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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 al-
ready 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.
TABLE 1 TO PARAGRAPH (G)(1) OF THIS AD — AFFECTED PARTS
______________________________________________________________________
PART NAME SERIES PART NUMBER
______________________________________________________________________
Rudder hinge bolt All A730514N
Rudder control cable screw (left) up to 79th series A730515N
Rudder control cable screw (right) up to 79th series A740259N
Rudder control cable stud bolt (left) from 80th series A730545N
Rudder control cable stud bolt (right) from 80th series A730540N
______________________________________________________________________
(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 Bull-
etin 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 in-
spection 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.
(2) Before using any approved AMOC, notify your appropriate principal in-
spector, 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: 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 & Airworthi-
ness Division, Aircraft Certification Service
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.
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