Airworthiness Directives; Air Tractor, Inc. Models AT-802 and AT-802A Airplanes, 43624-43625 [E9-20385]
Download as PDF
43624
Federal Register / Vol. 74, No. 165 / Thursday, August 27, 2009 / Rules and Regulations
Issued in Renton, Washington, on August
7, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E9–20274 Filed 8–26–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0489; Directorate
Identifier 2009–CE–025–AD; Amendment
39–16000; AD 2009–18–04]
RIN 2120–AA64
Airworthiness Directives; Air Tractor,
Inc. Models AT–802 and AT–802A
Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Air Tractor, Inc. Models AT–802 and
AT–802A airplanes. This AD requires
installing a rudder-aileron interconnect
cable system shield kit and securing any
items stowed in the baggage
compartment, using tie downs and/or a
cargo net until the cable shield kit is
installed. We are issuing this AD to
prevent jamming of the rudder-aileron
interconnect cables by unsecured items
in the baggage compartment, which
could result in failure of the rudderaileron interconnect cable system. This
failure could lead to loss of control.
DATES: This AD becomes effective on
October 1, 2009.
On October 1, 2009, the Director of
the Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: For service information
identified in this AD, contact Air
Tractor, Inc., P.O. Box 485, Olney, Texas
76374; telephone: (940) 564–5616;
facsimile: (940) 564–5612; E-mail:
parts@airtractor.com; Internet: https://
www.airtractor.com.
To view the AD docket, go to U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue, SE., Washington,
DC 20590, or on the Internet at https://
www.regulations.gov. The docket
number is FAA–2009–0489; Directorate
Identifier 2009–CE–025–AD.
FOR FURTHER INFORMATION CONTACT:
Andy McAnaul, Aerospace Engineer,
10100 Reunion Pl., Ste. 650, San
Antonio, Texas 78216; telephone: (210)
308–3365; fax: (210) 308–3370.
SUPPLEMENTARY INFORMATION:
airplanes. This proposal was published
in the Federal Register as a notice of
proposed rulemaking (NPRM) on May
29, 2009 (74 FR 25684). The NPRM
proposed to require installing a rudderaileron interconnect cable system shield
kit and securing any items stowed in the
baggage compartment, using tie downs
and/or a cargo net until the cable shield
kit is installed.
Discussion
On May 20, 2009, 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 Models AT–802 and AT–802A
Costs of Compliance
Parts
cost
Labor cost
Cable Shield Kit SL#274: 4.5 work-hours × $80 per hour = $360 ......................
Cable Shield Kit SL#274–2: 4.5 work-hours × $80 per hour = $360 ..................
srobinson on DSKHWCL6B1PROD with RULES
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
VerDate Nov<24>2008
16:19 Aug 26, 2009
Jkt 217001
$860
540
Fmt 4700
Sfmt 4700
Conclusion
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.
We estimate that this AD affects 210
airplanes in the U.S. registry.
We estimate the following costs to do
the modification:
affects 170 airplanes at $1,220 each ...
affects 40 airplanes at $900 each ........
Regulatory Findings
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.
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
Frm 00006
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.
Total cost per airplane
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this AD.
PO 00000
Comments
Total cost
on U.S.
operators
$207,400
36,000
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–2009–0489;
Directorate Identifier 2009–CE–025–
AD’’ in your request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
E:\FR\FM\27AUR1.SGM
27AUR1
Federal Register / Vol. 74, No. 165 / Thursday, August 27, 2009 / Rules and Regulations
§ 39.13
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
[Amended]
2. FAA amends § 39.13 by adding the
following new AD:
■
2009–18–04 Air Tractor, Inc.: Amendment
39–16000; Docket No. FAA–2009–0489;
Directorate Identifier 2009–CE–025–AD.
Effective Date
(a) This AD becomes effective on October
1, 2009.
Affected ADs
(b) None.
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
Applicability
(c) This AD applies to Models AT–802 and
AT–802A airplanes, serial numbers 802/
Actions
Before further flight after October 1, 2009 (the
effective date of this AD) until the installation of the rudder-aileron interconnect cable
shield kit required in paragraph (e)(2) of this
AD is done.
