22166 Federal Register / Vol. 78, No. 72 / Monday, April 15, 2013 / Rules and Regulations 

TABLE 3—MISCELLANEOUS SERVICES 1—Continued 

(10) Special mailing ......................................................................................................................................................................... Actual Cost 

(11) Preparing certificates onsite or during other than normal business hours (use hourly rates from Table 1). 

1Any requested service that is not listed will be performed at $72.90 per hour. 

2 Regular business hours—Monday through Friday—service provided at other than regular business hours will be charged at 1⁄2 times the applicable hourly rate. (See § 800.0(b)(14) for definition of ‘‘business day.’’) 3Foreign travel charged hourly fee of $94.80 plus travel, per diem, and related expenditures. 

Schedule B—Fees for FGIS Supervision 

of Official Inspection and Weighing 

Services Performed by Delegated States 

and/or Designated Agencies in the 

United States 

The supervision fee charged by the 

Service is $0.011 per metric ton of 

domestic U.S. grain shipments 

inspected and/or weighed, including 

land carrier shipments to Canada and 

Mexico. 

(a) Registration certificates and 

renewals. (1) The nature of your 

business will determine the fees that 

your business must pay for registration 

certificates and renewals: 

(i) If you operate a business that buys, 

handles, weighs, or transports grain for 

sale in foreign commerce, you must pay 

$135.00. 

(ii) If you operate a business that 

buys, handles, weighs, or transports 

grain for sale in foreign commerce and 

you are also in a control relationship 

(see definition in section 17A(b)(2) of 

the Act) with respect to a business that 

buys, handles, weighs, or transports 

grain for sale in interstate commerce, 

you must pay $270.00. 

(2) If you request extra copies of 

registration certificates, you must pay 

$2.30 for each copy. 

(b) Designation amendments. If you 

submit an application to amend a 

designation, you must pay $75.00. 

(c) If you submit an application to 

operate as a scale testing organization, 

you must pay $250.00. 

Larry Mitchell, 

Administrator, Grain Inspection, Packers and 

Stockyards Administration. 

[FR Doc. 2013–08809 Filed 4–12–13; 8:45 am] 

BILLING CODE 3410–KD–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0263; Directorate 

Identifier 2013–NE–12–AD; Amendment 39– 

17416; AD 2013–07–12] 

RIN 2120–AA64 

Airworthiness Directives; BRPPowertrain GmbH & Co KG Rotax 

Reciprocating Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

BRP-Powertrain GmbH & Co KG Rotax 

912 F2; 912 F3; 912 F4; 912 S2; 912 S3; 

912 S4; 914 F2; 914 F3; and 914 F4 

reciprocating engines. This AD requires 

a one-time visual inspection for 

excessive oil deposits or carbon deposits 

on the No. 2 and No. 3 spark plug center 

and grounding electrodes, and if found, 

replacement of the cylinder head before 

further flight. This AD was prompted by 

a report of certain No. 2 and No. 3 

cylinder heads not manufactured to 

proper specification. We are issuing this 

AD to prevent excessive oil 

consumption, which could result in an 

in-flight engine shutdown, forced 

landing, and damage to the airplane. 

DATES: This AD becomes effective April 

30, 2013. 

We must receive comments on this 

AD by May 30, 2013. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: U.S. Department of 

Transportation, 1200 New Jersey 

Avenue SE., West Building Ground 

Floor, Room W12–140, Washington, DC 

20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: 202–493–2251. 

For service information identified in 

this AD, contact BRP-Powertrain GmbH 

& Co KG, Welser Strasse 32, A–4623 

Gunskirchen, Austria, or go to: http:// 

www.FLYROTAX.com. You may view 

this service information at the FAA, 

Engine & Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803. For information on the 

availability of this material at the FAA, 

call 781–238–7125. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office 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 Operations office (phone: 

800–647–5527) is the same as the Mail 

address provided in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7779; fax: 781–238– 

7199; email: frederick.zink@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued EASA 

Emergency Airworthiness Directive 

2013–0055–E, dated March 6, 2013 

(referred to hereinafter as ‘‘the MCAI’’), 

to correct an unsafe condition for the 

specified products. The MCAI states: 

During a production test run, a noncompliance of the installed cylinder head 

assembly of cylinder No. 2 and 3 (2⁄3) was 

detected, which may result in a latent defect 

on a limited number of engines. The affected 

cylinder heads may not have been 

manufactured in accordance with the 

specification. 

This condition, if not detected and 

corrected, could lead to an oil leak in the 

intake channel in the area of the valve guide. 

