Airworthiness Directives; SOCATA Model TBM 700 Airplanes, 58539-58540 [E9-27321]

Download as PDF Federal Register / Vol. 74, No. 218 / Friday, November 13, 2009 / Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 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 September 2, 2009 (74 FR 45391), and proposed to revise AD 2009–13–05, Amendment 39–15944 (74 FR 29126, June 19, 2009). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states that: 14 CFR Part 39 [Docket No. FAA–2009–0557; Directorate Identifier 2009–CE–031–AD; Amendment 39–16086; AD 2009–23–12] RIN 2120–AA64 Airworthiness Directives; SOCATA Model TBM 700 Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. We are revising an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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: SUMMARY: mstockstill on DSKH9S0YB1PROD with RULES During a SOCATA flight test, it has been noted some difficulties for the pilot to release oxygen. After investigation it has been found that, due to the design of the oxygen generator release pin, one of the mask’s lanyard linked to the pin can be jammed when it is pulled by a pilot or a passenger. This condition, if not corrected, would lead, in case of an emergency procedure due to decompression, to a risk of generator fault with subsequent lack of oxygen on crew and/ or passenger. * * * This revision has been released to clarify the applicability. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective December 18, 2009. As of July 9, 2009 (74 FR 29126, June 19, 2009), the Director of the Federal Register approved the incorporation by reference of page 3.13.5 of Temporary Revision No. 3, dated March 2009, of SOCATA TBM 700 A & B Pilot Operating Handbook (POH), listed in this AD. ADDRESSES: You may examine the AD docket on the Internet at http:// www.regulations.gov or in person at the Docket Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Albert Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, VerDate Nov<24>2008 17:06 Nov 12, 2009 Jkt 220001 Missouri 64106; telephone: (816) 329– 4119; fax: (816) 329–4090. SUPPLEMENTARY INFORMATION: During a SOCATA flight test, it has been noted some difficulties for the pilot to release oxygen. After investigation it has been found that, due to the design of the oxygen generator release pin, one of the mask’s lanyard linked to the pin can be jammed when it is pulled by a pilot or a passenger. This condition, if not corrected, would lead, in case of an emergency procedure due to decompression, to a risk of generator fault with subsequent lack of oxygen on crew and/ or passenger. For the reason described above, SOCATA has released Pilot Operating Handbook (POH) Temporary Revision (TR) 03 which asks, in case of failure to release oxygen, to pull on the other mask lanyard in order to activate the oxygen generator. This revision has been released to clarify the applicability. A SOCATA modification enabling to solve this issue is under preparation. Once this modification has been released, this AD is expected to be revised to confirm the acceptability of that modification. 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 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 58539 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 FAA policies. Any such differences are highlighted in a NOTE within the AD. Costs of Compliance We estimate that this AD will affect 147 products of U.S. registry. We also estimate that it will take about 0.5 workhour per product to comply with the basic requirements of this AD. The average labor rate is $80 per work-hour. Based on these figures, we estimate the cost of this AD on U.S. operators to be $5,880, or $40 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 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. E:\FR\FM\13NOR1.SGM 13NOR1 58540 Federal Register / Vol. 74, No. 218 / Friday, November 13, 2009 / Rules and Regulations Examining the AD Docket You may examine the AD docket on the Internet at http:// www.regulations.gov; or in person at the Docket Management Facility 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 Office (telephone (800) 647–5527) 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 Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: ■ PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by removing Amendment 39–15944 (74 FR 29126, June 19, 2009) and adding the following new AD: ■ 2009–23–12 SOCATA: Amendment 39– 16086; Docket No. FAA–2009–0557; Directorate Identifier 2009–CE–031–AD. During a SOCATA flight test, it has been noted some difficulties for the pilot to release oxygen. After investigation it has been found that, due to the design of the oxygen generator release pin, one of the mask’s lanyard linked to the pin can be jammed when it is pulled by a pilot or a passenger. This condition, if not corrected, would lead, in case of an emergency procedure due to decompression, to a risk of generator fault with subsequent lack of oxygen on crew and/ or passenger. For the reason described above, SOCATA has released Pilot Operating Handbook (POH) Temporary Revision (TR) 03 which asks, in case of failure to release oxygen, to pull on the other mask lanyard in order to activate the oxygen generator. This revision has been released to clarify the applicability. A SOCATA modification enabling to solve this issue is under preparation. Once this modification has been released, this AD is expected to be revised to confirm the acceptability of that modification. Actions and Compliance (f) Unless already done, do the following actions. (1) Before further flight after July 9, 2009 (the effective date retained from AD 2009– 13–05), insert Page 3.13.5 of Temporary Revision No. 3, dated March 2009, into the Emergency Procedures section and the Limitations section of SOCATA TBM 700 A & B Pilot Operating Handbook (POH). (2) Under 14 CFR section 43.7 of the Federal Aviation Administration Regulations (14 CFR 43.7), the owner/operator holding at least a private pilot certificate is allowed to insert the temporary revision into the POH. Make an entry into the aircraft logbook showing compliance with this portion of the AD per compliance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9). FAA AD Differences Effective Date (a) This airworthiness directive (AD) becomes effective December 18, 2009. Note: This AD differs from the MCAI and/ or service information as follows: No differences. Affected ADs (b) This AD revises AD 2009–13–05, Amendment 39–15944. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, 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: Albert Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4119; fax: (816) 329– 4090. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (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 Applicability (c) This AD applies to the following model and serial number airplanes that are: (i) certificated in any category; and (ii) equipped with a chemical oxygen generation system. Model Serial Nos. mstockstill on DSKH9S0YB1PROD with RULES TBM 700 ............ 1 through 204, 206 through 239, and 241 through 243. Subject (d) Air Transport Association of America (ATA) Code 35: Oxygen. Reason (e) The mandatory continuing airworthiness information (MCAI) states: VerDate Nov<24>2008 17:06 Nov 12, 2009 Jkt 220001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 (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. Material Incorporated by Reference (h) You must use page 3.13.5 of Temporary Revision No. 3, dated March 2009, of SOCATA TBM 700 A & B Pilot Operating Handbook (POH), to do the actions required by this AD, unless the AD specifies otherwise. (1) On July 9, 2009 (74 FR 29126, June 19, 2009), the Director of the Federal Register previously approved the incorporation by reference of page 3.13.5 of Temporary Revision No. 3, dated March 2009, of SOCATA TBM 700 A & B Pilot Operating Handbook (POH). (2) For service information identified in this AD, contact SOCATA, 65921—TARBES Cedex 9, France; telephone: +33 6 07 32 62 24; or SOCATA, North Perry Airport, 7501 South Airport Rd., Pembrokes Pines, FL 33023; telephone: (954) 893–1400; fax: (954) 964–4141; Internet: http://mysocata.com. (3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329–3768. (4) You may also review copies of the service information incorporated by reference for this AD 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. Issued in Kansas City, Missouri, on November 6, 2009. Margaret Kline, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E9–27321 Filed 11–12–09; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF JUSTICE 28 CFR Part 2 Paroling, Recommitting, and Supervising Federal Prisoners: Prisoners Serving Sentences Under the United States and District of Columbia Codes AGENCY: United States Parole Commission, Department of Justice. ACTION: Final rule. SUMMARY: The Parole Commission is establishing an administrative remedy E:\FR\FM\13NOR1.SGM 13NOR1

