Modification of Class E Airspace; Peru, IL, 18383 [07-1803]
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Federal Register / Vol. 72, No. 70 / Thursday, April 12, 2007 / Rules and Regulations
Special Flight Permit
(f) Under 14 CFR 39.23, we are allowing
special flight permits for the purpose of
compliance with this AD under the following
conditions: Only operate under day visual
flight rules (VFR).
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, Wichita Aircraft
Certification Office (ACO), FAA, ATTN:
Trenton Shepherd, Aerospace Engineer,
Wichita ACO, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; telephone: (316) 946–
4143; fax: (316) 946–4107, has the authority
to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
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.
(h) AMOCs approved for AD 2006–17–04
are not approved for this AD.
Material Incorporated by Reference
(i) You must use Cessna Service Bulletin
No. SB07–71–01, Revision 1, dated March 16,
2007, 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 The Cessna Aircraft
Company, Product Support, P.O. Box 7706,
Wichita, Kansas 67277–7706; telephone:
(316) 517–5800; facsimile: (316) 942–9006.
(3) You may review copies at the FAA,
Central Region, Office of the Regional
Counsel, 901 Locust, 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
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Appendix to AD 2007–08–03—
Inspection Instructions—Cessna
Aircraft Company Models 172R, 172S,
182T, T182T, 206H, and T206H
Airplanes
1. Remove upper and side cowlings to
perform torque procedure.
2. Remove all signs of old torque putty or
paint.
3. Using a suitable tool loosen the hose end
fitting of each joint, while using a suitable
tool to restrain the other end fitting of the
joint to preclude rotation.
4. Using the applicable fitting torque from
the table Torque Values for Hose End Fittings
of this appendix to AD 2007–08–03, torque
the hose end fitting to the proper torque,
while using a suitable tool to restrain the
other end fitting of the joint to preclude
rotation.
5. After proper torque has been applied to
the hose end fitting, apply the applicable
torque paint or putty to the hose end fitting
joint.
6. If during any torque procedure any of
the non-hose end fittings rotate, stop the
torque procedure. Totally disconnect the
hose end joint and remove any fitting that
has rotated. After the cleaning, visual
examination, and/or replacement of the
fitting and/or any seals or sealant, reinstall
the fitting and torque it to the applicable
requirement. Then reconnect the hose end
fitting and repeat Step 4. of this appendix to
AD 2007–08–03.
7. Use the table below Torque Values for
Hose End Fittings for the correct torque
values to tighten the hose end fittings as
required in paragraphs (e)(1) and (e)(2) of this
AD:
TORQUE VALUES FOR HOSE END FITTINGS
Correct torque in inch-pounds
Flare hex sizes in fractions of an inch
Hose size
Minimum
¥4
¥6
¥8
⁄
................................................................................................................................................
..............................................................................................................................................
7⁄8 .................................................................................................................................................
9 16
⁄
11 16
Issued in Kansas City, Missouri, on April
5, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E7–6826 Filed 4–11–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2007–27110; Airspace
Docket No. 07–AGL–1]
Modification of Class E Airspace; Peru,
IL
Federal Aviation
Administration (FAA), DOT.
ACTION: Direct final rule; confirmation
of effective date.
rmajette on PROD1PC67 with RULES
AGENCY:
SUMMARY: This document confirms the
effective date of the direct final rule
which revises Class E airspace at Peru,
IL.
VerDate Aug<31>2005
14:18 Apr 11, 2007
Jkt 211001
EFFECTIVE DATE:
0901 UTC, May 10,
2007.
FOR FURTHER INFORMATION CONTACT:
Grant Nichols, System Support, DOT
Regional Headquarters Building, Federal
Aviation Administration, 901 Locust,
Kansas City, MO 64106; telephone (816)
329–2522.
The FAA
published this direct final rule with a
request for comments in the Federal
Register on February 26, 2007 (72 FR
8266). The FAA uses the direct final
rulemaking procedures for a noncontroversial rule where the FAA
believes that there will be no adverse
public comment. This direct final rule
advised the public that no adverse
comments were anticipated, and that
unless a written adverse comment, or a
written notice of intent to submit such
an adverse comment, were received
within the comment period, the
regulation would become effective on
May 10, 2007. No adverse comments
were received, and thus this notice
confirms that this direct final rule will
become effective on that date.
SUPPLEMENTARY INFORMATION:
PO 00000
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500
Issued in Forth Worth, Texas, on March 21,
2007.
Ronnie L. Uhlenhaker,
Manager, System Support Group, ATO
Central Service Area.
[FR Doc. 07–1803 Filed 4–11–07; 8:45 am]
BILLING CODE 4910–13–M
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2006–25997; Airspace
Docket No. 06–ANM–5]
Revision of Class E Airspace;
Redmond, OR
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This action will revise the
Class E airspace at Redmond, OR.
Additional Class E airspace is necessary
to accommodate aircraft using a new
Area Navigation (RNAV) Global
Positioning System (GPS) Standard
E:\FR\FM\12APR1.SGM
12APR1
]]>Agencies
[Federal Register Volume 72, Number 70 (Thursday, April 12, 2007)]
[Rules and Regulations]
[Page 18383]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 07-1803]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA-2007-27110; Airspace Docket No. 07-AGL-1]
Modification of Class E Airspace; Peru, IL
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Direct final rule; confirmation of effective date.
-----------------------------------------------------------------------
SUMMARY: This document confirms the effective date of the direct final
rule which revises Class E airspace at Peru, IL.
EFFECTIVE DATE: 0901 UTC, May 10, 2007.
FOR FURTHER INFORMATION CONTACT: Grant Nichols, System Support, DOT
Regional Headquarters Building, Federal Aviation Administration, 901
Locust, Kansas City, MO 64106; telephone (816) 329-2522.
SUPPLEMENTARY INFORMATION: The FAA published this direct final rule
with a request for comments in the Federal Register on February 26,
2007 (72 FR 8266). The FAA uses the direct final rulemaking procedures
for a non-controversial rule where the FAA believes that there will be
no adverse public comment. This direct final rule advised the public
that no adverse comments were anticipated, and that unless a written
adverse comment, or a written notice of intent to submit such an
adverse comment, were received within the comment period, the
regulation would become effective on May 10, 2007. No adverse comments
were received, and thus this notice confirms that this direct final
rule will become effective on that date.
Issued in Forth Worth, Texas, on March 21, 2007.
Ronnie L. Uhlenhaker,
Manager, System Support Group, ATO Central Service Area.
[FR Doc. 07-1803 Filed 4-11-07; 8:45 am]
BILLING CODE 4910-13-M
