Airworthiness Directives; Blanik Aircraft CZ s.r.o., 49235-49238 [2020-17650]
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Federal Register / Vol. 85, No. 157 / Thursday, August 13, 2020 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0714; Project
Identifier MCAI–2020–00589–G; Amendment
39–21189; AD 2020–16–05]
RIN 2120–AA64
the FAA, Airworthiness Products
Section, Operational Safety Branch, 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 https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–0714.
Examining the AD Docket
Airworthiness Directives; Blanik
Aircraft CZ s.r.o.
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Blanik Aircraft CZ s.r.o. Model L 23
Super-Blanik gliders. This AD requires
a one-time inspection of the rudder
control cable attachment screws and
hinge bolts, replacement of the cable
attachment screws and hinge bolts if a
crack is found, and reporting the
inspection results to the manufacturer.
This AD was prompted by reports of
cracked rudder cable attachment screws.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective August 28,
2020.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of August 28, 2020.
The FAA must receive comments on
this AD by September 28, 2020.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this final rule, contact Blanik Aircraft
CZ s.r.o., Beranovych 65, Letnany,
Praha, 199 00, Czech Republic; phone:
+420 731 425 699; internet: https://
www.blanik.aero/customer-support;
email: info@blanik.aero. You may view
this referenced service information at
SUMMARY:
VerDate Sep<11>2014
16:05 Aug 12, 2020
Jkt 250001
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0714; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the mandatory continuing airworthiness
information (MCAI), any comments
received, and other information. The
street address for Docket Operations is
listed above. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Jim
Rutherford, Aerospace Engineer, FAA,
General Aviation & Rotorcraft Section,
International Validation Branch, 901
Locust, Room 301, Kansas City,
Missouri 64106; phone: (816) 329–4165;
fax: (816) 329–4090; email:
jim.rutherford@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Community, has issued EASA
AD No. 2020–0068–E, dated March 23,
2020 (referred to after this as ‘‘the
MCAI’’), to address an unsafe condition
for Blanik Aircraft CZ s.r.o. Model L 23
Super-Blanik gliders. The MCAI states:
During a standard maintenance procedure
on an L 23 Super-Blanı´k sailplane, a crack
was detected on a rudder control cable
attachment screw.
This condition, if not detected and
corrected, could lead to rudder control
failure, possibly resulting in loss of
directional control of the sailplane.
To address this unsafe condition, BACZ
[Blanik Aircraft CZ s.r.o.] issued the MB
[mandatory bulletin] and the IB [information
bulletin] to provide inspection and
replacement instructions.
For the reasons described above, this
[EASA] AD requires a one-time inspection
and, depending on findings, replacement of
affected parts.
Blanik Aircraft CZ s.r.o. advises that
reporting by operators and maintenance
facilities indicates that this issue is not
an isolated event. You may obtain
further information by examining the
MCAI in the AD docket on the internet
PO 00000
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Fmt 4700
Sfmt 4700
49235
at https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–0714.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Blanik Mandatory
Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020,
which contains procedures for
inspecting the affected parts. The FAA
also reviewed Blanik Information
Bulletin Document No. L23/061b,
Revision 1, dated March 17, 2020,
which contains procedures for replacing
the affected parts. 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.
FAA’s Determination
This product has been approved by
EASA, and is approved for operation in
the United States. Pursuant to our
bilateral agreement with the European
Union, EASA has notified us of the
unsafe condition described in the MCAI
and service information referenced
above. The FAA is issuing this AD
because it evaluated all the relevant
information provided by EASA and
determined the unsafe condition is
likely to exist or develop in other
products of the same type design.
AD Requirements
This AD requires a one-time
inspection of the rudder control cable
attachment screws and hinge bolts and,
if a crack is found, replacement of the
affected parts as specified in the service
information described previously. This
AD also requires reporting certain
information to the manufacturer.
FAA’s Justification and Determination
of the Effective Date
An unsafe condition exists that
requires the immediate adoption of this
AD without providing an opportunity
for public comments prior to adoption.
The FAA has found that the risk to the
flying public justifies waiving notice
and comment prior to adoption of this
rule because the required corrective
actions must be accomplished before
further flight. Therefore, the FAA finds
good cause that notice and opportunity
for prior public comment are
impracticable. In addition, for the
reason stated above, the FAA finds that
good cause exists for making this
amendment effective in less than 30
days.
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49236
Federal Register / Vol. 85, No. 157 / Thursday, August 13, 2020 / Rules and Regulations
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety and
was not preceded by notice and an
opportunity for public comment.
