Airworthiness Directives; Bell Helicopter Textron Model 206A and 206B Helicopters, 45526-45527 [05-15581]
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45526
Federal Register / Vol. 70, No. 151 / Monday, August 8, 2005 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–21230; Directorate
Identifier 2004–SW–51–AD; Amendment 39–
14209; AD 2005–16–04]
RIN 2120–AA64
Airworthiness Directives; Bell
Helicopter Textron Model 206A and
206B Helicopters
Federal Aviation
Administration, DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This amendment adopts a
new airworthiness directive (AD) for
Bell Helicopter Textron (Bell) Model
206A and 206B helicopters modified by
Aeronautical Accessories, Inc.
Supplemental Type Certificate (STC)
SH1392SO with certain part-numbered
high crosstubes. This amendment
requires inspecting at specified time
intervals and replacing any cracked
crosstubes. This amendment is
prompted by the discovery of a cracked
high forward crosstube. The actions
specified by this AD are intended to
detect a crack in the crosstube which
could lead to failure of the crosstube,
collapse of the landing gear, and
subsequent loss of control of the
helicopter.
Effective September 12, 2005.
You may get the service
information identified in this AD from
Aeronautical Accessories, Inc., P.O. Box
3689, Bristol, Tennessee 37625–3689,
telephone (423) 538–5151 or (800) 251–
7094, fax (423) 538–8469, or e-mail at
sales@aero-access.com.
Examining the Docket: You may
examine the docket that contains this
AD, any comments, and other
information on the Internet at https://
dms.dot.gov, or at the Docket
Management System (DMS), U.S.
Department of Transportation, 400
Seventh Street SW., Room PL–401, on
the plaza level of the Nassif Building,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Marc Belhumeur, Aviation Safety
Engineer, FAA, Rotorcraft Directorate,
Rotorcraft Certification Office, Fort
Worth, Texas 76193–0170, telephone
(817) 222–5177, fax (817) 222–5783.
SUPPLEMENTARY INFORMATION: A
proposal to amend 14 CFR part 39 to
include an AD for Bell Model 206A and
206B helicopters that have Aeronautical
Accessories, Inc. crosstubes installed
was published in the Federal Register
DATES:
ADDRESSES:
VerDate jul<14>2003
18:56 Aug 05, 2005
Jkt 205001
on May 17, 2005 (70 FR 28220). That
action proposed to require the following
within 300 hours time-in-service (TIS)
or 60 days, whichever occurs first, and
after that at intervals not to exceed 300
hours TIS or 12 months, whichever
occurs first:
• Inspecting each forward crosstube,
part number (P/N) 206–321–001 with
serial number (S/N) 1001 through 1152,
for a crack and replacing any cracked
crosstube with an airworthy crosstube
before further flight; and
• Inspecting each high aft crosstube,
P/N 206–321–002, with S/N 2001
through 2152, for a crack and replacing
any cracked crosstube with an airworthy
crosstube before further flight.
Interested persons have been afforded
an opportunity to participate in the
making of this amendment. No
comments were received on the
proposal or the FAA’s determination of
the cost to the public. The FAA has
determined that air safety and the
public interest require the adoption of
the rule as proposed.
We estimate that this AD will affect
150 helicopters of U.S. registry.
Inspecting both crosstubes on each
helicopter will take approximately 3
work hours and replacing both
crosstubes, if necessary, will also take
approximately 3 work hours. The
average labor rate is $65 per work hour.
Required parts will cost approximately
$2,260 per crosstube. Based on these
figures, the total cost impact of the AD
on U.S. operators is estimated to be
$736,500 ($4,910 per helicopter,
assuming one inspection and one
forward and one aft crosstube
replacement on the entire fleet).
this AD. See the DMS to examine the
economic evaluation.
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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
Adoption of the Amendment
Accordingly, pursuant to 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:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Regulatory Findings
Authority: 49 U.S.C. 106(g), 40113, 44701.
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 the regulation:
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 an economic evaluation
of the estimated costs to comply with
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
§ 39.13
[Amended]
2. Section 39.13 is amended by adding
a new airworthiness directive to read as
follows:
I
2005–16–04 Bell Helicopter Textron:
Amendment 39–14209. Docket No.
