Airworthiness Directives; Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P Airplanes, 43397-43398 [2010-18023]
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Federal Register / Vol. 75, No. 142 / Monday, July 26, 2010 / Rules and Regulations
Actions and Compliance
(f) Unless already done, do the following
actions:
(1) Before further flight as of April 6, 2010
(the effective date of AD 2010–08–01),
inspect the elevator inner hinges on the
stabilizer following paragraphs A.1., A.2.,
and A.4. of Aircraft Industries, a.s.
Mandatory Bulletin MB No.: L23/052a, dated
March 2, 2010.
(2) Repetitively thereafter at intervals not
to exceed every 1,000 hours time-in-service,
inspect the elevator inner hinges on the
stabilizer following paragraphs A.1., A.2.,
and A.4. of Aircraft Industries, a.s.
Mandatory Bulletin MB No.: L23/052a, dated
March 2, 2010.
(3) If, as a result of the inspection required
by paragraph (f)(1) or (f)(2) of this AD, you
find any elevator inner hinge on the elevator
is cracked or damaged, before further flight,
replace it following paragraphs A.3. and A.4.
of Aircraft Industries, a.s. Mandatory Bulletin
MB No.: L23/052a, dated March 2, 2010.
FAA AD Differences
Note: This AD differs from the MCAI and/
or service information as follows: No
differences.
wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
Other FAA AD Provisions
(g) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Standards Office,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. Send information to
ATTN: Greg Davison, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4130; fax: (816) 329–
4090. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your appropriate principal inspector
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(3) Reporting Requirements: For any
reporting requirement in this AD, under the
provisions of the Paperwork Reduction Act
(44 U.S.C. 3501 et seq.), the Office of
Management and Budget (OMB) has
approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
(h) Refer to MCAI EASA Emergency AD
No.: 2010–0037–E, dated March 8, 2010; and
Aircraft Industries, a.s. Mandatory Bulletin
MB No.: L23/052a, dated March 2, 2010, for
related information.
Material Incorporated by Reference
(h) You must use Aircraft Industries, a.s.
Mandatory Bulletin MB No.: L23/052a, dated
VerDate Mar<15>2010
14:07 Jul 23, 2010
Jkt 220001
March 2, 2010, to do the actions required by
this AD, unless the AD specifies otherwise.
(1) On April 26, 2010 (75 FR 17295, April
6, 2010), the Director of the Federal Register
previously approved the incorporation by
reference of Aircraft Industries, a.s.
Mandatory Bulletin MB No.: L23/052a, dated
March 2, 2010.
(2) For service information identified in
this AD, contact Aircraft Industries, a.s.–
´
Nazahonech1177, 686 04 Kunovice, Czech
Republic; telephone: +420 572 817 660; fax:
+420 572 816 112; e-mail: ots@let.cz;
Internet: https://www.let.cz.
(3) You may review copies of the service
information incorporated by reference for
this AD at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas
City, Missouri 64106. For information on the
availability of this material at the Central
Region, call (816) 329–3768.
(4) You may also review copies of the
service information incorporated by reference
for this AD at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call (202) 741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/ibr_
locations.html.
Issued in Kansas City, Missouri, on July 15,
2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2010–18022 Filed 7–23–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0122; Directorate
Identifier 2009–CE–067–AD; Amendment
39–16338; AD 2010–13–07]
RIN 2120–AA64
Airworthiness Directives; Piper
Aircraft, Inc. Models PA–32R–301T and
PA–46–350P Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
This document makes a
correction to AD 2010–13–07, which
was published in the Federal Register
on June 23, 2010 (75 FR 35619), and
applies to certain Piper Aircraft, Inc.
Models PA–32R–301T and PA–46–350P
airplanes. AD 2010–13–07 requires you
to replace V-band exhaust couplings,
part number (P/N) Lycoming 40D21162–
340M or Eaton/Aeroquip 55677–340M
with an improved design Eaton/
Aeroquip P/N NH1009399–10 or
Lycoming P/N 40D23255–340M. In the
Summary and Discussion sections of the
SUMMARY:
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
43397
published AD, we incorrectly stated that
the AD requires replacing any spotwelded, V-band exhaust coupling with
a riveted, V-band exhaust coupling
instead of stating the specific P/N to be
replaced. Also, in the Cost of
Compliance section, we incorrectly
stated that Model PA–32R–301T
airplanes, instead of Model PA–46–350P
airplanes, are equipped with two of the
affected V-band clamps. We are issuing
this document to help eliminate any
confusion that this AD may have
created.
