Airworthiness Directives; Fokker Services B.V. Airplanes, 14743-14745 [2018-06822]

Download as PDF Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations (c) Applicability This AD applies to General Electric (GE) CF6–80A, –80A1, –80A2, and –80A3 turbofan engines with low-pressure turbine (LPT) stage 3 nozzles, part numbers (P/Ns) 9290M52P05 and 9290M52P06, installed. (d) Subject Joint Aircraft System Component (JASC) Code 7250, Turbine Section. (e) Unsafe Condition This AD was prompted by high cycle fatigue (HCF) cracking of the LPT stage 3 nozzles resulting in LPT uncontainment. We are issuing this AD to prevent cracking of the LPT stage 3 nozzles. The unsafe condition, if not addressed, could result in LPT uncontainment, damage to the engine, and damage to the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 36 months or during the next engine shop visit after the effective date of this AD, whichever occurs later, replace LPT stage 3 nozzles, P/Ns 9290M52P05 and 9290M52P06, with a part eligible for installation. daltland on DSKBBV9HB2PROD with RULES (h) Definition (1) For the purpose of this AD, an engine shop visit is defined as the induction of an engine into the shop for maintenance involving the separation of any major mating engine flanges. The separation of engine flanges is not considered an engine shop visit for the following purposes: (i) Transportation of an engine not attached to an aircraft without subsequent engine maintenance. (ii) Removing the turbine rear frame (TRF) for repair of TRF cracking. (iii) Removing the top or bottom highpressure compressor (HPC) case for HPC airfoil maintenance. (iv) Removing only the accessory gearbox and/or transfer gearbox. (2) Reserved. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, ECO Branch, 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 manager of the ECO Branch, send it to the attention of the person identified in paragraph (j) of this AD. You may email your request to: ANE-AD-AMOC@faa.gov. (2) 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. (j) Related Information For more information about this AD, contact Herman Mak, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 14743 Burlington, MA 01803; phone: 781–238– 7147; fax: 781–238–7199; email: herman.mak@faa.gov. Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. (k) Material Incorporated by Reference None. Examining the AD Docket Issued in Burlington, Massachusetts, on March 29, 2018. Robert Ganley, Manager, Engine and Propeller Standards Branch, Aircraft Certification Service. [FR Doc. 2018–06738 Filed 4–5–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2018–0268; Product Identifier 2017–NM–096–AD; Amendment 39–19242; AD 2018–07–11] RIN 2120–AA64 Airworthiness Directives; Fokker Services B.V. Airplanes Discussion We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by interference between certain passenger service unit (PSU) panels, when in the deployed/open position, and the nearby emergency exit door cover. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective April 23, 2018. We must receive comments on this AD by May 21, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, 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, PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206–231–3226. FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. AGENCY: SUMMARY: You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0268; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone: 800–647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017–0113, dated June 28, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for certain Fokker Services B.V. Model F28 Mark 0100 airplanes. The MCAI states: A report was received of an occurrence involving interference between certain Passenger Service Unit (PSU) panels, Part Number (P/N) A546011–501 and P/N A546011–503, when in the deployed/open position, and the nearby emergency exit door cover. This condition, if not detected and corrected, could prevent a complete opening of the overwing emergency exit door, possibly obstructing the evacuation of occupants in case of an emergency landing. To address this potential unsafe condition, Fokker Services published Service Bulletin (SB) SBF100–25–131 (hereafter referred to as ‘the SB’ in this AD) to provide inspection instructions. For the reasons described above, this [EASA] AD requires a one-time inspection to verify that the overwing emergency exit doors can be fully operated with the PSUpanels in the deployed/opened position and, depending on findings, accomplishment of applicable corrective action(s). This [EASA] AD also requires the reporting of findings. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018–0268. E:\FR\FM\06APR1.SGM 06APR1 14744 Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations FAA’s Determination and Requirements of This 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. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of these same type designs. FAA’s Determination of the Effective Date Since there are currently no domestic operators of this product, we find good cause that notice and opportunity for prior public comment are unnecessary. In addition, for the reasons stated above, we find that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2018–0268; Product Identifier 2017–NM–096–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this 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 AD. Costs of Compliance Currently, there are no affected U.S.registered airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition, and doing the actions specified in those instructions. Based on the actions specified in the MCAI AD, we are providing the following cost estimates for an affected airplane that is placed on the U.S. Register in the future: ESTIMATED COSTS Action Labor cost Inspection ......................................... Reporting ......................................... 1 work-hour × $85 per hour = $85 ............................................................ 1 work-hour × $85 per hour = $85 ............................................................ We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. daltland on DSKBBV9HB2PROD with RULES 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 Cost per product Parts cost period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. 