FAA–2005–21230; Directorate Identifier
2004–SW–51–AD.
Applicability: Model 206A and 206B
helicopters modified by Aeronautical
Accessories, Inc. Supplemental Type
Certificate SH1392SO, with high forward
crosstube, part number (P/N) 206–321–001
with serial number (S/N) 1001 through 1152,
and high aft crosstube, P/N 206–321–002
with S/N 2001 through 2152, installed,
certificated in any category.
Compliance: Required as indicated, unless
accomplished previously.
To detect a crack in the crosstube, which
could lead to failure of the crosstube,
collapse of the landing gear, and subsequent
loss of control of the helicopter, accomplish
the following:
E:\FR\FM\08AUR1.SGM
08AUR1
Federal Register / Vol. 70, No. 151 / Monday, August 8, 2005 / Rules and Regulations
(a) Within 300 hours time-in-service (TIS)
or 60 days, whichever occurs first, and after
that at intervals not to exceed 300 hours TIS
or 12 months, whichever occurs first, remove
each crosstube and inspect it for cracks.
Replace any cracked crosstube with an
airworthy crosstube before further flight.
Note: Aeronautical Accessories, Inc. Alert
Service Bulletin No. AA–03121, dated
October 25, 2004, pertains to the subject of
this AD.
(b) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Contact the Rotorcraft Certification
Office, Rotorcraft Directorate, FAA, for
information about previously approved
alternative methods of compliance.
(c) This amendment becomes effective on
September 12, 2005.
Issued in Fort Worth, Texas, on July 29,
2005.
S. Frances Cox,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 05–15581 Filed 8–5–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2005–21908; Airspace
Docket No. 05–AGL–6]
RIN 2120–AA66
Revision of VOR Federal Airways V–9,
V–50, V–67, V–69, V–129, V–173 and V–
233; and Jet Routes J–35, J–80, J–101
and J–137; Springfield, IL
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This action revises Very High
Frequency Omni-directional Range
(VOR) Federal Airways V–9, V–50, V–
67, V–69, V–129, V–173 and V–233; and
Jet Routes J–35, J–80, J–101 and J–137
over the Springfield, IL area. The FAA
is taking this action due to the
relocation of the Capital VOR/Tactical
Air Navigation (VORTAC) and the
renaming of the ‘‘Capital VORTAC’’ to
the ‘‘Spinner VORTAC’’ to enhance the
management of aircraft operations over
the Springfield, IL area.
DATES: Effective 0901 UTC, October 27,
2005.
FOR FURTHER INFORMATION CONTACT:
Steve Rohring, Airspace and Rules,
Office of System Operations and Safety,
Federal Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone: (202)
267–8783.
VerDate jul<14>2003
18:56 Aug 05, 2005
Jkt 205001
SUPPLEMENTARY INFORMATION:
History
On September 2, 2003, the FAA
published in the Federal Register a
notice of proposed rulemaking (NPRM)
proposing to realign V–233 northeast of
the Capital VORTAC (68 FR 52150).
This change was needed due to the
pending relocation of the Capital
VORTAC. This relocation will result in
a change of the VORTAC radials used in
the legal description of V–233; but
would not have changed the legal
description of any other airways or jet
routes because, at the time that the
NPRM was issued, the FAA did not plan
to change the name of the VORTAC.
Interested parties were invited to
participate in this rulemaking effort by
submitting written comments on the
proposal. No comments were received
in response to the proposal.
Subsequent to the issuance of the
NPRM and in the interest of safety, a
decision was made to change the name
of the ‘‘Capital VORTAC’’ to the
‘‘Spinner VORTAC’’. Because the name
of the VORTAC is contained in the legal
description of Federal Airways V–9, V–
50, V–67, V–69, V–129, V–173 and V–
233; and Jet Routes J–35, J–80, J–101
and J–137, the legal descriptions must
be changed.
Federal airways are published in
paragraph 6010(a) of FAA Order
7400.9M dated August 30, 2004, and
effective September 16, 2004, which is
incorporated by reference in 14 CFR
71.1. The Federal airways listed in this
document will be published
subsequently in the order.
