80 FR 36911 - Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa “PZL-Bielsko” Sailplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 124 (June 29, 2015)

Page Range		36911-36913
FR Document		2015-15620

We are adopting a new airworthiness directive (AD) for all Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa ``PZL-Bielsko'' 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.

Federal Register, Volume 80 Issue 124 (Monday, June 29, 2015)

[Federal Register Volume 80, Number 124 (Monday, June 29, 2015)]
[Rules and Regulations]
[Pages 36911-36913]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-15620]



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Rules and Regulations
                                                Federal Register
________________________________________________________________________

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.

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

[[Page 36911]]



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 Doswiadczalno-
Produkcyjne Szybownictwa ``PZL-Bielsko'' 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 Doswiadczalno-Produkcyjne Szybownictwa ``PZL-Bielsko'' 
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 
Doswiadczalno-Produkcyjne Szybownictwa ``PZL-Bielsko'' 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 work-hour 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.

[[Page 36912]]

    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

0
1. The authority citation for part 39 continues to read as follows:

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


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  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:

[[Page 36913]]

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/ibr-locations.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

36911

Rules and Regulations Federal Register
Vol. 80, No. 124

Monday, June 29, 2015

This section of the FEDERAL REGISTER Room W12–140, 1200 New Jersey inspection of both (right hand (RH) and left
contains regulatory documents having general Avenue SE., Washington, DC 20590. hand (LH)) rudder cable fitting blocks to
applicability and legal effect, most of which For service information identified in verify proper attachment to the fuselage shell
are keyed to and codified in the Code of this AD, contact Allstar PZL Glider, Sp. and, depending on finding(s), a repair. This
Federal Regulations, which is published under z o. o., ul. Cieszynska 325, 43–300 AD also requires reinforcement of the
50 titles pursuant to 44 U.S.C. 1510. affected structural area.
Bielsko-Biala, Poland; telephone: +48 33
812 50 26; fax: +48 33 812 37 39; email: The MCAI can be found in the AD
The Code of Federal Regulations is sold by
the Superintendent of Documents. Prices of techsupport@szd.com.pl; Internet: docket on the Internet at: http://
new books are listed in the first FEDERAL http://szd.com.pl/en/products/szd-50-3- www.regulations.gov/
REGISTER issue of each week. puchacz. You may view this referenced #!documentDetail;D=FAA-2015-0951-
service information at the FAA, Small 0002.
Airplane Directorate, 901 Locust, Comments
DEPARTMENT OF TRANSPORTATION Kansas City, Missouri 64106. For
information on the availability of this We gave the public the opportunity to
Federal Aviation Administration material at the FAA, call (816) 329– participate in developing this AD. We
4148. It is also available on the Internet received no comments on the NPRM (80
14 CFR Part 39 at http://www.regulations.gov by FR 21191, April 17, 2015) or on the
[Docket No. FAA–2015–0951; Directorate searching for and locating Docket No. determination of the cost to the public.
Identifier 2015–CE–007–AD; Amendment FAA–2015–0951. Conclusion
39–18190; AD 2015–13–03] FOR FURTHER INFORMATION CONTACT: Jim
Rutherford, Aerospace Engineer, FAA, We reviewed the relevant data and
RIN 2120–AA64 determined that air safety and the
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106; public interest require adopting the AD
Airworthiness Directives; as proposed except for minor editorial
Przedsiebiorstwo Doswiadczalno- telephone: (816) 329–4165; fax: (816)
329–4090; email: jim.rutherford@ changes. We have determined that these
Produkcyjne Szybownictwa ‘‘PZL- minor changes:
Bielsko’’ Sailplanes faa.gov.
• Are consistent with the intent that
SUPPLEMENTARY INFORMATION: was proposed in the NPRM (80 FR
AGENCY: Federal Aviation
Administration (FAA), Department of Discussion 21191, April 17, 2015) for correcting the
Transportation (DOT). unsafe condition; and
We issued a notice of proposed • Do not add any additional burden
ACTION: Final rule. rulemaking (NPRM) to amend 14 CFR upon the public than was already
part 39 to add an AD that would apply proposed in the NPRM (80 FR 21191,
SUMMARY: We are adopting a new to all Przedsiebiorstwo Doswiadczalno-
airworthiness directive (AD) for all April 17, 2015).
Produkcyjne Szybownictwa ‘‘PZL-
Przedsiebiorstwo Doswiadczalno- Bielsko’’ Model SZD–50–3 ‘‘Puchacz’’ Related Service Information Under 1
Produkcyjne Szybownictwa ‘‘PZL- sailplanes. The NPRM was published in CFR Part 51
Bielsko’’ Model SZD–50–3 ‘‘Puchacz’’ the Federal Register on April 17, 2015
sailplanes. This AD results from We reviewed Allstar PZL Glider
(80 FR 21191). The NPRM proposed to Service Bulletin BE–063/SZD–50–3/
mandatory continuing airworthiness correct an unsafe condition for the
information (MCAI) issued by an 2014 ‘‘Puchacz’’, dated December 14,
specified products and was based on 2014. The service bulletin describes
aviation authority of another country to mandatory continuing airworthiness
identify and correct an unsafe condition procedures for inspecting the area
information (MCAI) originated by an around the left-hand and right-hand
on an aviation product. The MCAI aviation authority of another country.
describes the unsafe condition as rudder cable fitting blocks for cracks
The MCAI states: and detachment and making all
detachment of the rudder cable fitting
block from the fuselage. We are issuing An occurrence was reported involving a necessary repairs. This service
this AD to require actions to address the SZD–50–3 ‘‘Puchacz’’ sailplane, where a information is reasonably available
rudder cable fitting block, located in the because the interested parties have
unsafe condition on these products. forward part of the fuselage, detached after access to it through their normal course
DATES: This AD is effective August 3, application of a high load on the steering of business or by the means identified
2015. pedal during spin recovery operation.
Subsequent investigations determined that in the ADDRESSES section of this AD.
The Director of the Federal Register
approved the incorporation by reference the failure was either caused by a Costs of Compliance
manufacturing deficiency or originated by a
of a certain publication listed in the AD crack. We estimate that this AD will affect 5
as of August 3, 2015. This condition, if not detected and products of U.S. registry. We also
ADDRESSES: You may examine the AD corrected, could lead to further cases of estimate that it will take about 1 work-
mstockstill on DSK4VPTVN1PROD with RULES