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 that this AD: 1. Is not a ‘‘significant regulatory action’’ under Executive Order 12866; 2. Is not a ‘‘significant rule’’ under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 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. $0 0 $85 85 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 adding the following new airworthiness directive (AD): ■ 2018–07–11 Fokker Services B.V.: Amendment 39–19242; Docket No. FAA–2018–0268; Product Identifier 2017–NM–096–AD. (a) Effective Date This AD becomes effective April 23, 2018. (b) Affected ADs None. List of Subjects in 14 CFR Part 39 (c) Applicability This AD applies to Fokker Services B.V. Model F28 Mark 0100 airplanes, certificated in any category, serial numbers 11359, 11361, 11367, 11397, 11404, 11446, 11456, 11460, 11468, 11483, 11490, 11499, 11502, 11515 and 11520. Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/furnishings. PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\06APR1.SGM 06APR1 Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations (e) Reason This AD was prompted by a report of interference between certain passenger service unit (PSU) panels, when in the deployed/open position, and the nearby emergency exit door cover. We are issuing this AD to detect and correct interference between certain PSU panels and the nearby emergency exit door cover, which could prevent a complete opening of the overwing emergency exit door, and possibly obstruct the evacuation of occupants in case of an emergency landing. DEPARTMENT OF TRANSPORTATION (f) Compliance Comply with this AD within the compliance times specified, unless already done. AGENCY: (g) Required Actions Within 30 days after the effective date of this AD, request instructions from the Manager, International Section, Transport Standards Branch, FAA, to address the unsafe condition specified in paragraph (e) of this AD; and accomplish the actions at the times specified in, and in accordance with, those instructions. Guidance can be found in Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) AD 2017–0113, dated June 28, 2017. SUMMARY: (h) Alternative Methods of Compliance (AMOCs) The Manager, International Section, Transport Standards Branch, 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 Section, send it to the attention of the person identified in paragraph (i)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOCREQUESTS@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. (i) Related Information (1) Refer to MCAI EASA AD 2017–0113, dated June 28, 2017, for related information. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018–0268. (2) For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206– 231–3226. daltland on DSKBBV9HB2PROD with RULES (j) Material Incorporated by Reference None. BILLING CODE 4910–13–P VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 14 CFR Part 71 [Docket No. FAA–2017–0953; Airspace Docket No. 17–AEA–15] Issued in College Park, Georgia, on March 29, 2018. Geoff Lelliott, Acting Manager, Operations Support Group, Eastern Service Center, Air Traffic Organization. [FR Doc. 2018–06997 Filed 4–5–18; 8:45 am] BILLING CODE 4910–13–P Amendment of Class E Airspace; Massena, NY DEPARTMENT OF THE TREASURY Federal Aviation Administration (FAA), DOT. Alcohol and Tobacco Tax and Trade Bureau ACTION: Final rule, withdrawal. This action withdraws the final rule published in the Federal Register on March 15, 2018. In that action, the FAA amended Class E surface airspace and Class E airspace extending upward from 700 feet above the surface at Massena, NY. The FAA has determined that withdrawal of the final rule is warranted since there has been a change in the date for the decommissioning of the Massena collocated VHF omnidirectional range tactical air navigation (VORTAC). DATES: Effective 0901 UTC, April 6, 2018. John Fornito, Operations Support Group, Eastern Service Center, Federal Aviation Administration, 1701 Columbia Avenue, College Park, Georgia 30337; telephone (404) 305–6364. FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: History The FAA published a final rule in the Federal Register for Docket No. FAA– 2017–0953 (83 FR 11407, March 15, 2018) amending Title 14 Code of Federal Regulations (14 CFR) part 71 amending Class E Airspace at Massena International-Richards Field Airport, Massena, NY. The FAA found that the Massena collocated VORTAC navigation aid will not be decommissioned at this time. As a result, the final rule is being withdrawn. Lists of Subjects in 14 CFR Part 71 Airspace, Incorporation by reference, Navigation (air). The Withdrawal Issued in Des Moines, Washington, on March 22, 2018. Michael Kaszicki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–06822 Filed 4–5–18; 8:45 am] Federal Aviation Administration 14745 In consideration of the foregoing, the final rule for Docket No. FAA–2017– 0953 (83 FR 11407, March 15, 2018), FR Doc. 2018–05045, is hereby withdrawn. ■ Authority: 49 U.S.C. 106(f), 106(g); 40103, 40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–1963 Comp., p. 389. PO 00000 Frm 00013 Fmt 4700 Sfmt 4700 27 CFR Part 9 [Docket No. TTB–2016–0007; T.D. TTB–150; Ref: Notice No. 161] RIN 1513–AC26 Establishment of the Cape May Peninsula Viticultural Area Alcohol and Tobacco Tax and Trade Bureau, Treasury. ACTION: Final rule; Treasury decision. AGENCY: The Alcohol and Tobacco Tax and Trade Bureau (TTB) establishes the approximately 126,635-acre ‘‘Cape May Peninsula’’ viticultural area in Cape May and Cumberland Counties, New Jersey. The viticultural area lies entirely within the established Outer Coastal Plain viticultural area. TTB designates viticultural areas to allow vintners to better describe the origin of their wines and to allow consumers to better identify wines they may purchase. DATES: This final rule is effective May 7, 2018. FOR FURTHER INFORMATION CONTACT: Kate M. Bresnahan, Regulations and Rulings Division, Alcohol and Tobacco Tax and Trade Bureau, 1310 G Street NW, Box 12, Washington, DC 20005; phone (202) 453–1039, ext. 151. SUPPLEMENTARY INFORMATION: SUMMARY: Background on Viticultural Areas TTB Authority Section 105(e) of the Federal Alcohol Administration Act (FAA Act), 27 U.S.C. 205(e), authorizes the Secretary of the Treasury to prescribe regulations for the labeling of wine, distilled spirits, and malt beverages. The FAA Act provides that these regulations should, among other things, prohibit consumer deception and the use of misleading statements on labels and ensure that labels provide the consumer with adequate information as to the identity and quality of the product. The Alcohol and Tobacco Tax and Trade Bureau (TTB) administers the FAA Act pursuant to section 1111(d) of the E:\FR\FM\06APR1.SGM 06APR1

