Airworthiness Directives; RECARO Aircraft Seating GmbH & Co. (RECARO) Model 3410 Seats, 49326-49327 [E6-13911]
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sroberts on PROD1PC70 with RULES
49326
Federal Register / Vol. 71, No. 163 / Wednesday, August 23, 2006 / Rules and Regulations
(vii) Shipments of such fruit must
move by direct route, in Customs bond
and under official seal, without
diversion or change of entry en route,
from the port of entry to the port of exit
or to an approved port in the United
States for export to another foreign
country.
(viii) Shipments of such fruit may not
traverse the counties of Cameron,
Hidalgo, Starr, or Willacy, TX.
Shipments of such fruit may only
traverse areas listed under each type of
carrier listed below.
(3) Truck movement. Trucks may haul
refrigerated containers of such fruit from
Mexico to shipside, or to approved
refrigerated storage pending lading
aboard ship, in Corpus Christi,
Galveston, or Houston, TX, or alongside
railway carriers or aircraft at the ports
named in paragraph (b)(2) of this section
for movement to a foreign country.
Shipments of such fruit via truck may
traverse only the territory within the
United States bounded on the west by
a line starting at Laredo, TX, on to El
Paso, TX, to Salt Lake City, UT, and
then to Portland, OR, and on the east by
a line drawn from Laredo, TX to
Hebbronville, TX, to Corpus Christi, TX,
to Galveston, TX, to Kinder, LA, to
Memphis, TN, and then to Louisville,
KY, and routes directly northward.
(4) Rail movement. Shipments must
move by direct route from the port of
entry to the port of exit or to an
approved North Atlantic port in the
United States for export to another
foreign country, as follows: The fruit
may be entered at Nogales, AZ, only for
direct rail routing to El Paso, TX, after
which it shall traverse only the territory
bounded on the west by a line drawn
from Laredo, TX, to El Paso, TX, to Salt
Lake City, UT, and then to Portland, OR,
and on the east by a line drawn from
Laredo, TX, to Hebbronville, TX, to
Corpus Christi, TX, to Galveston, TX, to
Kinder, LA, to Memphis, TN, and then
to Louisville, KY, and routes directly
northward. Such fruit may also enter the
United States from Mexico at any port
listed in paragraph (b)(1) of this section,
for direct eastward rail movement,
without diversion en route, for reentry
into Mexico.
(5) Air cargo movement. Shipments of
such fruit may move by direct route as
air cargo, without change of entry while
in the United States en route from the
port of entry, to Canada. If an emergency
occurs en route to the port of export that
will require transshipment to another
carrier, an inspector at the port of entry
must be contacted immediately.
*
*
*
*
*
(e) Untreated fruit from certain
municipalities in Mexico. Oranges,
VerDate Aug<31>2005
17:06 Aug 22, 2006
Jkt 208001
tangerines, and grapefruit in transit to
foreign countries may be imported from
certain municipalities in Mexico listed
in § 319.56–2(h) of this chapter in
accordance with the applicable
conditions in §§ 319.56 through 319.56–
8 of this chapter.
*
*
*
*
*
(Approved by the Office of Management and
Budget under control number 0579–0303)
Done in Washington, DC, this 17th day of
August 2006.
Kevin Shea,
Acting Administrator, Animal and Plant
Health Inspection Service.
[FR Doc. E6–13986 Filed 8–22–06; 8:45 am]
Room PL–401 on the plaza level of the
Nassif Building, 400 Seventh Street,
SW., Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Lee, Aerospace Engineer, Boston
Aircraft Certification Office, FAA,
Engine & Propeller Directorate, 12 New
England Executive Park, Burlington, MA
01803; telephone (781) 238–7161; fax
(781) 238–7170.
Federal Aviation Administration
The FAA
proposed to amend 14 CFR part 39 with
a proposed AD. The proposed AD
applies to certain RECARO Model 3410
302, 303, 306, 307, 314, 316, 317, 791,
792, and 795 series seats. We published
the proposed AD in the Federal Register
on February 8, 2006 (71 FR 6420). That
action proposed to require replacing the
existing attachment bolts for the seat
belts with longer attachment bolts.
14 CFR Part 39
Examining the AD Docket
BILLING CODE 3410–34–P
DEPARTMENT OF TRANSPORTATION
[Docket No. FAA–2005–22876; Directorate
Identifier 2005–NE–39–AD; Amendment 39–
14734; AD 2006–17–13]
RIN 2120–AA64
Airworthiness Directives; RECARO
Aircraft Seating GmbH & Co.