docket on the Internet at http:// rudder cable fitting block detachment, hour per product to comply with the
www.regulations.gov by searching for resulting in reduced control of the sailplane. inspection requirement of this AD. The
and locating Docket No. FAA–2015– To address this unsafe condition, Allstar
PZL issued Service Bulletin (SB) No. BE–
average labor rate is $85 per work-hour.
0951; or in person at Document 063/SZD–50–3/2014, to provide inspection Based on these figures, we estimate
Management Facility, U.S. Department and reinforcement instructions. the cost of the inspection requirement of
of Transportation, Docket Operations, For the reasons described above, this AD this AD on U.S. operators to be $425, or
M–30, West Building Ground Floor, requires accomplishment of a one-time $85 per product.

VerDate Sep<11>2014 17:11 Jun 26, 2015 Jkt 235001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\29JNR1.SGM 29JNR1

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

In addition, we estimate that it will other information. The street address for Glider Service Bulletin BE–063/SZD–50–3/
take about 2 work-hours per product to the Docket Office (telephone (800) 647– 2014 ‘‘Puchacz’’, dated December 14, 2014.
comply with the modification 5527) is in the ADDRESSES section. (2) If, during the inspection required in
paragraph (f)(1) of this AD, any crack or
requirement of this AD and will require Comments will be available in the AD fitting block detachment is found, before
parts costing $100, for a cost of $270 per docket shortly after receipt. further flight, repair and reinforce the
product. attachment of both the LH and RH rudder
List of Subjects in 14 CFR Part 39
cable fitting blocks. Do this repair and
Authority for This Rulemaking Air transportation, Aircraft, Aviation reinforcement following paragraph 3.2. of the
Title 49 of the United States Code safety, Incorporation by reference, INSTRUCTIONS section in Allstar PZL
specifies the FAA’s authority to issue Safety. Glider Service Bulletin BE–063/SZD–50–3/
rules on aviation safety. Subtitle I, 2014 ‘‘Puchacz’’, dated December 14, 2014.
Adoption of the Amendment (3) Unless already done following the
section 106, describes the authority of
Accordingly, under the authority requirement in paragraph (f)(2) of this AD,
the FAA Administrator. ‘‘Subtitle VII: within the next 12 months after August 3,
Aviation Programs,’’ describes in more delegated to me by the Administrator,
2015 (the effective date of this AD), reinforce
detail the scope of the Agency’s the FAA amends 14 CFR part 39 as the attachment of both the LH and RH rudder
authority. follows: cable fitting blocks. Do this reinforcement
We are issuing this rulemaking under following paragraph 3.2. of the
the authority described in ‘‘Subtitle VII, PART 39—AIRWORTHINESS INSTRUCTIONS section in Allstar PZL
Part A, Subpart III, section 44701: DIRECTIVES Glider Service Bulletin BE–063/SZD–50–3/
General requirements.’’ Under that 2014 ‘‘Puchacz’’, dated December 14, 2014.
■ 1. The authority citation for part 39
section, Congress charges the FAA with continues to read as follows: (g) Other FAA AD Provisions
promoting safe flight of civil aircraft in The following provisions also apply to this
air commerce by prescribing regulations Authority: 49 U.S.C. 106(g), 40113, 44701.
AD:
for practices, methods, and procedures § 39.13 [Amended] (1) Alternative Methods of Compliance
the Administrator finds necessary for (AMOCs): The Manager, Standards Office,
safety in air commerce. This regulation ■ 2. The FAA amends § 39.13 by adding FAA, has the authority to approve AMOCs
is within the scope of that authority the following new AD: for this AD, if requested using the procedures
