26124 Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations 

September 26, 2013, which was incorporated 

by reference in AD 2014–17–51. 

(iii) Bombardier Alert Service Bulletin 

A605–57–004, Revision 01, dated September 

26, 2013, including Appendices 1 and 2, 

dated September 26, 2013, which is 

incorporated by reference in AD 2014–03–17. 

(iv) Bombardier Alert Service Bulletin 

A604–57–004, Revision 02, dated January 22, 

2014, including Appendices 1 and 2, dated 

September 26, 2013, which was incorporated 

by reference in AD 2014–17–51. 

(m) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York Aircraft 

Certification Office (ACO), ANE–170, 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 ACO, send it to ATTN: 

Program Manager, Continuing Operational 

Safety, FAA, New York ACO, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 11590; 

telephone 516–228–7300; fax 516–794–5531. 

(i) 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. The AMOC 

approval letter must specifically reference 

this AD. 

(ii) AMOCs previously approved for AD 

2014–17–51 are acceptable for the 

corresponding requirements of this AD. 

(2) Contacting the Manufacturer: As of the 

effective date of this AD, for any requirement 

in this AD to obtain corrective actions from 

a manufacturer, the action must be 

accomplished using a method approved by 

the Manager, New York ACO, ANE–170, 

Engine and Propeller Directorate, FAA; or 

Transport Canada Civil Aviation (TCCA); or 

Bombardier, Inc.’s TCCA Design Approval 

Organization (DAO). If approved by the DAO, 

the approval must include the DAOauthorized signature. 

(n) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

Emergency Airworthiness Directive CF– 

2014–27R1, dated August 29, 2014, for 

related information. This MCAI may be 

found in the AD docket on the Internet at 

http://www.regulations.gov by searching for 

and locating Docket No. FAA–2015–3988. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (o)(6) and (o)(7) of this AD. 

(o) 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 this AD specifies otherwise. 

(3) The following service information was 

approved for IBR on June 6, 2016. 

(i) Bombardier Alert Service Bulletin 

A604–57–006, Revision 04, dated November 

12, 2014, including Appendices 1 and 2, 

dated September 26, 2013. 

(ii) Bombardier Alert Service Bulletin 

A605–57–004, Revision 04, dated November 

12, 2014, including Appendices 1 and 2, 

dated September 26, 2013. 

(4) The following service information was 

approved for IBR on November 12, 2014 (79 

FR 64088, October 28, 2014). 

(i) Bombardier Alert Service Bulletin 

A604–57–006, Revision 02, dated January 22, 

2014, including Appendices 1 and 2, dated 

September 26, 2013. 

(ii) Bombardier Alert Service Bulletin 

A605–57–004, Revision 02, dated January 22, 

2014, including Appendices 1 and 2, dated 

September 26, 2013. 

(5) The following service information was 

approved for IBR on March 6, 2014 (79 FR 

9389, February 19, 2014). 

(i) Bombardier Alert Service Bulletin 

A604–57–006, Revision 01, dated September 

26, 2013, including Appendices 1 and 2, 

dated September 26, 2013. 

(ii) Bombardier Alert Service Bulletin 

A605–57–004, Revision 01, dated September 

26, 2013, including Appendices 1 and 2, 

dated September 26, 2013. 

(6) For service information identified in 

this AD, contact Bombardier, Inc., 400 Coˆte 

Vertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–5000; fax 514– 

855–7401; email thd.crj@

aero.bombardier.com; Internet http://

www.bombardier.com. 

(7) You may view this 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. 

(8) 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/ibrlocations.html. 

Issued in Renton, Washington, on April 8, 

2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–08959 Filed 4–29–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1130; Directorate 

Identifier 2015–CE–008–AD; Amendment 

39–18492; AD 2015–09–04 R1] 

RIN 2120–AA64 

Airworthiness Directives; DG 

Flugzeugbau GmbH Gliders 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are revising Airworthiness 

Directive (AD) 2015–09–04 for DG 

Flugzeugbau GmbH Model DG–1000T 

gliders equipped with a Solo 

Kleinmotoren Model 2350 C engine. 