DATES: The effective date of this
correction is July 26, 2010. The effective
date of this AD (2010–13–07) remains
July 28, 2010.
FOR FURTHER INFORMATION CONTACT:
Darby Mirocha, Aerospace Engineer,
FAA, Atlanta Aircraft Certification
Office (ACO), 1701 Columbia Avenue,
College Park, Georgia 30337; telephone:
(404) 474–5573; fax: (404) 474–5606; email: darby.mirocha@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On June 14, 2010, the FAA issued AD
2010–13–07, Amendment 39–16338 (75
FR 35619, June 23, 2010), which applies
to certain Piper Aircraft, Inc. Models
PA–32R–301T and PA–46–350P
airplanes. AD 2010–13–07 requires you
to replace V-band exhaust couplings, P/
N Lycoming 40D21162–340M or Eaton/
Aeroquip 55677–340M with an
improved design Eaton/Aeroquip P/N
NH1009399–10 or Lycoming P/N
40D23255–340M.
In the published AD, we incorrectly
stated in the the Summary and
Discussion sections that the AD requires
replacing any spot-welded, V-band
exhaust coupling with a riveted, V-band
exhaust coupling instead of stating the
specific P/N to be replaced. Also, in the
Cost of Compliance section, we
incorrectly stated which of the affected
model airplanes are equipped with two
of the affected V-band clamps.
Need for the Correction
This correction is needed to help
eliminate any confusion that this AD
may have created.
Correction of Publication
Accordingly, the publication of June
23, 2010 (75 FR 35619), of Amendment
39–16338; AD 2010–13–07, which was
the subject of FR Doc. 2010–14991, is
corrected as follows:
On page 35619, under the heading
‘‘Summary,’’ in line 5, change the word
‘‘any’’ to ‘‘specific.’’
On page 35620, under the heading
‘‘Discussion,’’ in line 11, change the
word ‘‘any’’ to ‘‘specific.’’
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26JYR1
43398
Federal Register / Vol. 75, No. 142 / Monday, July 26, 2010 / Rules and Regulations
On page 35620, under the heading
‘‘Comments,’’ under the subheading
‘‘Comment Issue No. 2: Correct the Cost
of Compliance,’’ in paragraph 3, change
the second sentence to ‘‘After further
research, we determined that Model
PA–46–350P (Mirage) has two of the
affected V-Band clamps installed, and
Model PA–32R–301T (Saratoga II TC)
has one.’’
On page 35620, under the heading
‘‘Costs of Compliance,’’ change the entire
section to read as follows:
‘‘We estimate that this AD affects 596
airplanes in the U.S. registry provided
they have the affected V-band exhaust
coupling installed.
We estimate the following costs to do
the replacement for Model PA–32R–
301T airplanes. These airplanes have
one V-band clamp installed:
Labor cost
Parts cost
2 work-hours × $85 per hour = $170 ..............................................................................................................................
We estimate the following costs to do
the replacement for Model PA–46–350P
$714
Parts cost
2 work-hours per V-band clamp. 2 clamps per airplane: 4 work-hours × $85 per hour
= $340.
$714 per V-band clamp. $714 × 2 =
$1,428.
Issued in Kansas City, Missouri, on July 15,
2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
Effective date 0901 UTC, July 29,
2010. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA
Order 7400.9 and publication of
conforming amendments.
[FR Doc. 2010–18023 Filed 7–23–10; 8:45 am]
FOR FURTHER INFORMATION CONTACT:
BILLING CODE 4910–13–P
Gallant, Airspace and Rules Group,
Office of System Operations Airspace
and AIM, Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591;
telephone: (202) 267–8783.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
DATES:
Paul
SUPPLEMENTARY INFORMATION:
14 CFR Part 73
History
[Docket No. FAA–2008–1261; Airspace
Docket No. 06–ASO–18]
Amendment and Establishment of
Restricted Areas and Other Special
Use Airspace, Avon Park Air Force
Range, FL
Federal Aviation
Administration (FAA), DOT.
