[Federal Register Volume 84, Number 27 (Friday, February 8, 2019)]
[Proposed Rules]
[Pages 2796-2799]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-01527]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-1071; Product Identifier 2018-NM-119-AD]
RIN 2120-AA64
Airworthiness Directives; Fokker Services B.V. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This
proposed AD was prompted by a determination
[[Page 2797]]
that new or more restrictive airworthiness limitations are necessary.
This proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. We are proposing this AD to
address the unsafe condition on these products.
DATES: We must receive comments on this proposed AD by March 25, 2019.
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 http://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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, 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 service information at the
FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA.
For information on the availability of this material at the FAA, call
206-231-3195.
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-2018-
1071; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this NPRM, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations (phone: 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:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2018-1071;
Product Identifier 2018-NM-119-AD'' at the beginning of your comments.
We specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this NPRM. We will consider all
comments received by the closing date and may amend this NPRM because
of those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this NPRM.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2018-0159, dated July 25, 2018 (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 F28 Mark 0070 and
0100 airplanes. The MCAI states:
Fokker Services Engineering Report SE-623 contains the
Airworthiness Limitation Items (ALIs) and Safe Life Items (SLIs) for
Fokker F28 Mark 0070 and Mark 0100 aeroplanes. This report is Part 2
of the Airworthiness Limitations Section of the Instructions for
Continued Airworthiness, referred to in Section 06, Appendix 1, of
the Fokker 70/100 Maintenance Review Board document.
The complete Airworthiness Limitations Section consists of:
Part 1--Report SE-473, Certification Maintenance Requirements
(CMRs)--ref. EASA AD 2015-0027 [corresponds to FAA AD 2016-11-22,
Amendment 39-18549 (81 FR 36438, June 7, 2016)],
Part 2--Report SE-623, ALIs and SLIs--ref. EASA AD 2017-0095
[corresponds to FAA AD 2017-06-06, Amendment 39-18830 (83 FR 8328,
February 27, 2018), (``AD 2017-06-06'')], and
Part 3--Report SE-672, Fuel ALIs and CDCCLs--ref. EASA AD 2015-
0032 [corresponds to FAA AD 2016-11-15, Amendment 39-18542 (81 FR
36447, June 7, 2016)].
The instructions contained in those reports have been identified
as mandatory actions for continued airworthiness. Failure to
accomplish these actions could result in an unsafe condition.
EASA previously issued [EASA] AD 2017-0095, requiring the
actions described in Report SE-623 at issue 17. Since that [EASA] AD
was issued, Fokker Services published issue 18 of Report SE-623,
containing new and/or more restrictive maintenance tasks.
For the reason described above, this [EASA] AD retains the
requirements of [EASA] AD 2017-0095, which is superseded, and
requires implementation of the maintenance actions as specified in
the ALS.
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-2018-
1071.
Relationship Between Proposed AD and Related ADs
This NPRM does not propose to supersede AD 2017-06-06. Rather, we
have determined that a stand-alone AD is more appropriate to address
the changes in the MCAI. This proposed AD would require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations.
Accomplishment of the proposed actions would then terminate all of the
requirements of AD 2017-06-06, and, as pursuant to AD 2017-06-06, would
continue to provide terminating action for paragraph (g) of AD 2012-12-
07, Amendment 39-17087 (77 FR 37788, June 25, 2012).
Related Service Information Under 1 CFR Part 51
Fokker Services B.V. has issued Fokker Engineering Report SE-623,
Fokker 70/100 Airworthiness Limitations Section (ALS), Part 2--
(Structure ALI's and Safe Life Items), Issue 18, dated June 14, 2018.
This service information describes airworthiness limitations for safe
life limits. 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.
FAA's Determination
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all the relevant information and determined the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.
Proposed Requirements of This NPRM
This proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations.
[[Page 2798]]
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revised maintenance
documents. In this situation, to comply with 14 CFR 91.403(c), the
operator must request approval for an alternative method of compliance
according to paragraph (j)(1) of this proposed AD.
Costs of Compliance
We estimate that this proposed AD affects 4 airplanes of U.S.
registry. We estimate the following costs to comply with this proposed
AD:
We have determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although we recognize that this number may vary from operator to
operator. In the past, we have estimated that this action takes 1 work-
hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), we have
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, we estimate the total cost per operator
to be $7,650 (90 work-hours x $85 per work-hour).
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 proposed 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 and associated appliances to the
Director of the System Oversight Division.
Regulatory Findings
We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
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.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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):
Fokker Services B.V.: Docket No. FAA-2018-1071; Product Identifier
2018-NM-119-AD.
(a) Comments Due Date
We must receive comments by March 25, 2019.
(b) Affected ADs
(1) This AD affects AD 2017-06-06, Amendment 39-18830 (83 FR
8328, February 27, 2018) (``AD 2017-06-06'').
(2) This AD affects AD 2012-12-07, Amendment 39-17087 (77 FR
37788, June 25, 2012) (``AD 2012-12-07'').
(c) Applicability
This AD applies to all Fokker Services B.V. Model F28 Mark 0070
and 0100 airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Reason
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. We are issuing
this AD to address reduced structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision
Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Fokker Engineering Report
SE-623, Fokker 70/100 Airworthiness Limitations Section Part 2--
(Structure ALI's and Safe Life Items), Issue 18, dated June 14,
2018.
(1) The initial compliance time for doing the tasks is at the
time specified in Fokker Engineering Report SE-623, Fokker 70/100
Airworthiness Limitations Section Part 2--(Structure ALI's and Safe
Life Items), Issue 18, dated June 14, 2018, or within 90 days after
the effective date of this AD, whichever occurs later.
(2) If any discrepancy is found, before further flight, repair
using a method approved by the Manager, International Section,
Transport Standards Branch, 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.
(h) No Alternative Actions or Intervals
After the maintenance or inspection program has been revised as
required by paragraph (g) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions or
intervals are approved as an alternative method of compliance (AMOC)
in accordance with the procedures specified in paragraph (j)(1) of
this AD.
(i) Terminating Action for Affected ADs
(1) Accomplishing the actions required by this AD terminates all
requirements of AD 2017-06-06.
(2) Accomplishing the actions required by this AD terminates the
requirements of paragraph (g) of AD 2012-12-07.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International
[[Page 2799]]
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 (k)(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.
(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
Section, Transport Standards Branch, FAA; or the EASA; or Fokker
Services B.V.'s EASA DOA. If approved by the DOA, the approval must
include the DOA-authorized signature.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0159, dated July 25, 2018, 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-2018-1071.
(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.
(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. You may view this service information at the
FAA, Transport Standards Branch, 2200 South 216th St., Des Moines,
WA. For information on the availability of this material at the FAA,
call 206-231-3195.
Issued in Des Moines, Washington, on January 10, 2019.
Jeffrey E. Duven,
Director, System Oversight Division, Aircraft Certification Service.
[FR Doc. 2019-01527 Filed 2-7-19; 8:45 am]
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