Agencies

[Federal Register Volume 83, Number 67 (Friday, April 6, 2018)]
[Rules and Regulations]
[Pages 14743-14745]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-06822]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0268; Product Identifier 2017-NM-096-AD; Amendment 
39-19242; AD 2018-07-11]
RIN 2120-AA64


Airworthiness Directives; Fokker Services B.V. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD requires 
contacting the FAA to obtain instructions for addressing the unsafe 
condition on these products, and doing the actions specified in those 
instructions. This AD was prompted by interference between certain 
passenger service unit (PSU) panels, when in the deployed/open 
position, and the nearby emergency exit door cover. We are issuing this 
AD to address the unsafe condition on these products.

DATES: This AD becomes effective April 23, 2018.
    We must receive comments on this AD by May 21, 2018.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, 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.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0268; or in person at the Docket Operations office between 9 a.m. and 5 
p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this AD, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Operations office 
(telephone: 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 Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax: 206-231-3226.

SUPPLEMENTARY INFORMATION:

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA AD 
2017-0113, dated June 28, 2017 (referred to after this as the Mandatory 
Continuing Airworthiness Information, or ``the MCAI''), to correct an 
unsafe condition for certain Fokker Services B.V. Model F28 Mark 0100 
airplanes. The MCAI states:

    A report was received of an occurrence involving interference 
between certain Passenger Service Unit (PSU) panels, Part Number (P/
N) A546011-501 and P/N A546011-503, when in the deployed/open 
position, and the nearby emergency exit door cover.
    This condition, if not detected and corrected, could prevent a 
complete opening of the overwing emergency exit door, possibly 
obstructing the evacuation of occupants in case of an emergency 
landing.
    To address this potential unsafe condition, Fokker Services 
published Service Bulletin (SB) SBF100-25-131 (hereafter referred to 
as `the SB' in this AD) to provide inspection instructions.
    For the reasons described above, this [EASA] AD requires a one-
time inspection to verify that the overwing emergency exit doors can 
be fully operated with the PSU-panels in the deployed/opened 
position and, depending on findings, accomplishment of applicable 
corrective action(s). This [EASA] AD also requires the reporting of 
findings.

