator and propeller de-ice systems 

is located. The NPRM proposed to 

require an inspection of the affected EPs 

and attachment structure for damage, an 

inspection of the earth cables of the 

generator and propeller de-ice system 

for signs of overheating and arcing 

damage, a torque check of the affected 

EP stiff nuts, an electrical high current 

bonding check of the bracket, and 

corrective actions if necessary. We are 

issuing this AD to detect and correct an 

overheat failure of the EPs for the 

generator and propeller de-ice system, 

and possible degradation of the wing 

front spar cap and/or web, which could 

affect the structural integrity of the 

wing. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA Airworthiness 

Directive 2014–0006, dated January 7, 

2014 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition. The MCAI states: 

An occurrence was reported involving a 

Jetstream 4100 aeroplane, where a bracket, on 

which the earth post for the generator and 

propeller de-ice systems is located, failed due 

to overheat. Although the earth post and 

cables were not damaged, the mounting 

bracket and underlying structure were 

damaged to the extent that repair of the wing 

front spar web was necessary. Furthermore, 

the aft engine cross support rod, which is 

attached to the same bracket, was found 

damaged, as a result of excessive current 


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