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 engine shaft 

failure and consequent propeller 

detachment. We are issuing this AD to 

require actions to address the unsafe 

condition on these products. 

DATES: This AD is effective June 6, 2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of June 6, 2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain other publication listed in 

this AD as of May 26, 2015 (80 FR 

25591, May 5, 2015). 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

1130; 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 20590. 

For service information identified in 

this AD, contact Solo Kleinmotoren 

GmbH, Postfach 600152, 71050 

Sindelfingen, Germany; telephone: +49 

7031 301–0; fax: +49 7031 301–136; 

email: aircraft@solo-germany.com; 

Internet: http://aircraft.solo-online.com 

and DG Flugzeugbau GmbH, Otto 

Lilienthal Weg 2/Am Flugplatz, 76646 

Bruchsal, Germany; telephone: +49 7251 

3020–0; fax: +49 7251 3020–200; email: 

wassenaar@dg-flugzeugbau.de; Internet: 

http://www.dg-flugzeugbau.de/ 

index.php?id=1329. You may view this 

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Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations 26125 

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 Docket No. FAA–2015– 

1130. 

FOR FURTHER INFORMATION CONTACT: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: jim.rutherford@

faa.gov. 

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 DG Flugzeugbau GmbH Model 

DG–1000T gliders equipped with a Solo 

Kleinmotoren Model 2350 C engine. The 

NPRM was published in the Federal 

Register on February 4, 2016 (81 FR 

5944), and proposed to revise AD 2015– 

09–04, Amendment 39–18150 (80 FR 

25591, May 5, 2015). 

Since we issued AD 2015–09–04, 

Amendment 39–18150 (80 FR 25591, 

May 5, 2015), new service information 

has been issued that includes 

procedures for replacement of the 

excenter axle-pulley assembly and 

installation of an elastomeric damper 

element between the propeller and 

upper pulley. This optional 

modification will allow resuming 

engine operation. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued AD No.: 2015– 

0052R1, dated November 19, 2015 

(referred to after this as ‘‘the MCAI’’), to 

correct the above-referenced unsafe 

condition for the specified products. 

The MCAI states: 

An occurrence of engine shaft failure and 

consequent propeller detachment was 

reported on a Solo 2350 C engine. 

This condition, if not corrected, could lead 

to additional cases of release of the propeller 

from the engine, possibly resulting in damage 

to the sailplane, or injury to persons on the 

ground. 

To address this unsafe condition, EASA 

issued Emergency AD 2013–0217–E to 

prohibit operation of the engine. That AD 

was later revised to introduce an optional 

modification, through Solo Kleinmotoren 

Service Bulletin (SB) 4603–14, to install a 

modified excenter axle-pulley assembly, 

allowing to resume operation of the engine. 

Since EASA AD 2013–0217R1 was issued, 

another occurrence of engine shaft failure 

and propeller detachment was reported on a 

Solo 2350 C engine which had been modified 

in accordance with Solo Kleinmotoren SB 

4603–14. 

Consequently, EASA issued Emergency AD 

2015–0052–E, which superseded AD 2013– 

0217R1, to prohibit operation of all Solo 2350 

C engines, including those engines which 

had been modified in accordance with Solo 

Kleinmotoren SB 4603–14. That AD also 

required a one-time inspection of the 

propeller shaft to detect cracks and the 

reporting of findings. 

Since that AD was issued, Solo 

Kleinmotoren GmbH developed modification 

drawing nb. 2031211–V2 available for in 

service application through Solo SB 4603–17 

and DG Flugzeugbau GmbH developed 

modifications drawing nb. 10 M 067, 

available for in service application through 

DG Flugzeugbau Technical Note (TN) 1000/ 

26 which include replacement of excenter 

axle-pulley assembly and installation of an 

elastomeric damper element between the 

propeller and upper pulley. 

This AD is revised to introduce optional 

modifications to allow resuming operation of 

an engine. 