No later than December 31, 2009 ...................
(2) Install the following rudder-aileron interconnect cable shield kit, as applicable.
(i) For all airplanes equipped for agricultural spray operations and all fire-fighting
airplanes retrofitted with Gen II Fire Retardant Delivery System relay box, install
cable shield kit SL#274.
(ii) For all fire-fighting airplanes not
equipped with Gen II Fire Retardant Delivery System relay box, install cable
shield kit SL#274–2.
(iii) Installation of the applicable cable
shield kit SL#274 or SL#274–2 terminates the requirement of paragraph
(e)(1) of this AD.
Unsafe Condition
(d) This AD results from a report of the
rudder pedal cable becoming jammed in
flight. We are proposing this AD to prevent
jamming of the rudder-aileron interconnect
cables by unsecured items in the baggage
compartment, which could result in failure of
the rudder-aileron interconnect cable system.
This failure could lead to loss of control.
Compliance
(e) To address this problem, you must do
the following, unless already done:
Procedures
Alternative Methods of Compliance
(AMOCs)
(f) The Manager, Fort Worth Airplane
Certification 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: Andy McAnaul,
Aerospace Engineer, 10100 Reunion Pl., Ste.
650, San Antonio, Texas 78216; telephone:
(210) 308–3365; fax: (210) 308–3370. 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.
srobinson on DSKHWCL6B1PROD with RULES
802A–001 through 802/802A–0319, that are
certificated in any category.
Compliance
(1) Secure any items stowed in the baggage
compartment using tie down straps and/or a
cargo net.
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.
Material Incorporated by Reference
(g) You must use Snow Engineering Co.,
Service Letter #274, Revision A, dated April
6, 2009, 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 Air Tractor, Inc., P.O. Box
485, Olney, Texas 76374; telephone: (940)
564–5616; facsimile: (940) 564–5612; e-mail:
parts@airtractor.com; Internet: https://
www.airtractor.com.
(3) You may review copies of the service
information incorporated by reference for
Issued in Kansas City, Missouri, on August
18, 2009.
Scott A. Horn,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E9–20385 Filed 8–26–09; 8:45 am]
VerDate Nov<24>2008
16:19 Aug 26, 2009
Jkt 217001
BILLING CODE 4910–13–P
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
43625
Not applicable.
Snow Engineering Co., Service Letter #274,
Revision A, dated April 6, 2009.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0496; Directorate
Identifier 2008–NM–139–AD; Amendment
39–16001; AD 2009–18–05]
RIN 2120–AA64
Airworthiness Directives; Fokker
Model F.27 Mark 050 and F.28 Mark
0100 Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new
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 correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
E:\FR\FM\27AUR1.SGM
27AUR1
Agencies
[Federal Register Volume 74, Number 165 (Thursday, August 27, 2009)]
[Rules and Regulations]
[Pages 43624-43625]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-20385]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0489; Directorate Identifier 2009-CE-025-AD;
Amendment 39-16000; AD 2009-18-04]
RIN 2120-AA64
Airworthiness Directives; Air Tractor, Inc. Models AT-802 and AT-
802A Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Air Tractor, Inc. Models AT-802 and AT-802A airplanes. This AD requires
installing a rudder-aileron interconnect cable system shield kit and
securing any items stowed in the baggage compartment, using tie downs
and/or a cargo net until the cable shield kit is installed. We are
issuing this AD to prevent jamming of the rudder-aileron interconnect
cables by unsecured items in the baggage compartment, which could
result in failure of the rudder-aileron interconnect cable system. This
failure could lead to loss of control.
DATES: This AD becomes effective on October 1, 2009.
On October 1, 2009, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in this
AD.
ADDRESSES: For service information identified in this AD, contact Air
Tractor, Inc., P.O. Box 485, Olney, Texas 76374; telephone: (940) 564-
5616; facsimile: (940) 564-5612; E-mail: parts@airtractor.com;
Internet: https://www.airtractor.com.
