Federal Register, Volume 74, Number 46, March 11, 2009, Pages 10455-10672 Page: 10,457
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Federal Register/Vol. 74, No. 46/Wednesday, March 11, 2009/Rules and Regulations
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-2008-1319;Directorate Identifier 2008-CE-071-
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:
PART 39-AIRWORTHINESS
DIRECTIVES
m 1. The authority citation for part 39
continues to read as follows:Authority: 49 U.S.C. 106(g), 40113, 44701.
39.13 [Amended]
m 2. FAA amends 39.13 by adding the
following new AD:
2009-05-12 Cessna Aircraft Company:
Amendment 39-15836; Docket No.
FAA-2008-1319; Directorate Identifier
2008-CE-071-AD.
Effective Date
(a) This AD becomes effective on April 15,
2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following
airplane models and serial numbers that are
certificated in any category:Model Serial Nos.
208 ............... 20800001 through 20800415 and 20800417 through 20800419.
208B ............. 208B0001 through 208B1081, 208B1083 through 208B1215, 208B1217 through 208B1257, 208B1259 through 208B1305,
208B1307, and 208B1309 through 208B1310.
Unsafe Condition the aileron upper quadrant assembly from Compliance
(d) This AD results from reports of a rotating and possibly contacting or (e) To address this problem, you must do
"catch" in the aileron control system when interfering with the aileron lower quadrant the following, unless already done:
the control yoke is turned. We are issuing assembly, which could result in limited roll
this AD to prevent the cable attach fitting on control and reduced handling capabilities.
Actions Compliance Procedures
Modify the aileron carry-through cable attach- Within the next 100 hours time-in-service after Follow the Accomplishment Instructions in
ment to the aileron upper quadrant with parts April 15, 2009 (the effective date of this AD) Cessna Caravan Service Bulletin CAB08-6,
of improved design. or within the next 6 months after April 15, dated October 27, 2008.
2009 (the effective date of this AD), which-
ever occurs first.Alternative Methods of Compliance
(AMOCs)
(f) The Manager, Wichita Aircraft
Certification Office (ACO), 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: Ann
Johnson, Aerospace Engineer, FAA, Wichita
Aircraft Certification Office, 1801 Airport
Road, Room 100, Wichita, Kansas 67209;
telephone: 316-946-4105; fax: 316-946-
4107; e-mail address: ann.johnson@faa.gov.
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.
Material Incorporated by Reference
(g) You must use Cessna Caravan Service
Bulletin CABO8-6, dated October 27, 2008, 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 Cessna Aircraft Company,P.O. Box 7704, Wichita, Kansas 67277;
telephone: (800) 423-7762 or (316) 517-6056;
Internet: http://www.cessna.com.
(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: http://www.archives.gov/federal register/
code_ofjederalregulations/!
ibr locations.html.
Issued in Kansas City, Missouri, on
February 27, 2009.
John Colomy,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E9-4828 Filed 3-10-09; 8:45 am]
BILLING CODE 4910-13-PDEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-1318; Directorate
Identifier 2008-NM-155-AD; Amendment
39-15848; AD 2009-06-12]
RIN 2120-AA64
Airworthiness Directives; Bombardier
Model CL-600-2B19 (Regional Jet
Series 100 & 440) Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are superseding an
existing airworthiness directive (AD) for
the products listed above. This AD
results from mandatory continuing
airworthiness information (MCAI)
originated by an aviation authority of
another country to identify and correct10457
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United States. Office of the Federal Register. Federal Register, Volume 74, Number 46, March 11, 2009, Pages 10455-10672, periodical, March 11, 2009; Washington D.C.. (https://digital.library.unt.edu/ark:/67531/metadc132908/m1/11/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.