Airworthiness Directives; Fokker Services B.V. Airplanes, 8181-8183 [2012-3387]

Download as PDF Federal Register / Vol. 77, No. 30 / Tuesday, February 14, 2012 / Proposed Rules § 630.6 Funding Corporation committees. (a) System Audit Committee. * * * * * * * * (3) Resources. The Funding Corporation must provide the SAC monetary and nonmonetary resources the SAC determines necessary to enable it to perform the duties listed in paragraph (a)(4) of this section. The Funding Corporation must permit the SAC to contract, for reasons directly related to the duties listed in paragraph (a)(4), the services of external auditors, independent legal counsel, and outside advisors. The SAC must not use the resources of the Funding Corporation in a manner that would adversely affect the safety and soundness of the System or be contrary to law and regulation. The SAC must provide the Funding Corporation board of directors a quarterly accounting of expenditures made pursuant to this section. (4) Duties. * * * * * * * * (ii) External auditors. The external auditor must report directly to the SAC. The SAC must: (A) Determine, with the agreement of the Funding Corporation board of directors, the appointment, compensation, and retention of the external auditors issuing System-wide audit reports; * * * * * Subpart B—Annual Report to Investors 3. Section 630.20 is amended by revising paragraph (n) to read as follows: § 630.20 Contents of the annual report to investors. mstockstill on DSK4VPTVN1PROD with PROPOSALS * * * * * (n) System Audit Committee. The Funding Corporation must include in the System-wide Report to Investors a description of the System Audit Committee and its activities during the reporting period. At a minimum, the report must: (1) List the names of the System Audit Committee members, including each member’s term of office and principal occupation during the past 5 years. For each member, state the total cash and noncash compensation paid for services on the System Audit Committee during the reporting period. (2) Categorize and disclose the dollar value of monetary and nonmonetary resources used by the System Audit Committee during the reporting period. Describe the benefit(s) obtained from expenditures made under each category. Disclosures of fees paid for the audit of the System-wide financial statements and those categories of expenses having VerDate Mar<15>2010 16:41 Feb 13, 2012 Jkt 226001 an annual aggregate dollar value of less than $5,000 are not required. At a minimum, there must be separate categories for: (i) Administrative expenses, (ii) Contracted legal services, (iii) Contracted consultants and advisors, and (iv) Other contracted services, identifying the services. * * * * * Dated: February 9, 2012. Dale L. Aultman, Secretary, Farm Credit Administration Board. [FR Doc. 2012–3411 Filed 2–13–12; 8:45 am] BILLING CODE 6705–01–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2012–0141; Directorate Identifier 2011–NM–092–AD] RIN 2120–AA64 Airworthiness Directives; Fokker Services B.V. Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This proposed AD was prompted by an in-flight failure of the hydraulic control panel, which resulted in the absence of pressure and quantity indication of the hydraulic system and accompanying alerts for ‘‘hydraulic system 1 low quantity’’ and ‘‘hydraulic system 2 low quantity.’’ This proposed AD would require implementing new abnormal procedures for hydraulics in the airplane flight manual (AFM). We are proposing this AD to prevent loss of control of the airplane due to incorrect hydraulic system failure information being provided to the flightcrew, followed by application of inappropriate procedures. DATES: We must receive comments on this proposed AD by March 30, 2012. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590. SUMMARY: PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 8181 • Hand Delivery: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252– 627–350; fax +31 (0)252–627–211; email technicalservices.fokkerservices@ stork.com; Internet https:// www.myfokkerfleet.com. You may review copies of the referenced 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 425–227–1221. Examining the AD Docket You may examine the AD docket on the Internet at https:// 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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone (800) 647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 227–1137; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2012–0141; Directorate Identifier 2011–NM–092–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. E:\FR\FM\14FEP1.SGM 14FEP1 8182 Federal Register / Vol. 77, No. 30 / Tuesday, February 14, 2012 / Proposed Rules Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued EASA Airworthiness Directive 2011–0051, dated March 22, 2011 (referred to after this as ‘‘the MCAI’’), to