You may examine the MCAI on the 

Internet at https://www.regulations.gov/ 

#!documentDetail;D=FAA-2015-1130- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (81 

FR 5944, February 4, 2016) 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 (81 FR 5944, 

February 4, 2016) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (81 FR 5944, 

February 4, 2016). 

Related Service Information Under 1 

CFR 51 

We reviewed Solo Kleinmotoren 

GmbH Anleitung zur Inspektion 

(English translation: Inspection 

Instruction), Nr. 4603–1, Ausgabe 

(English translation: Dated) March 26, 

2015; Solo Kleinmotoren GmbH 

Technische Mitteilung (English 

translation: Service Bulletin) Nr. 4603– 

17, Ausgabe (English translation: Dated) 

July 15, 2015; and DG Flugzeugbau 

GmbH Technical note No. 1000/26, 

dated September 23, 2015, with 10M072 

titled Propellermontage nach TM 1000– 

26 (English translation: Propeller 

assembly TN 1000–26), dated July 14, 

2015. Solo Kleinmotoren GmbH 

Anleitung zur Inspektion (English 

translation: Inspection Instruction), Nr. 

4603–1, Ausgabe (English translation: 

Dated) March 26, 2015, describes 

procedures for inspecting the propeller 

shaft for cracking and reporting the 

results to the manufacturer. Solo 

Kleinmotoren GmbH Techniseche 

Mitteilung (English translation: Service 

Bulletin) Nr. 4603–17, Ausgabe (English 

translation: Dated) July 15, 2015, 

describes procedures for replacement of 

the excenter axle-pulley assembly. DG 

Flugzeugbau GmbH Technical note No. 

1000/26, dated September 23, 2015, 

describes procedures for removing the 

excenter axle-pulley assembly and 

sending it to Solo Kleinmotoren GmbH 

for modification with a new rear 

bearing, axle, and elastomeric damper 

element. This service information is 

reasonably available because the 

interested parties have access to it 

through their normal course of business 

or by the means identified in the 

ADDRESSES section. 

Costs of Compliance 

We estimate that this AD will affect 2 

products of U.S. registry. We also 

estimate that it will take about .5 workhour per product to comply with the 

basic operational limitation requirement 

of this AD. The average labor rate is $85 

per work-hour. 

Based on these figures, we estimate 

the cost of this portion of this AD on 

U.S. operators to be $85, or $42.50 per 

product. 

We also estimate that it will take 

about 1.5 work-hours per product to 

comply with the basic axle inspection 

(remove, inspect, and reinstall) 

requirement of this AD. The average 

labor rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of this portion of this AD on 

U.S. operators to be $255, or $127.50 per 

product. 

We also estimate that it will take 

about 2 work-hours per product to 

comply with the optional axle with 

drive belt pulley unit replacement and 

engine test run of this AD. The average 

labor rate is $85 per work-hour. 

Required parts will cost about $100 per 

product. 

Based on these figures, we estimate 

the cost of this optional AD action on 

U.S. operators to be $540, or $270 per 

product. 

We also estimate that it will take 

about .5 work-hour per product to 

comply with the removal of the 

operational limitation requirement after 

doing the optional replacement of this 

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26126 Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations 

AD. The average labor rate is $85 per 

work-hour. 

Based on these figures, we estimate 

the cost of this AD action on U.S. 

operators to be $85, or $42.50 per 

product. 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a current valid 

OMB control number. The control 

number for the collection of information 

required by this AD is 2120–0056. The 

paperwork cost associated with this AD 

has been detailed in the Costs of 

Compliance section of this document 

and includes time for reviewing 

instructions, as well as completing and 

reviewing the collection of information. 

Therefore, all reporting associated with 

this AD is mandatory. Comments 

concerning the accuracy of this burden 

and suggestions for reducing the burden 

should be directed to the FAA at 800 

Independence Ave. SW., Washington, 

DC 20591. ATTN: Information 

Collection Clearance Officer, AES–200. 

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–2015– 

1130; 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 

removing Amendment 39–18150 (80 FR 

25591, May 5, 2015) and adding the 

following new AD: 

2015–09–04 R1 DG Flugzeugbau GmbH: 

Amendment 39–18492; Docket No. 