Agencies

[Federal Register Volume 74, Number 218 (Friday, November 13, 2009)]
[Rules and Regulations]
[Pages 58539-58540]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-27321]



[[Page 58539]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0557; Directorate Identifier 2009-CE-031-AD; 
Amendment 39-16086; AD 2009-23-12]
RIN 2120-AA64


Airworthiness Directives; SOCATA Model TBM 700 Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are revising an existing airworthiness directive (AD) for 
the products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued 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:

    During a SOCATA flight test, it has been noted some difficulties 
for the pilot to release oxygen.
    After investigation it has been found that, due to the design of 
the oxygen generator release pin, one of the mask's lanyard linked 
to the pin can be jammed when it is pulled by a pilot or a 
passenger.
    This condition, if not corrected, would lead, in case of an 
emergency procedure due to decompression, to a risk of generator 
fault with subsequent lack of oxygen on crew and/or passenger. * * *
    This revision has been released to clarify the applicability.

    We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective December 18, 2009.
    As of July 9, 2009 (74 FR 29126, June 19, 2009), the Director of 
the Federal Register approved the incorporation by reference of page 
3.13.5 of Temporary Revision No. 3, dated March 2009, of SOCATA TBM 700 
A & B Pilot Operating Handbook (POH), listed in this AD.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the Docket Management Facility, 
U.S. Department of Transportation, Docket Operations, M-30, West 
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Albert Mercado, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090.

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 September 2, 2009 
(74 FR 45391), and proposed to revise AD 2009-13-05, Amendment 39-15944 
(74 FR 29126, June 19, 2009). That NPRM proposed to correct an unsafe 
condition for the specified products. The MCAI states that:

    During a SOCATA flight test, it has been noted some difficulties 
for the pilot to release oxygen.
    After investigation it has been found that, due to the design of 
the oxygen generator release pin, one of the mask's lanyard linked 
to the pin can be jammed when it is pulled by a pilot or a 
passenger.
    This condition, if not corrected, would lead, in case of an 
emergency procedure due to decompression, to a risk of generator 
fault with subsequent lack of oxygen on crew and/or passenger.
    For the reason described above, SOCATA has released Pilot 
Operating Handbook (POH) Temporary Revision (TR) 03 which asks, in 
case of failure to release oxygen, to pull on the other mask lanyard 
in order to activate the oxygen generator.
    This revision has been released to clarify the applicability.
    A SOCATA modification enabling to solve this issue is under 
preparation. Once this modification has been released, this AD is 
expected to be revised to confirm the acceptability of that 
modification.

