Airworthiness Directives; Fokker Services B.V. Airplanes, 8328-8331 [2018-03430]
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Federal Register / Vol. 83, No. 39 / Tuesday, February 27, 2018 / Rules and Regulations
(b) Affected ADs
This AD affects AD 2012–18–13 R1,
Amendment 39–17429 (78 FR 27020, May 9,
2013) (‘‘AD 2012–18–13 R1’’).
(c) Applicability
(1) This AD applies to all The Boeing
Company Model 737–100, –200, –200C,
–300, –400, and –500 series airplanes,
certificated in any category.
(2) Installation of Supplemental Type
Certificate (STC) ST01219SE (https://rgl.faa.
gov/Regulatory_and_Guidance_Library/
rgstc.nsf/0/EBD1CEC7B301293E86257CB30
045557A?OpenDocument&Highlight=
st01219se) does not affect the ability to
accomplish the actions required by this AD.
Therefore, for airplanes on which STC
ST01219SE is installed, a ‘‘change in
product’’ alternative method of compliance
(AMOC) approval request is not necessary to
comply with the requirements of 14 CFR
39.17.
(d) Subject
Air Transport Association (ATA) of
America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by an evaluation by
the design approval holder (DAH) indicating
that the gore web lap splices of the aft
pressure bulkhead are subject to widespread
fatigue damage (WFD). We are issuing this
AD to detect and correct cracking in the gore
webs, gore web lap splices, and repair webs
of the aft pressure bulkhead, which could
result in possible rapid decompression and
loss of structural integrity.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions for Group 1 Airplanes
For airplanes identified as Group 1 in
Boeing Alert Service Bulletin 737–53A1355,
dated March 10, 2017: Within 120 days after
the effective date of this AD, inspect the
airplane, using a method approved in
accordance with the procedures specified in
paragraph (k) of this AD.
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(h) Actions Required for Compliance
Except as required by paragraph (j) of this
AD: For airplanes identified as Group 2 in
Boeing Alert Service Bulletin 737–53A1355,
dated March 10, 2017, at the applicable times
specified in paragraph 1.E., ‘‘Compliance,’’ of
Boeing Alert Service Bulletin 737–53A1355,
dated March 10, 2017, do all applicable
actions identified as required for compliance
(‘‘RC’’) in, and in accordance with, the
Accomplishment Instructions of Boeing Alert
Service Bulletin 737–53A1355, dated March
10, 2017.
(i) Termination of Requirements of
Paragraph (o) of AD 2012–18–13 R1
Accomplishment of the initial inspection
for Zone 1, defined in Boeing Alert Service
Bulletin 737–53A1355, dated March 10,
2017, and required by paragraph (h) of this
AD terminates the requirements of paragraph
(o) of AD 2012–18–13 R1.
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(j) Exceptions to Service Information
Specifications
(1) For purposes of determining
compliance with the requirements of this AD:
Where Boeing Alert Service Bulletin 737–
53A1355, dated March 10, 2017, uses the
phrase ‘‘the original issue date of this service
bulletin,’’ this AD requires using ‘‘the
effective date of this AD.’’
(2) Although Boeing Alert Service Bulletin
737–53A1355, dated March 10, 2017,
specifies to contact Boeing for repair
instructions, and specifies that action as
‘‘RC’’ (Required for Compliance), this AD
requires repair before further flight using a
method approved in accordance with the
procedures specified in paragraph (k) of this
AD.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Los Angeles ACO Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or local Flight Standards
District Office, as appropriate. If sending
information directly to the manager of the
certification office, send it to the attention of
the person identified in paragraph (l) of this
AD. Information may be emailed to: 9-ANMLAACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by the Boeing
Commercial Airplanes Organization
Designation Authorization (ODA) that has
been authorized by the Manager, Los Angeles
ACO Branch, to make those findings. To be
approved, the repair method, modification
deviation, or alteration deviation must meet
the certification basis of the airplane, and the
approval must specifically refer to this AD.
(4) Except as required by paragraph (j)(2)
of this AD: For service information that
contains steps that are labeled as Required
for Compliance (RC), the provisions of
paragraphs (k)(4)(i) and (k)(4)(ii) of this AD
apply.
(i) The steps labeled as RC, including
substeps under an RC step and any figures
identified in an RC step, must be done to
comply with the AD. If a step or substep is
labeled ‘‘RC Exempt,’’ then the RC
requirement is removed from that step or
substep. An AMOC is required for any
deviations to RC steps, including substeps
and identified figures.