FAA–2015–1130; Directorate Identifier 

2015–CE–008–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective June 6, 2016. 

(b) Affected ADs 

This AD replaces AD 2015–09–04, 

Amendment 39–18150 (80 FR 25591, May 5, 

2015) (‘‘AD 2015–09–04’’). 

(c) Applicability 

This AD applies to DG Flugzeugbau GmbH 

Model DG–1000T gliders, all serial numbers, 

that are: 

(1) Equipped with a Solo Kleinmotoren 

Model 2350 C engine; and 

(2) Certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 72: Engine. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

issued by the aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as engine 

shaft failure with consequent propeller 

detachment. We are issuing this AD to 

prevent failure of the engine shaft with 

consequent propeller detachment, which 

could result in damage to the glider or injury 

of persons on the ground. 

(f) Actions and Compliance 

Unless already done, do the following 

actions: 

(1) As of November 25, 2013 (the effective 

date retained from AD 2013–22–14, 

Amendment 39–17646 (78 FR 65869, 

November 4, 2013)), do not operate the 

engine unless the engine is modified 

following instructions that are FAA-approved 

specifically for this AD. 

(2) Modification of an engine following the 

instructions in Solo Kleinmotoren Service 

Bulletin 4603–14, dated April 28, 2014, is not 

an acceptable modification to comply with 

paragraph (f)(1) of this AD. 

(3) As of May 26, 2015 (the effective date 

retained from AD 2015–09–04), place a copy 

of this AD into the Limitations section of the 

aircraft flight manual (AFM). 

(4) Within the next 30 days after May 26, 

2015 (the effective date retained from AD 

2015–09–04), do a one-time inspection 

(magnetic particle or dye penetrant) of the 

propeller shaft following Solo Kleinmotoren 

GmbH Anleitung zur Inspektion (English 

translation: Inspection Instruction), Nr. 

4603–1, Ausgabe (English translation: dated) 

March 26, 2015. 

Note 1 to paragraph (f)(4) of this AD: This 

service information contains German to 

English translation. The EASA used the 

English translation in referencing the 

document. For enforceability purposes, we 

will refer to the Solo Kleinmotoren service 

information as it appears on the document. 

(5) Within the next 30 days after May 26, 

2015 (the effective date retained from AD 

2015–09–04), report the results of the 

inspection required in paragraph (f)(4) of this 

AD to Solo Kleinmotoren GmbH. Include the 

serial number of the engine and the 

operational time since change of the axle in 

your report. You may find contact 

information for Solo Kleinmotoren GmbH in 

paragraph (i)(5) of this AD. 

(6) At any time after June 6, 2016 (the 

effective date of this AD), you may modify 

the engine following Solo Kleinmotoren 

GmbH Techniseche Mitteilung (English 

translation: Service Bulletin) Nr. 4603–17, 

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Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations 26127 

Ausgabe (English translation: Dated) July 15, 

2015; and DG Flugzeugbau GmbH Technical 

note No. 1000/26, dated September 23, 2015, 

with 10M072 titled Propellermontage nach 

TM 1000–26 (English translation: Propeller 

assembly TN 1000–26), dated July 14, 2015. 

This modification allows engine operation. 

Note 2 to paragraph (f)(6) of this AD: This 

service information contains German to 

English translation. The EASA used the 

English translation in referencing the 

document. For enforceability purposes, we 

will refer to the Solo Kleinmotoren service 

information and the DG Flugzeugbau GmbH 

as it appears on the document. 

(7) Before further flight after doing the 

modification allowed in (f)(6) of this AD, 

remove the AD placed into the Limitations 

section of the AFM as required in paragraph 

(f)(3) of this AD. 

(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: Jim Rutherford, Aerospace Engineer, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 329– 

4090; email: jim.rutherford@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. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No.: 2015–0052R1, dated 

November 19, 2015, for related information. 

You may examine the MCAI on the Internet 

at https://www.regulations.gov/#!document

Detail;D=FAA-2015-1130-0002. 

(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. 

