Airworthiness Directives; PZL-Swidnik S.A. Models PW-5 “Smyk” and PW-6U Gliders, 55248-55250 [05-18526]
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<![CDATA[
55248
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
of this material at NARA, go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html or call (202) 741–6030. To
view the AD docket, go to the Docket
Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW.,
Nassif Building, Room PL–401, Washington,
DC 20590–001 or on the Internet at https://
dms.dot.gov. The docket number is FAA–
2005–21174; Directorate Identifier 2005–CE–
23–AD.
Issued in Kansas City, Missouri, on
September 13, 2005.
James E. Jackson,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–18525 Filed 9–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20802; Directorate
Identifier 2005–CE–18–AD; Amendment 39–
14282; AD 2005–19–17]
RIN 2120–AA64
Airworthiness Directives; PZL-Swidnik
S.A. Models PW–5 ‘‘Smyk’’ and PW–6U
Gliders
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA adopts a new
airworthiness directive (AD) for certain
PZL-Swidnik S.A. (PZL-Swidnik)
Models PW–5 ‘‘Smyk’’ and PW–6U
gliders. This AD requires you to inspect
for the minimum dimension of the left
side aileron, right side aileron, and
airbrake push-rod ends for certain
Model PW–5 ‘‘Smyk’’ gliders; inspect
for the minimum dimension of the
aileron, airbrake, and elevator control
push-rod ends for certain Model PW–6U
gliders; and replace any push-rod end
that does not meet the minimum
dimension. This AD results from
mandatory continuing airworthiness
information (MCAI) issued by the
airworthiness authority for Poland. We
are issuing this AD to detect and replace
any push-rod end that does not meet the
minimum dimension, which could
result in failure of the control system.
This failure could lead to loss of control
of the glider.
DATES: This AD becomes effective on
October 31, 2005.
VerDate Aug<31>2005
14:27 Sep 20, 2005
Jkt 205001
As of October 31, 2005, the Director
of the Federal Register approved the
incorporation by reference of certain
publications listed in the regulation.
ADDRESSES: To get the service
information identified in this AD,
contact PZL-Swidnik S.A., Polish
Aviation Works, Al. Lotnikow Polskich
1, 21–045 Swidnik, Poland; telephone:
48 81 468 09 01 751 20 71; facsimile:
48 81 468 09 19 751 21 73.
To view the AD docket, go to the
Docket Management Facility; U.S.
Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
001 or on the Internet at https://
dms.dot.gov. The docket number is
FAA–2005–20802; Directorate Identifier
2005–CE–18–AD.
FOR FURTHER INFORMATION CONTACT: Greg
Davison, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4130; facsimile:
(816) 329–4090.
SUPPLEMENTARY INFORMATION:
Discussion
What events have caused this AD?
The General Inspectorate of Civil
Aviation (GICA), which is the
airworthiness authority for Poland,
recently notified FAA that an unsafe
condition may exist on certain PZLSwidnik S.A. (PZL-Swidnik) gliders.
The GICA reports that an owner of a
Model PW–6U glider found the
dimension of the push-rod end to not
meet the minimum dimension of 0.165
inches (in.) or 4.2 millimeter (mm).
Further, the GICA reports that the
manufacturer has identified a
production run of these parts that do not
meet the minimum dimension of the
push-rod end. Similar push-rod ends,
where applicable, are used to link the
ailerons, airbrakes, and elevator control
systems in the Models PW–5 ‘‘Smyk’’
and PW–6U gliders.
What is the potential impact if FAA
took no action? Any push-rod end that
does not meet the minimum dimension
could result in failure of the control
system. This failure could lead to loss
of control of the glider.
Has FAA taken any action to this
point? We issued a proposal to amend
part 39 of the Federal Aviation
Regulations (14 CFR part 39) to include
an AD that would apply to certain PZLSwidnik S.A. (PZL-Swidnik) Models
PW–5 ‘‘Smyk’’ and PW–6U gliders. This
proposal was published in the Federal
PO 00000
Frm 00024
Fmt 4700
Sfmt 4700
Register as a notice of proposed
rulemaking (NPRM) on April 27, 2005
(70 FR 21691). The NPRM proposed to
require you to inspect for the minimum
dimension of the left side aileron, right
side aileron, and airbrake push-rod ends
for certain Model PW–5 ‘‘Smyk’’ gliders;
inspect for the minimum dimension of
the aileron, airbrake, and elevator
control push-rod ends for certain Model
PW–6U gliders; and replace any pushrod end that does not meet the
minimum dimension.
