FR Doc E6-20325

[Federal Register: December 4, 2006 (Volume 71, Number 232)]
[Rules and Regulations]
[Page 70300-70302]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr04de06-7]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-25810; Directorate Identifier 2006-CE-49-AD;
Amendment 39-14838; AD 2006-24-09]
RIN 2120-AA64

Airworthiness Directives; PZL-Bielsko Model SZD-50-3 ``Puchacz''
Gliders

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. 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 a
discrepancy between the design documentation and the Technical Service
Manual. In 1981, a castellated nut with cotter pin was introduced to
secure the rudder, replacing the self-locking nut through PZL-Bielsko
Bulletin No. BE-06/50-3/81. This change has not been introduced to the
Technical Service Manual and use of a self-locking nut, in accordance
with the Manual, is still possible. We are issuing this AD to require
actions that are intended to address the unsafe condition described in
the MCAI.

DATES: This AD becomes effective January 8, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of January 8,
2007.

ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov
or in person at the Docket Management Facility, U.S.

Department of Transportation, 400 Seventh Street SW., Nassif Building,
Room PL-401, Washington, DC.

FOR FURTHER INFORMATION CONTACT: Gregory Davison, Glider Program
Manager, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone:
(816) 329-4130; fax: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Streamlined Issuance of AD

The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. The streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on September 27, 2006
(71 FR 56416). That NPRM proposed to correct an unsafe condition for
the specific products. The MCAI states that a discrepancy between the
design documentation and the Technical Service Manual has been
identified. In 1981, a castellated nut with cotter pin was introduced
to secure the rudder, replacing the self-locking nut through PZL-
Bielsko Bulletin No BE-06/50-3/81. This change has not been introduced
to the Technical Service Manual and use of a self-locking nut, in
accordance with the Manual, is still possible. This was probably the
reason of rudder disconnection during flight which occurred recently.
If not corrected, loss of the nut could result and allow the rudder to
slip out of its hinges, separate from the glider, and lead to loss of
control. This AD requires you to inspect and, if necessary, replace the
Rudder Attachment parts in accordance with the instruction contained in
the Allstar PZL Glider Sp. z o.o. Mandatory Bulletin No. BE-058/SZD-50-
3/2006 ``PUCHACZ'', dated August 10, 2006. Concurrently, changes in the
Technical Service Manual must be introduced in accordance with the
referenced bulletin.

Comments

We gave the public the opportunity to participate in developing
this AD. We have considered the comments received.
Jack Buster with the Modification and Replacement Parts Association
(MARPA) provides comments to the MCAI AD process pertaining to how the
FAA addresses publishing manufacturer service information as part of a
proposed AD action. Mr. Buster states that the rule, as proposed,
attempts to require compliance with a public law by reference to a
private writing (as referenced in paragraph (e) of the proposed AD).
Mr. Buster would like the FAA to incorporate by reference (IBR) the
Allstar PZL Glider Sp. z o.o. Mandatory Bulletin.
We agree with Mr. Buster. However, we do not IBR any document in a
proposed AD action, instead we IBR the document in the final rule.
Since we are issuing the proposal as a final rule AD action, Allstar
PZL Glider Sp. z o.o. Mandatory Bulletin No. BE-058/SZD-50-3/2006
``PUCHACZ'', dated August 10, 2006, is incorporated by reference.
Mr. Buster requests that IBR documents be made available to the
public by publication in the Federal Register or in the Docket
Management System (DMS).
We are currently reviewing issues surrounding the posting of
service bulletins in the Department of Transportation's DMS as part of
the AD docket. Once we have thoroughly examined all aspects of this
issue and have made a final determination, we will consider whether our
current practice needs to be revised.

Conclusion

We reviewed the available data, including the comments received,
and determined that air safety and the public interest require adopting
the AD as proposed.