(3) The following service information was 

approved for IBR on June 6, 2016. 

(i) Solo Kleinmotoren GmbH Techniseche 

Mitteilung (English translation: Service 

Bulletin) Nr. 4603–17, Ausgabe (English 

translation: Dated) July 15, 2015. 

Note 3 to paragraphs (i)(3)(i) and (i)(3)(ii) 

of this AD: This service information contains 

German to English translation. The EASA 

used the English translation in referencing 

the document. For enforceability purposes, 

we will refer to the Solo Kleinmotoren 

service information and the DG Flugzeugbau 

GmbH as it appears on the document. 

(ii) DG Flugzeugbau GmbH Technical note 

No. 1000/26, dated September 23, 2015, with 

10M072 titled Propellermontage nach TM 

1000–26 (English translation: Propeller 

assembly TN 1000–26), dated July 14, 2015. 

(4) The following service information was 

approved for IBR on May 26, 2015 (80 FR 

25591, May 5, 2015). 

(i) Solo Kleinmotoren GmbH Anleitung zur 

Inspektion (English translation: Inspection 

Instruction), Nr. 4603–1, Ausgabe (English 

translation: Dated) March 26, 2015. 

Note 4 to paragraph (i)(4)(i) of this AD: 

This service information contains German to 

English translation. The EASA used the 

English translation in referencing the 

document. For enforceability purposes, we 

will refer to the Solo Kleinmotoren service 

information as it appears on the document. 

(ii) Reserved. 

(5) For service information identified in 

this AD, contact Solo Kleinmotoren GmbH, 

Postfach 600152, 71050 Sindelfingen, 

Germany; telephone: +49 7031 301–0; fax: 

+49 7031 301–136; email: aircraft@sologermany.com; Internet: http://aircraft.soloonline.com/com. 

(6) You may view this service information 

at 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–2015–1130. 

(7) 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/ibrlocations.html. 

Issued in Kansas City, Missouri, on April 

11, 2016. 

Melvin Johnson, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2016–08961 Filed 4–29–16; 8:45 am] 

BILLING CODE 4910–13–P 

RAILROAD RETIREMENT BOARD 

20 CFR Part 356 

RIN 3220–AB68 

Civil Monetary Penalty Inflation 

Adjustment 

AGENCY: Railroad Retirement Board. 

ACTION: Interim final rule. 

SUMMARY: As required by Section 701 of 

the Bipartisan Budget Act of 2015, 

entitled the Federal Civil Penalties 

Inflation Adjustment Act Improvements 

Act of 2015, the Railroad Retirement 

Board (Board) hereby amends its 

regulations to provide for adjustments 

in the minimum and maximum amounts 

of civil monetary penalties under the 

Board’s jurisdiction. The amendment 

will increase the amount of penalties to 

adjust for inflation since the Board last 

adjusted its penalty amounts, and will 

provide the formula to be used for 

required annual adjustments in the 

penalty amounts. 

DATES: Effective August 1, 2016. 

Comments must be received on or 

before July 1, 2016. 

ADDRESSES: You may submit comments, 

identified by RIN 3220–AB68, by any of 

the following methods: 

1. Internet—Send comments via email 

to SecretarytotheBoard@rrb.gov. 

2. Fax—(312) 751–3336. 

3. Mail—Secretary to the Board, 

Railroad Retirement Board, 844 N. Rush 

Street, Chicago, Illinois 60611–2092. 

Do not submit the same comments 

multiple times or by more than one 

method. Regardless of which method 

you choose, please state that your 

comments refer to RIN 3220–AB68. 

Caution: You should be careful to 

include in your comments only 

information that you wish to make 

publicly available as comments are 

posted without change, with any 

personal information provided. The 

Board strongly urges you not to include 

in your comments any personal 

information, such as Social Security 

numbers or medical information. 

FOR FURTHER INFORMATION CONTACT: 

Marguerite P. Dadabo, Assistant General 

Counsel, Railroad Retirement Board, 

844 North Rush Street, Chicago, IL 

60611–2092, (312) 751–4945, TTD (312) 

751–4701. 

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