[Federal Register Volume 84, Number 235 (Friday, December 6, 2019)]
[Rules and Regulations]
[Pages 66838-66840]
[FR Doc No: 2019-26298]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-1105; Product Identifier 2017-SW-023-AD; Amendment
39-19803; AD 2019-23-09]
RIN 2120-AA64

Airworthiness Directives; Bell Helicopter Textron Canada Limited
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Bell Helicopter Textron Canada Limited (BHTC) Model 427 helicopters.
This AD requires inspecting the inboard skin of the vertical fin around
the four tailboom attachment points. This AD was prompted by reports of
cracked vertical fin skins that resulted from metal fatigue. The
actions of this AD are intended to prevent an unsafe condition on these
products.

DATES: This AD is effective January 10, 2020.
    The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of January 10,
2020.

ADDRESSES: For service information identified in this final rule,
contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir,
Mirabel, Quebec J7J1R4; telephone<PHONE_NUMBER> or<PHONE_NUMBER>; fax
450-433-0272; or at

https://www.bellcustomer.com. You may review the referenced service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. It is
also available on the internet at https://www.regulations.gov by
searching for and locating Docket No. FAA-2017-1105.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1105; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this AD, the Transport Canada AD, any service information that is
incorporated by reference, the economic evaluation, any comments
received, and other information. The street address for Docket
Operations is listed above. Comments will be available in the AD docket
shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Matt Fuller, Senior Aviation Safety
Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA,
10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone<PHONE_NUMBER>;
email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    On June 1, 2018, at 83 FR 25408, the Federal Register published the
FAA's notice of proposed rulemaking (NPRM), which proposed to amend 14
CFR part 39 by adding an AD that would apply to BHTC Model 427
helicopters with a vertical fin part number (P/N) 427-035-840-105 or P/
N 427-035-840-109 installed. The NPRM proposed to require inspecting
the inboard skin of the vertical fin around the four tailboom
attachment points. The proposed requirements were intended to detect a
crack on the vertical fin skin. This condition could lead to structural
failure of the fin, separation of the skin from the helicopter, damage
to the main or tail rotor blades and loss of helicopter control.
    The NPRM was prompted by Canadian AD No. CF-2017-03, dated January
31, 2017 (Transport Canada AD CF-2017-03), issued by Transport Canada,
which is the aviation authority for Canada, to correct an unsafe
condition for BHTC Model 427 helicopters with vertical fin P/N 427-035-
840-105 or P/N 427-035-840-109 installed. Transport Canada advises of
three reports of cracked vertical fin skins that resulted from metal
fatigue. If not detected, the crack may grow to a critical length,
causing the fin to fail, separate from the helicopter, and damage the
main or tail rotor blades, leading to their in-flight failure. Loss of
the fin may also adversely affect the helicopter's directional
stability, leading to loss of directional control, Transport Canada
advises.
    Transport Canada consequently requires repetitively inspecting the
vertical fins for a crack, and if a crack is detected, replacing the
fin before further flight.

Comments

    After the NPRM was published, the FAA received comments from one
commenter. However, the comment addressed neither the proposed actions
nor the determination of the cost to the public. Therefore, the FAA has
made no changes to this AD.

FAA's Determination

    These helicopters have been approved by the aviation authority of
Canada and are approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with Canada, Transport Canada, its
technical representative, has notified the FAA about the unsafe
condition described in the Transport Canada AD. The FAA is issuing this
AD after evaluating all known relevant information and determined that
an unsafe condition exists and is likely to exist or develop on other
helicopters of these same type designs and that air safety and the
public interest require adopting the AD requirements as proposed.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Bell Helicopter Alert Service Bulletin 427-15-38,
Revision A, dated November 14, 2016, which specifies repetitive
inspections of the vertical fins every 100 hours time-in-service (TIS)
once the vertical fin has accumulated 1,500 hours TIS. This inspection
also was incorporated in Chapter 4 of the maintenance manual. This
service information also specifies serial numbers are to be assigned to
vertical fins that do not have a serial number.
    This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD affects 27 helicopters of U.S.
Registry. The FAA estimates that operators may incur the following
costs in order to comply with this AD. Labor costs are estimated at $85
per work-hour.
     Performing the visual inspection requires about 2.25 work-
hours for an estimated cost of $191 per helicopter and $5,157 for the
U.S. fleet.
     Replacing the fin requires about 4 work-hours, and parts
cost about $10,000, for an estimated cost of $10,340 per helicopter.
     Assigning a serial number to the fin takes about 0.5 work-
hours for an estimated cost of $43 per helicopter.