Comments
Was the public invited to comment?
We provided the public the opportunity
to participate in developing this AD. We
received no comments on the proposal
or on the determination of the cost to
the public.
Conclusion
What is FAA’s final determination on
this issue? We have carefully reviewed
the available data and determined that
air safety and the public interest require
adopting the AD as proposed except for
minor editorial corrections. We have
determined that these minor
corrections:
—Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
—Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Changes to 14 CFR Part 39—Effect on
the AD
How does the revision to 14 CFR part
39 affect this AD? On July 10, 2002, the
FAA published a new version of 14 CFR
part 39 (67 FR 47997, July 22, 2002),
which governs the FAA’s AD system.
This regulation now includes material
that relates to altered products, special
flight permits, and alternative methods
of compliance. This material previously
was included in each individual AD.
Since this material is included in 14
CFR part 39, we will not include it in
future AD actions.
Costs of Compliance
How many gliders does this AD
impact? We estimate that this AD affects
67 gliders in the U.S. registry.
What is the cost impact of this AD on
owners/operators of the affected gliders?
We estimate the following costs to do
the inspection of the push-rod ends:
E:\FR\FM\21SER1.SGM
21SER1
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
55249
Labor cost
Parts cost
Total cost per
glider
Total cost on
U.S. operators
1 work hour × $65 = $65 .........................................
Not applicable .........................................................
$65
67 × $65 = $4,355.
We estimate the following costs to do
any necessary push-rod end
replacements that would be required
based on the results of this inspection.
We have no way of determining the
number of gliders that may need this
replacement:
Labor cost per push-rod end
Parts cost
Total cost per
push-rod
end per glider
1 work hour × $65 = $65 ..........................................................
Not applicable ...........................................................................
$65
The manufacturer has stated that the
costs for any required parts and
transportation of the parts will be
covered under the manufacturer’s
warranty.
Authority for This Rulemaking
What authority does FAA have for
issuing this rulemaking action? 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 AD.
Regulatory Findings
Will this AD impact various entities?
We have 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.
VerDate Aug<31>2005
14:27 Sep 20, 2005
Jkt 205001
Will this AD involve a significant rule
or regulatory action? For the reasons
discussed above, I certify that 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); 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 summary of the costs
to comply with this AD (and other
information as included in the
Regulatory Evaluation) and placed it in
the AD Docket. You may get a copy of
this summary by sending a request to us
at the address listed under ADDRESSES.
Include ‘‘Docket No. FAA–2005–20802;
Directorate Identifier 2005–CE–18–AD’’
in your request.
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 Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (14 CFR part 39) as follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
PO 00000
Frm 00025
Fmt 4700
Sfmt 4700
§ 39.13
[Amended]
I 2. FAA amends § 39.13 by adding a
new AD to read as follows:
2005–19–17 PZL-Swidnik S.A.:
Amendment 39–14282; Docket No.
FAA–2005–20802; Directorate Identifier
2005–CE–18–AD.
When Does This AD Become Effective?
(a) This AD becomes effective on October
31, 2005.
What Other ADs Are Affected by This
Action?
(b) None.
What Gliders Are Affected by This AD?
(c) This AD affects the following glider
models and serial numbers that are
certificated in any category:
Model
Serial Nos.
PW–5 ‘‘Smyk’’ ..
17.12.022 through
17.12.024.
78.02.07 through 78.02.10
and 78.03.01 through
78.03.03.
PW–6U .............
What Is the Unsafe Condition Presented in
This AD?
(d) This AD is the result of mandatory
continuing airworthiness information (MCAI)
issued by the airworthiness authority for
Poland. The actions specified in this AD are
intended to detect and replace any push-rod
end that does not meet the minimum
dimension, which could result in failure of
the control system. This failure could lead to
loss of control of the glider.
What Must I Do To Address This Problem?