Differences Between This AD and the MCAI or Service Information

We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable in a U.S. court of
law. In making these changes, we do not intend to differ substantively
from the information provided in the MCAI and related service
information.
We might also have required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
described in a separate paragraph of the AD. These requirements, if
any, take precedence over the actions copied from the MCAI.

[[Page 70301]]

Costs of Compliance

We estimate that this AD will affect about 8 products of U.S.
registry. We also estimate that it will take about 1.5 work-hours per
product to comply with this AD. The average labor rate is $80 per work-
hour. Required parts will cost about $2 per product. Where the service
information lists required parts costs that are covered under warranty,
we have assumed that there will be no charge for these parts. As we do
not control warranty coverage for affected parties, some parties may
incur costs higher than estimated here. Based on these figures, we
estimate the cost of this AD to the U.S. operators to be $976 or $122
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 DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) 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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD Docket.

Examining the AD Docket

You may examine the AD docket on the Internet at http://dms.dot.gov
; 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) 647-5227) 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

0
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:

2006-24-09 PZL-Bielsko: Amendment 39-14838; Docket No. FAA-2006-
25810; Directorate Identifier 2006-CE-49-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective January
8, 2007.

Affected ADs

(b) None.

Applicability

Reason

(d) The mandatory continuing airworthiness information (MCAI)
states that the aircraft manufacturer has identified a discrepancy
between the design documentation and the Technical Service Manual.
In 1981, a castellated nut with cotter pin was introduced to secure
the rudder, replacing the self-locking nut, through PZL Bielsko
Bulletin No. BE-06/50-3/81. This change has not been introduced to
the Technical Service Manual and use of a self-locking nut, in
accordance with the Manual, is still possible. This was probably the
reason for rudder disconnection during flight which occurred
recently. If not corrected, loss of the nut could result and allow
the rudder to slip out of its hinges, separate from the glider, and
lead to loss of control.

Actions and Compliance

(e) Unless already done, do the following actions except as
stated in paragraph (f) below: Within 30 days of January 3, 2007
(the effective date of this AD) or before further flight, whichever
occurs later, inspect and, if necessary, replace the Rudder
Attachment parts in accordance with the instruction contained in
Allstar PZL Glider Sp. z o.o. Mandatory Bulletin No. BE-058/SZD-50-
3/2006 ``PUCHACZ'', dated August 10, 2006. Concurrently, changes in
the Technical Service Manual must be introduced in accordance with
the referenced Bulletin.

FAA AD Differences

(f) None.

Other FAA AD Provisions

(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Gregory Davison, Glider Program Manager,
901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816)
329-4130; fax: (816) 329-4090, has the authority to approve AMOCs
for this AD, if requested using the procedures found in 14 CFR
39.19.
(2) Return to Airworthiness: For any requirement in this AD to
obtain corrective actions from a manufacturer or other source, use
these actions if they are FAA-approved. Corrective actions are
considered FAA-approved if they are approved by the State of Design
Authority (or their delegated agent). You are required to assure the
product is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.

Related Information

(h) This AD is related to EASA EAD No.: 2006-0243-E, which
references Allstar PZL Glider Sp. z o.o. Mandatory Bulletin No BE-
058/SZD-50-3/2006 ``PUCHACZ'', dated August 10, 2006.

Material Incorporated by Reference

(i) You must use Allstar PZL Glider Sp. z o.o. Mandatory
Bulletin No. BE-058/SZD-50-3/2006 ``PUCHACZ'', dated August 10,
2006, to do the actions required by this AD, unless the AD specifies
otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
AllStar PZL Glider Sp. z o.o., ul. Cieszynska 325, 43 300 Bielsko-
Biala; telephone: +48 (0)33 8125021; fax: +48 (0)33 8123739; e-mail:
office@szd.com.pl.

(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri
64106; or at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go

[[Page 70302]]

to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
.

Issued in Kansas City, Missouri, on November 22, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E6-20325 Filed 12-1-06; 8:45 am]

BILLING CODE 4910-13-P