80_FR_35310 80 FR 35192 - Airworthiness Directives; Fokker Services B.V. Airplanes

80 FR 35192 - Airworthiness Directives; Fokker Services B.V. Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 118 (June 19, 2015)

Page Range35192-35195
FR Document2015-14994

We are adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This AD was prompted by a report of two cases of heavy (hard to move) aileron control caused by aileron cables stuck in a clump of ice in the wheel bay. This AD requires installing drain tubes on the center wing rear spar. We are issuing this AD to prevent accumulated water near or on the aileron control cables, which could freeze and result in reduced control of the airplane.

Federal Register, Volume 80 Issue 118 (Friday, June 19, 2015) 
[Federal Register Volume 80, Number 118 (Friday, June 19, 2015)]
[Rules and Regulations]
[Pages 35192-35195]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-14994]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0492; Directorate Identifier 2013-NM-134-AD; 
Amendment 39-18187; AD 2015-12-12]
RIN 2120-AA64


Airworthiness Directives; Fokker Services B.V. Airplanes

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

[[Page 35193]]


ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This AD 
was prompted by a report of two cases of heavy (hard to move) aileron 
control caused by aileron cables stuck in a clump of ice in the wheel 
bay. This AD requires installing drain tubes on the center wing rear 
spar. We are issuing this AD to prevent accumulated water near or on 
the aileron control cables, which could freeze and result in reduced 
control of the airplane.

DATES: This AD becomes effective July 24, 2015.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of July 24, 
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0492; 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.
    For service information identified in this AD, contact Fokker 
Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL 
Hoofddorp, the Netherlands; telephone: +31 (0)88-6280-350; fax: +31 
(0)88-6280-111; email: [email protected]; Internet http://www.myfokkerfleet.com. You may view this referenced service information 
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., 
Renton, WA. For information on the availability of this material at the 
FAA, call 425-227-1221. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0492.

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

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply Fokker Services B.V. Model 
F.28 Mark 0070 and 0100 airplanes. The NPRM published in the Federal 
Register on August 4, 2014 (79 FR 45137). The NPRM was prompted by a 
report of two cases of heavy (hard to move) aileron control caused by 
aileron cables stuck in a clump of ice in the wheel bay. The NPRM 
proposed to require installing drain tubes on the center wing rear 
spar. We are issuing this AD to prevent accumulated water near or on 
the aileron control cables, which could freeze and result in reduced 
control of the airplane.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA AD 
2013-0140, dated July 12, 2013 (referred to after this as the Mandatory 
Continuing Airworthiness Information, or ``the MCAI''), to correct an 
unsafe condition for all Fokker Services B.V. Model F.28 Mark 0070 and 
0100 airplanes. The MCAI states:

    Two cases have been reported of heavy aileron control caused by 
aileron cables stuck in a clump of ice in the wheel bay. 
Investigation results revealed that, in case of water accumulation 
on the top of the center wing torsion box inside the cabin (zones 
171 and 172), the water drains through the existing drain holes/gaps 
in the web plates on top of the center wing rear spar. The water 
could then accumulate in the area where the aileron control cables 
are situated. With the freezing temperatures normally encountered 
during flight, ice accretion could occur near or even on the aileron 
control cables.
    This condition, if not corrected, could result in reduced 
control of the aeroplane.
    For the reasons described above, this [EASA] AD requires the 
installation of drain tubes on the center wing rear spar.

You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0492-0002.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (79 FR 45137, August 4, 
2014) or on the determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (79 FR 45137, August 4, 2014) for correcting the unsafe condition; 
and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (79 FR 45137, August 4, 2014).

Related Service Information Under 1 CFR Part 51

    Fokker Services B.V. has issued Fokker Service Bulletin SBF100-51-
021, dated April 23, 2013, including the following attachments:
     Fokker Parts List Local SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
     Fokker Parts List Supply SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
     Fokker Parts List Local SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
     Fokker Parts List Supply SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
     Fokker Manual Change Notification MCNM F100-160, dated 
April 23, 2013.
    This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section of this 
AD.