    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 FAA policies. Any such differences are 
highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect 147 products of U.S. registry. 
We also estimate that it will take about 0.5 work-hour per product to 
comply with the basic requirements of this AD. The average labor rate 
is $80 per work-hour.
    Based on these figures, we estimate the cost of this AD on U.S. 
operators to be $5,880, or $40 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 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.

[[Page 58540]]

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility 
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 Office (telephone (800) 647-5527) 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 removing Amendment 39-15944 (74 FR 
29126, June 19, 2009) and adding the following new AD:

2009-23-12 SOCATA: Amendment 39-16086; Docket No. FAA-2009-0557; 
Directorate Identifier 2009-CE-031-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective December 
18, 2009.

Affected ADs

    (b) This AD revises AD 2009-13-05, Amendment 39-15944.

Applicability

    (c) This AD applies to the following model and serial number 
airplanes that are:
    (i) certificated in any category; and
    (ii) equipped with a chemical oxygen generation system.

------------------------------------------------------------------------
                   Model                             Serial Nos.
------------------------------------------------------------------------
TBM 700...................................  1 through 204, 206 through
                                             239, and 241 through 243.
------------------------------------------------------------------------

Subject

    (d) Air Transport Association of America (ATA) Code 35: Oxygen.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    During a SOCATA flight test, it has been noted some difficulties 
for the pilot to release oxygen.
    After investigation it has been found that, due to the design of 
the oxygen generator release pin, one of the mask's lanyard linked 
to the pin can be jammed when it is pulled by a pilot or a 
passenger.
    This condition, if not corrected, would lead, in case of an 
emergency procedure due to decompression, to a risk of generator 
fault with subsequent lack of oxygen on crew and/or passenger.
    For the reason described above, SOCATA has released Pilot 
Operating Handbook (POH) Temporary Revision (TR) 03 which asks, in 
case of failure to release oxygen, to pull on the other mask lanyard 
in order to activate the oxygen generator.
    This revision has been released to clarify the applicability.
    A SOCATA modification enabling to solve this issue is under 
preparation. Once this modification has been released, this AD is 
expected to be revised to confirm the acceptability of that 
modification.

Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Before further flight after July 9, 2009 (the effective date 
retained from AD 2009-13-05), insert Page 3.13.5 of Temporary 
Revision No. 3, dated March 2009, into the Emergency Procedures 
section and the Limitations section of SOCATA TBM 700 A & B Pilot 
Operating Handbook (POH).
    (2) Under 14 CFR section 43.7 of the Federal Aviation 
Administration Regulations (14 CFR 43.7), the owner/operator holding 
at least a private pilot certificate is allowed to insert the 
temporary revision into the POH. Make an entry into the aircraft 
logbook showing compliance with this portion of the AD per 
compliance with section 43.9 of the Federal Aviation Regulations (14 
CFR 43.9).

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows: No differences.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, 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: Albert Mercado, Aerospace Engineer, FAA, Small 
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4119; fax: (816) 329-4090. Before using 
any approved AMOC on any airplane to which the AMOC applies, notify 
your appropriate principal inspector (PI) in the FAA Flight 
Standards District Office (FSDO), or lacking a PI, your local FSDO.
    (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.

Material Incorporated by Reference

    (h) You must use page 3.13.5 of Temporary Revision No. 3, dated 
March 2009, of SOCATA TBM 700 A & B Pilot Operating Handbook (POH), 
to do the actions required by this AD, unless the AD specifies 
otherwise.
    (1) On July 9, 2009 (74 FR 29126, June 19, 2009), the Director 
of the Federal Register previously approved the incorporation by 
reference of page 3.13.5 of Temporary Revision No. 3, dated March 
2009, of SOCATA TBM 700 A & B Pilot Operating Handbook (POH).
    (2) For service information identified in this AD, contact 
SOCATA, 65921--TARBES Cedex 9, France; telephone: +33 6 07 32 62 24; 
or SOCATA, North Perry Airport, 7501 South Airport Rd., Pembrokes 
Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141; 
Internet: http://mysocata.com.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD 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.

    Issued in Kansas City, Missouri, on November 6, 2009.
Margaret Kline,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E9-27321 Filed 11-12-09; 8:45 am]
BILLING CODE 4910-13-P