The Rule
This action amends Title 14 Code of
Federal Regulations (14 CFR) part 71 by
revising the legal descriptions for
Federal Airways V–9, V–50, V–67, V–
69, V–129, V–173 and V–233; and Jet
Routes J–35, J–80, J–101 and J–137 over
the Springfield, IL, area. The FAA is
taking this action due to the relocation
and renaming of the Capitol VORTAC
and to enhance the management of
aircraft operations over the Springfield,
IL area.
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
current. Therefore, this regulation: (1) Is
not a ‘‘significant regulatory action’’
under Executive Order 12866; (2) is not
a ‘‘significant rule’’ under Department of
Transportation (DOT) Regulatory
Policies and Procedures (44 FR 11034,
February 26, 1979); and (3) does not
warrant preparation of a regulatory
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
45527
evaluation as the anticipated impact is
so minimal. Since this is a routine
matter that will only affect air traffic
procedures and air navigation, it is
certified that this rule, when
promulgated, will not have a significant
economic impact on a substantial
number of small entities under the
criteria of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference,
Navigation (air).
Adoption of the Amendment
In consideration of the foregoing, the
Federal Aviation Administration
amends 14 CFR part 71 as follows:
I
PART 71—DESIGNATION OF CLASS A,
B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND
REPORTING POINTS
1. The authority citation for part 71
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40103, 40113,
40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–
1963 Comp., p. 389.
§ 71.1
[Amended]
2. The incorporation by reference in 14
CFR 71.1 of FAA Order 7400.9M,
Airspace Designations and Reporting
Points, dated August 30, 2004, and
effective September 16, 2004, is
amended as follows:
I
Paragraph 6010(a)
Airways
*
*
*
Domestic VOR Federal
*
*
V–9 (Revised)
From Leeville, LA; McComb, MS; Jackson,
MS; Sidon, MS; Marvell, AR; Gilmore, AR;
Malden, MO; Farmington, MO; St. Louis,
MO; Spinner, IL; Pontiac, IL; INT Pontiac, IL
343° and Rockford, IL, 169° radials;
Rockford; Janesville, WI; Madison, WI;
Oshkosh, WI; Green Bay, WI; Iron Mountain,
MI; to Houghton, MI.
*
*
*
*
*
V–50 (Revised)
From Hastings, NE; Pawnee City, NE; St.
Joseph, MO; Kirksville, MO; Quincy, IL;
Spinner, IL; Decatur, IL; Terre Haute, IN;
Brickyard, IN; Dayton, OH.
*
*
*
*
*
V–67 (Revised)
From Choo Choo, GA; Shelbyville, TN;
Graham, TN; Cunningham, KY; Marion, IL;
Centralia, IL; INT Centralia 010° and
Vandalia, IL, 162° radials; Vandalia; Spinner,
IL; Burlington, IA; Iowa City, IA; Cedar
Rapids, IA; Waterloo, IA; Rochester, MN.
*
*
*
*
*
V–69 (Revised)
From El Dorado, AR; Pine Bluff, AR; INT
Pine Bluff 038° and Walnut Ridge, AR, 187°
E:\FR\FM\08AUR1.SGM
08AUR1
Agencies
[Federal Register Volume 70, Number 151 (Monday, August 8, 2005)]
[Rules and Regulations]
[Pages 45526-45527]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-15581]
[[Page 45526]]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21230; Directorate Identifier 2004-SW-51-AD;
Amendment 39-14209; AD 2005-16-04]
RIN 2120-AA64
Airworthiness Directives; Bell Helicopter Textron Model 206A and
206B Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron (Bell) Model 206A and 206B helicopters modified
by Aeronautical Accessories, Inc. Supplemental Type Certificate (STC)
SH1392SO with certain part-numbered high crosstubes. This amendment
requires inspecting at specified time intervals and replacing any
cracked crosstubes. This amendment is prompted by the discovery of a
cracked high forward crosstube. The actions specified by this AD are
intended to detect a crack in the crosstube which could lead to failure
of the crosstube, collapse of the landing gear, and subsequent loss of
control of the helicopter.
DATES: Effective September 12, 2005.