(ii) Steps not labeled as RC may be
deviated from using accepted methods in
accordance with the operator’s maintenance
or inspection program without obtaining
approval of an AMOC, provided the RC steps,
including substeps and identified figures, can
still be done as specified, and the airplane
can be put back in an airworthy condition.
(l) Related Information
For more information about this AD,
contact George Garrido, Aerospace Engineer,
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Airframe Section, FAA, Los Angeles ACO
Branch, 3960 Paramount Boulevard,
Lakewood, CA 90712–4137; phone: 562–627–
5232; fax: 562–627–5210; email:
george.garrido@faa.gov.
(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 the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 737–
53A1355, dated March 10, 2017.
(ii) Reserved.
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd.,
MC 110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet https://
www.myboeingfleet.com.
(4) 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.
(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: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on February
14, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2018–03600 Filed 2–26–18; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2016–9435; Product
Identifier 2016–NM–108–AD; Amendment
39–18830; AD 2017–06–06]
RIN 2120–AA64
Airworthiness Directives; Fokker
Services B.V. Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are superseding
Airworthiness Directive (AD) 2012–22–
15, which applied to all Fokker Services
B.V. Model F28 Mark 0070 and Mark
0100 airplanes. AD 2012–22–15
required revising the maintenance
program to incorporate the limitations,
SUMMARY:
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tasks, thresholds, and intervals specified
in certain revised Fokker maintenance
review board (MRB) documents. This
new AD requires revising the
maintenance or inspection program, as
applicable, to incorporate new
maintenance requirements and
airworthiness limitations. This AD was
prompted by new and more restrictive
airworthiness limitations. We are
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective April 3,
2018.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of April 3, 2018.
The Director of the Federal Register
approved the incorporation by reference
of a certain other publication listed in
this AD as of December 20, 2012 (77 FR
68063, November 15, 2012).
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: technicalservices@
fokker.com; internet https://
www.myfokkerfleet.com. You may view
this referenced service information at
the FAA, Transport Standards Branch,
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
https://www.regulations.gov by searching
for and locating Docket No. FAA–2016–
9435.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
9435; 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 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 Section, Transport
Standards Branch, FAA, 1601 Lind
Avenue SW, Renton, WA 98057–3356;
telephone 425–227–1137; fax 425–227–
1149.
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SUPPLEMENTARY INFORMATION:
Discussion
We issued a supplemental notice of
proposed rulemaking (SNPRM) to
amend 14 CFR part 39 to supersede AD
2012–22–15, Amendment 39–17252 (77
FR 68063, November 15, 2012) (‘‘AD
2012–22–15’’). AD 2012–22–15 applied
to all Fokker Services B.V. Model F28
Mark 0070 and Mark 0100 airplanes.
The SNPRM published in the Federal
Register on October 19, 2017 (82 FR
48671) (‘‘the SNPRM’’). We preceded
the SNPRM with a notice of proposed
rulemaking (NPRM) that published in
the Federal Register on December 16,
2016 (81 FR 91068) (‘‘the NPRM’’). The
NPRM was prompted by new and more
restrictive airworthiness limitations.
The NPRM proposed to revise the
maintenance or inspection program, as
applicable, to incorporate the new and
more restrictive airworthiness
limitations. The SNPRM proposed to
require revising the maintenance or
inspection program, as applicable, to
incorporate new and more restrictive
airworthiness limitations that were
issued since the NPRM was released.
We are issuing this AD to prevent
reduced structural integrity 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 Airworthiness
Directive AD 2017–0095, dated May 30,
2017 (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
Mark 0100 airplanes. The MCAI states:
Fokker Services Engineering Report SE–
623 contains the Airworthiness Limitation
Items (ALIs) and Safe Life Items (SLIs). This
report is Part 2 of the Airworthiness
Limitations Section (ALS Part 2) of the
Instructions for Continued Airworthiness,
referred to in Section 06, Appendix 1, of the
Fokker 70/100 Maintenance Review Board
document.
The complete ALS consists of:
Part 1—Report SE–473, Certification
Maintenance Requirements (CMRs)—ref.
EASA AD 2015–0027 [which 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 2016–0125 [which corresponds to
certain requirements in FAA AD 2012–22–
15], and
Part 3—Report SE–672, Fuel ALIs and
CDCCLs—ref. EASA AD 2015–0032 [which
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
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8329
accomplish these actions could result in an
unsafe condition.
