Airworthiness Directives; Fokker Services B.V. Airplanes

[Federal Register Volume 81, Number 229 (Tuesday, November 29, 2016)]
[Rules and Regulations]
[Pages 85841-85843]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-28341]



[[Page 85841]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-6895; Directorate Identifier 2015-NM-068-AD; 
Amendment 39-18673; AD 2016-20-07]
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 certain 
Fokker Services B.V. Model F28 airplanes. This AD was prompted by 
reports indicating that the main landing gear (MLG) could not be 
extended and locked down during approach. This AD requires inspection 
of the restrictor check valve filter screens to detect any degraded or 
failed filter screens, and installation of serviceable parts. We are 
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective January 3, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of January 3, 
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 [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-2016-6895.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
6895; 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 certain Fokker Services 
B.V. Model F28 airplanes. The NPRM published in the Federal Register on 
June 1, 2016 (81 FR 34929) (``the NPRM''). The NPRM was prompted by 
reports indicating that the MLG could not be extended and locked down 
during approach. The NPRM proposed to require a detailed inspection of 
the restrictor check valve filter screens to detect any degraded or 
failed filter screens, and installation of serviceable parts. We are 
issuing this AD to detect and correct any degraded or failed filter 
screens. This condition, if not corrected, could prevent MLG extension 
and lock-down and result in an emergency landing with consequent injury 
to occupants and damage to the airplane.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2015-0077, dated May 6, 2015 (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 airplanes. The MCAI states:

    Two occurrences were reported concerning two different 
aeroplanes, where during approach, after selecting landing gear 
down, one of the main landing gears (MLG) could not be extended and 
locked down. In both cases, subsequent investigation revealed that 
the filter screen of the corresponding restrictor check valve 
(integrated in a hydraulic hose assembly) was broken, and debris 
inside the restrictor check valve was blocking the return flow from 
the affected MLG actuator. Additional inspection of the fleet of the 
operator involved revealed more damaged or failed filter screens.
    This condition, if not detected and corrected, could prevent MLG 
extension and lock-down, possibly resulting in an emergency landing 
with consequent damage to the aeroplane and injury to occupants.
    To address this unsafe condition, Fokker Services published 
SBF28-32-164 and SBF100-32-166 to provide instructions for removal 
of the affected hydraulic hoses (including the restrictor check 
valve) to be inspected in-shop, and for installation of serviceable 
parts. Fokker Services also published Component SB CSB-32-026 to 
provide those in-shop inspection instructions to detect any damaged 
filter screen.
    For the reasons described above, this [EASA] AD requires a 
onetime removal of the landing gear hydraulic hoses for the purpose 
of an in-shop inspection of the affected restrictor check valves 
filter screens and, depending on findings, re-installation, or 
replacement of the affected hose(s) with a serviceable part.
    This [EASA] AD is considered to be an interim action to detect 
any degraded or failed filter screens and remove them from service 
and to collect additional data; further [EASA] AD action may follow. 
More information on this subject can be found in Fokker Services All 
Operators Messages AOF28.041 and AOF100.189#02.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
6895.

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

    Fokker Services B.V. has issued the following service information, 
which describes procedures for the replacement of hydraulic hose 
assemblies. These service bulletins are distinct because they apply to 
different airplane models.
    <bullet> Fokker Service Bulletin SBF28-32-164, dated January 14, 
2015.
    <bullet> Fokker Service Bulletin SBF100-32-166, dated January 14, 
2015.
    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.

[[Page 85842]]

Costs of Compliance

    We estimate that this AD affects 8 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
----------------------------------------------------------------------------------------------------------------
Inspection............................  1 work-hour x $85 per             $3,100          $3,185         $25,480
                                         hour = $85.
Reporting.............................  1 work-hour x $85 per                  0              85             680
                                         hour = $85.
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Paperwork Reduction Act

    A federal agency may not conduct or sponsor, and a person is not 
required to respond to, nor shall a person be subject to penalty for 
failure to comply with a collection of information subject to the 
requirements of the Paperwork Reduction Act unless that collection of 
information displays a current valid OMB control number. The control 
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in 
the Costs of Compliance section of this document and includes time for 
reviewing instructions, as well as completing and reviewing the 
collection of information. Therefore, all reporting associated with 
this AD is mandatory. Comments concerning the accuracy of this burden 
and suggestions for reducing the burden should be directed to the FAA 
at 800 Independence Ave. SW., Washington, DC 20591, ATTN: Information 
Collection Clearance Officer, AES-200.

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.


Sec.  39.13   [Amended]

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

2016-20-07 Fokker Services B.V.: Amendment 39-18673; Docket No. FAA-
2016-6895; Directorate Identifier 2015-NM-068-AD.

