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

36911 

Vol. 80, No. 124 

Monday, June 29, 2015 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0951; Directorate 

Identifier 2015–CE–007–AD; Amendment 

39–18190; AD 2015–13–03] 

RIN 2120–AA64 

Airworthiness Directives; 

Przedsiebiorstwo DoswiadczalnoProdukcyjne Szybownictwa ‘‘PZLBielsko’’ Sailplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Przedsiebiorstwo DoswiadczalnoProdukcyjne Szybownictwa ‘‘PZLBielsko’’ Model SZD–50–3 ‘‘Puchacz’’ 

sailplanes. 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 

detachment of the rudder cable fitting 

block from the fuselage. We are issuing 

this AD to require actions to address the 

unsafe condition on these products. 

DATES: This AD is effective August 3, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of August 3, 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– 

0951; 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 Allstar PZL Glider, Sp. 

z o. o., ul. Cieszynska 325, 43–300 

Bielsko-Biala, Poland; telephone: +48 33 

812 50 26; fax: +48 33 812 37 39; email: 

techsupport@szd.com.pl; Internet: 

http://szd.com.pl/en/products/szd-50-3- 

puchacz. 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–2015–0951. 

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 to add an AD that would apply 

to all Przedsiebiorstwo DoswiadczalnoProdukcyjne Szybownictwa ‘‘PZLBielsko’’ Model SZD–50–3 ‘‘Puchacz’’ 

sailplanes. The NPRM was published in 

the Federal Register on April 17, 2015 

(80 FR 21191). 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: 

An occurrence was reported involving a 

SZD–50–3 ‘‘Puchacz’’ sailplane, where a 

rudder cable fitting block, located in the 

forward part of the fuselage, detached after 

application of a high load on the steering 

pedal during spin recovery operation. 

Subsequent investigations determined that 

the failure was either caused by a 

manufacturing deficiency or originated by a 

crack. 

This condition, if not detected and 

corrected, could lead to further cases of 

rudder cable fitting block detachment, 

resulting in reduced control of the sailplane. 

To address this unsafe condition, Allstar 

PZL issued Service Bulletin (SB) No. BE– 

063/SZD–50–3/2014, to provide inspection 

and reinforcement instructions. 

For the reasons described above, this AD 

requires accomplishment of a one-time 

inspection of both (right hand (RH) and left 

hand (LH)) rudder cable fitting blocks to 

verify proper attachment to the fuselage shell 

and, depending on finding(s), a repair. This 

AD also requires reinforcement of the 

affected structural area. 

The MCAI can be found in the AD 

docket on the Internet at: http://

www.regulations.gov/

#!documentDetail;D=FAA-2015-0951- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (80 

FR 21191, April 17, 2015) 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 (80 FR 

21191, April 17, 2015) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (80 FR 21191, 

April 17, 2015). 

Related Service Information Under 1 

CFR Part 51 

We reviewed Allstar PZL Glider 

Service Bulletin BE–063/SZD–50–3/

2014 ‘‘Puchacz’’, dated December 14, 

2014. The service bulletin describes 

procedures for inspecting the area 

around the left-hand and right-hand 

rudder cable fitting blocks for cracks 

and detachment and making all 

necessary repairs. 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 of this AD. 

Costs of Compliance 

We estimate that this AD will affect 5 

products of U.S. registry. We also 

estimate that it will take about 1 workhour per product to comply with the 

inspection requirement of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of the inspection requirement of 

this AD on U.S. operators to be $425, or 

$85 per product. 

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36912 Federal Register / Vol. 80, No. 124 / Monday, June 29, 2015 / Rules and Regulations 

In addition, we estimate that it will 

take about 2 work-hours per product to 

comply with the modification 

requirement of this AD and will require 

parts costing $100, for a cost of $270 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–2015– 

0951; 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: 

2015–13–03 Przedsiebiorstwo 

Doswiadczalno-Produkcyjne 

Szybownictwa ‘‘PZL-Bielsko’’: 

Amendment 39–18190; Docket No. 

FAA–2015–0951; Directorate Identifier 

2015–CE–007–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective August 3, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Przedsiebiorstwo 

Doswiadczalno-Produkcyjne Szybownictwa 

‘‘PZL-Bielsko’’ Model SZD–50–3 ‘‘Puchacz’’ 

sailplanes, all serial numbers, certificated in 

any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

(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 detachment 

of the rudder cable fitting block from the 

fuselage. We are issuing this AD to prevent 

detachment of the rudder cable fitting block 

from the fuselage, which if not detected and 

corrected, could result in reduced control. 