EASA previously issued AD 2016–0125,
requiring the actions described in ALS Part
2, Report SE–623 at issue 15 and 16.
Since that AD was issued, Fokker Services
published issue 17 of Report SE–623,
containing new and/or more restrictive
maintenance tasks.
For the reasons described above, this
[EASA] AD retains the requirements of AD
2016–0125, which is superseded, and
requires implementation of the maintenance
actions as specified in ALS Part 2 of the
Instructions for Continued Airworthiness,
Fokker Services Engineering Report SE–623
at issue 17 (hereafter referred to as ‘‘ALS Part
2’’ in this [EASA] AD).
You may examine the MCAI in the
AD docket on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
9435.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the SNPRM or
on the determination of the cost to the
public.
Conclusion
We reviewed the available 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 SNPRM for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the SNPRM.
Related Service Information Under 1
CFR Part 51
Fokker Services B.V. has issued
Engineering Report SE–623, ‘‘Fokker 70/
100 ALI’s and SLI’s,’’ Issue 17, issued
April 26, 2017. The service information
describes new and more restrictive
airworthiness limitations. 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.
Costs of Compliance
We estimate that this AD affects 15
airplanes of U.S. registry.
The actions required by AD 2012–22–
15, and retained in this AD, take about
1 work-hour per product, at an average
labor rate of $85 per work-hour. Based
on these figures, the estimated cost of
the actions that are required by AD
2012–22–15 is $85 per product.
We also estimate that it would take
about 1 work-hour per product to
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comply with the new basic
requirements of this AD. The average
labor rate is $85 per work-hour. Based
on these figures, we estimate the cost of
this AD on U.S. operators to be $1,275,
or $85 per product.
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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.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to transport category
airplanes to the Director of the System
Oversight Division.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in
Alaska; and
4. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
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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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing Airworthiness Directive 2012–
22–15, Amendment 39–17252 (77 FR
68063, November 15, 2012), and adding
the following new AD.
■
2017–06–06 Fokker Services B.V:
Amendment 39–18830; Docket No.
FAA–2016–9435; Product Identifier
2016–NM–108–AD.
(a) Effective Date
This AD is effective April 3, 2018.
(b) Affected ADs
(1) This AD replaces AD 2012–22–15,
Amendment 39–17252 (77 FR 68063,
November 15, 2012) (‘‘AD 2012–22–15’’).
(2) This AD affects AD 2012–12–07,
Amendment 39–17087 (77 FR 37788, June
25, 2012) (‘‘AD 2012–12–07’’).
(3) This AD affects AD 2008–06–20 R1,
Amendment 39–16089 (74 FR 61018,
November 23, 2009) (‘‘AD 2008–06–20 R1’’).
(c) Applicability
This AD applies to Fokker Services B.V.
Model F28 Mark 0070 and Mark 0100
airplanes, certificated in any category, all
serial numbers.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time Limits/Maintenance
Checks.
(e) Reason
This AD was prompted by a revision of an
airworthiness limitations items (ALI)
document, which introduces new and more
restrictive maintenance requirements and
airworthiness limitations. We are issuing this
AD to prevent reduced structural integrity of
the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Retained Maintenance Program Revision,
with Revised Compliance Language
This paragraph restates the requirements of
paragraph (i) of AD 2012–22–15, with revised
compliance language. Within 3 months after
December 20, 2012 (the effective date of AD
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2012–22–15), revise the maintenance
program to incorporate the airworthiness
limitations specified in Fokker Report SE–
623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
8, released March 17, 2011. For all tasks and
retirement lives identified in Fokker Report
SE–623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
8, released March 17, 2011, the initial
compliance times start from the later of the
times specified in paragraphs (g)(1) and (g)(2)
of this AD, and the repetitive inspections
must be accomplished thereafter at the
applicable interval specified in Fokker
Report SE–623, ‘‘Fokker 70/100
Airworthiness Limitation Items and Safe Life
Items,’’ Issue 8, released March 17, 2011.
Doing the revision required by paragraph (k)
of this AD terminates the requirements of this
paragraph.
(1) Within 3 months after December 20,
2012 (the effective date of AD 2012–22–15).
(2) At the time specified in Fokker Report
SE–623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
8, released March 17, 2011.