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.
    The FAA is 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 helicopters identified in this rulemaking action.

Regulatory Findings

    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) Will not affect intrastate aviation in Alaska, 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.
    The FAA prepared an economic evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

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 FAA 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 (AD):

2019-23-09 Bell Helicopter Textron Canada Limited: Amendment 39-
19803; Docket No. FAA-2017-1105; Product Identifier 2017-SW-023-AD.

(a) Applicability

    This AD applies to Bell Helicopter Textron Canada Limited Model
427 helicopters with a vertical fin part number (P/N) 427-035-840-
105 or P/N 427-035-840-109 installed, certificated in any category.

(b) Unsafe Condition

    This AD defines the unsafe condition as a crack on the vertical
fin skin. This condition could lead to structural failure of the
fin, separation of the skin from the helicopter, damage to the main
or tail rotor blades and loss of helicopter control.

(c) Effective Date

    This AD becomes effective January 10, 2020.

(d) Compliance

    You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.

(e) Required Actions

    Within 25 hours time-in-service (TIS) or before the helicopter
has accumulated 1,500 hours TIS, whichever occurs later, and
thereafter at intervals not to exceed 100 hours TIS:
    (1) Remove the vertical fin and clean the vertical fin
attachment area with a soap solution to remove all traces of dirt,
stains, exhaust residue, and oil. Rinse the area with water and let
dry.
    (i) Using a 10X power magnifying glass, visually inspect the
inboard skin of the vertical fin for a crack around the four
tailboom attachment points as depicted in Figure 1 of Bell
Helicopter Alert Service Bulletin 427-15-38, Revision A, dated
November 14, 2016. Pay particular attention to the upper aft
attachment point.
    (ii) If there is a crack, replace the vertical fin before
further flight.
    (2) If the vertical fin does not have a serial number, assign a
serial number using the helicopter serial number, and permanently
mark the new serial number on the vertical fin data plate. Create a
component history card or equivalent record and annotate the serial
number.

(f) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Safety Management Section, Rotorcraft Standards
Branch, FAA, may approve AMOCs for this AD. Send your proposal to:
Matt Fuller, Senior Aviation Safety Engineer, Safety Management
Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy.,
Fort Worth, TX 76177; telephone<PHONE_NUMBER>; email<EMAIL_ADDRESS>    (2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, the FAA suggests you
notify your principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office or
certificate holding district office, before operating any aircraft
complying with this AD through an AMOC.

(g) Additional Information

    The subject of this AD is addressed in Transport Canada AD No.
CF-2017-03, dated January 31, 2017. You may view the Transport
Canada AD on the internet at https://www.regulations.gov in Docket
No. FAA-2017-1105.

(h) Subject

    Joint Aircraft Service Component (JASC) Code: 55, Empennage
Structure.

(i) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
    (i) Bell Helicopter Alert Service Bulletin 427-15-38, Revision
A, dated November 14, 2016.
    (ii) [Reserved]
    (3) For Bell Helicopter Textron Canada Limited service
information identified in this AD, contact Bell Helicopter Textron
Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4;
telephone<PHONE_NUMBER> or<PHONE_NUMBER>; fax<PHONE_NUMBER>; or at
https://www.bellcustomer.com.
    (4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call<PHONE_NUMBER>.
    (5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email<EMAIL_ADDRESS>or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Fort Worth, Texas, on November 19, 2019.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2019-26298 Filed 12-5-19; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register: September 13, 2006 (Volume 71, Number 177)]
[Notices]
[Page 54038-54039]
[DOCID:fr13se06-55]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Gulf South Pipeline Company, LP; Notice of Cash-Out Report