Costs of Compliance

    We estimate that this AD affects 4 airplanes of U.S. registry.
    We also estimate that it will take about 8 work-hours per product 
to comply with the basic requirements of this AD. The average labor 
rate is $85 per work-hour. Required parts will cost about $1,380 per 
product. Based on these figures, we estimate the cost of this AD on 
U.S. operators to be $8,240, or $2,060 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

[[Page 35194]]

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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0492; 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 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.

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):

2015-12-12 Fokker Services B.V.: Amendment 39-18187. Docket No. FAA-
2014-0492; Directorate Identifier 2013-NM-134-AD.

(a) Effective Date

    This AD becomes effective July 24, 2015.

(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 51, Standard 
Practices/Structures.

(e) Reason

    This AD was prompted by a report of two cases of heavy 
(difficult to move) aileron control caused by aileron cables stuck 
in a clump of ice in the wheel bay. We are issuing this AD to 
prevent accumulated water near or on the aileron control cables, 
which could freeze and result in reduced control of the airplane.

(f) Compliance

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

(g) Modification

    Within 36 months after the effective date of this AD, install 
water drain tubes on the center wing rear spar, in accordance with 
the Accomplishment Instructions of Fokker Service Bulletin SBF100-
51-021, dated April 23, 2013, including the attachments identified 
in paragraphs (g)(1) through (g)(5) of this AD.
    (1) Fokker Parts List Local SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
    (2) Fokker Parts List Supply SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
    (3) Fokker Parts List Local SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
    (4) Fokker Parts List Supply SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
    (5) Fokker Manual Change Notification MCNM F100-160, dated April 
23, 2013.

(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, 
WA 98057-3356; telephone: 425-227-1137; fax: 425-227-1149. 
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. The AMOC approval letter must specifically reference this 
AD.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Branch, ANM-116, Transport Airplane Directorate, FAA; or the 
European Aviation Safety Agency (EASA); or Fokker Services B.V.'s 
EASA Design Organization Approval (DOA). If approved by the DOA, the 
approval must include the DOA-authorized signature.

(i) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI) 
EASA AD 2013-0140, dated July 12, 2013, for related information. 
This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0492-0002.

(j) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (i) Fokker Service Bulletin SBF100-51-021, dated April 23, 2013, 
including the attachments identified in paragraphs (j)(2)(i)(A) 
through (j)(2)(i)(E) of this AD.
    (A) Fokker Parts List Local SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
    (B) Fokker Parts List Supply SB10051021-XU-B, Revision A, 
Sequence 1, dated April 10, 2013.
    (C) Fokker Parts List Local SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
    (D) Fokker Parts List Supply SB10051021-XU-A, Revision B, 
Sequence 1, dated April 10, 2013.
    (E) Fokker Manual Change Notification MCNM F100-160, dated April 
23, 2013.
    (ii) Reserved.
    (3) For service information identified in this AD, contact 
Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 
EL Hoofddorp, the Netherlands; telephone: +31 (0)88-6280-350; fax: 
+31 (0)88-6280-111; email: [email protected]; Internet 
http://www.myfokkerfleet.com.
    (4) You may view this service information at the FAA, Transport 
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For 
information on the availability of this material at the FAA, call 
425-227-1221.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.


[[Page 35195]]


    Issued in Renton, Washington, on June 10, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-14994 Filed 6-18-15; 8:45 am]
 BILLING CODE 4910-13-P