However, we invite you to send any
written data, views, or arguments about
this final rule. Send your comments to
an address listed under the ADDRESSES
section. Include ‘‘Docket No. FAA–
2020–0714; Product Identifier MCAI–
2020–00589–G’’ at the beginning of your
comments. The FAA will consider all
comments received by the closing date
and may amend this AD because of
those comments.
Except for Confidential Business
Information as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
we receive, without change, to https://
regulations.gov, including any personal
information you provide. The FAA will
also post a report summarizing each
substantive verbal contact it receives
about this AD.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this AD contain
commercial or financial information
that is customarily treated as private,
that you actually treat as private, and
that is relevant or responsive to this AD,
it is important that you clearly designate
the submitted comments as CBI. Please
mark each page of your submission
containing CBI as ‘‘PROPIN.’’ The FAA
will treat such marked submissions as
confidential under the FOIA, and they
will not be placed in the public docket
of this AD. Submissions containing CBI
should be sent to Jim Rutherford,
Aerospace Engineer, FAA, General
Aviation & Rotorcraft Section,
International Validation Branch, 901
Locust, Room 301, Kansas City,
Missouri 64106. Any commentary that
the FAA receives which is not
specifically designated as CBI will be
placed in the public docket for this
rulemaking.
Regulatory Flexibility Act
The requirements of the Regulatory
Flexibility Act (RFA) do not apply when
an agency finds good cause pursuant to
5 U.S.C. 553 to adopt a rule without
prior notice and comment. Because the
FAA has determined that it has good
cause to adopt this rule without notice
and comment, RFA analysis is not
required.
Costs of Compliance
The FAA estimates that this AD
affects 91 gliders of U.S. registry. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Parts cost
Inspect rudder cable attach fasteners ............
Reporting results to the manufacturer ............
2.5 work-hours × $85.00 per hour = $212.50
1 hour × $85.00 per hour = $85.00 ...............
The FAA estimates the following
costs to do any necessary replacements
that would be required based on the
results of the inspection. The FAA has
no way of determining the number of
$0.00
0.00
Cost per
product
$212.50
85.00
Cost on U.S.
operators
$19,337.50
7,735.00
parts that might need these
replacements.
ON-CONDITION COSTS
Action
Labor cost
Replace fasteners .........................................................
3.5 work-hours × $85.00 per hour = $297.50 ..............
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 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 currently 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 1 hour per response,
including the time for reviewing
instructions, searching existing data
sources, gathering and maintaining the
data needed, completing and reviewing
the collection of information. All
responses to this collection of
information are mandatory. Send
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16:05 Aug 12, 2020
Jkt 250001
comments regarding this burden
estimate or any other aspect of this
collection of information, including
suggestions for reducing this burden to:
Information Collection Clearance
Officer, Federal Aviation
Administration, 10101 Hillwood
Parkway, Fort Worth, TX 76177–1524.
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.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
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Parts cost
$213.00
Cost per
product
$510.50
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
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.
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Federal Register / Vol. 85, No. 157 / Thursday, August 13, 2020 / Rules and Regulations
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:
(2) Before further flight after August 28,
2020 (the effective date of this AD), inspect
each affected part in accordance with the
Working Procedure, paragraphs A.1(1)
through A.1(4) or paragraphs A.2(1) through
A.2(4), as applicable for each part, of Blanik
Mandatory Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020.
(3) If there are no cracks in the inspection
area of a part during the inspection required
by paragraph (g)(2) of this AD, before further
flight, install the rudder in accordance with
the Working Procedure, paragraph A.1(8) or
A.2(8), as applicable for each part, of Blanik
Mandatory Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020.
(4) If there are any cracks in the inspection
area of a part during the inspection required
by paragraph (g)(2) of this AD, before further
flight, replace the part in accordance with the
Working Procedure, paragraphs A.1, A.2,
either A.3.1. or A.3.2 (as applicable), and A.4,
of Blanik Information Bulletin Document No.
L23/061b, Revision 1, dated March 17, 2020,
and install the rudder in accordance with the
Working Procedure, paragraph A.1(8) or
A.2(8), as applicable for each part, of Blanik
Mandatory Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020.
Jkt 250001
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2020–16–05 Blanik Aircraft CZ s.r.o.:
Amendment 39–21189; Docket No.
FAA–2020–0714; Project Identifier
MCAI–2020–00589–G.