(e) To address this problem, you must do
the following:
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55250
Federal Register / Vol. 70, No. 182 / Wednesday, September 21, 2005 / Rules and Regulations
Actions
Compliance
Procedures
(1) Inspect for the minimum dimension (0.165
inches (in.) or 4.2 millimeter (mm)):
(i) Any left side aileron, right side aileron,
and airbrake push-rod end (part number
(P/N) 511.00.20.00) for the Model PW–5
‘‘Smyk’’ glider; and.
(ii) Any aileron, airbake, and elevator control push-rod end (P/N 78.21.215.00.00)
for the Model PW–6U glider.
(2) Replace any push-rod end (P/N
511.00.20.00 or 78.21.215.00.00) that you
find as a result of the inspection requried by
paragraph (e)(1) of this AD that has a pushrod end that is less than the minimum dimension (0.165 in. or 4.2 mm).
Within the next 25 hours time-in-service (TIS)
after October 31, 2005 (the effective date of
this AD), unless already done.
For the Model PW–5 ‘‘Smyk’’ glider: Follow
Communication Equipment Factory PZLSwidnik Mandatory Bulletin Number BO–
17–03–18, dated December 22, 2003. For
the Model PW–6U glider: Follow Communication Equipment PZL-Swidnik Mandatory
Bulletin Number BO–78–03–06, dated December 22, 2003.
Before further flight after the the inspection
requried by paragraph (e)(1) of this AD.
For the Model PW–5 ‘‘Smyk’’ glider: Follow
Communication Equipment PZL-Swidnik
Mandatory Bulletin Number BO–17–03–18,
dated December 22, 2003. For the Model
PW–6U glider: Follow Communication
Equipment Factory PZL-Swidnik Mandatory
Bulletin NumberBO–17–03–18, dated December 22, 2003.
For the Model PW–5 ‘‘Smyk’’ glider: Follow
Communicaton Equipment Factory PZLSwidnik Mandatory Bulletin Number BO–
17–03–18, dated December 22, 2003. For
the Model PW–6U glider: Follow Communication Equipment Factory PZL-Swidnik
Mandatory Bulletin Number BO–78–03–06,
dated December 22, 2003.
(3) Do not install any push-rod end (P/N
511.00.20.00 or 78.21.215.00.00) with a dimension that is less than the minimum dimension (0.165 in. or 4.2 mm):
(i) Any push-rod end for the left side aileron, right side aileron, or airbrake of the
Model PW–5 Swidnik glider; and.
(ii) Any push-rod end for the ailerons,
airbake, or elevator control of the Model
PW–6U glider.
As of October 31, 200 (the effective date of
this AD).
May I Request an Alternative Method of
Compliance?
Polskich 1, 21–045 Swidnik, Poland;
telephone: 48 81 468 09 01 751 20 71;
facsimile: 48 81 468 09 19 751 21 73. To
review copies of this service information, go
to the National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html or call (202) 741–6030. To
view the AD docket, go to the Docket
Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW.,
Nassif Building, Room PL–401, Washington,
DC 20590–001 or on the Internet at https://
dms.dot.gov. The docket number is FAA–
2005–20802; Directorate Identifier 2005–CE–
18–AD.
(f) You may request a different method of
compliance or a different compliance time
for this AD by following the procedures in 14
CFR 39.19. Unless FAA authorizes otherwise,
send your request to your principal
inspector. The principal inspector may add
comments and will send your request to the
Manager, Standards Office, Small Airplane
Directorate, FAA. For information on any
already approved alternative methods of
compliance, contact Greg Davison, Aerospace
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4130; facsimile:
(816) 329–4090.
Is There Other Information That Relates to
This Subject?
(g) Polish AD Numbers SP–0085–2003–A,
dated December 22, 2003, and SP–0086–
2003, dated December 22, 2003, also address
the subject of this AD.
Does This AD Incorporate Any Material by
Reference?
(h) You must do the actions required by
this AD following the instructions in
Communication Equipment Factory PZLSwidnik Mandatory Bulletin Number BO–
17–03–18, dated December 22, 2003, and
Communication Equipment Factory PZLSwidnik Mandatory Bulletin Number BO–
78–03–06, dated December 22, 2003. The
Director of the Federal Register approved the
incorporation by reference of this service
bulletin in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. To get a copy of this
service information, contact PZL-Swidnik
S.A., Polish Aviation Works, Al. Lotnikow
VerDate Aug<31>2005
15:20 Sep 20, 2005
Jkt 205001
Issued in Kansas City, Missouri, on
September 12, 2005.