35192 Federal Register / Vol. 80, No. 118 / Friday, June 19, 2015 / Rules and Regulations estimate the total cost of this AD to U.S. Authority: 49 U.S.C. 106(g), 40113, 44701. (h) Alternative Methods of Compliance operators to be $0. (AMOCs) § 39.13 [Amended] The Manager, Engine Certification Office, Authority for This Rulemaking FAA, may approve AMOCs for this AD. Use Title 49 of the United States Code ■ 2. The FAA amends § 39.13 by adding the procedures found in 14 CFR 39.19 to specifies the FAA’s authority to issue the following new airworthiness make your request. You may email your rules on aviation safety. Subtitle I, directive (AD): request to: ANE-AD-AMOC@faa.gov. section 106, describes the authority of 2015–12–10 Pratt & Whitney Division: (i) Related Information the FAA Administrator. ‘‘Subtitle VII: Amendment 39–18185; Docket No. FAA–2015–0266; Directorate Identifier For more information about this AD, Aviation Programs’’ describes in more contact Wego Wang, Aerospace Engineer, detail the scope of the Agency’s 2015–NE–03–AD. Engine Certification Office, FAA, Engine & authority. (a) Effective Date Propeller Directorate, 12 New England We are issuing this rulemaking under This AD is effective July 6, 2015. Executive Park, Burlington, MA 01803; the authority described in Subtitle VII, phone: 781–238–7134; fax: 781–238–7199; Part A, Subpart III, Section 44701: (b) Affected ADs email: wego.wang@faa.gov. ‘‘General requirements.’’ Under that None. (j) Material Incorporated by Reference section, Congress charges the FAA with (c) Applicability (1) The Director of the Federal Register promoting safe flight of civil aircraft in approved the incorporation by reference This AD applies to all Pratt & Whitney air commerce by prescribing regulations Division (PW) PW6122A and PW6124A (IBR) of the service information listed in this for practices, methods, and procedures turbofan engines with high-pressure paragraph under 5 U.S.C. 552(a) and 1 CFR the Administrator finds necessary for compressor (HPC) 7th stage integrally bladed part 51. safety in air commerce. This regulation (IB) rotor, part number (P/N) 5495637, (2) You must use this service information is within the scope of that authority installed. as applicable to do the actions required by this AD, unless the AD specifies otherwise. because it addresses an unsafe condition (d) Unsafe Condition (i) Pratt & Whitney Division (PW) that is likely to exist or develop on Engineering Authorization No. 15MM008, products identified in this rulemaking This AD was prompted by reports of crack finds in the HPC 7th stage IB rotor. We are Revision A, dated March 24, 2015. action. issuing this AD to prevent HPC 7th stage IB (ii) PW Service Bulletin No. PW6ENG 72– rotor fractures, which could lead to 46, dated March 5, 2015. Regulatory Findings uncontained engine failure and damage to (3) For PW service information identified This AD will not have federalism the airplane. in this AD, contact Pratt & Whitney, 400 implications under Executive Order Main St., East Hartford, CT 06108; phone: 13132. This AD will not have a (e) Compliance 860–565–8770; fax: 860–565–4503. substantial direct effect on the States, on Comply with this AD within the (4) You may view this service information the relationship between the national compliance times specified, unless already at the FAA, Engine & Propeller Directorate, done. 12 New England Executive Park, Burlington, government