The affected non-conforming cylinder heads 

may have small machined through holes, 

which can increase the oil consumption and 

can lead to oil starvation, possibly resulting 

in engine stoppage or in-flight engine 

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Federal Register / Vol. 78, No. 72 / Monday, April 15, 2013 / Rules and Regulations 22167 

shutdown and forced landing, with 

consequent risk of damage to the aeroplane 

and injury to occupants. 

You may obtain further information 

by examining the MCAI in the AD 

docket. 

Relevant Service Information 

BRP-Powertrain GmbH & Co KG has 

issued Rotax Aircraft Engines ASB No. 

ASB–912–062, Revision 1 and ASB– 

914–044, Revision 1 (combined into one 

document), dated March 5, 2013. The 

actions described in this service 

information are intended to correct the 

unsafe condition identified in the 

MCAI. 

FAA’s Determination and Requirements 

of This AD 

This product has been approved by 

the aviation authority of Austria, and is 

approved for operation in the United 

States. Pursuant to our bilateral 

agreement with the European 

Community, EASA has notified us of 

the unsafe condition described in the 

MCAI and service information 

referenced above. We are proposing this 

AD because we evaluated all 

information provided by EASA and 

determined the unsafe condition exists 

and is likely to exist or develop on other 

products of the same type design. This 

proposed AD would require a one-time 

visual inspection for excessive oil 

deposits or carbon deposits on the No. 

2 and No. 3 spark plug center and 

grounding electrodes, and if found, 

replacement of the cylinder head before 

further flight. Any excess indicates the 

cylinder head is not manufactured to 

proper specification and is leaking oil 

into the combustion chamber. 

FAA’s 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 of the short compliance 

time requirement. Therefore, we 

determined that notice and opportunity 

for public comment before issuing this 

AD are impracticable and that good 

cause exists for making this amendment 

effective in fewer than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2013–0263; 

Directorate Identifier 2013–NE–12–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 with FAA 

personnel concerning this AD. Using the 

search function of the Web site, anyone 

can find and read the comments in any 

of our dockets, including, if provided, 

the name of the individual who sent the 

comment (or signed the comment on 

behalf of an association, business, labor 

union, etc.). You may review the DOT’s 

complete Privacy Act Statement in the 

Federal Register published on April 11, 

2000 (65 FR 19477–78). 

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); and 

3. Will not affect intrastate aviation in 

Alaska to the extent that it justifies 

making a regulatory distinction, 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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this proposed AD and placed it in the 

AD docket. 

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: 

2013–07–12 BRP-Powertrain GmbH & Co. 

KG (formerly BRP-Rotax GmbH & Co 

KG, Bombardier-Rotax GmbH & Co. KG, 

and Bombardier-Rotax GmbH): 

Amendment 39–17416; Docket No. 

FAA–2013–0263; Directorate Identifier 

2013–NE–12–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective April 30, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the following BRP 

Powertrain GmbH & Co KG Rotax 

reciprocating engines: 

(1) Rotax 912 F2; 912 F3; and 912 F4, from 

serial number (S/N) 4,413,013 up to S/N 

4,413,017 inclusive. 

(2) Rotax 912 S2; 912 S3; and 912 S4, from 

S/N 4,924,468 up to S/N 4,924,491 inclusive. 

(3) Rotax 914 F2; 914 F3; and 914 F4, from 

S/N 4,421,156 up to S/N 4,421,169 inclusive. 

(d) Reason 

This AD was prompted by a report of 

certain No. 2 and No. 3 cylinder heads not 

manufactured to proper specification. The 

cylinder heads may have an oil leak in the 

intake channel in the area of the valve guide. 

There is the possibility that the heads have 

small machined through holes, which can 

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22168 Federal Register / Vol. 78, No. 72 / Monday, April 15, 2013 / Rules and Regulations 

increase the oil consumption. We are issuing 

this AD to prevent excessive oil 

consumption, which could result in an inflight engine shutdown, forced landing, and 

damage to the airplane. 

(e) Actions and Compliance 

Unless already done, do the following 

actions. 

(1) Within 5 flight hours or 20 days after 

the effective date of this AD, whichever 

occurs first, perform a one-time visual 

inspection of the center and grounding 

electrodes of both top and bottom spark plugs 

on cylinder 2, and cylinder 3, for unusual 

deposits (excessive carbon or oil). Any excess 

indicates the cylinder head is not 

manufactured to proper specification and is 

leaking oil into the combustion chamber. 