(f) Actions and Compliance 

Unless already done, do the actions in 

paragraphs (f)(1) through (f)(3) of this AD: 

(1) Within 30 days after August 13, 2015 

(the effective date of this AD), inspect the 

area around both the left-hand (LH) and the 

right-hand (RH) rudder cable fitting blocks 

following paragraph 3.1. of the 

INSTRUCTIONS section in Allstar PZL 

Glider Service Bulletin BE–063/SZD–50–3/

2014 ‘‘Puchacz’’, dated December 14, 2014. 

(2) If, during the inspection required in 

paragraph (f)(1) of this AD, any crack or 

fitting block detachment is found, before 

further flight, repair and reinforce the 

attachment of both the LH and RH rudder 

cable fitting blocks. Do this repair and 

reinforcement following paragraph 3.2. of the 

INSTRUCTIONS section in Allstar PZL 

Glider Service Bulletin BE–063/SZD–50–3/

2014 ‘‘Puchacz’’, dated December 14, 2014. 

(3) Unless already done following the 

requirement in paragraph (f)(2) of this AD, 

within the next 12 months after August 3, 

2015 (the effective date of this AD), reinforce 

the attachment of both the LH and RH rudder 

cable fitting blocks. Do this reinforcement 

following paragraph 3.2. of the 

INSTRUCTIONS section in Allstar PZL 

Glider Service Bulletin BE–063/SZD–50–3/

2014 ‘‘Puchacz’’, dated December 14, 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: 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. Before 

using any approved AMOC on any sailplane 

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 European Aviation Safety 

Agency (EASA) AD No.: 2015–0046, dated 

March 16, 2015, for related information. You 

may examine the MCAI on the Internet at: 

http://www.regulations.gov/

#!documentDetail;D=FAA-2015-0951-0002. 

(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) Allstar PZL Glider Service Bulletin BE– 

063/SZD–50–3/2014 ‘‘Puchacz’’, dated 

December 14, 2014. 

(ii) Reserved. 

(3) For PZL-Bielsko service information 

identified in this AD, contact Allstar PZL 

Glider, Sp. z o. o., ul. Cieszynska 325, 43– 

300 Bielsko-Biala, Poland; telephone: +48 33 

812 50 26; fax: +48 33 812 37 39; email: 

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Federal Register / Vol. 80, No. 124 / Monday, June 29, 2015 / Rules and Regulations 36913 

1We originally adopted the Filer Manual on April 

1, 1993, with an effective date of April 26, 1993. 

Release No. 33–6986 (April 1, 1993) [58 FR 18638]. 

We implemented the most recent update to the Filer 

Manual on May 11, 2015. See Release No. 33–9773 

(May 26, 2015) [80 FR 29942]. 

2See Rule 301 of Regulation S–T (17 CFR 

232.301). 

3See Release No. 33–9773 in which we 

implemented EDGAR Release 15.1.1. For additional 

history of Filer Manual rules, please see the cites 

therein. 

4 5 U.S.C. 553(b). 

5 5 U.S.C. 601–612. 

techsupport@szd.com.pl; Internet: http://

szd.com.pl/en/products/szd-50-3-puchacz. 

(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–2015–0951. 

(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/ibrlocations.html 

Issued in Kansas City, Missouri, on June 

18, 2015. 

William Schinstock, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–15620 Filed 6–26–15; 8:45 am] 

BILLING CODE 4910–13–P 

SECURITIES AND EXCHANGE 

COMMISSION 

17 CFR Part 232 

[Release Nos. 33–9849; 34–75242; 39–2504; 

IC–31680] 

Adoption of Updated EDGAR Filer 

Manual 

AGENCY: Securities and Exchange 

Commission. 

ACTION: Final rule. 

SUMMARY: The Securities and Exchange 

Commission (the Commission) is 

adopting revisions to the Electronic Data 

Gathering, Analysis, and Retrieval 

System (EDGAR) Filer Manual and 

related rules to reflect updates to the 

EDGAR system. The updates are being 

made primarily to add new submission 

form types N–CR and N–CR/A for 

Current Report of Money Market Fund 

Material Events; update submission 

form types ABS–15G and ABS–15G/A 

for Asset-backed securities reporting 

based on Rule 15Ga-2; no longer display 

OMB expiration date on submission 

form types 13F and 13H; no longer 

provide support for the 2013 US GAAP 

financial reporting and 2013 EXCH 

taxonomies; documentation only 

corrections to Chapter 3, ‘‘Index to 

Forms,’’ of the ‘‘EDGAR Filer Manual, 

Volume II: EDGAR Filing,’’ which 

include adding submission types 

8–K12B and 8–K12B/A to Table 3–3, 

‘‘Securities Exchange Act—Registration 

and Report Submission Types Accepted 

by EDGAR’’; and documentation only 

changes to ‘‘EDGAR Filer Manual, 

Volume II: EDGAR Filing’’ for Section 

508 compliance. The EDGAR system is 

scheduled to be upgraded to support 

this functionality on June 15, 2015. 