September 6, 2006.
    Take notice that on August 28, 2006, Gulf South Pipeline Company,
LP (Gulf South) tendered for filing its report of the net revenues
attributable to the operation of its cash-in/cash-out program for the
period beginning April 1, 2005 and ending June 30, 2006.
    Gulf South states that copies of this filing have been served upon
Gulf

South's customers, state commissions and other interested parties.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211 and 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken, but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, on or before the date as indicated
below. Such notices, motions, or protests must be filed in accordance
with the provisions of Section 154.210 of the Commission's regulations
(18 CFR 154.210). Anyone filing an intervention or protest must serve a
copy of that document on the Applicant. Anyone filing an intervention
or protest on or before the intervention or protest date need not serve
motions to intervene or protests on persons other than the Applicant.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper using the ``eFiling'' link at http://www.ferc.gov.
 Persons unable to file electronically should submit an

original and 14 copies of the protest or intervention to the Federal
Energy Regulatory Commission, 888 First Street, NE., Washington, DC
20426.
    This filing is accessible on-line at http://www.ferc.gov, using the

``eLibrary'' link and is available for review in the Commission's
Public Reference Room in Washington, DC. There is an ``eSubscription''
link on the Web site that enables subscribers to receive e-mail
notification when a document is added to a subscribed docket(s). For
assistance with any FERC Online service, please e-mail
<EMAIL_ADDRESS>or call<PHONE_NUMBER> (toll free). For

TTY, call<PHONE_NUMBER>.
    Comment Date: 5 p.m. Eastern Time September 13, 2006.

Magalie R. Salas,
Secretary.
 [FR Doc. E6-15159 Filed 9-12-06; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 77, Number 18 (Friday, January 27, 2012)]
[Notices]
[Pages 4384-4385]
[FR Doc No: 2012-1742]

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SECURITIES AND EXCHANGE COMMISSION

Submission for OMB Review; Comment Request

Upon Written Request, Copies Available From: Securities and Exchange
Commission, Office of Investor Education and Advocacy, Washington, DC
20549-0213.

Extension:

Regulation S-K; OMB Control No. 3235-0071; SEC File No. 270-2.

    Notice is hereby given that pursuant to the Paperwork Reduction Act
of 1995 (44 U.S.C. 3501 et seq.) the Securities and Exchange Commission
(``Commission'') has submitted to the Office of Management and Budget a
request for extension of the previously approved collection of
information discussed below.
    Regulation S-K (17 CFR 229.101 et seq.) specifies the non-financial
disclosure requirements applicable to registration statements under the
Securities Act of 1933 (15 U.S.C. 77a et seq.); and registration
statements, periodic reports, going-private transaction and tender
offer statements, proxy and information statements, and any other
documents required to be filed under Sections 12, 13, 14, and 15 of the
Securities Exchange Act of 1934 (15 U.S.C. 78l, 78m, 78n, 78o(d)).
Regulation S-K is assigned one burden hour for administrative
convenience.
    An agency may not conduct or sponsor, and a person is not required
to respond to, a collection of information unless it displays a
currently valid control number.
    The public may view the background documentation for this
information collection at the following Web site, www.reginfo.gov.
Comments should be directed to: (i) Desk Officer for the Securities and
Exchange Commission, Office of Information and Regulatory Affairs,
Office of Management and Budget, Room 10102, New Executive Office
Building, Washington, DC 20503, or by sending an email to<EMAIL_ADDRESS>and (ii) Thomas Bayer, Director/Chief Information
Officer, Securities and Exchange Commission, c/o Remi Pavlik-Simon,
6432 General Green Way, Alexandria, VA 22312 or send an email to<EMAIL_ADDRESS>Comments must be submitted to OMB within 30 days of
this notice.