(a) Effective Date
This AD is effective August 28, 2020.
(d) Subject
Joint Aircraft System Component (JASC)
Code 2720, RUDDER CONTROL SYSTEM.
1. The authority citation for part 39
continues to read as follows:
16:05 Aug 12, 2020
[Amended]
(c) Applicability
This AD applies to Blanik Aircraft CZ s.r.o.
Model L 23 Super-Blanik gliders, all serial
numbers, certificated in any category.
■
VerDate Sep<11>2014
§ 39.13
(b) Affected ADs
None.
PART 39—AIRWORTHINESS
DIRECTIVES
(h) Reporting Requirement
Within 10 days after each inspection
required by paragraph (g)(1) of this AD,
Authority: 49 U.S.C. 106(g), 40113, 44701.
report the following information to Blanik
Aircraft CZ s.r.o. at the address provided in
paragraph (m)(3) of this AD.
(1) Glider registration number (N number).
(2) Glider serial number.
(3) Glider total hours time-in-service.
(4) Number of starts by winch and tow (if
known).
(5) Inspection results (including no
findings).
(i) Credit for Previous Actions
You may take credit for the actions
required by paragraphs (g)(2) and (g)(3) of
this AD if you accomplish those actions
before the effective date of this AD using
Blanik Mandatory Bulletin Document No.
L23/060a, Revision 1, dated March 4, 2020,
and, Blanik Information Bulletin Document
No. L23/061b, original issue, dated March 4,
2020. If you take this credit, you do not have
to comply with the reporting requirement in
paragraph (h) of this AD.
(j) Paperwork Reduction Act Burden
Statement
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
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Sfmt 4700
(e) Unsafe Condition
This AD was prompted by reports of
cracking on the rudder control cable
attachment screw. The FAA is issuing this
AD to detect and prevent a crack in a rudder
control cable attachment screw, which could
result in in-flight collapse of the screw. The
unsafe condition, if not addressed, could
result in rudder control failure and loss of
control of the glider.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Inspection and Replacement
(1) For purposes of this AD, an affected
part means a part identified in table 1 to
paragraph (g)(1) of this AD. The series refers
to the second pair of digits in the glider serial
number.
displays a currently 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 1 hour per
response, including the time for reviewing
instructions, searching existing data sources,
gathering and maintaining the data needed,
completing and reviewing the collection of
information. All responses to this collection
of information are mandatory. Send
comments regarding this burden estimate or
any other aspect of this collection of
information, including suggestions for
reducing this burden to: Information
Collection Clearance Officer, Federal
Aviation Administration, 10101 Hillwood
Parkway, Fort Worth, TX 76177–1524.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Small Airplane Standards
Branch, 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 manager of the certification office,
send it to the attention of the person
identified in paragraph (l) of this AD.
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ER13AU20.001</GPH>
For the reasons discussed above, I
certify this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
and
(2) Will not affect intrastate aviation
in Alaska.
49237
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Federal Register / Vol. 85, No. 157 / Thursday, August 13, 2020 / Rules and Regulations
(2) 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.
DEPARTMENT OF TRANSPORTATION
(l) Related Information
[Docket No. FAA–2020–0711; Project
Identifier MCAI–2020–00719–A; Amendment
39–21188; AD 2020–16–04]
(1) For more information about this AD,
contact Jim Rutherford, Aerospace Engineer,
FAA, General Aviation & Rotorcraft Section,
International Validation Branch, 901 Locust,
Room 301, Kansas City, Missouri 64106;
phone: (816) 329–4165; fax: (816) 329–4090;
email: jim.rutherford@faa.gov.
(2) Refer to European Union Aviation
Safety Agency (EASA) AD No. 2020–0068–E,
dated March 23, 2020, for more information.
You may examine the EASA AD in the AD
docket on the internet at https://
www.regulations.gov by searching for and
locating it in Docket No. FAA–2020–0714.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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) Blanik Mandatory Bulletin Document
No. L23/060a, Revision 2, dated March 17,
2020.
(ii) Blanik Information Bulletin Document
No. L23/061b, Revision 1, dated March 17,
2020.
(3) For Blanik service information
identified in this AD, contact Blanik Aircraft
CZ s.r.o., Beranovych 65, Letnany, Praha, 199
00, Czech Republic; phone: +420 731 425
699; internet: https://www.blanik.aero/
customer-support; email: info@blanik.aero.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 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 https://
www.regulations.gov by searching for
locating Docket No. FAA–2020–0714.