To view the AD docket, go to U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at
https://www.regulations.gov. The docket number is FAA-2009-0489;
Directorate Identifier 2009-CE-025-AD.
FOR FURTHER INFORMATION CONTACT: Andy McAnaul, Aerospace Engineer,
10100 Reunion Pl., Ste. 650, San Antonio, Texas 78216; telephone: (210)
308-3365; fax: (210) 308-3370.
SUPPLEMENTARY INFORMATION:
Discussion
On May 20, 2009, 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 Models AT-802 and AT-802A airplanes. This
proposal was published in the Federal Register as a notice of proposed
rulemaking (NPRM) on May 29, 2009 (74 FR 25684). The NPRM proposed to
require installing a rudder-aileron interconnect cable system shield
kit and securing any items stowed in the baggage compartment, using tie
downs and/or a cargo net until the cable shield kit is installed.
Comments
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
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.
Costs of Compliance
We estimate that this AD affects 210 airplanes in the U.S.
registry.
We estimate the following costs to do the modification:
------------------------------------------------------------------------
Total cost
Labor cost Parts Total cost per on U.S.
cost airplane operators
------------------------------------------------------------------------
Cable Shield Kit SL274: 4.5 work-hours x $80 airplanes at
per hour = $360. $1,220 each.
Cable Shield Kit SL274- 540 affects 40 36,000
2: 4.5 work-hours x $80 per airplanes at
hour = $360. $900 each.
------------------------------------------------------------------------
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 AD.
Regulatory Findings
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.
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-2009-0489; Directorate Identifier 2009-CE-025-AD'' in your
request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
[[Page 43625]]
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 the following new AD:
2009-18-04 Air Tractor, Inc.: Amendment 39-16000; Docket No. FAA-
2009-0489; Directorate Identifier 2009-CE-025-AD.
Effective Date
(a) This AD becomes effective on October 1, 2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Models AT-802 and AT-802A airplanes,
serial numbers 802/802A-001 through 802/802A-0319, that are
certificated in any category.
Unsafe Condition
(d) This AD results from a report of the rudder pedal cable
becoming jammed in flight. We are proposing this AD to prevent
jamming of the rudder-aileron interconnect cables by unsecured items
in the baggage compartment, which could result in failure of the
rudder-aileron interconnect cable system. This failure could lead to
loss of control.
Compliance
(e) To address this problem, you must do the following, unless
already done:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Secure any items stowed Before further Not applicable.
in the baggage compartment flight after
using tie down straps and/ October 1, 2009
or a cargo net. (the effective date
of this AD) until
the installation of
the rudder-aileron
interconnect cable
shield kit required
in paragraph (e)(2)
of this AD is done.
(2) Install the following No later than Snow Engineering
rudder-aileron interconnect December 31, 2009. Co., Service Letter
cable shield kit, as 274,
applicable. Revision A, dated
April 6, 2009.
(i) For all airplanes
equipped for
agricultural spray
operations and all
fire[dash]fighting
airplanes retrofitted
with Gen II Fire
Retardant Delivery
System relay box,
install cable shield kit
SL274.
(ii) For all fire-
fighting airplanes not
equipped with Gen II
Fire Retardant Delivery
System relay box,
install cable shield kit
SL274-2.
(iii) Installation of the
applicable cable shield
kit SL274 or
SL274-2
terminates the
requirement of paragraph
(e)(1) of this AD.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(f) The Manager, Fort Worth Airplane Certification 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: Andy
McAnaul, Aerospace Engineer, 10100 Reunion Pl., Ste. 650, San
Antonio, Texas 78216; telephone: (210) 308-3365; fax: (210) 308-
3370. 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 Snow Engineering Co., Service Letter
274, Revision A, dated April 6, 2009, 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 Air
Tractor, Inc., P.O. Box 485, Olney, Texas 76374; telephone: (940)
564-5616; facsimile: (940) 564-5612; e-mail: parts@airtractor.com;
Internet: https://www.airtractor.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: https://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Kansas City, Missouri, on August 18, 2009.
Scott A. Horn,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-20385 Filed 8-26-09; 8:45 am]
BILLING CODE 4910-13-P