AGENCY:
wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
ACTION:
Final rule, correction.
This action makes minor
corrections to the geographic
coordinates of restricted areas R–2901B,
R–2910J, R–2901K, R–2901L and R–
2901N, Avon Park, FL, in a final rule
published in the Federal Register on
Monday, May 24, 2010. The National
Aeronautical Navigation Services Office
requested these adjustments be made to
better align the restricted areas.
SUMMARY:
VerDate Mar<15>2010
17:01 Jul 23, 2010
Jkt 220001
$884
airplanes. These airplanes have two Vband clamps installed:
Labor cost
The effective date of this AD (2010–
13–07) remains July 28, 2010.
Total cost
per Model
PA–32R–
301T
airplane
On May 24, 2010, a final rule was
published in the Federal Register (75
FR 28752), Airspace Docket No. 06–
ASO–18, to modify the special use
airspace at the Avon Park Air Force
Range in Florida. As a result of further
review of the latitude/longitude
coordinates for the Avon Park Air Force
Range restricted areas, the Aeronautical
Navigation Services Office (formerly the
National Aeronautical Charting Office)
determined that a minor refinement was
needed for two points in several
restricted area descriptions. The
correction adjusts the longitude
coordinate by six seconds for one point
and by two seconds for the second
point. Specifically, the longitude point
in lat. 27°32′31″ N., long. 81°07′ 29″ W.,
is corrected to read ‘‘long. 81°07′23″ W.″,
and; the longitude point in lat.
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
Total cost
per Model
PA–46–
350P
airplane
$1,768
27°29′31″ N., long. 81°05′29″ W., is
corrected to read ‘‘long. 81°05′27″ W’’
List of Subjects in 14 CFR Part 73
Airspace, Prohibited Areas, Restricted
Areas.
Correction to Final Rule
Accordingly, pursuant to the authority
delegated to me, the legal descriptions
of R–2901B, R–2901J, R–2901K, R–
2901L, and R–2901N, as published in
the Federal Register on May 24, 2010
(75 FR 28752), Airspace Docket 06–
ASO–18, and incorporated by reference
in 14 CFR part 73, is corrected as
follows:
■
§ 73.29
[Amended]
On page 28755, column 2, correct two
coordinates for restricted areas R–2901B
and R–2910J; and on page 28756,
columns 1 and 2, correct two
coordinates for restricted areas
R–2901K, R–2901L and R–2901N, Avon
Park, FL, to read as follows:
*
*
*
*
*
R–2901B Avon Park, FL [Corrected]
By removing lat. 27°32′31″ N., long.
81°07′29″ W., and substituting lat. 27°32′21″
N., long. 81°07′23″ W.; and by removing lat.
27°29′31″ N., long. 81°05′29″ W., and
substituting lat. 27°29′31″ N., long. 81°05′27″
W.
R–2901J Avon Park, FL [Corrected]
By removing lat. 27°32′31″ N., long.
81°07′29″ W., and substituting lat. 27°32′21″
N., long. 81°07′23″ W.; and by removing lat.
27°29′31″ N., long. 81°05′29″ W., and
E:\FR\FM\26JYR1.SGM
26JYR1
]]>Agencies
[Federal Register Volume 75, Number 142 (Monday, July 26, 2010)]
[Rules and Regulations]
[Pages 43397-43398]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-18023]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0122; Directorate Identifier 2009-CE-067-AD;
Amendment 39-16338; AD 2010-13-07]
RIN 2120-AA64
Airworthiness Directives; Piper Aircraft, Inc. Models PA-32R-301T
and PA-46-350P Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to AD 2010-13-07, which was
published in the Federal Register on June 23, 2010 (75 FR 35619), and
applies to certain Piper Aircraft, Inc. Models PA-32R-301T and PA-46-
350P airplanes. AD 2010-13-07 requires you to replace V-band exhaust
couplings, part number (P/N) Lycoming 40D21162-340M or Eaton/Aeroquip
55677-340M with an improved design Eaton/Aeroquip P/N NH1009399-10 or
Lycoming P/N 40D23255-340M. In the Summary and Discussion sections of
the published AD, we incorrectly stated that the AD requires replacing
any spot-welded, V-band exhaust coupling with a riveted, V-band exhaust
coupling instead of stating the specific P/N to be replaced. Also, in
the Cost of Compliance section, we incorrectly stated that Model PA-
32R-301T airplanes, instead of Model PA-46-350P airplanes, are equipped
with two of the affected V-band clamps. We are issuing this document to
help eliminate any confusion that this AD may have created.