(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,
email: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on July 28, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–17650 Filed 8–12–20; 8:45 am]
BILLING CODE 4910–13–P
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Federal Aviation Administration
14 CFR Part 39
RIN 2120–AA64
Airworthiness Directives; Pacific
Aerospace Limited Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Pacific Aerospace Limited Model 750XL
airplanes. This AD results from
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 an
incorrect illustration of the screw jack
assembly in the airplane maintenance
manual, which may cause potential
errors with installation. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective September 2,
2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of September 2, 2020.
The FAA must receive comments on
this AD by September 28, 2020.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: (202) 493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this AD, contact Pacific Aerospace
Limited, Airport Road, Hamilton,
Private Bag 3027, Hamilton 3240, New
Zealand; phone: +64 7843 6144; fax: +64
843 6134; email: pacific@
aerospace.co.nz; internet: https://
www.aerospace.co.nz/. You may view
SUMMARY:
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this referenced service information at
the FAA, Airworthiness Products
Section, Operational Safety Branch, 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 https://www.regulations.gov by
searching for locating Docket No. FAA–
2020–0711.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0711; or in person at Docket Operations
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 Docket Operations is
listed above. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT:
Mike Kiesov, Aerospace Engineer, FAA,
General Aviation & Rotorcraft Section,
International Validation Branch, 901
Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329–
4144; fax: (816) 329–4090; email:
mike.kiesov@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Authority (CAA),
which is the aviation authority for New
Zealand, has issued AD DCA/750XL/
38A, dated September 5, 2019 (referred
to after this as ‘‘the MCAI’’), to correct
an unsafe condition for Pacific
Aerospace Limited Model 750XL
airplanes. The MCAI states:
DCA/750XL/38A with effective date 5
September 2019 and a 5 hour TIS compliance
is prompted by two reports of finding
incorrectly assembled flap screw jacks on
affected aircraft. This AD is revised to
introduce Pacific Aerospace Mandatory
Service Bulletin (MSB) PACSB/XL/117 issue
2, dated 21 August 2019 and expand the AD
applicability to include additional aircraft S/
N and parts held as spares.
There are no additional AD requirements
for aircraft and affected parts in compliance
with DCA/750XL/38.
A Pacific Aerospace Ltd (PAL) review of
the 750XL Maintenance Manual (MM) and
the 750XL Illustrated Parts Manual (IPM) has
determined that the orientation shown in
these two manuals for the flap screw jack
bearing stop is incorrect. PAL has
subsequently issued temporary revisions
dated 5 June 2019, for both the 750XL MM
and the 750XL IPM to correct the orientation
shown for the flap screw jack bearing stop.
These temporary revisions can be obtained
from Pacific Aerospace Ltd, Hamilton, New
Zealand.
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]]>Agencies
[Federal Register Volume 85, Number 157 (Thursday, August 13, 2020)]
[Rules and Regulations]
[Pages 49235-49238]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-17650]
[[Page 49235]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0714; Project Identifier MCAI-2020-00589-G;
Amendment 39-21189; AD 2020-16-05]
RIN 2120-AA64
Airworthiness Directives; Blanik Aircraft CZ s.r.o.
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Blanik Aircraft CZ s.r.o. Model L 23 Super-Blanik gliders. This AD
requires a one-time inspection of the rudder control cable attachment
screws and hinge bolts, replacement of the cable attachment screws and
hinge bolts if a crack is found, and reporting the inspection results
to the manufacturer. This AD was prompted by reports of cracked rudder
cable attachment screws. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective August 28, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of August 28,
2020.
The FAA must receive comments on this AD by September 28, 2020.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this final rule, contact
Blanik Aircraft CZ s.r.o., Beranovych 65, Letnany, Praha, 199 00, Czech
Republic; phone: +420 731 425 699; internet: https://www.blanik.aero/customer-support; email: [email protected]. You may view this referenced
service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 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 https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0714.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0714; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the mandatory continuing airworthiness information
(MCAI), any comments received, and other information. The street
address for Docket Operations is listed above. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer,
FAA, General Aviation & Rotorcraft Section, International Validation
Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; phone: (816)
329-4165; fax: (816) 329-4090; email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Community, has
issued EASA AD No. 2020-0068-E, dated March 23, 2020 (referred to after
this as ``the MCAI''), to address an unsafe condition for Blanik
Aircraft CZ s.r.o. Model L 23 Super-Blanik gliders. The MCAI states:
During a standard maintenance procedure on an L 23 Super-
Blan[iacute]k sailplane, a crack was detected on a rudder control
cable attachment screw.
