AD 2017-06-02

[Federal Register Volume 82, Number 54 (Wednesday, March 22, 2017)]
[Rules and Regulations]
[Pages 14602-14604]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2017-05161]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9302; Directorate Identifier 2016-NM-037-AD; 
Amendment 39-18826; AD 2017-06-02]
RIN 2120-AA64


Airworthiness Directives; Fokker Services B.V. Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for Fokker 
Services B.V. Model F28 Mark 0100 airplanes equipped with Rolls-Royce 
TAY 650-15 engines. This AD was prompted by reports of uncontained 
engine fan blade failures in Rolls-Royce TAY 650-15 engines. This AD 
requires installation of a caution placard in the flight compartment. 
We are issuing this AD to address the unsafe condition on these 
products.

DATES: This AD is effective April 26, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of April 26, 
2017.

ADDRESSES: For service information identified in this final rule, 
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: <a href="/cdn-cgi/l/email-protection#dbafbeb8b3b5b2b8bab7a8bea9adb2b8bea89bbdb4b0b0bea9f5b8b4b6"><span class="__cf_email__" data-cfemail="e59180868d8b8c868489968097938c868096a5838a8e8e8097cb868a88">[email&#160;protected]</span></a>; Internet 
<a href="http://www.myfokkerfleet.com">http://www.myfokkerfleet.com</a>. 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating 
Docket No. FAA-2016-9302.

Examining the AD Docket

    You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2016-
9302; 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 Office (telephone 
800-647-5527) is Docket Management Facility, U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: 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 to Fokker Services B.V. Model 
F28 Mark 0100 airplanes equipped with Rolls-Royce TAY 650-15 engines. 
The NPRM published in the Federal Register on November 1, 2016 (81 FR 
75759) (``the NPRM''). The NPRM was prompted by reports of uncontained 
engine fan blade failures in Rolls-Royce

[[Page 14603]]

TAY 650-15 engines. The fan blade failures occurred due to cracking of 
the fan blades, which was initiated under conditions of fan blade 
flutter during engine ground operation. The NPRM proposed to require 
installation of a caution placard in the flight compartment. We are 
issuing this AD to prevent certain engine thrust settings during ground 
operation, which can cause the fan blades to flutter and fail, 
resulting in damage to the airplane and possible injury to personnel.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive Airworthiness Directive 2013-0141, dated July 
12, 2013 (referred to after this as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for Fokker Services B.V. Model F28 Mark 0100 airplanes 
equipped with Rolls-Royce TAY 650-15 engines. The MCAI states:

    In the past, two F28 [Mark] 0100 aeroplanes with TAY [650-15] 
engines were involved in incidents as a result of uncontained engine 
fan blade failures. The fan blade failures occurred due to cracking 
of the fan blades, which was initiated under conditions of fan blade 
flutter. This fan blade flutter can occur during stabilized reverse 
thrust operation within a specific N1 RPM-range [revolutions per 
minute], known as Keep Out Zone (KOZ), which has been identified to 
be between 57% and 75% N1 RPM.
    To address this potential unsafe condition [which can result in 
damage to the airplane and possible injury to personnel], [Civil 
Aviation Authority--The Netherlands] CAA-NL issued [Dutch] AD (BLA) 
nr. 2002-119 for the aeroplane, while Luftfahrt-Bundesamt (LBA) 
Germany issued [German] AD (LTA) 2002-090 (later revised) for the 
Rolls-Royce Tay [650-15] engines. More recently, LBA [German] AD 
2002-090R1 was superseded by EASA AD 2013-0070.
    During stabilized forward thrust operation of an engine with the 
aeroplane stationary on the ground (e.g. maintenance engine ground 
running), the same type of fan blade flutter can occur. To ensure 
maintenance personnel awareness of the engine speed KOZ when 
performing engine ground running (in forward or reverse thrust), a 
caution placard must be introduced in the flight compartment.
    For the reasons described above, this [EASA] AD requires the 
installation of a caution placard in the flight compartment, between 
the Standby Engine Indicator (SEI) and the Multi-Functional Display 
Unit (MFDU).

    You may examine the MCAI in the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2016-
9302.

Comments

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

Conclusion

    We reviewed the 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:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    We reviewed Fokker Service Bulletin SBF100-11-027, dated April 18, 
2013. This service information describes procedures for the 
installation of a caution placard. 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.

Costs of Compliance

    We estimate that this AD affects 4 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
              Action                        Labor cost            Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
Installation of placard...........  1 work-hour x $85 per                 $46             $131             $524
                                     hour = $85.
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Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. ``Subtitle VII: Aviation 
Programs,'' describes in more detail the scope of the Agency's 
authority.
    We are issuing this rulemaking under the authority described in 
``Subtitle VII, Part A, Subpart III, Section 44701: General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We determined that this AD will not have federalism implications 
under Executive Order 13132. This AD will not have a substantial direct 
effect on the States, on the relationship between the national 
government and the States, or on the distribution of power and 
responsibilities among the various levels of government.
    For the reasons discussed above, I certify 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.

[[Page 14604]]

Sec.  39.13  [Amended]

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

2017-06-02 Fokker Services B.V.: Amendment 39-18826; Docket No. FAA-
2016-9302; Directorate Identifier 2016-NM-037-AD.

(a) Effective Date

    This AD is effective April 26, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Fokker Services B.V. Model F28 Mark 0100 
airplanes, certificated in any category, all serial numbers if 
equipped with Rolls-Royce TAY 650-15 engines.

(d) Subject

    Air Transport Association (ATA) of America Code 11, Placards and 
Markings.

(e) Reason

    This AD was prompted by reports of uncontained engine fan blade 
failures in Rolls-Royce TAY 650-15 engines. We are issuing this AD 
to prevent certain engine thrust settings during ground operation, 
which can cause the fan blades to flutter and fail, resulting in 
damage to the airplane and possible injury to personnel.

(f) Compliance

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

(g) Installation of Caution Placard

    Within 6 months after the effective date of this AD, install a 
caution placard in the flight compartment, between the standby 
engine indicator (SEI) and the multi-functional display unit (MFDU), 
in accordance with the Accomplishment Instructions of Fokker Service 
Bulletin SBF100-11-027, dated April 18, 2013.

    Note 1 to paragraph (g) of this AD: Additional information can 
be found in Fokker All Operators Message AOF100.177 #05, dated April 
18, 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: <a href="/cdn-cgi/l/email-protection#21180c606f6c0c1010170c606c6e620c7364707464727572614740400f464e57"><span class="__cf_email__" data-cfemail="caf3e78b8487e7fbfbfce78b878589e7988f9b9f8f999e998aacababe4ada5bc">[email&#160;protected]</span></a>. 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.
    (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

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2013-0141, dated July 12, 2013, for related 
information. This MCAI may be found in the AD docket on the Internet 
at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket 
No. FAA-2016-9302.
    (2) For more information about this AD, 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.
    (3) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (j)(3) and (j)(4) of this AD.

(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 SBF100-11-027, dated April 18, 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: <a href="/cdn-cgi/l/email-protection#cebaabada6a0a7adafa2bdabbcb8a7adabbd8ea8a1a5a5abbce0ada1a3"><span class="__cf_email__" data-cfemail="61150402090f0802000d120413170802041221070e0a0a04134f020e0c">[email&#160;protected]</span></a>; Internet 
<a href="http://www.myfokkerfleet.com">http://www.myfokkerfleet.com</a>.
    (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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued in Renton, Washington, on March 7, 2017.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-05161 Filed 3-21-17; 8:45 am]
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