correct an unsafe condition for the specified products. The MCAI states: An in-flight failure of the hydraulic control panel resulted in the absence of pressure and quantity indication of the hydraulic system and accompanying alerts for ‘‘hydraulic system 1 low quantity’’ and ‘‘hydraulic system 2 low quantity’’. The procedures prescribed the shut-off of the engine driven hydraulic pumps, resulting in complete absence of hydraulic pressure, which made it impossible to hydraulically control the flight controls, including the stabiliser. The status information contained in the procedures for these alerts may give the false impression that the stabiliser is still hydraulically controllable on one channel. The flight crew regained control by using the alternate electrically powered stabiliser control. A safety review revealed that a ‘‘hydraulic system 1 and 2 low quantity’’ alert could give the right information, however this alert is not available in the Flight Warning System. To solve this problem, Fokker Services improved the Hydraulic 1(2) Low Quantity Procedures in the Airplane Flight Manual (AFM). For the reasons described above, this [EASA] AD requires the implementation of new abnormal procedures for hydraulics in the AFM. The unsafe condition is possible loss of control of the airplane due to incorrect hydraulic system failure information being provided to the flightcrew, followed by application of inappropriate procedures. You may obtain further information by examining the MCAI in the AD docket. mstockstill on DSK4VPTVN1PROD with PROPOSALS Relevant Service Information Fokker Services B.V. has issued Manual Change Notification— Operational Documentation MCNO F100–057, dated December 17, 2010. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI. FAA’s Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe VerDate Mar<15>2010 16:41 Feb 13, 2012 Jkt 226001 condition exists and is likely to exist or develop on other products of the same type design. Costs of Compliance Based on the service information, we estimate that this proposed AD would affect about 4 products of U.S. registry. We also estimate that it would take about 1 work-hour per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $340, or $85 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 proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed regulation: 1. Is not a ‘‘significant regulatory action’’ under Executive Order 12866; 2. Is not a ‘‘significant rule’’ under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and 3. Will not affect intrastate aviation in Alaska; and 4. 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 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 this proposed 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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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 adding the following new AD: Fokker Services B.V.: Docket No. FAA– 2012–0141; Directorate Identifier 2011– NM–092–AD. (a) Comments Due Date We must receive comments by March 30, 2012. (b) Affected ADs None. (c) Applicability This AD applies to Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers. (d) Subject Air Transport Association (ATA) of America Code 29: Hydraulic power. (e) Reason This AD was prompted by an in-flight failure of the hydraulic control panel, which resulted in the absence of pressure and quantity indication of the hydraulic system and accompanying alerts for ‘‘hydraulic system 1 low quantity’’ and ‘‘hydraulic system 2 low quantity.’’ This proposed AD would require implementing new abnormal procedures for hydraulics in the airplane flight manual (AFM). We are issuing this AD to prevent loss of control of the airplane due to incorrect hydraulic system failure information being provided to the flightcrew, followed by application of inappropriate procedures. (f) Compliance You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. (g) Airplane Flight Manual (AFM) Revision Within 3 months after the effective date of this AD, revise the Abnormal Procedures— Hydraulics section of the Fokker F.28 AFM by incorporating the information specified in Fokker Manual Change Notification— Operational Documentation (MCNO) MCNO– E:\FR\FM\14FEP1.SGM 14FEP1 Federal Register / Vol. 77, No. 30 / Tuesday, February 14, 2012 / Proposed Rules F100–057, dated December 17, 2010, into the Abnormal Procedures—Hydraulics section of the AFM. Note 1 to paragraph (g): The actions required by paragraph (g) of this AD may be done by inserting a copy of MCNO Fokker MCNO–F100–057, dated December 17, 2010, into the Abnormal Procedures—Hydraulics section of the Fokker F.28 AFM. When MCNO Fokker MCNO–F100–057, dated December 17, 2010, has been included in the general revisions of the AFM, the general revisions may be inserted in the AFM, provided the relevant information in the general revision is identical to that in MCNO Fokker MCNO–F100–057, dated December 17, 2010, and that MCNO may be removed. (h) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 227–1137; fax (425) 227–1149. Information may be emailed to: 9ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding 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. mstockstill on DSK4VPTVN1PROD with PROPOSALS (i) Related Information Refer to MCAI European Aviation Safety Agency (EASA) Airworthiness Directive 2011–0051, dated March 22, 2011; and MCNO Fokker MCNO-F100-057, dated December 17, 2010; for related information. Issued in Renton, Washington on February 7, 2012. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2012–3387 Filed 2–13–12; 8:45 am] BILLING CODE 4910–13–P VerDate Mar<15>2010 16:41 Feb 13, 2012 Jkt 226001 8183 RAILROAD RETIREMENT BOARD List of Subjects in 20 CFR Parts 200, 320, and 345 20 CFR Parts 200, 320, and 345 Railroad employees, Railroad employers, Railroad retirement, Railroad unemployment. For the reasons set out in the preamble, the Railroad Retirement Board proposes to amend title 20, chapter II, subchapter A, part 200 and subchapter C, parts 320 and 345 of the Code of Federal Regulations as follows: RIN 3220—AB65 Restructuring of the Office of Programs; Elimination of Regional Offices AGENCY: ACTION: Railroad Retirement Board. Proposed rule. The Railroad Retirement Board (Board) proposes to amend its regulations to reflect the restructuring of the Office of Programs and the elimination of the Regional Offices. SUMMARY: Submit comments on or before April 16, 2012. DATES: Address any comments concerning this proposed rule to Martha P. Rico, Secretary to the Board, Railroad Retirement Board, 844 N. Rush Street, Chicago, Illinois 60611–2092. ADDRESSES: FOR FURTHER INFORMATION CONTACT: Marguerite P. Dadabo, Assistant General Counsel, (312) 751–4945, TTD (312) 751–4701. The Railroad Retirement Board has restructured its Office of Assessment and Training in a Board-approved reorganization plan. The Office of Assessment and Training, formerly a single component of the Office of Programs, is now intermingled with other subcomponents of the Office of Programs. Therefore, issues that were formerly under the jurisdiction of the Office of Programs/Assessment and Training are now under the jurisdiction of the Office of Programs/Policy and Systems for purposes of the following regulations. Additionally, the Railroad Retirement Board underwent a reorganization of its regional offices in an effort to improve efficiency and eliminate duplication. As a result of this reorganization, the Railroad Retirement Board eliminated its Regional Offices in Atlanta, Georgia, Denver, Colorado, and Philadelphia, Pennsylvania. The work done by the Regional Offices is now handled by the Field Services Headquarters staff. The Board, with the concurrence of the Office of Management and Budget, has determined that this is not a significant regulatory action under Executive Order 12866, as amended. Therefore, no regulatory impact analysis is required. There are no changes to the information collections associated with Parts 200, 320 and 345. SUPPLEMENTARY INFORMATION: PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 PART 200—GENERAL ADMINISTRATION 1. The authority citation for part 200 continues to read as follows: Authority: 45 U.S.C. 231f(b)(5) and 45 U.S.C. 362; 200.4 also issued under 5 U.S.C. 552; 200.5 also issued under 5 U.S.C. 552a; 200.6 also issued under 5 U.S.C. 552b; and 200.7 also issued under 31 U.S.C. 3717. 2. In § 200.1, paragraph (a)(4) is revised to read as follows: § 200.1 Designation of central and field organization. (a) * * * (4) The headquarters of the Board is in Chicago, Illinois, at 844 North Rush Street. The Board maintains numerous district offices across the country in localities easily accessible to large numbers of railroad workers. * * * * * 3. In § 200.4, paragraphs (d)(1), (d)(2), and (d)(5) are revised to read as follows: § 200.4 public. Availability of information to the * * * * * (d) * * * (1) In the Office of Programs/ Operations: The Retirement Claims Manual, RCM Circulars, Special Services Manual, Policy Decisions, Procedural Memoranda containing information on the adjudication of claims not contained in the Retirement Claims Manual or in RCM Circulars, Field Operating Manual (Parts I and VI), FOM Circulars and Memoranda, the Occupational Disability Rating Schedule, Adjudication Instruction Manual, memorandum instructions on adjudication, and circular letters of instruction to railroad officials. (2) In the Office of Programs/Policy and Systems: The Instructions to Employers, and Circular Letters to Employers. * * * * * (5) Field offices shall also make available to the extent practicable such of these materials and indexes as are furnished them in the ordinary course of business. * * * * * E:\FR\FM\14FEP1.SGM 14FEP1