(h) Retained Corrective Actions, With
Specific Delegation Approval Language
This paragraph restates the requirements of
paragraph (j) of AD 2012–22–15, with
specific delegation approval language. If any
discrepancy, as defined in Fokker Report SE–
623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
8, released March 17, 2011, is found during
accomplishment of any task specified in
Fokker Report SE–623, ‘‘Fokker 70/100
Airworthiness Limitation Items and Safe Life
Items,’’ Issue 8, released March 17, 2011:
Within the applicable compliance time
specified in Fokker Report SE–623, ‘‘Fokker
70/100 Airworthiness Limitation Items and
Safe Life Items,’’ Issue 8, released March 17,
2011, accomplish the applicable corrective
actions in accordance with Fokker Report
SE–623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
8, released March 17, 2011, except as
required by paragraphs (h)(1) and (h)(2) of
this AD.
(1) If no compliance time is identified in
Fokker Report SE–623, ‘‘Fokker 70/100
Airworthiness Limitation Items and Safe Life
Items,’’ Issue 8, released March 17, 2011,
accomplish the applicable corrective actions
before further flight.
(2) If any discrepancy is found and there
is no corrective action specified in Fokker
Report SE–623, ‘‘Fokker 70/100
Airworthiness Limitation Items and Safe Life
Items,’’ Issue 8, released March 17, 2011:
Before further flight, contact the Manager,
International Section, Transport Standards
Branch, FAA; or the European Aviation
Safety Agency (EASA); or Fokker B.V.
Services’ EASA Design Organization
Approval (DOA); for approved corrective
actions, and accomplish those actions before
further flight.
(i) Retained ‘‘No Alternative Actions or
Intervals,’’ With a New Exception
This paragraph restates the requirements of
paragraph (k) of AD 2012–22–15, with a new
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exception. Except as required by paragraph
(k) of this AD, after accomplishing the
revision 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 (m)(1) of this AD.
(j) Retained Method of Compliance With AD
2008–06–20 R1, With Revised Compliance
Language
This paragraph restates the terminating
action specified in paragraph (m) of AD
2012–22–15, with revised compliance
language. Accomplishing the actions
specified in paragraph (g) of this AD
terminates the requirements of paragraphs
(f)(1) through (f)(5) of AD 2008–06–20 R1.
(k) New Requirement of This AD:
Maintenance or Inspection Program
Revision
Within 30 days of the effective date of this
AD, revise the maintenance or inspection
program, as applicable, to incorporate the
airworthiness limitations specified in Fokker
Services B.V. Engineering Report SE–623,
‘‘Fokker 70/100 ALI’s and SLI’s,’’ Issue 17,
issued April 26, 2017. Accomplishing the
revision required by this paragraph
terminates the requirements of paragraph (g)
of this AD. Accomplishing the revision
required by this paragraph also terminates
the requirements of paragraph (g) of AD
2012–12–07.
(1) The initial compliance times for the
tasks specified in Fokker Services B.V.
Engineering Report SE–623, ‘‘Fokker 70/100
ALI’s and SLI’s,’’ Issue 17, issued April 26,
2017, are at the later of the applicable
compliance times specified in Fokker
Services B.V. Engineering Report SE–623,
‘‘Fokker 70/100 ALI’s and SLI’s,’’ Issue 17,
issued April 26, 2017, or within 30 days after
the effective date of this AD, whichever is
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 EASA; or Fokker B.V. Service’s EASA
DOA. If approved by the DOA, the approval
must include the DOA-authorized signature.
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(l) No Alternative Actions or Intervals
After the maintenance or inspection
program, as applicable, has been revised as
required by paragraph (k) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an AMOC in
accordance with the procedures specified in
paragraph (m)(1) of this AD.
(m) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal
inspector or local Flight Standards District
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Office, as appropriate. If sending information
directly to the International Section, send it
to the attention of the person identified in
paragraph (n)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: As of the
effective date of this AD, 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 EASA; or Fokker
B.V. Services’ EASA DOA. If approved by the
DOA, the approval must include the DOAauthorized signature.
(n) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive AD 2017–0095,
dated May 30, 2017, for related information.
This MCAI may be found in the AD docket
on the internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2016–9435.
(2) For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 1601 Lind Avenue SW,
Renton, WA 98057–3356; telephone 425–
227–1137; fax 425–227–1149.
(o) 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.
(3) The following service information was
approved for IBR on April 3, 2018.