because it addresses an unsafe condition 2015–13–03 Przedsiebiorstwo found in 14 CFR 39.19. Send information to
Doswiadczalno-Produkcyjne ATTN: Jim Rutherford, Aerospace Engineer,
that is likely to exist or develop on FAA, Small Airplane Directorate, 901 Locust,
products identified in this rulemaking Szybownictwa ‘‘PZL-Bielsko’’:
Amendment 39–18190; Docket No. Room 301, Kansas City, Missouri 64106;
action. FAA–2015–0951; Directorate Identifier telephone: (816) 329–4165; fax: (816) 329–
2015–CE–007–AD. 4090; email: jim.rutherford@faa.gov. Before
Regulatory Findings
using any approved AMOC on any sailplane
We determined that this AD will not (a) Effective Date to which the AMOC applies, notify your
have federalism implications under This airworthiness directive (AD) becomes appropriate principal inspector (PI) in the
Executive Order 13132. This AD will effective August 3, 2015. FAA Flight Standards District Office (FSDO),
not have a substantial direct effect on or lacking a PI, your local FSDO.
(b) Affected ADs (2) Airworthy Product: For any requirement
the States, on the relationship between
None. in this AD to obtain corrective actions from
the national government and the States, a manufacturer or other source, use these
or on the distribution of power and (c) Applicability actions if they are FAA-approved. Corrective
responsibilities among the various This AD applies to Przedsiebiorstwo actions are considered FAA-approved if they
levels of government. Doswiadczalno-Produkcyjne Szybownictwa are approved by the State of Design Authority
For the reasons discussed above, I ‘‘PZL-Bielsko’’ Model SZD–50–3 ‘‘Puchacz’’ (or their delegated agent). You are required
certify this AD: sailplanes, all serial numbers, certificated in to assure the product is airworthy before it
(1) Is not a ‘‘significant regulatory any category. is returned to service.
action’’ under Executive Order 12866, (d) Subject (h) Related Information
(2) Is not a ‘‘significant rule’’ under Air Transport Association of America Refer to MCAI European Aviation Safety
the DOT Regulatory Policies and (ATA) Code 27: Flight Controls. Agency (EASA) AD No.: 2015–0046, dated
Procedures (44 FR 11034, February 26, March 16, 2015, for related information. You
1979), (e) Reason
may examine the MCAI on the Internet at:
(3) Will not affect intrastate aviation This AD was prompted by mandatory http://www.regulations.gov/
in Alaska, and continuing airworthiness information (MCAI) #!documentDetail;D=FAA-2015-0951-0002.
(4) Will not have a significant originated by an aviation authority of another
country to identify and correct an unsafe (i) Material Incorporated by Reference
economic impact, positive or negative,
condition on an aviation product. The MCAI (1) The Director of the Federal Register
on a substantial number of small entities describes the unsafe condition as detachment approved the incorporation by reference
under the criteria of the Regulatory of the rudder cable fitting block from the (IBR) of the service information listed in this
Flexibility Act. fuselage. We are issuing this AD to prevent paragraph under 5 U.S.C. 552(a) and 1 CFR
Examining the AD Docket detachment of the rudder cable fitting block part 51.
from the fuselage, which if not detected and (2) You must use this service information
You may examine the AD docket on corrected, could result in reduced control. as applicable to do the actions required by
the Internet at http:// this AD, unless the AD specifies otherwise.
(f) Actions and Compliance (i) Allstar PZL Glider Service Bulletin BE–
www.regulations.gov by searching for
mstockstill on DSK4VPTVN1PROD with RULES