This condition, if not detected and corrected, could lead to
rudder control failure, possibly resulting in loss of directional
control of the sailplane.
To address this unsafe condition, BACZ [Blanik Aircraft CZ
s.r.o.] issued the MB [mandatory bulletin] and the IB [information
bulletin] to provide inspection and replacement instructions.
For the reasons described above, this [EASA] AD requires a one-
time inspection and, depending on findings, replacement of affected
parts.
Blanik Aircraft CZ s.r.o. advises that reporting by operators and
maintenance facilities indicates that this issue is not an isolated
event. You may obtain further information by examining the MCAI in the
AD docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2020-0714.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Blanik Mandatory Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020, which contains procedures for
inspecting the affected parts. The FAA also reviewed Blanik Information
Bulletin Document No. L23/061b, Revision 1, dated March 17, 2020, which
contains procedures for replacing the affected parts. 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.
FAA's Determination
This product has been approved by EASA, and is approved for
operation in the United States. Pursuant to our bilateral agreement
with the European Union, EASA has notified us of the unsafe condition
described in the MCAI and service information referenced above. The FAA
is issuing this AD because it evaluated all the relevant information
provided by EASA and determined the unsafe condition is likely to exist
or develop in other products of the same type design.
AD Requirements
This AD requires a one-time inspection of the rudder control cable
attachment screws and hinge bolts and, if a crack is found, replacement
of the affected parts as specified in the service information described
previously. This AD also requires reporting certain information to the
manufacturer.
FAA's Justification and Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies waiving notice and comment prior to adoption of this rule
because the required corrective actions must be accomplished before
further flight. Therefore, the FAA finds good cause that notice and
opportunity for prior public comment are impracticable. In addition,
for the reason stated above, the FAA finds that good cause exists for
making this amendment effective in less than 30 days.
[[Page 49236]]
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety and was not preceded by notice and an opportunity for public
comment. However, we invite you to send any written data, views, or
arguments about this final rule. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2020-0714;
Product Identifier MCAI-2020-00589-G'' at the beginning of your
comments. The FAA will consider all comments received by the closing
date and may amend this AD because of those comments.
Except for Confidential Business Information as described in the
following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments we receive, without change, to
https://regulations.gov, including any personal information you
provide. The FAA will also post a report summarizing each substantive
verbal contact it receives about this AD.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this AD. Submissions containing CBI should be sent to Jim
Rutherford, Aerospace Engineer, FAA, General Aviation & Rotorcraft
Section, International Validation Branch, 901 Locust, Room 301, Kansas
City, Missouri 64106. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because the FAA has determined
that it has good cause to adopt this rule without notice and comment,
RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 91 gliders of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspect rudder cable attach fasteners. 2.5 work-hours x $85.00 $0.00 $212.50 $19,337.50
per hour = $212.50.
Reporting results to the manufacturer. 1 hour x $85.00 per hour 0.00 85.00 7,735.00
= $85.00.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
inspection. The FAA has no way of determining the number of parts that
might need these replacements.
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replace fasteners.......................... 3.5 work-hours x $85.00 per hour = $213.00 $510.50
$297.50.
----------------------------------------------------------------------------------------------------------------
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 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 currently 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 1 hour per response, including the time for reviewing
instructions, searching existing data sources, gathering and
maintaining the data needed, completing and reviewing the collection of
information. All responses to this collection of information are
mandatory. Send comments regarding this burden estimate or any other
aspect of this collection of information, including suggestions for
reducing this burden to: Information Collection Clearance Officer,
Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX
76177-1524.
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.
The FAA is 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
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.
[[Page 49237]]
For the reasons discussed above, I certify this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866, and
(2) Will not affect intrastate aviation in Alaska.
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 airworthiness
directive (AD):
2020-16-05 Blanik Aircraft CZ s.r.o.: Amendment 39-21189; Docket No.
FAA-2020-0714; Project Identifier MCAI-2020-00589-G.
(a) Effective Date
This AD is effective August 28, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Blanik Aircraft CZ s.r.o. Model L 23 Super-
Blanik gliders, all serial numbers, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 2720, RUDDER CONTROL
SYSTEM.