James E. Jackson,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–18526 Filed 9–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
ACTION:
Final rule; correction.
SUMMARY: This action corrects an error
in the effective date contained in a Final
Rule that was published in the Federal
Register on September 1, 2005 (70 FR
52012). That Final Rule amended Title
14 Code of Federal Regulations (14 CFR)
part 71 relating to airspace designations
to reflect the approval by the Director of
the Federal Register of the incorporation
by reference of FHA Order 7400.9N,
Airspace Designations and Reporting
Points.
These regulations are effective
September 15, 2005. The incorporation
by reference of FAA Order 7400.9N is
approved by the Director of the Federal
Register as of September 15, 2005,
through September 15, 2006.
DATES:
FOR FURTHER INFORMATION CONTACT:
Tameka Bentley, telephone (202) 267–
8783.
Issued in Washington, DC on September
16, 2005.
Michael Chase,
[Docket No. 29334; Amendment No. 71–37]
Airspace Designations; Incorporation
by Reference; Correction
Branch Manager, Air Traffic and Airman and
Airport Certification Law, Regulations
Division.
[FR Doc. 05–18890 Filed 9–16–05; 3:48pm]
BILLING CODE 4910–13–M
14 CFR Part 71
Federal Aviation
Administration (FAA), DOT.
AGENCY:
PO 00000
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21SER1
]]>Agencies
[Federal Register Volume 70, Number 182 (Wednesday, September 21, 2005)]
[Rules and Regulations]
[Pages 55248-55250]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-18526]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20802; Directorate Identifier 2005-CE-18-AD;
Amendment 39-14282; AD 2005-19-17]
RIN 2120-AA64
Airworthiness Directives; PZL-Swidnik S.A. Models PW-5 ``Smyk''
and PW-6U Gliders
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA adopts a new airworthiness directive (AD) for certain
PZL-Swidnik S.A. (PZL-Swidnik) Models PW-5 ``Smyk'' and PW-6U gliders.
This AD requires you to inspect for the minimum dimension of the left
side aileron, right side aileron, and airbrake push-rod ends for
certain Model PW-5 ``Smyk'' gliders; inspect for the minimum dimension
of the aileron, airbrake, and elevator control push-rod ends for
certain Model PW-6U gliders; and replace any push-rod end that does not
meet the minimum dimension. This AD results from mandatory continuing
airworthiness information (MCAI) issued by the airworthiness authority
for Poland. We are issuing this AD to detect and replace any push-rod
end that does not meet the minimum dimension, which could result in
failure of the control system. This failure could lead to loss of
control of the glider.
DATES: This AD becomes effective on October 31, 2005.
As of October 31, 2005, the Director of the Federal Register
approved the incorporation by reference of certain publications listed
in the regulation.
ADDRESSES: To get the service information identified in this AD,
contact PZL-Swidnik S.A., Polish Aviation Works, Al. Lotnikow Polskich
1, 21-045 Swidnik, Poland; telephone: 48 81 468 09 01 751 20 71;
facsimile: 48 81 468 09 19 751 21 73.
To view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC 20590-001 or on the Internet at https://
dms.dot.gov. The docket number is FAA-2005-20802; Directorate
Identifier 2005-CE-18-AD.
FOR FURTHER INFORMATION CONTACT: Greg Davison, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4130; facsimile: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
What events have caused this AD? The General Inspectorate of Civil
Aviation (GICA), which is the airworthiness authority for Poland,
recently notified FAA that an unsafe condition may exist on certain
PZL-Swidnik S.A. (PZL-Swidnik) gliders. The GICA reports that an owner
of a Model PW-6U glider found the dimension of the push-rod end to not
meet the minimum dimension of 0.165 inches (in.) or 4.2 millimeter
(mm). Further, the GICA reports that the manufacturer has identified a
production run of these parts that do not meet the minimum dimension of
the push-rod end. Similar push-rod ends, where applicable, are used to
link the ailerons, airbrakes, and elevator control systems in the
Models PW-5 ``Smyk'' and PW-6U gliders.
What is the potential impact if FAA took no action? Any push-rod
end that does not meet the minimum dimension could result in failure of
the control system. This failure could lead to loss of control of the
glider.