(RECARO) Model 3410 Seats
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
RECARO Model 3410 302, 303, 306,
307, 314, 316, 317, 791, 792, and 795
series seats. This AD requires replacing
the existing attachment bolts for the seat
belts with longer attachment bolts. This
AD results from a report of short
attachment bolts that don’t allow
enough thread to properly secure the
locknuts. We are issuing this AD to
prevent a seat belt from detaching due
to a loose locknut and attachment bolt,
which could result in injury to an
occupant during emergency conditions.
DATES: This AD becomes effective
September 27, 2006. The Director of the
Federal Register approved the
incorporation by reference of certain
publications listed in the regulations as
of September 27, 2006.
ADDRESSES: You can get the service
information identified in this AD from
RECARO Aircraft Seating GmbH & Co.
K, Technical Publications,
Daimlerstrasse 21, 74523 Schwebisch
Hall, Germany; Telephone 49 791 503
7183; fax 49 791 503 7220.
You may examine the AD docket on
the Internet at https://dms.dot.gov or in
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
SUPPLEMENTARY INFORMATION:
You may examine the docket that
contains the AD, any comments
received, and any final disposition in
person at the Docket Management
Facility Docket Offices between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The Docket
Office (telephone (800) 647–5227) is
located on the plaza level of the
Department of Transportation Nassif
Building at the street address stated in
ADDRESSES. Comments will be available
in the AD docket shortly after the DMS
receives them.
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comment received.
One commenter, the Boeing Airplane
Company, asks us to remove the 737
aircraft minor model designator ‘‘–200’’
from the applicability of this AD. Boeing
states that research of the configurations
for all delivered Boeing 737–200
airplanes failed to reveal any of the
affected seats installed on those
airplanes. However, Boeing states that
RECARO reported to Boeing that seats
were installed in a 737–200 airplane.
Boeing believes an operator installed the
seats after production of the airplane.
Boeing also has records of installing
seats with the affected model numbers
on 737–700 and 737–800 airplanes.
Boeing states that those seats
incorporate the longer bolts specified in
RECARO service bulletin SB–No.: 3410–
25MR477, Revision 3, dated May 17,
2004, and we should use the generic 737
designation without a minor model
designator. We partially agree. This AD
applies to the RECARO seat models
identified in paragraph (c) of this AD.
E:\FR\FM\23AUR1.SGM
23AUR1
Federal Register / Vol. 71, No. 163 / Wednesday, August 23, 2006 / Rules and Regulations
We list the known airplane models that
use these types of seats to help owners
and operators to determine if their
airplane might use these seats. Listing
the minor model designators for the 737
airplanes that could use these seats will
help operators determine if this AD
might apply to them. We retained the
–200 designation, and added the –700
and –800 designations to the ‘‘used on
but not limited to’’ statement in the
Applicability.
Conclusion
We have carefully reviewed the
available data, including the comment
received, and determined that air safety
and the public interest require adopting
the AD with the changes described
previously. We have determined that
these changes will neither increase the
economic burden on any operator nor
increase the scope of the AD.
Costs of Compliance
We estimate that this AD will affect
3,101 seats installed in airplanes of U.S.
registry. We also estimate that it will
take about 0.10 work-hour per seat to
perform the actions, and that the
average labor rate is $65 per work-hour.
Required parts will cost about $10 per
seat. Based on these figures, we estimate
the total cost of this AD to U.S.
operators to be $51,166.
sroberts on PROD1PC70 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
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
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
VerDate Aug<31>2005
15:49 Aug 22, 2006
Jkt 208001
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
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 placed it in
the AD Docket. You may get a copy of
this summary at the address listed
under ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
49327
Compliance
(e) You are responsible for having the
actions required by this AD performed within
60 days after the effective date of this AD,
unless the actions have already been done.
Replacing the Attachment Bolt
(f) For RECARO Model 3410 302, 303, 306,
307, 314, 316, 317, 791, 792, and 795 series
seats with a serial number listed in section
1.A. Effectivity of RECARO service bulletin
SB–No.: 3410–25MR477, Revision 3, dated
May 17, 2004, replace the seat belt
attachment bolt and nut. Use section 2.
Accomplishment Instructions of RECARO
service bulletin SB–No.: 3410–25MR477,
Revision 3, dated May 17, 2004.