and the States, or on the (1) Within 180 cycles after the effective MA. For information on the availability of distribution of power and this material at the FAA, call 781–238–7125. date of this AD or within 6,500 cycles responsibilities among the various accumulated on the HPC 7th stage IB rotor, (5) You may view this service information levels of government. whichever occurs later, borescope inspect the at the National Archives and Records For the reasons discussed above, I HPC 7th stage IB rotor for cracks. Use Administration (NARA). For information on certify that this AD: Appendix 1, paragraphs 5 and 6 of PW the availability of this material at NARA, call (1) Is not a ‘‘significant regulatory Engineering Authorization 15MM008, 202–741–6030, or go to: http:// action’’ under Executive Order 12866, Revision A, dated March 24, 2015, to do your www.archives.gov/federal-register/cfr/ibr- (2) Is not a ‘‘significant rule’’ under inspection. Thereafter, repeat the inspection locations.html. DOT Regulatory Policies and Procedures at every 1,000 cycles since last inspection. Issued in Burlington, Massachusetts, on (44 FR 11034, February 26, 1979), (2) If any crack is detected on the HPC 7th June 9, 2015. (3) Will not affect intrastate aviation stage IB rotor, then before further flight, Ann C. Mollica, in Alaska to the extent that it justifies replace the HPC 7th stage IB rotor with a part eligible for installation. Acting Directorate Manager, Engine & making a regulatory distinction, and Propeller Directorate, Aircraft Certification (4) Will not have a significant (f) Mandatory Terminating Action Service. economic impact, positive or negative, (1) At the next shop visit after the effective [FR Doc. 2015–14992 Filed 6–18–15; 8:45 am] on a substantial number of small entities date of this AD: BILLING CODE 4910–13–P under the criteria of the Regulatory (i) Replace the affected HPC 7th stage IB Flexibility Act. rotor, P/N 5495637, with a new, zero-time, HPC 7th stage IB rotor, P/N 5495637, and DEPARTMENT OF TRANSPORTATION List of Subjects in 14 CFR Part 39 (ii) Remove the HPC 7th stage IB rotor Air transportation, Aircraft, Aviation silver-plated nuts, P/N 4301682, and replace Federal Aviation Administration safety, Incorporation by reference, with non-silver-plated nuts. Use the Safety. Accomplishment Instructions of PW Service Bulletin No. PW6ENG 72–46, dated March 5, 14 CFR Part 39 Adoption of the Amendment 2015 to perform the removal and [Docket No. FAA–2014–0492; Directorate Accordingly, under the authority replacement. Identifier 2013–NM–134–AD; Amendment delegated to me by the Administrator, (g) Definition 39–18187; AD 2015–12–12] the FAA amends 14 CFR part 39 as For the purposes of this AD an ‘‘engine RIN 2120–AA64 rmajette on DSK2TPTVN1PROD with RULES follows: shop visit’’ is the induction of an engine into the shop for maintenance involving the Airworthiness Directives; Fokker PART 39—AIRWORTHINESS separation of pairs of major mating engine Services B.V. Airplanes DIRECTIVES flanges. The separation of engine flanges solely for the purposes of transportation AGENCY: Federal Aviation ■ 1. The authority citation for part 39 without subsequent engine maintenance, is Administration (FAA), Department of continues to read as follows: not an engine shop visit. Transportation (DOT). VerDate Sep<11>2014 15:11 Jun 18, 2015 Jkt 235001 PO 00000 Frm 00016 Fmt 4700 Sfmt 4700 E:\FR\FM\19JNR1.SGM 19JNR1