    You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0268.

[[Page 14744]]

FAA's Determination and Requirements of This 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. We are 
issuing this AD because we evaluated all pertinent information and 
determined the unsafe condition exists and is likely to exist or 
develop on other products of these same type designs.

FAA's Determination of the Effective Date

    Since there are currently no domestic operators of this product, we 
find good cause that notice and opportunity for prior public comment 
are unnecessary. In addition, for the reasons stated above, we find 
that good cause exists for making this amendment effective in less than 
30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety, and we did not precede it by notice and opportunity for public 
comment. We invite you to send any written relevant data, views, or 
arguments about this AD. Send your comments to an address listed under 
the ADDRESSES section. Include ``Docket No. FAA-2018-0268; Product 
Identifier 2017-NM-096-AD'' at the beginning of your comments. We 
specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this AD. We will consider all 
comments received by the closing date and may amend this 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 AD.

Costs of Compliance

    Currently, there are no affected U.S.-registered airplanes. This AD 
requires contacting the FAA to obtain instructions for addressing the 
unsafe condition, and doing the actions specified in those 
instructions. Based on the actions specified in the MCAI AD, we are 
providing the following cost estimates for an affected airplane that is 
placed on the U.S. Register in the future:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                   Action                                 Labor cost                Parts cost        product
----------------------------------------------------------------------------------------------------------------
Inspection.................................  1 work-hour x $85 per hour = $85...              $0             $85
Reporting..................................  1 work-hour x $85 per hour = $85...               0              85
----------------------------------------------------------------------------------------------------------------

    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this AD.

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.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes to 
the Director of the System Oversight Division.

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 that this AD:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    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.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2018-07-11 Fokker Services B.V.: Amendment 39-19242; Docket No. FAA-
2018-0268; Product Identifier 2017-NM-096-AD.

(a) Effective Date

    This AD becomes effective April 23, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Fokker Services B.V. Model F28 Mark 0100 
airplanes, certificated in any category, serial numbers 11359, 
11361, 11367, 11397, 11404, 11446, 11456, 11460, 11468, 11483, 
11490, 11499, 11502, 11515 and 11520.

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.

[[Page 14745]]

(e) Reason

    This AD was prompted by a report of interference between certain 
passenger service unit (PSU) panels, when in the deployed/open 
position, and the nearby emergency exit door cover. We are issuing 
this AD to detect and correct interference between certain PSU 
panels and the nearby emergency exit door cover, which could prevent 
a complete opening of the overwing emergency exit door, and possibly 
obstruct the evacuation of occupants in case of an emergency 
landing.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Required Actions

    Within 30 days after the effective date of this AD, request 
instructions from the Manager, International Section, Transport 
Standards Branch, FAA, to address the unsafe condition specified in 
paragraph (e) of this AD; and accomplish the actions at the times 
specified in, and in accordance with, those instructions. Guidance 
can be found in Mandatory Continuing Airworthiness Information 
(MCAI) European Aviation Safety Agency (EASA) AD 2017-0113, dated 
June 28, 2017.

(h) Alternative Methods of Compliance (AMOCs)

    The Manager, International Section, Transport Standards Branch, 
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 Section, send it to the 
attention of the person identified in paragraph (i)(2) of this AD. 
Information may be emailed to: [email protected]. 
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.

(i) Related Information

    (1) Refer to MCAI EASA AD 2017-0113, dated June 28, 2017, for 
related information. You may examine the MCAI on the internet at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2018-0268.
    (2) For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax: 206-231-3226.

(j) Material Incorporated by Reference

    None.

    Issued in Des Moines, Washington, on March 22, 2018.
Michael Kaszicki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-06822 Filed 4-5-18; 8:45 am]
 BILLING CODE 4910-13-P
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