Has FAA taken any action to this point? We issued a proposal to
amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to
include an AD that would apply to certain PZL-Swidnik S.A. (PZL-
Swidnik) Models PW-5 ``Smyk'' and PW-6U gliders. This proposal was
published in the Federal Register as a notice of proposed rulemaking
(NPRM) on April 27, 2005 (70 FR 21691). The NPRM proposed to require
you to inspect for the minimum dimension of the left side aileron,
right side aileron, and airbrake push-rod ends for certain Model PW-5
``Smyk'' gliders; inspect for the minimum dimension of the aileron,
airbrake, and elevator control push-rod ends for certain Model PW-6U
gliders; and replace any push-rod end that does not meet the minimum
dimension.
Comments
Was the public invited to comment? We provided the public the
opportunity to participate in developing this AD. We received no
comments on the proposal or on the determination of the cost to the
public.
Conclusion
What is FAA's final determination on this issue? We have carefully
reviewed the available data and determined that air safety and the
public interest require adopting the AD as proposed except for minor
editorial corrections. We have determined that these minor corrections:
--Are consistent with the intent that was proposed in the NPRM for
correcting the unsafe condition; and
--Do not add any additional burden upon the public than was already
proposed in the NPRM.
Changes to 14 CFR Part 39--Effect on the AD
How does the revision to 14 CFR part 39 affect this AD? On July 10,
2002, the FAA published a new version of 14 CFR part 39 (67 FR 47997,
July 22, 2002), which governs the FAA's AD system. This regulation now
includes material that relates to altered products, special flight
permits, and alternative methods of compliance. This material
previously was included in each individual AD. Since this material is
included in 14 CFR part 39, we will not include it in future AD
actions.
Costs of Compliance
How many gliders does this AD impact? We estimate that this AD
affects 67 gliders in the U.S. registry.
What is the cost impact of this AD on owners/operators of the
affected gliders? We estimate the following costs to do the inspection
of the push-rod ends:
[[Page 55249]]
----------------------------------------------------------------------------------------------------------------
Total cost per
Labor cost Parts cost glider Total cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
1 work hour x $65 = $65............. Not applicable......... $65 67 x $65 = $4,355.
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to do any necessary push-rod end
replacements that would be required based on the results of this
inspection. We have no way of determining the number of gliders that
may need this replacement:
------------------------------------------------------------------------
Total cost per
Labor cost per push-rod end Parts cost push-rod end per
glider
------------------------------------------------------------------------
1 work hour x $65 = $65......... Not applicable..... $65
------------------------------------------------------------------------
The manufacturer has stated that the costs for any required parts
and transportation of the parts will be covered under the
manufacturer's warranty.
Authority for This Rulemaking
What authority does FAA have for issuing this rulemaking action?
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 AD.
Regulatory Findings
Will this AD impact various entities? We have 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.
Will this AD involve a significant rule or regulatory action? For
the reasons discussed above, I certify that 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); 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 summary of the costs to comply with this AD (and
other information as included in the Regulatory Evaluation) and placed
it in the AD Docket. You may get a copy of this summary by sending a
request to us at the address listed under ADDRESSES. Include ``Docket
No. FAA-2005-20802; Directorate Identifier 2005-CE-18-AD'' in your
request.
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 Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (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. FAA amends Sec. 39.13 by adding a new AD to read as follows:
2005-19-17 PZL-Swidnik S.A.: Amendment 39-14282; Docket No. FAA-
2005-20802; Directorate Identifier 2005-CE-18-AD.
When Does This AD Become Effective?
(a) This AD becomes effective on October 31, 2005.
What Other ADs Are Affected by This Action?
(b) None.
What Gliders Are Affected by This AD?
(c) This AD affects the following glider models and serial
numbers that are certificated in any category:
------------------------------------------------------------------------
Model Serial Nos.
------------------------------------------------------------------------
PW-5 ``Smyk''......................... 17.12.022 through 17.12.024.
PW-6U................................. 78.02.07 through 78.02.10 and
78.03.01 through 78.03.03.
------------------------------------------------------------------------
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for Poland.