Federal Register / Vol. 80, No. 118 / Friday, June 19, 2015 / Rules and Regulations 35193 ACTION: Final rule. report of two cases of heavy (hard to Related Service Information Under 1 move) aileron control caused by aileron CFR Part 51 SUMMARY: We are adopting a new cables stuck in a clump of ice in the airworthiness directive (AD) for all Fokker Services B.V. has issued wheel bay. The NPRM proposed to Fokker Service Bulletin SBF100–51– Fokker Services B.V. Model F.28 Mark require installing drain tubes on the 0070 and 0100 airplanes. This AD was 021, dated April 23, 2013, including the center wing rear spar. We are issuing following attachments: prompted by a report of two cases of this AD to prevent accumulated water heavy (hard to move) aileron control • Fokker Parts List Local near or on the aileron control cables, SB10051021–XU–B, Revision A, caused by aileron cables stuck in a which could freeze and result in clump of ice in the wheel bay. This AD Sequence 1, dated April 10, 2013. reduced control of the airplane. • Fokker Parts List Supply requires installing drain tubes on the The European Aviation Safety Agency SB10051021–XU–B, Revision A, center wing rear spar. We are issuing (EASA), which is the Technical Agent Sequence 1, dated April 10, 2013. this AD to prevent accumulated water • Fokker Parts List Local near or on the aileron control cables, for the Member States of the European Union, has issued EASA AD 2013–0140, SB10051021–XU–A, Revision B, which could freeze and result in Sequence 1, dated April 10, 2013. reduced control of the airplane. dated July 12, 2013 (referred to after this as the Mandatory Continuing • Fokker Parts List Supply DATES: This AD becomes effective July SB10051021–XU–A, Revision B, Airworthiness Information, or ‘‘the 24, 2015. MCAI’’), to correct an unsafe condition Sequence 1, dated April 10, 2013. The Director of the Federal Register for all Fokker Services B.V. Model F.28 • Fokker Manual Change Notification approved the incorporation by reference MCNM F100–160, dated April 23, 2013. Mark 0070 and 0100 airplanes. The of a certain publication listed in this AD This service information is reasonably MCAI states: as of July 24, 2015. available because the interested parties ADDRESSES: You may examine the AD Two cases have been reported of heavy have access to it through their normal aileron control caused by aileron cables stuck course of business or by the means docket on the Internet at http:// in a clump of ice in the wheel bay. www.regulations.gov/ Investigation results revealed that, in case of identified in the ADDRESSES section of #!docketDetail;D=FAA-2014-0492; or in water accumulation on the top of the center this AD. person at the Docket Management wing torsion box inside the cabin (zones 171 Costs of Compliance Facility, U.S. Department of and 172), the water drains through the Transportation, Docket Operations, M– existing drain holes/gaps in the web plates We estimate that this AD affects 4 30, West Building Ground Floor, Room on top of the center wing rear spar. The water airplanes of U.S. registry. W12–140, 1200 New Jersey Avenue SE., could then accumulate in the area where the We also estimate that it will take Washington, DC. aileron control cables are situated. With the about 8 work-hours per product to For service information identified in freezing temperatures normally encountered comply with the basic requirements of during flight, ice accretion could occur near this AD. The average labor rate is $85 this AD, contact Fokker Services B.V., or even on the aileron control cables. Technical Services Dept., P.O. Box per work-hour. Required parts will cost This condition, if not corrected, could 1357, 2130 EL Hoofddorp, the result in reduced control of the aeroplane. about $1,380 per product. Based on Netherlands; telephone: +31 (0)88– For the reasons described above, this these figures, we estimate the cost of 6280–350; fax: +31 (0)88–6280–111; [EASA] AD requires the installation of drain this AD on U.S. operators to be $8,240, email: technicalservices@fokker.com; tubes on the center wing rear spar. or $2,060 per product. Internet http://www.myfokkerfleet.com. Authority for This Rulemaking You may view this referenced service You may examine the MCAI in the AD information at the FAA, Transport docket on the Internet at http:// Title 49 of the United States Code Airplane Directorate, 1601 Lind Avenue www.regulations.gov/ specifies the FAA’s authority to issue SW., Renton, WA. For information on #!documentDetail;D=FAA-2014-0492- rules on aviation safety. Subtitle I, the availability of this material at the 0002. section 106, describes the authority of FAA, call 425–227–1221. It is also the FAA Administrator. ‘‘Subtitle VII: Comments available on the Internet at http:// Aviation Programs,’’ describes in more www.regulations.gov by searching for We gave the public the opportunity to detail the scope of the Agency’s and locating Docket No. FAA–2014– participate in developing this AD. We authority. received no comments on the NPRM (79 We are issuing this rulemaking under 0492. FR 45137, August 4, 2014) or on the the authority described in ‘‘Subtitle VII, FOR FURTHER INFORMATION CONTACT: Tom determination of the cost to the public. Part A, Subpart III, Section 44701: Rodriguez, Aerospace Engineer, General requirements.’’ Under that International Branch, ANM–116, Conclusion section, Congress charges the FAA with Transport Airplane Directorate, FAA, promoting safe flight of civil aircraft in We reviewed the relevant data and 1601 Lind Avenue SW., Renton, WA air commerce by prescribing regulations determined that air safety and the 98057–3356; telephone: 425–227–1137; for practices, methods, and procedures public interest require adopting this AD fax: 425–227–1149. the Administrator finds necessary for as proposed except for minor editorial SUPPLEMENTARY INFORMATION: changes. We have determined that these safety in air commerce. This regulation minor changes: is within the scope of that authority Discussion because it addresses an unsafe condition We issued a notice of proposed • Are consistent with the intent that that is likely to exist or develop on rulemaking (NPRM) to amend 14 CFR was proposed in the NPRM (79 FR rmajette on DSK2TPTVN1PROD with RULES products identified in this rulemaking part 39 by adding an AD that would 45137, August 4, 2014) for correcting action. apply Fokker Services B.V. Model F.28 the unsafe condition; and Mark 0070 and 0100 airplanes. The • Do not add any additional burden Regulatory Findings NPRM published in the Federal upon the public than was already We determined that this AD will not Register on August 4, 2014 (79 FR proposed in the NPRM (79 FR 45137, have federalism implications under 45137). The NPRM was prompted by a August 4, 2014). Executive Order 13132. This AD will VerDate Sep<11>2014 15:11 Jun 18, 2015 Jkt 235001 PO 00000 Frm 00017 Fmt 4700 Sfmt 4700 E:\FR\FM\19JNR1.SGM 19JNR1