Agencies

[Federal Register Volume 77, Number 30 (Tuesday, February 14, 2012)]
[Proposed Rules]
[Pages 8181-8183]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-3387]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0141; Directorate Identifier 2011-NM-092-AD]
RIN 2120-AA64


Airworthiness Directives; Fokker Services B.V. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all 
Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This 
proposed AD was prompted by an in-flight failure of the hydraulic 
control panel, which resulted in the absence of pressure and quantity 
indication of the hydraulic system and accompanying alerts for 
``hydraulic system 1 low quantity'' and ``hydraulic system 2 low 
quantity.'' This proposed AD would require implementing new abnormal 
procedures for hydraulics in the airplane flight manual (AFM). We are 
proposing this AD to prevent loss of control of the airplane due to 
incorrect hydraulic system failure information being provided to the 
flightcrew, followed by application of inappropriate procedures.

DATES: We must receive comments on this proposed AD by March 30, 2012.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact 
Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE 
Nieuw-Vennep, the Netherlands; telephone +31 (0)252-627-350; fax +31 
(0)252-627-211; email technicalservices.fokkerservices@stork.com; 
Internet https://www.myfokkerfleet.com. You may review copies of the 
referenced 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 425-227-1221.

Examining the AD Docket

    You may examine the AD docket on the Internet at https://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 proposed AD, the regulatory 
evaluation, any comments received, and other information. The street 
address for the Docket Operations office (telephone (800) 647-5527) is 
in the ADDRESSES section. Comments will be available in the AD docket 
shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 
227-1137; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-0141; 
Directorate Identifier 2011-NM-092-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on those comments.
    We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

[[Page 8182]]

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued EASA 
Airworthiness Directive 2011-0051, dated March 22, 2011 (referred to 
after this as ``the MCAI''), to correct an unsafe condition for the 
specified products. The MCAI states:

    An in-flight failure of the hydraulic control panel resulted in 
the absence of pressure and quantity indication of the hydraulic 
system and accompanying alerts for ``hydraulic system 1 low 
quantity'' and ``hydraulic system 2 low quantity''. The procedures 
prescribed the shut-off of the engine driven hydraulic pumps, 
resulting in complete absence of hydraulic pressure, which made it 
impossible to hydraulically control the flight controls, including 
the stabiliser. The status information contained in the procedures 
for these alerts may give the false impression that the stabiliser 
is still hydraulically controllable on one channel. The flight crew 
regained control by using the alternate electrically powered 
stabiliser control.
    A safety review revealed that a ``hydraulic system 1 and 2 low 
quantity'' alert could give the right information, however this 
alert is not available in the Flight Warning System. To solve this 
problem, Fokker Services improved the Hydraulic 1(2) Low Quantity 
Procedures in the Airplane Flight Manual (AFM).
    For the reasons described above, this [EASA] AD requires the 
implementation of new abnormal procedures for hydraulics in the AFM.

The unsafe condition is possible loss of control of the airplane due to 
incorrect hydraulic system failure information being provided to the 
flightcrew, followed by application of inappropriate procedures. You 
may obtain further information by examining the MCAI in the AD docket.

Relevant Service Information

    Fokker Services B.V. has issued Manual Change Notification--
Operational Documentation MCNO F100-057, dated December 17, 2010. The 
actions described in this service information are intended to correct 
the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all pertinent information and determined an unsafe condition 
exists and is likely to exist or develop on other products of the same 
type design.

Costs of Compliance

    Based on the service information, we estimate that this proposed AD 
would affect about 4 products of U.S. registry. We also estimate that 
it would take about 1 work-hour per product to comply with the basic 
requirements of this proposed AD. The average labor rate is $85 per 
work-hour. Based on these figures, we estimate the cost of the proposed 
AD on U.S. operators to be $340, or $85 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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 proposed 
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not affect intrastate aviation in Alaska; and
    4. 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 proposed 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.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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.


Sec.  39.13  [Amended]

    2. The FAA amends Sec.  39.13 by adding the following new AD:

Fokker Services B.V.: Docket No. FAA-2012-0141; Directorate 
Identifier 2011-NM-092-AD.

(a) Comments Due Date

    We must receive comments by March 30, 2012.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Fokker Services B.V. Model F.28 Mark 0070 and 
0100 airplanes, certificated in any category, all serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 29: Hydraulic 
power.

(e) Reason

    This AD was prompted by an in-flight failure of the hydraulic 
control panel, which resulted in the absence of pressure and 
quantity indication of the hydraulic system and accompanying alerts 
for ``hydraulic system 1 low quantity'' and ``hydraulic system 2 low 
quantity.'' This proposed AD would require implementing new abnormal 
procedures for hydraulics in the airplane flight manual (AFM). We 
are issuing this AD to prevent loss of control of the airplane due 
to incorrect hydraulic system failure information being provided to 
the flightcrew, followed by application of inappropriate procedures.

(f) Compliance

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

(g) Airplane Flight Manual (AFM) Revision

    Within 3 months after the effective date of this AD, revise the 
Abnormal Procedures--Hydraulics section of the Fokker F.28 AFM by 
incorporating the information specified in Fokker Manual Change 
Notification--Operational Documentation (MCNO) MCNO-

[[Page 8183]]

F100-057, dated December 17, 2010, into the Abnormal Procedures--
Hydraulics section of the AFM.

    Note 1 to paragraph (g): The actions required by paragraph (g) 
of this AD may be done by inserting a copy of MCNO Fokker MCNO-F100-
057, dated December 17, 2010, into the Abnormal Procedures--
Hydraulics section of the Fokker F.28 AFM. When MCNO Fokker MCNO-
F100-057, dated December 17, 2010, has been included in the general 
revisions of the AFM, the general revisions may be inserted in the 
AFM, provided the relevant information in the general revision is 
identical to that in MCNO Fokker MCNO-F100-057, dated December 17, 
2010, and that MCNO may be removed.

(h) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. In accordance with 14 CFR 
39.19, send your request to your principal inspector or local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Branch, send it to ATTN: Tom 
Rodriguez, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
Washington 98057-3356; telephone (425) 227-1137; fax (425) 227-1149. 
Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
local flight standards district office/certificate holding 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.

(i) Related Information

    Refer to MCAI European Aviation Safety Agency (EASA) 
Airworthiness Directive 2011-0051, dated March 22, 2011; and MCNO 
Fokker MCNO-F100-057, dated December 17, 2010; for related 
information.

    Issued in Renton, Washington on February 7, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-3387 Filed 2-13-12; 8:45 am]
BILLING CODE 4910-13-P
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