DATES: The effective date of this correction is July 26, 2010. The
effective date of this AD (2010-13-07) remains July 28, 2010.
FOR FURTHER INFORMATION CONTACT: Darby Mirocha, Aerospace Engineer,
FAA, Atlanta Aircraft Certification Office (ACO), 1701 Columbia Avenue,
College Park, Georgia 30337; telephone: (404) 474-5573; fax: (404) 474-
5606; e-mail: darby.mirocha@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On June 14, 2010, the FAA issued AD 2010-13-07, Amendment 39-16338
(75 FR 35619, June 23, 2010), which applies to certain Piper Aircraft,
Inc. Models PA-32R-301T and PA-46-350P airplanes. AD 2010-13-07
requires you to replace V-band exhaust couplings, P/N Lycoming
40D21162-340M or Eaton/Aeroquip 55677-340M with an improved design
Eaton/Aeroquip P/N NH1009399-10 or Lycoming P/N 40D23255-340M.
In the published AD, we incorrectly stated in the the Summary and
Discussion sections that the AD requires replacing any spot-welded, V-
band exhaust coupling with a riveted, V-band exhaust coupling instead
of stating the specific P/N to be replaced. Also, in the Cost of
Compliance section, we incorrectly stated which of the affected model
airplanes are equipped with two of the affected V-band clamps.
Need for the Correction
This correction is needed to help eliminate any confusion that this
AD may have created.
Correction of Publication
Accordingly, the publication of June 23, 2010 (75 FR 35619), of
Amendment 39-16338; AD 2010-13-07, which was the subject of FR Doc.
2010-14991, is corrected as follows:
On page 35619, under the heading ``Summary,'' in line 5, change the
word ``any'' to ``specific.''
On page 35620, under the heading ``Discussion,'' in line 11, change
the word ``any'' to ``specific.''
[[Page 43398]]
On page 35620, under the heading ``Comments,'' under the subheading
``Comment Issue No. 2: Correct the Cost of Compliance,'' in paragraph
3, change the second sentence to ``After further research, we
determined that Model PA-46-350P (Mirage) has two of the affected V-
Band clamps installed, and Model PA-32R-301T (Saratoga II TC) has
one.''
On page 35620, under the heading ``Costs of Compliance,'' change
the entire section to read as follows:
``We estimate that this AD affects 596 airplanes in the U.S.
registry provided they have the affected V-band exhaust coupling
installed.
We estimate the following costs to do the replacement for Model PA-
32R-301T airplanes. These airplanes have one V-band clamp installed:
------------------------------------------------------------------------
Total cost
per Model
Labor cost Parts cost PA-32R-301T
airplane
------------------------------------------------------------------------
2 work-hours x $85 per hour = $170............ $714 $884
------------------------------------------------------------------------
We estimate the following costs to do the replacement for Model
PA-46-350P airplanes. These airplanes have two V-band clamps installed:
------------------------------------------------------------------------
Total cost
per Model
Labor cost Parts cost PA-46-350P
airplane
------------------------------------------------------------------------
2 work-hours per V-band clamp. 2 $714 per V-band clamp. $1,768
clamps per airplane: 4 work-hours $714 x 2 = $1,428.
x $85 per hour = $340.
------------------------------------------------------------------------
The effective date of this AD (2010-13-07) remains July 28, 2010.
Issued in Kansas City, Missouri, on July 15, 2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-18023 Filed 7-23-10; 8:45 am]
BILLING CODE 4910-13-P