(a) Effective Date

    This AD is effective January 3, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Fokker Services B.V. airplanes, certificated 
in any category, as identified in paragraphs (c)(1) and (c)(2) of 
this AD.
    (1) Model F28 Mark 0070 and Mark 0100 airplanes, all serial 
numbers (S/Ns).
    (2) Model F28 Mark 1000, 2000, 3000, and 4000 airplanes, S/Ns 
11003 through 11110 inclusive and S/N 11992, modified in service as 
specified in Fokker Service Bulletin SBF28-32-123; and S/Ns 11111 
through 11241 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 32, Landing 
Gear.

(e) Reason

    This AD was prompted by reports indicating that the main landing 
gear (MLG) could not be extended and locked down during approach. We 
are issuing this AD to detect and correct any degraded or failed 
filter screens. This condition, if not corrected, could prevent MLG 
extension and lock-down and result in an emergency landing with 
consequent injury to occupants and damage to the airplane.

(f) Compliance

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

(g) Inspection

    Within 18 months after the effective date of this AD, do a 
detailed inspection of the restrictor check valve filter screens to 
detect any degraded or failed filter screens including dents and 
missing wire, and install serviceable parts (hydraulic hose 
assemblies), in accordance with the Accomplishment Instructions of 
Fokker Service Bulletin SBF28-32-164, dated January 14, 2015 (for 
Model F28 Mark 1000, 2000, 3000, and 4000 airplanes); or SBF100-32-
166, dated January 14, 2015 (for Model F28 Mark 0070 and 0100 
airplanes); as applicable. Any affected hydraulic hose assembly must 
be replaced before further flight after the inspection.

(h) Serviceable Part

    For the purpose of this AD, a serviceable part is a part number 
(P/N) 97867-1 or P/N 97867-3 hydraulic hose assembly (including the 
restrictor check valve) that has not previously been installed on an 
airplane, or a P/N 97867-1 or P/N 97867-3 hydraulic hose assembly 
(including the restrictor check valve) that has passed an inspection 
as specified in Fokker Services Component Service Bulletin CSB-32-
026.

[[Page 85843]]

(i) Parts Installation Prohibition

    As of the effective date of this AD, no person may install a 
replacement P/N 97867-1 or P/N 97867-3 hydraulic hose assembly on an 
airplane, unless the hydraulic hose assembly is a serviceable part 
as defined in paragraph (h) of this AD.

(j) Reporting Requirements

    At the applicable time specified in paragraph (j)(1) or (j)(2) 
of this AD, submit a report of the results (including no findings) 
of the inspection required by paragraph (g) of this AD. Send the 
report to Fokker Services B.V., Technical Services, Service 
Engineering, P.O. Box 1357, 2130 EL Hoofddorp, The Netherlands, 
email [email protected]. The report must include the type 
of damage found and airplane flight cycles and also any no findings.
    (1) If the inspection was done on or after the effective date of 
this AD: Submit the report within 30 days after the inspection.
    (2) If the inspection was done before the effective date of this 
AD: Submit the report within 30 days after the effective date of 
this AD.

(k) 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.
    (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 B.V. Service's 
EASA Design Organization Approval (DOA). If approved by the DOA, the 
approval must include the DOA-authorized signature.
    (3) Reporting Requirements: A federal agency may not conduct or 
sponsor, and a person is not required to respond to, nor shall a 
person be subject to a penalty for failure to comply with a 
collection of information subject to the requirements of the 
Paperwork Reduction Act unless that collection of information 
displays a current valid OMB Control Number. The OMB Control Number 
for this information collection is 2120-0056. Public reporting for 
this collection of information is estimated to be approximately 5 
minutes per response, including the time for reviewing instructions, 
completing and reviewing the collection of information. All 
responses to this collection of information are mandatory. Comments 
concerning the accuracy of this burden and suggestions for reducing 
the burden should be directed to the FAA at: 800 Independence Ave. 
SW., Washington, DC 20591, Attn: Information Collection Clearance 
Officer, AES-200.

(l) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI) 
European Aviation Safety Agency (EASA) Airworthiness Directive 2015-
0077, dated May 6, 2015, for related information. This MCAI may be 
found in the AD docket on the Internet at http://www.regulations.gov 
by searching for and locating Docket No. FAA-2016-6895.

(m) 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 SBF28-32-164, dated January 14, 
2015.
    (ii) Fokker Service Bulletin SBF100-32-166, dated January 14, 
2015.
    (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.

    Issued in Renton, Washington, on September 15, 2016.
Suzanne Masterson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-28341 Filed 11-28-16; 8:45 am]
 BILLING CODE 4910-13-P

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