(i) Fokker Services B.V. Engineering Report
SE–623, ‘‘Fokker 70/100 ALI’s and SLI’s,’’
Issue 17, issued April 26, 2017.
(ii) Reserved.
(4) The following service information was
approved for IBR on December 20, 2012 (77
FR 68063, November 15, 2012).
(i) Fokker Report SE–623, ‘‘Fokker 70/100
Airworthiness Limitation Items and Safe Life
Items,’’ Issue 8, released March 17, 2011.
(ii) Reserved.
(5) 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: technicalservices@
fokker.com; internet https://
www.myfokkerfleet.com.
(6) You may view this service information
at the FAA, Transport Standards Branch,
1601 Lind Avenue SW, Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
(7) You may view this service information
that is incorporated by reference at the
National Archives and Records
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
8331
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on February
9, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2018–03430 Filed 2–26–18; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 97
[Docket No. 31180; Amdt. No. 3788]
Standard Instrument Approach
Procedures, and Takeoff Minimums
and Obstacle Departure Procedures;
Miscellaneous Amendments
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This rule amends, suspends,
or removes Standard Instrument
Approach Procedures (SIAPs) and
associated Takeoff Minimums and
Obstacle Departure Procedures for
operations at certain airports. These
regulatory actions are needed because of
the adoption of new or revised criteria,
or because of changes occurring in the
National Airspace System, such as the
commissioning of new navigational
facilities, adding new obstacles, or
changing air traffic requirements. These
changes are designed to provide for the
safe and efficient use of the navigable
airspace and to promote safe flight
operations under instrument flight rules
at the affected airports.
DATES: This rule is effective February
27, 2018. The compliance date for each
SIAP, associated Takeoff Minimums,
and ODP is specified in the amendatory
provisions.
The incorporation by reference of
certain publications listed in the
regulations is approved by the Director
of the Federal Register as of February
27, 2018.
ADDRESSES: Availability of matter
incorporated by reference in the
amendment is as follows:
SUMMARY:
For Examination
1. U.S. Department of Transportation,
Docket Ops–M30, 1200 New Jersey
Avenue SE, West Bldg., Ground Floor,
Washington, DC 20590–0001;
E:\FR\FM\27FER1.SGM
27FER1
]]>Agencies
[Federal Register Volume 83, Number 39 (Tuesday, February 27, 2018)]
[Rules and Regulations]
[Pages 8328-8331]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-03430]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-9435; Product Identifier 2016-NM-108-AD; Amendment
39-18830; AD 2017-06-06]
RIN 2120-AA64
Airworthiness Directives; Fokker Services B.V. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding Airworthiness Directive (AD) 2012-22-15,
which applied to all Fokker Services B.V. Model F28 Mark 0070 and Mark
0100 airplanes. AD 2012-22-15 required revising the maintenance program
to incorporate the limitations,
[[Page 8329]]
tasks, thresholds, and intervals specified in certain revised Fokker
maintenance review board (MRB) documents. This new AD requires revising
the maintenance or inspection program, as applicable, to incorporate
new maintenance requirements and airworthiness limitations. This AD was
prompted by new and more restrictive airworthiness limitations. We are
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective April 3, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 3,
2018.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
December 20, 2012 (77 FR 68063, November 15, 2012).
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
https://www.myfokkerfleet.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 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
https://www.regulations.gov by searching for and locating Docket No.
FAA-2016-9435.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9435; 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 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 Section, Transport Standards Branch, FAA, 1601 Lind
Avenue SW, Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-
1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a supplemental notice of proposed rulemaking (SNPRM) to
amend 14 CFR part 39 to supersede AD 2012-22-15, Amendment 39-17252 (77
FR 68063, November 15, 2012) (``AD 2012-22-15''). AD 2012-22-15 applied
to all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100
airplanes. The SNPRM published in the Federal Register on October 19,
2017 (82 FR 48671) (``the SNPRM''). We preceded the SNPRM with a notice
of proposed rulemaking (NPRM) that published in the Federal Register on
December 16, 2016 (81 FR 91068) (``the NPRM''). The NPRM was prompted
by new and more restrictive airworthiness limitations. The NPRM
proposed to revise the maintenance or inspection program, as
applicable, to incorporate the new and more restrictive airworthiness
limitations. The SNPRM proposed to require revising the maintenance or
inspection program, as applicable, to incorporate new and more
restrictive airworthiness limitations that were issued since the NPRM
was released. We are issuing this AD to prevent reduced structural
integrity 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
Airworthiness Directive AD 2017-0095, dated May 30, 2017 (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 Mark 0100 airplanes. The MCAI states:
Fokker Services Engineering Report SE-623 contains the
Airworthiness Limitation Items (ALIs) and Safe Life Items (SLIs).