Alternative Methods of Compliance
(g) The Manager, Boston Aircraft
Certification Office, has the authority to
approve alternative methods of compliance
for this AD if requested using the procedures
found in 14 CFR 39.19.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
amends 14 CFR part 39 as follows:
Related Information
PART 39—AIRWORTHINESS
DIRECTIVES
(i) You must use RECARO service bulletin
SB–No.: 3410–25MR477, Revision 3, dated
May 17, 2004 to perform the bolt
replacements required by this AD. 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. Contact RECARO Aircraft
Seating GmbH & Co. K, Technical
Publications, Daimlerstrasse 21, 74523
¨
Schwebisch Hall, Germany; telephone 49 791
503 7183; fax 49 791 503 7220, for a copy of
this service information. You may review
copies at the FAA, New England Region,
Office of the Regional Counsel, 12 New
England Executive Park, Burlington, MA; 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/cfr/ibrlocations.html.
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
I
2006–17–13 RECARO Aircraft Seats GmbH
& Co.: Amendment 39–14734. Docket
No. FAA–2005–22876; Directorate
Identifier 2005–NE–39–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective September 27, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to certain RECARO
Aircraft Seats GmbH & Co. (RECARO) Model
3410 302, 303, 306, 307, 314, 316, 317, 791,
792, and 795 series seats. These seats are
installed on, but not limited to, Boeing 737–
200, 737–700, and 737–800 series, 747–400
series, 777–200 and 777–300 series; and
Airbus Industries A319–100 series, A320–
200 series, and A321–200 series airplanes.
(h) Luftfahrt-Bundesamt airworthiness
directive D–2004–151R1, dated June 6, 2004,
also addresses the subject of this AD.
Material Incorporated by Reference
Issued in Burlington, Massachusetts, on
August 16, 2006.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. E6–13911 Filed 8–22–06; 8:45 am]
BILLING CODE 4910–13–P
Unsafe Condition
(d) This AD results from a report of short
attachment bolts that don’t allow enough
thread to secure the locknuts properly. We
are issuing this AD to prevent a seat belt from
detaching due to a loose locknut and
attachment bolt, which could result in injury
to an occupant during emergency conditions.
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
E:\FR\FM\23AUR1.SGM
23AUR1
Agencies
[Federal Register Volume 71, Number 163 (Wednesday, August 23, 2006)]
[Rules and Regulations]
[Pages 49326-49327]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-13911]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22876; Directorate Identifier 2005-NE-39-AD;
Amendment 39-14734; AD 2006-17-13]
RIN 2120-AA64
Airworthiness Directives; RECARO Aircraft Seating GmbH & Co.
(RECARO) Model 3410 Seats
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain RECARO Model 3410 302, 303, 306, 307, 314, 316, 317, 791, 792,
and 795 series seats. This AD requires replacing the existing
attachment bolts for the seat belts with longer attachment bolts. This
AD results from a report of short attachment bolts that don't allow
enough thread to properly secure the locknuts. We are issuing this AD
to prevent a seat belt from detaching due to a loose locknut and
attachment bolt, which could result in injury to an occupant during
emergency conditions.
DATES: This AD becomes effective September 27, 2006. The Director of
the Federal Register approved the incorporation by reference of certain
publications listed in the regulations as of September 27, 2006.
ADDRESSES: You can get the service information identified in this AD
from RECARO Aircraft Seating GmbH & Co. K, Technical Publications,
Daimlerstrasse 21, 74523 Schwebisch Hall, Germany; Telephone 49 791 503
7183; fax 49 791 503 7220.
You may examine the AD docket on the Internet at https://dms.dot.gov
or in Room PL-401 on the plaza level of the Nassif Building, 400
Seventh Street, SW., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Jeffrey Lee, Aerospace Engineer,
Boston Aircraft Certification Office, FAA, Engine & Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803;
telephone (781) 238-7161; fax (781) 238-7170.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with a proposed AD. The proposed AD applies to certain RECARO Model
3410 302, 303, 306, 307, 314, 316, 317, 791, 792, and 795 series seats.
We published the proposed AD in the Federal Register on February 8,
2006 (71 FR 6420). That action proposed to require replacing the
existing attachment bolts for the seat belts with longer attachment
bolts.
Examining the AD Docket
You may examine the docket that contains the AD, any comments
received, and any final disposition in person at the Docket Management
Facility Docket Offices between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The Docket Office (telephone (800)
647-5227) is located on the plaza level of the Department of
Transportation Nassif Building at the street address stated in
ADDRESSES. Comments will be available in the AD docket shortly after
the DMS receives them.