(2) Before further flight, replace cylinder 

heads found to be not manufactured to 

proper specification. 

(3) From the effective date of this AD, do 

not install any engine listed in the 

applicability of this AD on an airplane, 

unless the engine has been inspected and, 

depending on the findings, affected cylinder 

heads have been replaced as required by this 

AD. 

(f) Definitions 

For the purpose of this AD, unusual 

deposits (excessive carbon or oil) is when: 

(1) Carbon is a visual buildup of dark 

carbon deposits on the center and grounding 

electrodes as well as the immediate 

surrounding area, and 

(2) Excessive oil is a visual buildup 

indicated by the presence of oil on the center 

and grounding electrodes as well as the 

immediate surrounding area, giving a wet 

appearance. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs to this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(h) Related Information 

(1) For more information about this AD, 

contact Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7779; fax: 781–238–7199; 

email: frederick.zink@faa.gov. 

(2) Refer to European Aviation Safety 

Agency Emergency Airworthiness Directive 

2013–0055–E, dated March 6, 2013, and BRPPowertrain GmbH & Co KG Rotax Aircraft 

Engines Alert Service Bulletin No. ASB–912– 

062, Revision 1 and ASB–914–044, Revision 

1 (combined into one document), dated 

March 5, 2013, for related information. 

(3) For service information identified in 

this AD, contact BRP-Powertrain GmbH & Co 

KG, Welser Strasse 32, A–4623 Gunskirchen, 

Austria, or go to: http:// 

www.FLYROTAX.com. You may view this 

service information at the FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. For 

information on the availability of this 

material at the FAA, call 781–238–7125. 

(i) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

April 4, 2013. 

Colleen M. D’Alessandro, 

Manager, Engine & Propeller Directorate, 

Aircraft Certification Service. 

[FR Doc. 2013–08460 Filed 4–12–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1217; Directorate 

Identifier 2012–NE–39–AD; Amendment 39– 

17414; AD 2013–07–10] 

RIN 2120–AA64 

Airworthiness Directives; International 

Aero Engines AG Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

International Aero Engines AG (IAE), 

V2525–D5 and V2528–D5 turbofan 

engines, with a certain No. 4 bearing 

internal scavenge tube and a certain No. 

4 bearing external scavenge tube 

installed. This AD was prompted by a 

report of an engine under-cowl fire and 

commanded in-flight shutdown. This 

AD would require replacement of 

certain part number (P/N) No. 4 bearing 

internal scavenge tubes, and alignment 

checks of certain P/N No. 4 bearing 

external scavenge tubes. We are issuing 

this AD to prevent engine fire and 

damage to the airplane. 

DATES: This AD is effective May 20, 

2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of May 20, 2013. 

ADDRESSES: For service information 

identified in this AD, contact 

International Aero Engines, 628 Hebron 

Avenue, Suite 400, Glastonbury, CT 

06033; phone: 860–368–3823; fax: 860– 

755–6876. You may view this service 

information at the FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803. 

For information on the availability of 

this material at the FAA, call 781–238– 

7125. 

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 address for the 

Docket Office (phone: 800–647–5527) is 

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 FURTHER INFORMATION CONTACT: 

Martin Adler, Aerospace Engineer, 

Engine & Propeller Directorate, FAA, 12 

New England Executive Park, 

Burlington, MA 01803; phone: 781– 

238–7157; fax: 781–238–7199; email: 

martin.adler@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM published in the Federal 

Register on January 9, 2013 (78 FR 

1776). That NPRM proposed to require 

the replacement of all No. 4 bearing 

internal scavenge tubes, P/N 2A2074– 

01. That NPRM also proposed to require 

checking the alignment of the No. 4 

bearing external scavenge tube, P/N 

6A5254, and if it fails the check, 

proposed to require replacement of the 

external scavenge tube. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comment 

received on the proposal and the FAA’s 

response to the comment. 

Request To Change the Compliance 

Time 

The National Transportation Safety 

Board (NTSB) requested that the AD 

include a maximum number of 

allowable cycles for the No. 4 bearing 

internal scavenge tube. The NTSB is 

concerned that the proposed AD 

requirement to remove the internal 

scavenge tube at the next combustor 

module-level exposure has the potential 

to leave the tube installed indefinitely. 

We do not agree. Required 

maintenance provides sufficient 

limitations on the maximum number of 

cycles that the No. 4 bearing internal 

scavenge tube can experience. We did 

not change the AD. 

Conclusion 

We reviewed the relevant data, 

considered the comment received, and 

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