35194 Federal Register / Vol. 80, No. 118 / Friday, June 19, 2015 / Rules and Regulations not have a substantial direct effect on (c) Applicability approval letter must specifically reference the States, on the relationship between This AD applies to Fokker Services B.V. this AD. the national government and the States, Model F.28 Mark 0070 and 0100 airplanes, (2) Contacting the Manufacturer: For any or on the distribution of power and certificated in any category, all serial requirement in this AD to obtain corrective responsibilities among the various numbers. actions from a manufacturer, the action must levels of government. be accomplished using a method approved (d) Subject For the reasons discussed above, I by the Manager, International Branch, ANM– Air Transport Association (ATA) of 116, Transport Airplane Directorate, FAA; or certify that this AD: America Code 51, Standard Practices/ the European Aviation Safety Agency 1. Is not a ‘‘significant regulatory Structures. (EASA); or Fokker Services B.V.’s EASA action’’ under Executive Order 12866; Design Organization Approval (DOA). If (e) Reason 2. Is not a ‘‘significant rule’’ under the approved by the DOA, the approval must DOT Regulatory Policies and Procedures This AD was prompted by a report of two cases of heavy (difficult to move) aileron include the DOA-authorized signature. (44 FR 11034, February 26, 1979); control caused by aileron cables stuck in a (i) Related Information 3. Will not affect intrastate aviation in clump of ice in the wheel bay. We are issuing Alaska; and this AD to prevent accumulated water near Refer to Mandatory Continuing 4. Will not have a significant or on the aileron control cables, which could Airworthiness Information (MCAI) EASA AD economic impact, positive or negative, freeze and result in reduced control of the 2013–0140, dated July 12, 2013, for related on a substantial number of small entities airplane. information. This MCAI may be found in the under the criteria of the Regulatory AD docket on the Internet at http:// (f) Compliance www.regulations.gov/ Flexibility Act. Comply with this AD within the #!documentDetail;D=FAA-2014-0492-0002. Examining the AD Docket compliance times specified, unless already done. (j) Material Incorporated by Reference You may examine the AD docket on (1) The Director of the Federal Register the Internet at http:// (g) Modification approved the incorporation by reference www.regulations.gov/ Within 36 months after the effective date (IBR) of the service information listed in this #!docketDetail;D=FAA-2014-0492; or in of this AD, install water drain tubes on the paragraph under 5 U.S.C. 552(a) and 1 CFR person at the Docket Management center wing rear spar, in accordance with the part 51. Facility between 9 a.m. and 5 p.m., Accomplishment Instructions of Fokker (2) You must use this service information Service Bulletin SBF100–51–021, dated April Monday through Friday, except Federal as applicable to do the actions required by 23, 2013, including the attachments holidays. The AD docket contains this identified in paragraphs (g)(1) through (g)(5) this AD, unless this AD specifies otherwise. AD, the regulatory evaluation, any of this AD. (i) Fokker Service Bulletin SBF100–51– comments received, and other (1) Fokker Parts List Local SB10051021– 021, dated April 23, 2013, including the information. The street address for the XU–B, Revision A, Sequence 1, dated April attachments identified in paragraphs Docket Operations office (telephone: 10, 2013. (j)(2)(i)(A) through (j)(2)(i)(E) of this AD. 800–647–5527) is in the ADDRESSES (2) Fokker Parts List Supply SB10051021– (A) Fokker Parts List Local SB10051021– section. XU–B, Revision A, Sequence 1, dated April XU–B, Revision A, Sequence 1, dated April 10, 2013. 