    Dated: January 23, 2012.
Kevin M. O'Neill,
Deputy Secretary.
[FR Doc. 2012-1742 Filed 1-26-12; 8:45 am]
BILLING CODE 8011-01-P


[Federal Register: April 2, 2010 (Volume 75, Number 63)]
[Rules and Regulations]
[Page 16662-16664]
[DOCID:fr02ap10-9]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-1259; Directorate Identifier 2009-NE-41-AD;
Amendment 39-16253; AD 2010-07-08]
RIN 2120-AA64

Airworthiness Directives; Kelly Aerospace Energy Systems, LLC
Rebuilt Turbochargers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Kelly Aerospace Energy Systems, LLC (KAES) rebuilt
turbochargers. This AD requires removal from service of certain part
number (P/N) and serial number (S/N) rebuilt turbochargers. This AD
results from three reports of infant mortality turbine wheel failure in
rebuilt turbochargers, since June of 2007. We are issuing this AD to
prevent separation or seizure of the turbocharger turbine, which could
result in full or partial engine power loss, loss of engine oil, and
smoke in the airplane cabin.

DATES: This AD becomes effective April 19, 2010. The Director of the
Federal Register approved the incorporation by reference of certain
publications listed in the regulations as of April 19, 2010.
    We must receive any comments on this AD by June 1, 2010.

ADDRESSES: Use one of the following addresses to comment on this AD:
     Federal eRulemaking Portal: Go to http://
www.regulations.gov and follow the instructions for sending your
comments electronically.
     Mail: U.S. Docket Management Facility, Department of
Transportation, 1200 New Jersey Avenue, SE., West Building Ground
Floor, Room W12-140, Washington, DC 20590-0001.
     Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax:<PHONE_NUMBER>.
    Contact Kelly Aerospace Energy Systems, LLC, 2900 Selma Highway,
Montgomery, Alabama 36108; telephone<PHONE_NUMBER>; fax (334) 386-
5450; or go to: http://www.kellyaerospace.com, for the service
information identified in this AD.

FOR FURTHER INFORMATION CONTACT: Gary Wechsler, Aerospace Engineer,
Propulsion, Atlanta Aircraft Certification Office, 1701 Columbia
Avenue, College Park, GA 30337; telephone<PHONE_NUMBER>; fax (404)
474-5606.

SUPPLEMENTARY INFORMATION: In October 2009, we were made aware by KAES
that since June 2007, three turbochargers rebuilt by KAES have failed.
Two had turbine wheel head separation and the third had a turbine shaft
seizure. Investigation revealed that a steel wire brush was used to
remove the accumulated coking that had built up on these turbine wheels
being reclaimed for re-use in rebuilt turbochargers. This procedure
created a rough surface finish on the turbine wheel shaft that exceeded
allowable limits. The rough surface finish can disrupt the required
formation of a hydrodynamic layer of oil between the shaft and mating
bearings. This condition, if not corrected, could result in separation
or seizure of the turbocharger turbine, which could result in full or
partial engine power loss, loss of engine oil, and smoke in the
airplane cabin.

Relevant Service Information

    We have reviewed and approved the technical contents of Kelly
Aerospace Energy Systems, LLC Service Bulletin (SB) No. 039 A, dated
February 10, 2010. That SB identifies the rebuilt turbochargers by P/N
and S/N that are suspect of having a rough shaft surface finish
exceeding allowable limits.

FAA's Determination and Requirements of This AD

    The unsafe condition described previously is likely to exist or
develop on other KAES rebuilt turbochargers of the same type design.
For that reason, we are issuing this AD to prevent separation or
seizure of the turbocharger turbine, which could result in full or
partial engine power loss, loss of engine oil, and smoke in the
airplane cabin. This AD requires removal from service of certain P/N
and S/N rebuilt turbochargers. You must use the service information
described previously to determine what S/N rebuilt turbochargers are
affected by this AD.

FAA's Determination of the Effective Date

    Since an unsafe condition exists that requires the immediate
adoption of this AD, we have found that notice and opportunity for
public comment before issuing this AD are impracticable, and that good
cause exists for making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety and was not preceded by notice and an opportunity for public
comment; however, we invite you to send us any written relevant data,
views, or arguments regarding this AD. Send your comments to an address
listed under ADDRESSES. Include ``AD Docket No. FAA-2009-1259;
Directorate Identifier 2009-NE-41-AD'' in the subject line of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify it.
    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 the Web
site, anyone can find and read the comments in any of our dockets,
including, if provided, the name of the individual who sent the comment
(or signed the comment on behalf of an association, business, labor
union, etc.). You may review the DOT's complete Privacy Act Statement
in the Federal Register published on April 11, 2000 (65 FR 19477-78).

Examining the AD Docket

    You may examine the AD docket 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 AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone<PHONE_NUMBER>) is the same as
the Mail address provided in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.

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 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
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

0
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. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive:

2010-07-08 Kelly Aerospace Energy Systems, LLC (formerly Kelly
Aerospace Power Systems): Amendment 39-16253. Docket No. FAA-2009-
1259; Directorate Identifier 2009-NE-41-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective April
19, 2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to certain serial numbers (S/Ns) of Kelly
Aerospace Energy Systems, LLC (KAES) rebuilt turbochargers listed by
part number (P/N) in the following Table 1 of this AD. The affected
S/Ns are listed in Table III of Kelly Aerospace Energy Systems, LLC
Service Bulletin (SB) No. 039 A, dated February 10, 2010.

                             Table 1--Part Numbers of Rebuilt Turbochargers Affected
----------------------------------------------------------------------------------------------------------------

----------------------------------------------------------------------------------------------------------------
406610-9005<PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER>
406610-9025<PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER>
407810-9001<PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER>
465680-9004<PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER>
465398-9002<PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER><PHONE_NUMBER>
466304-9003<PHONE_NUMBER>*<PHONE_NUMBER>*<PHONE_NUMBER>*<PHONE_NUMBER>*<PHONE_NUMBER>*
600576-9000*<PHONE_NUMBER>*<PHONE_NUMBER>*<PHONE_NUMBER>*       N/A                N/A
----------------------------------------------------------------------------------------------------------------
* P/Ns with an asterisk may have a CF prefix.

    These rebuilt turbochargers are installed on, but not limited
to, the engines and aircraft listed in Table IV of Kelly Aerospace
Energy Systems, LLC SB No. 039 A, dated February 10, 2010.

Unsafe Condition

    (d) This AD results from three reports of infant mortality
turbine wheel failure in rebuilt turbochargers, since June of 2007.
We are issuing this AD to prevent separation or seizure of the
turbocharger turbine, which could result in full or partial engine
power loss, loss of engine oil, and smoke in the airplane cabin.

Compliance

    (e) You are responsible for having the actions required by this
AD performed within 10 hours time-in-service after the effective
date of this AD, unless the actions have already been done.

Turbocharger Removal From Service

    (f) Remove from service the rebuilt turbochargers listed by P/N
in paragraph (c) of this AD that have a S/N listed in Table III of
Kelly Aerospace Energy Systems, LLC SB No. 039 A, dated February 10,
2010.

Installation Eligibility of Removed Turbochargers

    (g) Removed turbochargers listed in Table III of Kelly Aerospace
Energy Systems, LLC SB No. 039 A, dated February 10, 2010, are
eligible for installation once they are overhauled by an FAA-
approved repair station. That overhaul must include replacing the
turbine wheels listed by P/N in Table II of Kelly Aerospace Energy
Systems, LLC SB No. 039 A, dated February 10, 2010, replacing the
turbine wheel mating bushings, and marking the attached Return To
Service Tag with this AD number, which is AD 2010-07-08.

Installation Prohibition

    (h) After the effective date of this AD, do not install any of
the turbochargers listed in Table III of Kelly Aerospace Energy
Systems, LLC SB No. 039 A, dated February 10, 2010, unless the
turbocharger is overhauled as specified in paragraph (g) of this AD.

Alternative Methods of Compliance

    (i) The Manager, Atlanta 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.

Special Flight Permits

    (j) Under 14 CFR 39.23, we are limiting the special flight
permits for this AD by the following conditions:
    (1) Use of minimum crew.
    (2) Flight made during daytime, using visual flight rule
conditions.
    (3) Maximum flight altitude of 12,000 feet mean-sea-level, based
upon terrain.

Related Information

    (k) Contact Gary Wechsler, Aerospace Engineer, Propulsion,
Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College
Park, GA 30337; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>, for
more information about this AD.

Material Incorporated by Reference

    (l) You must use Kelly Aerospace Energy Systems, LLC Service
Bulletin No. 039 A, dated February 10, 2010, to determine which
turbocharger(s) are affected 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 Kelly Aerospace Energy Systems, LLC, 2900 Selma Highway,
Montgomery, Alabama 36108, telephone<PHONE_NUMBER>, fax (334) 386-
5450, or go to: http://www.kellyaerospace.com, for a copy of this
service information. You may review copies at the FAA, New England
Region, 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<PHONE_NUMBER>, or
go to: http://www.archives.gov/federal-register/cfr/ibr-
locations.html.

    Issued in Burlington, Massachusetts, on March 23, 2010.
Robert J. Ganley,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2010-7056 Filed 4-1-10; 8:45 am]
BILLING CODE 4910-13-P


                                                                                Table B-2. Fish Tissue Data Template                                        A                                        B                                        C                                        D                                        E                                        F                                        G                                        H                                        I                                        J                                        K                                        L                                        M ADVISORY STATE OR TRIBE* AGENCY or ORGANIZATION* CONTACT SITENAME* LOCATION MONITORING LOCATION ID* LAT_DD* LONG_DD* SAMPLE ID* SAMPLE DATE* SAMPLE TYPE* SPECIES* Advisory Name - Typically a waterbody  (links fish tissue data with associated fish advisory reported in Table 1,if any) Name of state of tribe supplying data Agency or organization responsible for the data Agency responsible for the data Waterbody name Location of collection within water body Unique identifier for the monitoring location X coordinate of collection location (NAD83) Y coordinate of collection location (NAD83) Unique sample identifier Date sample was taken Sample type (fillet, whole body, fillet skin on, etc). Species name

Template Notes: * Data for these fields are needed in order to include the data in the Water Quality Exchange (WQX).  Use "N/A" for data Not Applicable Use "UKN" for data Not Available or Unknown

                                                                                Table B-2. Fish Tissue Template  -  Continued                                         N                                        O                                        P                                        Q                                        R                                        S                                        T                                        U                                        V                                        W                                        X                                        Y                                        Z                                       AA AGE SEX COMPOSITE [Y/N] * NUMBER FISH* LENGTH* MIN_LENGTH MAX_LENGTH LENGTH UNIT* STD_LENGTH WEIGHT MIN_WEIGHT MAX_WEIGHT STD_WEIGHT WEIGHT UNIT Age of organism Sex of organism Is fish sample a composite [Y/N] Number of individual fish in sample Length of individual fish sample  Minimum length of composite Maximum length of composite Fish length units  Standard deviation of length of composite Weight or average weight  Minimum weight of composite Maximum weight of composite Standard deviation of weight of composite Fish weight units

Template Notes: * Data for these fields are needed in order to include the data in the Water Quality Exchange (WQX) Use "N/A" for data Not Applicable Use "UKN" for data Not Available or Unknown

                Table B-2. Fish Tissue Template  -  Continued                                        BB                                       CC                                       DD                                       EE                                       FF                                       GG                                       HH                                       II                                       JJ                                       KK                                       LL                                       MM PREPARATION* ANALYTE/CONTAMINANT NAME* RESULT NUMBER* RESULT UNIT*  RESULT QUALIFIER DETECT* REPORTING LIMIT* REPORTING LIMIT_UNIT* DETECTION LIMIT DETECTION LIMIT_UNIT BASIS* COMMENTS Portion of fish analyzed Name of Contaminant

Contaminant concentration [Populate non-detects as "ND"] Contaminant concentration units  Analytical qualifiers Analyte detected  [Y/N] Minimum reporting limit Reporting limit units Limit of Detection Detection limit units  Results reported as dry weight or wet weight  [Dry or Wet]

                 Template Notes:      * Data for these fields are needed in order to include the data in the Water Quality Exchange (WQX).       Use "N/A" for data Not Applicable      Use "UKN" for data Not Available or Unknown