[Federal Register: June 12, 2009 (Volume 74, Number 112)]
[Rules and Regulations]
[Page 27915-27917]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr12jn09-6]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0484; Directorate Identifier 2008-SW-44-AD;
Amendment 39-15924; AD 2009-12-01]
RIN 2120-AA64
Airworthiness Directives; Bell Helicopter Textron, Inc. Model 47,
47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B,
47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A, 47H-1,
47J, 47J-2, 47J-2A, and 47K Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
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SUMMARY: This amendment adopts a new airworthiness directive (AD) for
the specified Bell Helicopter Textron, Inc. (Bell) helicopters. This
action requires visually inspecting each main rotor blade box beam clip
(clip) for correct installation. This amendment is prompted by a report
of a main rotor blade with an incorrectly installed clip. The actions
specified in this AD are intended to prevent a main rotor blade spar
crack as a result of an incorrectly installed clip, loss of a main
rotor blade, and subsequent loss of control of the helicopter.
DATES: Effective June 29, 2009.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of June 29, 2009.
Comments for inclusion in the Rules Docket must be received on or
before August 11, 2009.
ADDRESSES: Use one of the following addresses to submit comments on
this AD:
Federal eRulemaking Portal: Go to http://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
You may get the service information identified in this AD from Bell
Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101, telephone
(817) 280-3391, fax (817) 280-6466, or at http://www.bellcustomer.com/
files/.
Examining the Docket: You may examine the docket that contains the
AD, any comments, and other information on the Internet at http://
www.regulations.gov, or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Operations office (telephone (800) 647-5527) is
located in Room W12-140 on the ground floor of the West Building at the
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Michael Kohner, Aviation Safety
Engineer, FAA, Rotorcraft Directorate, Rotorcraft Certification Office,
Fort Worth, Texas 76193-0170, telephone (817) 222-5170, fax (817) 222-
5783.
SUPPLEMENTARY INFORMATION: This amendment adopts a new AD for the
specified Bell helicopters. This action requires visually inspecting
each clip for correct installation. This amendment is prompted by a
report of a main rotor blade with an incorrectly installed clip. This
condition, if not corrected, could result in a main rotor blade spar
crack, loss of a main rotor blade, and subsequent loss of control of
the helicopter.
We have reviewed Bell Alert Service Bulletin No. 47-08-25, dated
May 26, 2008 (ASB), which describes procedures for visually inspecting
each clip on the affected main rotor blade for correct installation.
The ASB specifies that a clip incorrectly installed may cause a main
rotor blade spar crack.
This unsafe condition is likely to exist or develop on other
helicopters of these same type designs. Therefore, this AD is being
issued to prevent a main rotor blade spar crack as a result of an
incorrectly installed clip, loss of a main rotor blade, and subsequent
loss of control of the helicopter. This AD requires visually inspecting
the entire length of each clip on an affected main rotor blade by
following specified portions of the ASB described previously. The short
compliance time involved is required because the previously described
critical unsafe condition can adversely affect the structural integrity
and controllability of the helicopter. Therefore, visually inspecting
each main rotor blade for an incorrectly installed clip within 10 hours
time-in-service and replacing any main rotor blade that has an
incorrectly installed clip with an airworthy main rotor blade before
further flight is a very short time period, and this AD must be issued
immediately.
Since a situation exists that requires the immediate adoption of
this regulation, it is found that notice and opportunity for prior
public comment hereon are impracticable, and that good cause exists for
making this amendment effective in less than 30 days.
We estimate that this AD will affect 1,130 helicopters. It will
require a minimal amount of time to locate the 7 affected blades. The
visual inspection for an incorrectly installed clip will take about 5
work hours at an average labor rate of $80 per work hour. Required
parts will cost about $42,640. Based on these figures, we estimate the
total cost impact of the AD on U.S. operators to be $45,440 ($2,800 for
labor costs and $42,640 in parts costs) assuming only one blade will
need to be replaced in the helicopter fleet.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any written data,
views, or arguments regarding this AD. Send your comments to an address
listed under ADDRESSES. Include ``Docket No. FAA-2009-0484;
[[Page 27916]]
Directorate Identifier 2008-44-SW-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD. We will consider
all comments received by the closing date and may amend the AD in light
of those comments.
We will post all comments we receive, without change, to http://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact
with FAA personnel concerning this AD. Using the search function of our
docket Web site, you can find and read the comments to any of our
dockets, including the name of the individual who sent the comment. You
may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78).
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 AD docket 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, Incorporation by
reference, 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:
2009-12-01 Bell Helicopter Textron, Inc.: Amendment 39-15924. Docket
No. FAA-2009-15924; Directorate Identifier 2008-SW-44-AD.
Applicability: Model 47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2,
47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-
4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A, and 47K
helicopters with a main rotor blade, installed, with a part number
(P/N) and serial number (S/N), listed as follows, certificated in
any category:
------------------------------------------------------------------------
Main rotor blade, P/N With a S/N of
------------------------------------------------------------------------
047-110-250-021..................... A-303, A-304, A-312, or A-316.
047-110-250-023..................... A-298, A-301, or A-305.
------------------------------------------------------------------------
Compliance: Required as indicated, unless done previously.
To prevent a main rotor blade spar crack as a result of an
incorrectly installed main rotor blade box beam clip (clip), loss of
a main rotor blade, and subsequent loss of control of the
helicopter, do the following:
(a) Within 10 hours time-in-service (TIS), visually inspect the
entire length of each upper and lower clip of each main rotor blade
from the main rotor blade tip to the root by following Part II of
the Accomplishment Instructions, paragraphs 1. through 8., of Bell
Helicopter Textron, Inc. Alert Service Bulletin No. 47-08-25, dated
May 26, 2008 (ASB) and referring to the depictions in Figures 1 and
2 of the ASB and Figure 1 of this AD for correct installation.
Note: Figure 3 of the ASB depicts a clip installed incorrectly.
[[Page 27917]]
[GRAPHIC] [TIFF OMITTED] TR12JN09.000
(b) Before further flight, if you find a main rotor blade with
an incorrectly installed clip, replace that unairworthy main rotor
blade with an airworthy main rotor blade that has a clip that is
installed correctly.
(c) 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 Manager, Rotorcraft Certification Office, FAA, ATTN:
Michael Kohner, Aviation Safety Engineer, Rotorcraft Directorate,
Fort Worth, Texas 76193-0170, telephone (817) 222-5170, fax (817)
222-5783.
(d) Special flight permits may be issued under 14 CFR 21.197 and
21.199 to operate the helicopter to a location where the
requirements of this AD can be done provided the onetime ferry
flight does not exceed 5 hours TIS.
(e) The visual inspection shall be done by following the
specified portions of Bell Helicopter Textron, Inc., Alert Service
Bulletin No. 47-08-25, dated May 26, 2008. The Director of the
Federal Register approved this incorporation by reference in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be
obtained from Bell Helicopter Textron, Inc., P.O. Box 482, Fort
Worth, TX 76101, telephone (817) 280-3391, fax (817) 280-6466, or at
http://www.bellcustomer.com/files/. Copies may be inspected at the
FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham
Blvd., Room 663, Fort Worth, Texas 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: http://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.
(f) This amendment becomes effective on June 29, 2009.
Issued in Fort Worth, Texas, on May 19, 2009.
Mark R. Schilling,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. E9-13563 Filed 6-11-09; 8:45 am]
BILLING CODE 4910-13-P