10, 2013. List of Subjects in 14 CFR Part 39 (3) Fokker Parts List Local SB10051021– (B) Fokker Parts List Supply SB10051021– XU–A, Revision B, Sequence 1, dated April XU–B, Revision A, Sequence 1, dated April Air transportation, Aircraft, Aviation 10, 2013. safety, Incorporation by reference, 10, 2013. (4) Fokker Parts List Supply SB10051021– (C) Fokker Parts List Local SB10051021– Safety. XU–A, Revision B, Sequence 1, dated April XU–A, Revision B, Sequence 1, dated April Adoption of the Amendment 10, 2013. 10, 2013. (5) Fokker Manual Change Notification (D) Fokker Parts List Supply SB10051021– Accordingly, under the authority MCNM F100–160, dated April 23, 2013. XU–A, Revision B, Sequence 1, dated April delegated to me by the Administrator, (h) Other FAA AD Provisions 10, 2013. the FAA amends 14 CFR part 39 as (E) Fokker Manual Change Notification The following provisions also apply to this follows: MCNM F100–160, dated April 23, 2013. AD: (1) Alternative Methods of Compliance (ii) Reserved. PART 39—AIRWORTHINESS (3) For service information identified in (AMOCs): The Manager, International DIRECTIVES Branch, ANM–116, Transport Airplane this AD, contact Fokker Services B.V., Directorate, FAA, has the authority to Technical Services Dept., P.O. Box 1357, ■ 1. The authority citation for part 39 approve AMOCs for this AD, if requested 2130 EL Hoofddorp, the Netherlands; continues to read as follows: using the procedures found in 14 CFR 39.19. telephone: +31 (0)88–6280–350; fax: +31 Authority: 49 U.S.C. 106(g), 40113, 44701. In accordance with 14 CFR 39.19, send your (0)88–6280–111; email: request to your principal inspector or local technicalservices@fokker.com; Internet § 39.13 [Amended] Flight Standards District Office, as http://www.myfokkerfleet.com. appropriate. If sending information directly (4) You may view this service information ■ 2. The FAA amends § 39.13 by adding to the International Branch, send it to ATTN: the following new airworthiness at the FAA, Transport Airplane Directorate, Tom Rodriguez, Aerospace Engineer, 1601 Lind Avenue SW., Renton, WA. For directive (AD): International Branch, ANM–116, Transport information on the availability of this 2015–12–12 Fokker Services B.V.: Airplane Directorate, FAA, 1601 Lind material at the FAA, call 425–227–1221. Amendment 39–18187. Docket No. Avenue SW., Renton, WA 98057–3356; telephone: 425–227–1137; fax: 425–227– (5) You may view this service information FAA–2014–0492; Directorate Identifier rmajette on DSK2TPTVN1PROD with RULES 1149. Information may be emailed to: 9- that is incorporated by reference at the 2013–NM–134–AD. ANM-116-AMOC-REQUESTS@faa.gov. National Archives and Records (a) Effective Date Before using any approved AMOC, notify Administration (NARA). For information on This AD becomes effective July 24, 2015. your appropriate principal inspector, or the availability of this material at NARA, call lacking a principal inspector, the manager of 202–741–6030, or go to: http:// (b) Affected ADs the local flight standards district office/ www.archives.gov/federal-register/cfr/ibr- None. certificate holding district office. The AMOC locations.html. VerDate Sep<11>2014 15:11 Jun 18, 2015 Jkt 235001 PO 00000 Frm 00018 Fmt 4700 Sfmt 4700 E:\FR\FM\19JNR1.SGM 19JNR1