and locating Docket No. FAA–2015– Unless already done, do the actions in 063/SZD–50–3/2014 ‘‘Puchacz’’, dated
paragraphs (f)(1) through (f)(3) of this AD: December 14, 2014.
0951; or in person at the Docket
(1) Within 30 days after August 13, 2015 (ii) Reserved.
Management Facility between 9 a.m. (the effective date of this AD), inspect the (3) For PZL-Bielsko service information
and 5 p.m., Monday through Friday, area around both the left-hand (LH) and the identified in this AD, contact Allstar PZL
except Federal holidays. The AD docket right-hand (RH) rudder cable fitting blocks Glider, Sp. z o. o., ul. Cieszynska 325, 43–
contains the NPRM, the regulatory following paragraph 3.1. of the 300 Bielsko-Biala, Poland; telephone: +48 33
evaluation, any comments received, and INSTRUCTIONS section in Allstar PZL 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

techsupport@szd.com.pl; Internet: http:// Volume II: EDGAR Filing’’ for Section EDGAR Filing Web site. Additionally,
szd.com.pl/en/products/szd-50-3-puchacz. 508 compliance. The EDGAR system is filers can construct XML submissions
(4) You may view this service information scheduled to be upgraded to support for these submission form types by
at the FAA, Small Airplane Directorate, 901 this functionality on June 15, 2015. following the ‘‘EDGARLink Online XML
Locust, Kansas City, Missouri 64106. For
information on the availability of this DATES: Effective June 29, 2015. The Technical Specification’’ document
material at the FAA, call (816) 329–4148. In incorporation by reference of the available on the SEC’s Public Web site
addition, you can access this service EDGAR Filer Manual is approved by the (http://www.sec.gov/info/edgar.shtml).
information on the Internet at http:// Director of the Federal Register as of Submission form types ABS–15G and
www.regulations.gov by searching for and June 29, 2015. ABS–15G/A will be updated based on
locating Docket No. FAA–2015–0951. FOR FURTHER INFORMATION CONTACT: In
final Rule 15Ga–2.
(5) You may view this service information The OMB expiration date will no
that is incorporated by reference at the
the Division of Corporate Finance, for
longer be displayed on submission form
National Archives and Records questions concerning Form ABS–15G,
types 13F–HR, 13F–HR/A, 13F–NT,
Administration (NARA). For information on contact Heather Mackintosh at (202)
13F–NT/A, 13H, 13H–A, 13H–Q,
the availability of this material at NARA, call 551–8111, in the Division of Investment
13H–I, 13H–T, and 13H–R.
202–741–6030, or go to: http:// Management, for questions concerning
www.archives.gov/federal-register/cfr/ibr-
EDGAR will no longer provide
Form N–CR, contact Heather Fernandez
locations.html support for the US–GAAP–2013 and
at (202) 551–6708, and in the Office of
EXCH–2013 taxonomies. Please see
Issued in Kansas City, Missouri, on June Information Technology, contact
http://www.sec.gov/info/edgar/
18, 2015. Tammy Borkowski at (202) 551–7208.
edgartaxonomies.shtml for a complete
William Schinstock, SUPPLEMENTARY INFORMATION: We are listing of supported standard
Acting Manager, Small Airplane Directorate, adopting an updated EDGAR Filer taxonomies.
Aircraft Certification Service. Manual, Volume II. The Filer Manual Documentation only corrections were
[FR Doc. 2015–15620 Filed 6–26–15; 8:45 am] describes the technical formatting made to Chapter 3, ‘‘Index to Forms,’’ of
BILLING CODE 4910–13–P requirements for the preparation and the ‘‘EDGAR Filer Manual, Volume II:
submission of electronic filings through EDGAR Filing,’’ which include adding
the EDGAR system.1 It also describes submission types 8–K12B and
SECURITIES AND EXCHANGE the requirements for filing using 8–K12B/A to Table 3–3, ‘‘Securities
COMMISSION EDGARLink Online and the Online Exchange Act—Registration and Report
Forms/XML Web site. Submission Types Accepted by
17 CFR Part 232 The revisions to the Filer Manual EDGAR.’’
reflect changes within Volume II Documentation only changes were
[Release Nos. 33–9849; 34–75242; 39–2504;
entitled EDGAR Filer Manual, Volume made to ‘‘EDGAR Filer Manual, Volume
IC–31680]
II: ‘‘EDGAR Filing,’’ Version 32 (June II: EDGAR Filing’’ for Section 508