DATES: Effective June 29, 2015. The 

incorporation by reference of the 

EDGAR Filer Manual is approved by the 

Director of the Federal Register as of 

June 29, 2015. 

FOR FURTHER INFORMATION CONTACT: In 

the Division of Corporate Finance, for 

questions concerning Form ABS–15G, 

contact Heather Mackintosh at (202) 

551–8111, in the Division of Investment 

Management, for questions concerning 

Form N–CR, contact Heather Fernandez 

at (202) 551–6708, and in the Office of 

Information Technology, contact 

Tammy Borkowski at (202) 551–7208. 

SUPPLEMENTARY INFORMATION: We are 

adopting an updated EDGAR Filer 

Manual, Volume II. The Filer Manual 

describes the technical formatting 

requirements for the preparation and 

submission of electronic filings through 

the EDGAR system.1 It also describes 

the requirements for filing using 

EDGARLink Online and the Online 

Forms/XML Web site. 

The revisions to the Filer Manual 

reflect changes within Volume II 

entitled EDGAR Filer Manual, Volume 

II: ‘‘EDGAR Filing,’’ Version 32 (June 

2015). The updated manual will be 

incorporated by reference into the Code 

of Federal Regulations. 

The Filer Manual contains all the 

technical specifications for filers to 

submit filings using the EDGAR system. 

Filers must comply with the applicable 

provisions of the Filer Manual in order 

to assure the timely acceptance and 

processing of filings made in electronic 

format.2 Filers may consult the Filer 

Manual in conjunction with our rules 

governing mandated electronic filing 

when preparing documents for 

electronic submission.3

The EDGAR system will be upgraded 

to Release 15.2 on June 15, 2015 and 

will introduce the following changes: 

EDGAR will be updated to add new 

submission form types N–CR and 

N–CR/A to EDGARLink Online. These 

new submission form types can be 

accessed by selecting the ‘EDGARLink 

Online Form Submission’ link on the 

EDGAR Filing Web site. Additionally, 

filers can construct XML submissions 

for these submission form types by 

following the ‘‘EDGARLink Online XML 

Technical Specification’’ document 

available on the SEC’s Public Web site 

(http://www.sec.gov/info/edgar.shtml). 

Submission form types ABS–15G and 

ABS–15G/A will be updated based on 

final Rule 15Ga–2. 

The OMB expiration date will no 

longer be displayed on submission form 

types 13F–HR, 13F–HR/A, 13F–NT, 

13F–NT/A, 13H, 13H–A, 13H–Q, 

13H–I, 13H–T, and 13H–R. 

EDGAR will no longer provide 

support for the US–GAAP–2013 and 

EXCH–2013 taxonomies. Please see 

http://www.sec.gov/info/edgar/

edgartaxonomies.shtml for a complete 

listing of supported standard 

taxonomies. 

Documentation only corrections were 

made to Chapter 3, ‘‘Index to Forms,’’ of 

the ‘‘EDGAR Filer Manual, Volume II: 

EDGAR Filing,’’ which include adding 

submission types 8–K12B and 

8–K12B/A to Table 3–3, ‘‘Securities 

Exchange Act—Registration and Report 

Submission Types Accepted by 

EDGAR.’’ 

Documentation only changes were 

made to ‘‘EDGAR Filer Manual, Volume 

II: EDGAR Filing’’ for Section 508 

compliance. 

Along with the adoption of the Filer 

Manual, we are amending Rule 301 of 

Regulation S–T to provide for the 

incorporation by reference into the Code 

of Federal Regulations of today’s 

revisions. This incorporation by 

reference was approved by the Director 

of the Federal Register in accordance 

with 5 U.S.C. 552(a) and 1 CFR part 51. 

The updated EDGAR Filer Manual 

will be available for Web site viewing 

and printing; the address for the Filer 

Manual is http://www.sec.gov/info/

edgar.shtml. You may also obtain paper 

copies of the EDGAR Filer Manual from 

the following address: Public Reference 

Room, U.S. Securities and Exchange 

Commission, 100 F Street, NE., 

Washington, DC 20549, on official 

business days between the hours of 

10:00 a.m. and 3:00 p.m. 

Since the Filer Manual and the 

corresponding rule changes relate solely 

to agency procedures or practice, 

publication for notice and comment is 

not required under the Administrative 

Procedure Act (APA).4 It follows that 

the requirements of the Regulatory 

Flexibility Act 5 do not apply. 

The effective date for the updated 

Filer Manual and the rule amendments 

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