Federal Register / Vol. 80, No. 118 / Friday, June 19, 2015 / Rules and Regulations 35195 Issued in Renton, Washington, on June 10, DEPARTMENT OF COMMERCE Tuesday, July 22, 2014, make the 2015. following correction: Michael Kaszycki, Bureau of Industry and Security Supplement No. 4 to Part 744—Entity Acting Manager, Transport Airplane 15 CFR Part 744 List [Corrected] Directorate, Aircraft Certification Service. [FR Doc. 2015–14994 Filed 6–18–15; 8:45 am] [Docket No. 140429382–4382–01] On page 42458, in Supplement No. 4 BILLING CODE 4910–13–P to Part 744, in the table, beginning with RIN 0694–AG16 the row in which the entry in the first Addition of Certain Persons to the column reads ‘‘UKRAINE’’, the table Entity List should appear as follows: Correction In rule document 2014–17196, beginning on page 42452 in the issue of UKRAINE ......... * * * * * * Donetsk People’s Republic, Donetsk For all items subject to Presumption of denial ...... 79 FR [INSERT FR PAGE Region, Ukraine the EAR. (See § 744.11 NUMBER] 7/22/14. of the EAR). * * * * * * Feodosiya Enterprise, a.k.a., the fol- For all items subject to Presumption of denial ...... 79 FR [INSERT FR PAGE lowing four aliases: the EAR. (See § 744.11 NUMBER] 7/22/14. of the EAR). Feodosia Oil Products Supply Co.; and —Feodosiya Enterprise on Providing Oil Products; and —Feodosiyske Company for the Oil; and —Theodosiya Oil Terminal. Feodosiya, Geologicheskaya str. 2, Cri- mea 98107, Ukraine; and Feodosia, Str. Geological 2, Crimea 98107, Ukraine (See alternate ad- dresses under Crimea (Occupied)). * * * * * * Luhansk People’s Republic, a.k.a., the For all items subject to Presumption of denial ...... 79 FR [INSERT FR PAGE following two aliases: the EAR. (See § 744.11 NUMBER] 7/22/14. of the EAR). —Lugansk People’s Republic —People’s Republic of Luhansk. Luhansk Region, Ukraine. * * * * * * * * * * * * * [FR Doc. C1–2014–17196 Filed 6–18–15; 8:45 am] DEPARTMENT OF COMMERCE Atmospheric Administration (NOAA), BILLING CODE 1505–01–D Commerce. National Oceanic and Atmospheric ACTION: Final rule. Administration SUMMARY: NMFS issues regulations that 15 CFR Part 902 revise Federal regulations regarding sport fishing guide services for Pacific 50 CFR Part 300 halibut in International Pacific Halibut Commission Regulatory Areas 2C [Docket No. 140724618–5506–02] (Southeast Alaska) and 3A (Central Gulf of Alaska). The regulations remove the RIN 0648–BE41 requirement that a guided sport (charter) rmajette on DSK2TPTVN1PROD with RULES Pacific Halibut Fisheries; Revisions to vessel guide be on board the same vessel Charter Halibut Fisheries Management as a charter vessel angler to meet the in Alaska definition of providing sport fishing guide services. This final rule clarifies AGENCY: National Marine Fisheries that all sport fishing for halibut in Service (NMFS), National Oceanic and which anglers receive assistance from a VerDate Sep<11>2014 22:32 Jun 18, 2015 Jkt 235001 PO 00000 Frm 00019 Fmt 4700 Sfmt 4700 E:\FR\FM\19JNR1.SGM 19JNR1


Document Created: 2018-02-22 11:10:35
Document Modified: 2018-02-22 11:10:35
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionRules and Regulations
ActionFinal rule.
DatesThis AD becomes effective July 24, 2015.
ContactTom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-1137; fax: 425-227-1149.
FR Citation80 FR 35192 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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