ADDRESSES: You may get the service information identified in this AD
from Aeronautical Accessories, Inc., P.O. Box 3689, Bristol, Tennessee
37625-3689, telephone (423) 538-5151 or (800) 251-7094, fax (423) 538-
8469, or e-mail at sales@aero-access.com.
Examining the Docket: You may examine the docket that contains this
AD, any comments, and other information on the Internet at https://
dms.dot.gov, or at the Docket Management System (DMS), U.S. Department
of Transportation, 400 Seventh Street SW., Room PL-401, on the plaza
level of the Nassif Building, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Marc Belhumeur, Aviation Safety
Engineer, FAA, Rotorcraft Directorate, Rotorcraft Certification Office,
Fort Worth, Texas 76193-0170, telephone (817) 222-5177, fax (817) 222-
5783.
SUPPLEMENTARY INFORMATION: A proposal to amend 14 CFR part 39 to
include an AD for Bell Model 206A and 206B helicopters that have
Aeronautical Accessories, Inc. crosstubes installed was published in
the Federal Register on May 17, 2005 (70 FR 28220). That action
proposed to require the following within 300 hours time-in-service
(TIS) or 60 days, whichever occurs first, and after that at intervals
not to exceed 300 hours TIS or 12 months, whichever occurs first:
Inspecting each forward crosstube, part number (P/N) 206-
321-001 with serial number (S/N) 1001 through 1152, for a crack and
replacing any cracked crosstube with an airworthy crosstube before
further flight; and
Inspecting each high aft crosstube, P/N 206-321-002, with
S/N 2001 through 2152, for a crack and replacing any cracked crosstube
with an airworthy crosstube before further flight.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments were received on the
proposal or the FAA's determination of the cost to the public. The FAA
has determined that air safety and the public interest require the
adoption of the rule as proposed.
We estimate that this AD will affect 150 helicopters of U.S.
registry. Inspecting both crosstubes on each helicopter will take
approximately 3 work hours and replacing both crosstubes, if necessary,
will also take approximately 3 work hours. The average labor rate is
$65 per work hour. Required parts will cost approximately $2,260 per
crosstube. Based on these figures, the total cost impact of the AD on
U.S. operators is estimated to be $736,500 ($4,910 per helicopter,
assuming one inspection and one forward and one aft crosstube
replacement on the entire fleet).
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 the regulation:
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 an economic evaluation of the estimated costs to comply
with this AD. See the DMS to examine the economic evaluation.
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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
0
Accordingly, pursuant to 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. Section 39.13 is amended by adding a new airworthiness directive to
read as follows:
2005-16-04 Bell Helicopter Textron: Amendment 39-14209. Docket No.
FAA-2005-21230; Directorate Identifier 2004-SW-51-AD.
Applicability: Model 206A and 206B helicopters modified by
Aeronautical Accessories, Inc. Supplemental Type Certificate
SH1392SO, with high forward crosstube, part number (P/N) 206-321-001
with serial number (S/N) 1001 through 1152, and high aft crosstube,
P/N 206-321-002 with S/N 2001 through 2152, installed, certificated
in any category.
Compliance: Required as indicated, unless accomplished
previously.
To detect a crack in the crosstube, which could lead to failure
of the crosstube, collapse of the landing gear, and subsequent loss
of control of the helicopter, accomplish the following:
[[Page 45527]]
(a) Within 300 hours time-in-service (TIS) or 60 days, whichever
occurs first, and after that at intervals not to exceed 300 hours
TIS or 12 months, whichever occurs first, remove each crosstube and
inspect it for cracks. Replace any cracked crosstube with an
airworthy crosstube before further flight.
Note: Aeronautical Accessories, Inc. Alert Service Bulletin No.
AA-03121, dated October 25, 2004, pertains to the subject of this
AD.
(b) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Contact the Rotorcraft Certification Office, Rotorcraft Directorate,
FAA, for information about previously approved alternative methods
of compliance.
(c) This amendment becomes effective on September 12, 2005.
Issued in Fort Worth, Texas, on July 29, 2005.
S. Frances Cox,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 05-15581 Filed 8-5-05; 8:45 am]
BILLING CODE 4910-13-P