The actions specified in this AD are intended to detect and replace
any push-rod end that does not meet the minimum dimension, which
could result in failure of the control system. This failure could
lead to loss of control of the glider.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
[[Page 55250]]
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Actions Compliance Procedures
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(1) Inspect for the minimum Within the next 25 For the Model PW-5
dimension (0.165 inches (in.) hours time-in- ``Smyk'' glider:
or 4.2 millimeter (mm)): service (TIS) Follow
(i) Any left side aileron, right after October 31, Communication
side aileron, and airbrake push- 2005 (the Equipment Factory
rod end (part number (P/N) effective date of PZL-Swidnik
511.00.20.00) for the Model PW- this AD), unless Mandatory
5 ``Smyk'' glider; and. already done. Bulletin Number
(ii) Any aileron, airbake, and BO-17-03-18,
elevator control push-rod end dated December
(P/N 78.21.215.00.00) for the 22, 2003. For the
Model PW-6U glider. Model PW-6U
glider: Follow
Communication
Equipment PZL-
Swidnik Mandatory
Bulletin Number
BO-78-03-06,
dated December
22, 2003.
(2) Replace any push-rod end (P/ Before further For the Model PW-5
N 511.00.20.00 or flight after the ``Smyk'' glider:
78.21.215.00.00) that you find the inspection Follow
as a result of the inspection requried by Communication
requried by paragraph (e)(1) of paragraph (e)(1) Equipment PZL-
this AD that has a push-rod end of this AD. Swidnik Mandatory
that is less than the minimum Bulletin Number
dimension (0.165 in. or 4.2 mm). BO-17-03-18,
dated December
22, 2003. For the
Model PW-6U
glider: Follow
Communication
Equipment Factory
PZL-Swidnik
Mandatory
Bulletin NumberBO-
17-03-18, dated
December 22,
2003.
(3) Do not install any push-rod As of October 31, For the Model PW-5
end (P/N 511.00.20.00 or 200 (the ``Smyk'' glider:
78.21.215.00.00) with a effective date of Follow
dimension that is less than the this AD). Communicaton
minimum dimension (0.165 in. or Equipment Factory
4.2 mm): PZL-Swidnik
(i) Any push-rod end for the Mandatory
left side aileron, right side Bulletin Number
aileron, or airbrake of the BO-17-03-18,
Model PW-5 Swidnik glider; and. dated December
(ii) Any push-rod end for the 22, 2003. For the
ailerons, airbake, or elevator Model PW-6U
control of the Model PW-6U glider: Follow
glider. Communication
Equipment Factory
PZL-Swidnik
Mandatory
Bulletin Number
BO-78-03-06,
dated December
22, 2003.
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May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Standards Office, Small
Airplane Directorate, FAA. For information on any already approved
alternative methods of compliance, contact Greg Davison, Aerospace
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone: (816) 329-4130; facsimile:
(816) 329-4090.
Is There Other Information That Relates to This Subject?
(g) Polish AD Numbers SP-0085-2003-A, dated December 22, 2003,
and SP-0086-2003, dated December 22, 2003, also address the subject
of this AD.
Does This AD Incorporate Any Material by Reference?
(h) You must do the actions required by this AD following the
instructions in Communication Equipment Factory PZL-Swidnik
Mandatory Bulletin Number BO-17-03-18, dated December 22, 2003, and
Communication Equipment Factory PZL-Swidnik Mandatory Bulletin
Number BO-78-03-06, dated December 22, 2003. The Director of the
Federal Register approved the incorporation by reference of this
service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part
51. To get a copy of this service information, contact PZL-Swidnik
S.A., Polish Aviation Works, Al. Lotnikow Polskich 1, 21-045
Swidnik, Poland; telephone: 48 81 468 09 01 751 20 71; facsimile: 48
81 468 09 19 751 21 73. To review copies of this service
information, go to the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, go to: https://www.archives.gov/federal_register/code_of_
federal_regulations/ibr_locations.html or call (202) 741-6030. To
view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif
Building, Room PL-401, Washington, DC 20590-001 or on the Internet
at https://dms.dot.gov. The docket number is FAA-2005-20802;
Directorate Identifier 2005-CE-18-AD.
Issued in Kansas City, Missouri, on September 12, 2005.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-18526 Filed 9-20-05; 8:45 am]
BILLING CODE 4910-13-P