(e) Unsafe Condition
This AD was prompted by reports of cracking on the rudder
control cable attachment screw. The FAA is issuing this AD to detect
and prevent a crack in a rudder control cable attachment screw,
which could result in in-flight collapse of the screw. The unsafe
condition, if not addressed, could result in rudder control failure
and loss of control of the glider.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Replacement
(1) For purposes of this AD, an affected part means a part
identified in table 1 to paragraph (g)(1) of this AD. The series
refers to the second pair of digits in the glider serial number.
[GRAPHIC] [TIFF OMITTED] TR13AU20.001
(2) Before further flight after August 28, 2020 (the effective
date of this AD), inspect each affected part in accordance with the
Working Procedure, paragraphs A.1(1) through A.1(4) or paragraphs
A.2(1) through A.2(4), as applicable for each part, of Blanik
Mandatory Bulletin Document No. L23/060a, Revision 2, dated March
17, 2020.
(3) If there are no cracks in the inspection area of a part
during the inspection required by paragraph (g)(2) of this AD,
before further flight, install the rudder in accordance with the
Working Procedure, paragraph A.1(8) or A.2(8), as applicable for
each part, of Blanik Mandatory Bulletin Document No. L23/060a,
Revision 2, dated March 17, 2020.
(4) If there are any cracks in the inspection area of a part
during the inspection required by paragraph (g)(2) of this AD,
before further flight, replace the part in accordance with the
Working Procedure, paragraphs A.1, A.2, either A.3.1. or A.3.2 (as
applicable), and A.4, of Blanik Information Bulletin Document No.
L23/061b, Revision 1, dated March 17, 2020, and install the rudder
in accordance with the Working Procedure, paragraph A.1(8) or
A.2(8), as applicable for each part, of Blanik Mandatory Bulletin
Document No. L23/060a, Revision 2, dated March 17, 2020.
(h) Reporting Requirement
Within 10 days after each inspection required by paragraph
(g)(1) of this AD, report the following information to Blanik
Aircraft CZ s.r.o. at the address provided in paragraph (m)(3) of
this AD.
(1) Glider registration number (N number).
(2) Glider serial number.
(3) Glider total hours time-in-service.
(4) Number of starts by winch and tow (if known).
(5) Inspection results (including no findings).
(i) Credit for Previous Actions
You may take credit for the actions required by paragraphs
(g)(2) and (g)(3) of this AD if you accomplish those actions before
the effective date of this AD using Blanik Mandatory Bulletin
Document No. L23/060a, Revision 1, dated March 4, 2020, and, Blanik
Information Bulletin Document No. L23/061b, original issue, dated
March 4, 2020. If you take this credit, you do not have to comply
with the reporting requirement in paragraph (h) of this AD.
(j) Paperwork Reduction Act Burden Statement
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 currently 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 1 hour per response, including the
time for reviewing instructions, searching existing data sources,
gathering and maintaining the data needed, completing and reviewing
the collection of information. All responses to this collection of
information are mandatory. Send comments regarding this burden
estimate or any other aspect of this collection of information,
including suggestions for reducing this burden to: Information
Collection Clearance Officer, Federal Aviation Administration, 10101
Hillwood Parkway, Fort Worth, TX 76177-1524.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Small Airplane Standards Branch, 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 manager of the certification office, send it to the
attention of the person identified in paragraph (l) of this AD.
[[Page 49238]]
(2) 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.
(l) Related Information
(1) For more information about this AD, contact Jim Rutherford,
Aerospace Engineer, FAA, General Aviation & Rotorcraft Section,
International Validation Branch, 901 Locust, Room 301, Kansas City,
Missouri 64106; phone: (816) 329-4165; fax: (816) 329-4090; email:
[email protected].
(2) Refer to European Union Aviation Safety Agency (EASA) AD No.
2020-0068-E, dated March 23, 2020, for more information. You may
examine the EASA AD in the AD docket on the internet at https://www.regulations.gov by searching for and locating it in Docket No.
FAA-2020-0714.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) Blanik Mandatory Bulletin Document No. L23/060a, Revision 2,
dated March 17, 2020.
(ii) Blanik Information Bulletin Document No. L23/061b, Revision
1, dated March 17, 2020.
(3) For Blanik service information identified in this AD,
contact Blanik Aircraft CZ s.r.o., Beranovych 65, Letnany, Praha,
199 00, Czech Republic; phone: +420 731 425 699; internet: https://www.blanik.aero/customer-support; email: [email protected].
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 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 https://www.regulations.gov by
searching for locating Docket No. FAA-2020-0714.
(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, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on July 28, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-17650 Filed 8-12-20; 8:45 am]
BILLING CODE 4910-13-P