Adoption of Updated EDGAR Filer 2015). The updated manual will be compliance.
Manual incorporated by reference into the Code Along with the adoption of the Filer
of Federal Regulations. Manual, we are amending Rule 301 of
AGENCY: Securities and Exchange The Filer Manual contains all the Regulation S–T to provide for the
Commission. technical specifications for filers to incorporation by reference into the Code
ACTION: Final rule. submit filings using the EDGAR system. of Federal Regulations of today’s
Filers must comply with the applicable revisions. This incorporation by
SUMMARY: The Securities and Exchange provisions of the Filer Manual in order reference was approved by the Director
Commission (the Commission) is to assure the timely acceptance and of the Federal Register in accordance
adopting revisions to the Electronic Data processing of filings made in electronic with 5 U.S.C. 552(a) and 1 CFR part 51.
Gathering, Analysis, and Retrieval format.2 Filers may consult the Filer The updated EDGAR Filer Manual
System (EDGAR) Filer Manual and Manual in conjunction with our rules will be available for Web site viewing
related rules to reflect updates to the governing mandated electronic filing and printing; the address for the Filer
EDGAR system. The updates are being when preparing documents for Manual is http://www.sec.gov/info/
made primarily to add new submission electronic submission.3 edgar.shtml. You may also obtain paper
form types N–CR and N–CR/A for The EDGAR system will be upgraded copies of the EDGAR Filer Manual from
Current Report of Money Market Fund to Release 15.2 on June 15, 2015 and the following address: Public Reference
Material Events; update submission will introduce the following changes: Room, U.S. Securities and Exchange
form types ABS–15G and ABS–15G/A EDGAR will be updated to add new Commission, 100 F Street, NE.,
for Asset-backed securities reporting submission form types N–CR and Washington, DC 20549, on official
based on Rule 15Ga-2; no longer display N–CR/A to EDGARLink Online. These business days between the hours of
OMB expiration date on submission new submission form types can be 10:00 a.m. and 3:00 p.m.
form types 13F and 13H; no longer accessed by selecting the ‘EDGARLink Since the Filer Manual and the
provide support for the 2013 US GAAP Online Form Submission’ link on the corresponding rule changes relate solely
financial reporting and 2013 EXCH to agency procedures or practice,
taxonomies; documentation only 1 We originally adopted the Filer Manual on April
publication for notice and comment is
corrections to Chapter 3, ‘‘Index to 1, 1993, with an effective date of April 26, 1993.
Release No. 33–6986 (April 1, 1993) [58 FR 18638].
not required under the Administrative
Forms,’’ of the ‘‘EDGAR Filer Manual, Procedure Act (APA).4 It follows that
mstockstill on DSK4VPTVN1PROD with RULES

We implemented the most recent update to the Filer
Volume II: EDGAR Filing,’’ which Manual on May 11, 2015. See Release No. 33–9773 the requirements of the Regulatory
include adding submission types (May 26, 2015) [80 FR 29942]. Flexibility Act 5 do not apply.
8–K12B and 8–K12B/A to Table 3–3, 2 See Rule 301 of Regulation S–T (17 CFR
The effective date for the updated
‘‘Securities Exchange Act—Registration 232.301).
3 See Release No. 33–9773 in which we
Filer Manual and the rule amendments
and Report Submission Types Accepted implemented EDGAR Release 15.1.1. For additional
by EDGAR’’; and documentation only history of Filer Manual rules, please see the cites 45 U.S.C. 553(b).
changes to ‘‘EDGAR Filer Manual, therein. 55 U.S.C. 601–612.

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Document Created: 2015-12-15 14:25:15
Document Modified: 2015-12-15 14:25:15

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
Action		Final rule.
Dates		This AD is effective August 3, 2015.
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: [email protected]
FR Citation		80 FR 36911
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

80 FR 36911 - Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa “PZL-Bielsko” Sailplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 80, Issue 124 (June 29, 2015)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration