PAPERWORK REDUCTION ACT SUBMISSION Please read the instructions before completing this form. For additional forms or assistance in completing this form, contact your agency's Paperwork Clearance Officer. Send two copies of this form, the collection instrument to be reviewed, the Supporting Statement and any additional documentation to: Office of Information and Regulatory Affairs, Office of Management and Budget, Docket Library, Room 10102, 725 17th Street NW Washington, DC 20503.

1. Agency/ Subagency originating request EPA, Office of Transportation and Air Quality 2. OMB control number b. G None a_ 2060 0395 __ __ __ __

3. Type of information collection ( check one) a. G New collection b. G Revision of a currently approved collection c. X Extension of a currently approved collection d. G Reinstatement, without change, of a previously approved collection for which approval has expired e. G Reinstatement, with change, of a previously approved collection for which approval has expired f. G Existing collection in use without an OMB control number 4. Type of review requested ( check one) a. X Regular b. G Emergency  Approval requested by: / / c. G Delegated 5. Small entities Will this information collection have a significant economic impact on a substantial number of small entities? G Yes X No For b f, note item A2 of Supporting Statement Instructions 6. Requested expiration date a. X Three years from approval date b. G Other Specify: / /___

7. Title Exclusion Determinations for New Non road Spark ignited Engines at or Below 19 Kilowatts, New Non road Compressionignited Engines, New Marine Engines, and New On road Heavy Duty Engines ( Renewal)

8. Agency form number( s) ( If applicable) 1852.03 9. Keywords Environmental Protection, Engine Pollution, Clean Air Act 10. Abstract: Motor vehicles and non road engines not meeting the applicable definitions are excluded from compliance with current regulations. A manufacturer may make an exclusion determination by itself; however, to be certain, manufacturers and importers may routinely request that EPA make the determination. To do so, manufacturers submit a letter describing the engine and/ or vehicle ( engine type, horsepower rating, intended usage, etc.) and a sales brochures to the Engine Programs Group ( EPG), of the Certification and Compliance Division ( CCD). EPG uses this information to determine whether the engine or vehicle is excluded from compliance with one or more emission regulations.

11. Affected public ( Mark primary with " P" and all others that apply with " X") a. Individuals or households d. Farms b. P Business or other for profit e. Federal Government c. Not for profit institutions f. State, Local or Tribal Government 12. Obligation to respond ( Mark primary with " P" and all others that apply with " X") a. P Voluntary b. G Required to obtain or retain benefits c. G Mandatory 13. Annual reporting and recordkeeping hour burden a. Number of respondents 12 b. Total annual responses 12 1. Percentage of these responses collected electronically 90 % c. Total hours requested 69 d. Current OMB inventory 69 e. Difference 0 f. Explanation of difference 1. Program Change 0 2. Adjustment 0 14. Annual reporting and recordkeeping cost burden ( in thousands of dollars)

a. Total annualized capital/ startup costs 0 b. Total annual costs ( O& M) $ 1 c. Total annualized cost requested $ 1 d. Current OMB inventory $ 1 e. Difference $ 0 f. Explanation of difference 1. Program change $ 0 2. Adjustment $ 0 15. Purpose of information collection ( Mark Primary With " P" and all others that apply with " X") a. _ Application for benefits e. __ Program planning or management b. __ Program evaluation f. __ Research c. __ General purpose statistics g. P Regulatory or compliance d. __ Audit 16. Frequency of recordkeeping or reporting ( check all that apply) a. X Recordkeeping b. Q Third party disclosure c. X Reporting 1. X On occasion 2. Q Weekly 3. Q Monthly 4. Q Quarterly 5. Q Semi annually 6. Q Annually 7. Q Biannually 8. a Other ( describe)

17. Statistical methods Does this information collection employ statistical methods?

Q Yes x No 18. Agency contact ( person who can best answer questions regarding the content of this submission) Name: Nydia Yanira Reyes Morales Phone: 202 343 9264 OMB 83 I 10/ 95 19. Certification for Paperwork Reduction Act Submissions On behalf of this Federal agency, 1 certify that the collection of information encompassed by this request complies with' 5 CFR 1320.9.

NOTE: The text of 5 CFR 1320.9, and the related provisions of 5 CFR 1320.8( b)( 3), appear at the end of the instructions. The certification is to be made with reference to those regulatory provisions as set forth in the instructions.

The following is a summary of the topics, regarding the proposed collection of information, that the certification covers:

( a) It is necessary for the proper performance of agency functions;

( b) It avoids unnecessary duplication;

( c) It reduces burden on small entities;

( d) It uses plain, coherent, and unambiguous terminology that is understandable to respondents;

( e) Its implementation will be consistent and compatible with current reporting and recordkeeping practices;

( f) It indicates the retention periods for recordkeeping requirements;

( g) It informs respondents of the information called for under 5 CFR 1320.8( b)( 3): ( I) Why the information is being collected' ( ii) Use of information; ( iii) Burden estimate; ( iv) Nature of response ( voluntary, required for a benefit, or mandatory); ( v) Nature and extent of confidentiality; and ( vi) Need to display currently valid OMB control number;

( h) It was developed by an office that has planned and allocated resources for the efficient and effective management and use of the information to be collected ( see note in Item 19 of the instructions);

( I) It uses effective and efficient statistical survey methodology; and ( j) It makes appropriate use of information technology.

If you are unable to certify compliance with any of these provisions, identify the item below and explain the reason in Item 18 of the Supporting Statement.

Signature of Program Official Merrylin Zaw Mon, Director Certification and Compliance Division Office of Transportation and Air Quality Date Signature of Senior Official or designee Oscar Morales, Director Collection Strategies Division Office of Environmental Information Collection Date OMB 83 I 10/ 95 Certification Requirement for Paperwork Reduction Act Submissions 5 CFR 1320.9 reads " As part of the agency submission to OMB of a proposed collection of information, the agency ( through the head of the agency, the Senior Official or their designee) shall certify ( and provide a record supporting such certification) that the proposed collection of information

"( a) is necessary for the proper performance of the functions of the agency, including that the information to be collected will have practical utility;

"( b) is not unnecessarily duplicative of information otherwise reasonably accessible to the agency;

"( c) reduces to the extent practicable and appropriate the burden on persons who shall provide information to or for the agency, including with respect to small entities, as defined in the Regulatory Flexibility Act 5 U. S. C § 601( 6)), the use of such techniques as:

"( 1) establishing differing compliance or reporting requirements or timetables that take into account the resources available to those who are to respond; "( 2) the clarification, consolidation, or simplification of compliance and reporting requirements; or collection of information , or any part thereof; "( 3) an exemption from coverage of the collection of information, or any part thereof;

"( d) is written using plain, coherent, and unambiguous terminology and is understandable to those who are to respond;

"( e) is to be implemented in ways consistent and compatible, to the maximum extent practicable, with the existing reporting and recordkeeping practices of those who are to respond;

"( f) indicates for each recordkeeping requirement the length of time persons are required to maintain the records specified;

"( g) informs potential respondents of the information called for under § 1320.8( b)( 3); [ see below]

"( h) has been developed by an office that has planned and allocated resources for the efficient and effective management and use of the information to be collected, including the processing of the information in a manner which shall enhance, where appropriate, the utility of the information to agencies and the public;

"( I) uses effective and efficient statistical survey methodology appropriate to the purpose for which the information is to be collected; and "( j) to the maximum extent practicable, uses appropriate information technology to reduce burden and improve data quality, agency efficiency and responsiveness to the public."

NOTE: 5 CFR 1320.8( b)( 3) requires that each collection of information:

"( 3) informs and provides reasonable notice to the potential persons to whom the collection of information is addressed of: "( I) the reasons the information is planned to be and/ or has been used to further the proper performance of the functions of the agency; "( ii) the way such information is planned to be and/ or has been used to further the proper performance of the functions of the agency; "( iii) an estimate, to the extent practicable, of the average burden of the collection ( together with a request that the public direct to the agency any comments concerning the accuracy of this burden estimate and any suggestions for reducing this burden); "( iv) whether responses to the collection of information are voluntary, required to obtain or retain a benefit ( citing authority), or mandatory ( citing authority); "( v) the nature and extent of confidentiality to be provided, if any ( citing authority); and "( vi) the fact that any 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 OMB control number."

OMB 83 I ( Instructions) 10/ 95


[Federal Register Volume 86, Number 232 (Tuesday, December 7, 2021)]
[Notices]
[Page 69235]
[FR Doc No: 2021-26491]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. ER22-497-000]

NG Renewables Energy Marketing, LLC; Supplemental Notice That
Initial Market-Based Rate Filing Includes Request for Blanket Section
204 Authorization

    This is a supplemental notice in the above-referenced proceeding of
NG Renewables Energy Marketing, LLC's application for market-based rate
authority, with an accompanying rate tariff, noting that such
application includes a request for blanket authorization, under 18 CFR
part 34, of future issuances of securities and assumptions of
liability.
    Any person desiring to intervene or to protest should file with the
Federal Energy Regulatory Commission, 888 First Street NE, Washington,
DC 20426, in accordance with Rules 211 and 214 of the Commission's
Rules of Practice and Procedure (18 CFR 385.211 and 385.214). Anyone
filing a motion to intervene or protest must serve a copy of that
document on the Applicant.
    Notice is hereby given that the deadline for filing protests with
regard to the applicant's request for blanket authorization, under 18
CFR part 34, of future issuances of securities and assumptions of
liability, is December 21, 2021.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper, using the FERC Online links at http://www.ferc.gov. To facilitate electronic service, persons with internet
access who will eFile a document and/or be listed as a contact for an
intervenor must create and validate an eRegistration account using the
eRegistration link. Select the eFiling link to log on and submit the
intervention or protests.
    Persons unable to file electronically may mail similar pleadings to
the Federal Energy Regulatory Commission, 888 First Street NE,
Washington, DC 20426. Hand delivered submissions in docketed
proceedings should be delivered to Health and Human Services, 12225
Wilkins Avenue, Rockville, Maryland 20852.
    In addition to publishing the full text of this document in the
Federal Register, the Commission provides all interested persons an
opportunity to view and/or print the contents of this document via the
internet through the Commission's Home Page (http://www.ferc.gov) using
the ``eLibrary'' link. Enter the docket number excluding the last three
digits in the docket number field to access the document. At this time,
the Commission has suspended access to the Commission's Public
Reference Room, due to the proclamation declaring a National Emergency
concerning the Novel Coronavirus Disease (COVID-19), issued by the
President on March 13, 2020. For assistance, contact the Federal Energy
Regulatory Commission at [email protected] or call toll-free,
(886) 208-3676 or TYY,<PHONE_NUMBER>.

    Dated: December 1, 2021.
Kimberly D. Bose,
Secretary.
[FR Doc. 2021-26491 Filed 12-6-21; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register: September 27, 2010 (Volume 75, Number 186)]
[Rules and Regulations]
[Page 59071-59073]
[DOCID:fr27se10-9]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0439; Directorate Identifier 2010-NM-029-AD;
Amendment 39-16437; AD 2010-20-03]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. Model CL-600-2B16 (CL-
604 Variants (Including CL-605 Marketing Variant)) Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:

    Following five reported cases of * * * balance washer screw
failure on similar ADGs [air-driven generators]/ram air turbines
installed on other aircraft types, investigation by Hamilton
Sundstrand determined that a specific batch of the screws had a
metallographic non-conformity that increased their susceptibility to
brittle fracture. * * *
    Failure of a balance washer screw can result in loss of the
related balance washer, with consequent turbine imbalance. Such
imbalance could potentially result in ADG structural failure
(including blade failure), loss of ADG electrical power and
structural damage to the aircraft and, if deployment was activated
by a dual engine shutdown, could also result in loss of hydraulic
power for the flight controls [and consequent reduced ability of the
flightcrew to maintain the safe flight and landing of the airplane].
* * * * *
    We are issuing this AD to require actions to correct the unsafe
condition on these products.

DATES: This AD becomes effective November 1, 2010.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 1,
2010.

ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Christopher Alfano, Aerospace
Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New
York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410,
Westbury, New York 11590; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on June 2, 2010 (75 FR
30740). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:

    Following five reported cases of * * * balance washer screw
failure on similar ADGs [air-driven generators]/ram air turbines
installed on other aircraft types, investigation by Hamilton
Sundstrand determined that a specific batch of the screws had a
metallographic non-conformity that increased their susceptibility to
brittle fracture. Subsequently, it was established that 152 ``dry''
ADGs [Hamilton Sundstrand Part Numbers (P/Ns) in the 761339 series
and 1711405; see Note] either had non-conforming screws installed
during production or possibly during maintenance or repair at
Hamilton Sundstrand repair stations.
    Failure of a balance washer screw can result in loss of the
related balance washer, with consequent turbine imbalance. Such
imbalance could potentially result in ADG structural failure
(including blade failure), loss of ADG electrical power and
structural damage to the aircraft and, if deployment was activated
by a dual engine shutdown, could also result in loss of hydraulic
power for the flight controls [and consequent reduced ability of the
flightcrew to maintain the safe flight and landing of the airplane].
    This [Canadian] directive mandates checking of the ADG and
replacing the balance washer screws, if required. It also prohibits
future installation of unmodified ADGs.
    Note: ADGs with Hamilton Sundstrand P/Ns in the 761339 series
and 1711405 are installed on the aircraft model listed in the
Applicability section above in addition to Bombardier Inc. Models
CL-600-2B19, CL-600-2C10 and CL-600-2D24. The latter three models
are covered in a separate directive.

    You may obtain further information by examining the MCAI in the AD
docket.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S.

operators and is enforceable. In making these changes, we do not intend
to differ substantively from the information provided in the MCAI and
related service information.
    We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect 155 products of U.S. registry.
We also estimate that it will take about 10 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $0 per product.
Where the service information lists required parts costs that are
covered under warranty, we have assumed that there will be no charge
for these parts. As we do not control warranty coverage for affected
parties, some parties may incur costs higher than estimated here. Based
on these figures, we estimate the cost of this AD to the U.S. operators
to be $131,750, or $850 per product.

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 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 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 regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

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 the NPRM, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone<PHONE_NUMBER>) is in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

0
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 AD:

2010-20-03 Bombardier, Inc.: Amendment 39-16437. Docket No. FAA-
2010-0439; Directorate Identifier 2010-NM-029-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective November
1, 2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Bombardier, Inc. Model CL-600-2B16 (CL-
604 Variant) airplanes; certificated in any category; serial numbers
(S/N) 5408 and subsequent.

    Note 1: Some Model CL-600-2B16 (CL-604 Variant) airplanes might
be referred to by a marketing designation of CL-605.

Subject

    (d) Air Transport Association (ATA) of America Code 24:
Electrical power.

Reason

    (e) The mandatory continuing airworthiness information (MCAI)
states:
    Following five reported cases of * * * balance washer screw
failure on similar ADGs [air-driven generators]/ram air turbines
installed on other aircraft types, investigation by Hamilton
Sundstrand determined that a specific batch of the screws had a
metallographic non-conformity that increased their susceptibility to
brittle fracture. Subsequently, it was established that 152 ``dry''
ADGs [Hamilton Sundstrand Part Numbers (P/Ns) in the 761339 series
and 1711405; see Note] either had non-conforming screws installed
during production or possibly during maintenance or repair at
Hamilton Sundstrand repair stations.
    Failure of a balance washer screw can result in loss of the
related balance washer, with consequent turbine imbalance. Such
imbalance could potentially result in ADG structural failure
(including blade failure), loss of ADG electrical power and
structural damage to the aircraft and, if deployment was activated
by a dual engine shutdown, could also result in loss of hydraulic
power for the flight controls [and consequent reduced ability of the
flightcrew to maintain the safe flight and landing of the airplane].
    This [Canadian] directive mandates checking of the ADG and
replacing the balance washer screws, if required. It also prohibits
future installation of unmodified ADGs.

    Note: ADGs with Hamilton Sundstrand P/Ns in the 761339 series
and 1711405 are installed on the aircraft model listed in the
Applicability section above in addition to Bombardier Inc. Models
CL-600-2B19, CL-600-2C10 and CL-600-2D24. The latter three models
are covered in a separate directive.

Compliance

    (f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.

Actions

    (g) At the earliest of the times identified in paragraphs
(g)(1), (g)(2), (g)(3), and (g)(4) of this AD, do an inspection to
determine the serial number of the installed ADG. A review of
airplane maintenance records is acceptable in lieu of this
inspection if the serial number of the ADG can be conclusively
determined from that review.
    (1) Within 400 flight hours or 12 months after the effective
date of this AD, whichever occurs first, or
    (2) Prior to the next in-flight or on-ground functional test of
the ADG, whichever occurs first after the effective date of this AD,
or
    (3) Prior to the next in-flight or on-ground operational test of
the ADG, whichever occurs first after the effective date of this AD,
or
    (4) Prior to the next scheduled ADG in-flight deployment.

    (h) If the ADG serial number, as determined in paragraph (g) of
this AD, is not listed in paragraph 1.A of the applicable Bombardier
service bulletin listed in Table 1 of this AD, no further action is
required by this AD, except as required by paragraph (j) of this AD.

                       Table 1--Service Bulletins
------------------------------------------------------------------------
                                 Bombardier
           Model--                 Service              Dated--
                                 Bulletin--
------------------------------------------------------------------------
CL-600-2B16 (CL-604)               604-24-021  July 13, 2009.
 airplanes.
CL-600-2B16 (CL-605)               605-24-001  July 13, 2009.
 airplanes.
------------------------------------------------------------------------

     (i) If the ADG serial number determined in paragraph (g) of
this AD is identified in paragraph 1.A. of the applicable service
bulletin listed in Table 1 of this AD, before further flight, do an
inspection to determine if the symbol ``24-5'' is marked on the ADG
identification plate. A review of airplane maintenance records is
acceptable in lieu of this inspection if the symbol ``24-5'' can be
conclusively determined from that review.
    (1) If the symbol ``24-5'' is marked on the ADG identification
plate, and the balance washer screws have already been replaced, no
further action is required by this AD, except as required by
paragraph (j) of this AD.
    (2) If the symbol ``24-5'' is not marked on the ADG
identification plate, before further flight, replace all balance
washer screws with new screws having part number MS24667-14 and mark
the ADG identification plate with symbol ``24-5'', in accordance
with the Accomplishment Instructions of the applicable service
bulletin listed in Table 1 of this AD.
    (j) As of the effective date of this AD, no person may install
on any airplane a replacement or spare ADG, Hamilton Sundstrand part
number in the 761339 or 1711405 series, having one of the serial
numbers identified in paragraph 1.A. of the applicable service
bulletin listed in Table 1 of this AD, unless the ADG is identified
with the symbol ``24-5'' on the identification plate.

FAA AD Differences

    Note 2:  This AD differs from the MCAI and/or service
information as follows: The MCAI specifies to inspect only airplanes
having certain serial numbers that are part of the MCAI
applicability. Because the affected part could be rotated onto any
of the airplanes listed in the applicability, this AD requires the
inspection be done on all airplanes. We have coordinated this
difference with TCCA.

Other FAA AD Provisions

    (k) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. Send information to ATTN: Program
Manager, Continuing Operational Safety, FAA, New York ACO, 1600
Stewart Avenue, Suite 410, Westbury, New York, 11590; telephone 516-
228-7300; fax<PHONE_NUMBER>. Before using any approved AMOC on any
airplane to which the AMOC applies, notify your principal
maintenance inspector (PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal inspector, your local Flight
Standards District Office. The AMOC approval letter must
specifically reference this AD.
    (2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.

Related Information

    (l) Refer to MCAI Canadian Airworthiness Directive CF-2009-50,
dated December 17, 2009; and Bombardier Service Bulletins 604-24-
021, dated July 13, 2009, and 605-24-001, dated July 13, 2009; for
related information.

Material Incorporated by Reference

    (m) You must use Bombardier Service Bulletin 604-24-021, dated
July 13, 2009; or Bombardier Service Bulletin 605-24-001, dated July
13, 2009; as applicable; to do the actions required by this AD,
unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone<PHONE_NUMBER>; fax 514-855-
7401; e-mail<EMAIL_ADDRESS>Internet http://
www.bombardier.com.
    (3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.
    (4) You may also review copies of the 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, call<PHONE_NUMBER>, or go to: http://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.

    Issued in Renton, Washington, on September 10, 2010.
Jeffrey E. Duven,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-23742 Filed 9-24-10; 8:45 am]
BILLING CODE 4910-13-P