We provided the public the opportunity to participate in the
development of this AD. We have considered the comment received.
One commenter, the Boeing Airplane Company, asks us to remove the
737 aircraft minor model designator ``-200'' from the applicability of
this AD. Boeing states that research of the configurations for all
delivered Boeing 737-200 airplanes failed to reveal any of the affected
seats installed on those airplanes. However, Boeing states that RECARO
reported to Boeing that seats were installed in a 737-200 airplane.
Boeing believes an operator installed the seats after production of the
airplane. Boeing also has records of installing seats with the affected
model numbers on 737-700 and 737-800 airplanes. Boeing states that
those seats incorporate the longer bolts specified in RECARO service
bulletin SB-No.: 3410-25MR477, Revision 3, dated May 17, 2004, and we
should use the generic 737 designation without a minor model
designator. We partially agree. This AD applies to the RECARO seat
models identified in paragraph (c) of this AD.
[[Page 49327]]
We list the known airplane models that use these types of seats to help
owners and operators to determine if their airplane might use these
seats. Listing the minor model designators for the 737 airplanes that
could use these seats will help operators determine if this AD might
apply to them. We retained the -200 designation, and added the -700 and
-800 designations to the ``used on but not limited to'' statement in
the Applicability.
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the changes described previously.
We have determined that these changes will neither increase the
economic burden on any operator nor increase the scope of the AD.
Costs of Compliance
We estimate that this AD will affect 3,101 seats installed in
airplanes of U.S. registry. We also estimate that it will take about
0.10 work-hour per seat to perform the actions, and that the average
labor rate is $65 per work-hour. Required parts will cost about $10 per
seat. Based on these figures, we estimate the total cost of this AD to
U.S. operators to be $51,166.
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
rulemaking action.
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 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
placed it in the AD Docket. You may get a copy of this summary at the
address listed under ADDRESSES.
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 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. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2006-17-13 RECARO Aircraft Seats GmbH & Co.: Amendment 39-14734.
Docket No. FAA-2005-22876; Directorate Identifier 2005-NE-39-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective
September 27, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to certain RECARO Aircraft Seats GmbH & Co.
(RECARO) Model 3410 302, 303, 306, 307, 314, 316, 317, 791, 792, and
795 series seats. These seats are installed on, but not limited to,
Boeing 737-200, 737-700, and 737-800 series, 747-400 series, 777-200
and 777-300 series; and Airbus Industries A319-100 series, A320-200
series, and A321-200 series airplanes.
Unsafe Condition
(d) This AD results from a report of short attachment bolts that
don't allow enough thread to secure the locknuts properly. We are
issuing this AD to prevent a seat belt from detaching due to a loose
locknut and attachment bolt, which could result in injury to an
occupant during emergency conditions.
Compliance
(e) You are responsible for having the actions required by this
AD performed within 60 days after the effective date of this AD,
unless the actions have already been done.
Replacing the Attachment Bolt
(f) For RECARO Model 3410 302, 303, 306, 307, 314, 316, 317,
791, 792, and 795 series seats with a serial number listed in
section 1.A. Effectivity of RECARO service bulletin SB-No.: 3410-
25MR477, Revision 3, dated May 17, 2004, replace the seat belt
attachment bolt and nut. Use section 2. Accomplishment Instructions
of RECARO service bulletin SB-No.: 3410-25MR477, Revision 3, dated
May 17, 2004.
Alternative Methods of Compliance
(g) The Manager, Boston Aircraft Certification Office, has the
authority to approve alternative methods of compliance for this AD
if requested using the procedures found in 14 CFR 39.19.
Related Information
(h) Luftfahrt-Bundesamt airworthiness directive D-2004-151R1,
dated June 6, 2004, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use RECARO service bulletin SB-No.: 3410-25MR477,
Revision 3, dated May 17, 2004 to perform the bolt replacements
required by this AD. 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. Contact RECARO
Aircraft Seating GmbH & Co. K, Technical Publications,
Daimlerstrasse 21, 74523 Schwebisch Hall, Germany; telephone 49 791
503 7183; fax 49 791 503 7220, for a copy of this service
information. You may review copies at the FAA, New England Region,
Office of the Regional Counsel, 12 New England Executive Park,
Burlington, MA; 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/cfr/ibr-locations.html.
Issued in Burlington, Massachusetts, on August 16, 2006.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E6-13911 Filed 8-22-06; 8:45 am]
BILLING CODE 4910-13-P