This report is Part 2 of the Airworthiness Limitations Section (ALS
Part 2) of the Instructions for Continued Airworthiness, referred to
in Section 06, Appendix 1, of the Fokker 70/100 Maintenance Review
Board document.
The complete ALS consists of:
Part 1--Report SE-473, Certification Maintenance Requirements
(CMRs)--ref. EASA AD 2015-0027 [which 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 2016-0125
[which corresponds to certain requirements in FAA AD 2012-22-15],
and
Part 3--Report SE-672, Fuel ALIs and CDCCLs--ref. EASA AD 2015-
0032 [which 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 AD 2016-0125, requiring the actions
described in ALS Part 2, Report SE-623 at issue 15 and 16.
Since that AD was issued, Fokker Services published issue 17 of
Report SE-623, containing new and/or more restrictive maintenance
tasks.
For the reasons described above, this [EASA] AD retains the
requirements of AD 2016-0125, which is superseded, and requires
implementation of the maintenance actions as specified in ALS Part 2
of the Instructions for Continued Airworthiness, Fokker Services
Engineering Report SE-623 at issue 17 (hereafter referred to as
``ALS Part 2'' in this [EASA] AD).
You may examine the MCAI in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9435.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the SNPRM or on the determination
of the cost to the public.
Conclusion
We reviewed the available 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
SNPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the SNPRM.
Related Service Information Under 1 CFR Part 51
Fokker Services B.V. has issued Engineering Report SE-623, ``Fokker
70/100 ALI's and SLI's,'' Issue 17, issued April 26, 2017. The service
information describes new and more restrictive airworthiness
limitations. 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.
Costs of Compliance
We estimate that this AD affects 15 airplanes of U.S. registry.
The actions required by AD 2012-22-15, and retained in this AD,
take about 1 work-hour per product, at an average labor rate of $85 per
work-hour. Based on these figures, the estimated cost of the actions
that are required by AD 2012-22-15 is $85 per product.
We also estimate that it would take about 1 work-hour per product
to
[[Page 8330]]
comply with the new basic requirements of this AD. The average labor
rate is $85 per work-hour. Based on these figures, we estimate the cost
of this AD on U.S. operators to be $1,275, or $85 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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes to
the Director of the System Oversight Division.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by removing Airworthiness Directive 2012-
22-15, Amendment 39-17252 (77 FR 68063, November 15, 2012), and adding
the following new AD.
2017-06-06 Fokker Services B.V: Amendment 39-18830; Docket No. FAA-
2016-9435; Product Identifier 2016-NM-108-AD.
(a) Effective Date
This AD is effective April 3, 2018.
(b) Affected ADs
(1) This AD replaces AD 2012-22-15, Amendment 39-17252 (77 FR
68063, November 15, 2012) (``AD 2012-22-15'').
(2) This AD affects AD 2012-12-07, Amendment 39-17087 (77 FR
37788, June 25, 2012) (``AD 2012-12-07'').
(3) This AD affects AD 2008-06-20 R1, Amendment 39-16089 (74 FR
61018, November 23, 2009) (``AD 2008-06-20 R1'').
(c) Applicability
This AD applies to Fokker Services B.V. Model F28 Mark 0070 and
Mark 0100 airplanes, certificated in any category, all serial
numbers.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Reason
This AD was prompted by a revision of an airworthiness
limitations items (ALI) document, which introduces new and more
restrictive maintenance requirements and airworthiness limitations.
We are issuing this AD to prevent reduced structural integrity of
the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Maintenance Program Revision, with Revised Compliance
Language
This paragraph restates the requirements of paragraph (i) of AD
2012-22-15, with revised compliance language. Within 3 months after
December 20, 2012 (the effective date of AD 2012-22-15), revise the
maintenance program to incorporate the airworthiness limitations
specified in Fokker Report SE-623, ``Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,'' Issue 8, released March 17,
2011. For all tasks and retirement lives identified in Fokker Report
SE-623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life
Items,'' Issue 8, released March 17, 2011, the initial compliance
times start from the later of the times specified in paragraphs
(g)(1) and (g)(2) of this AD, and the repetitive inspections must be
accomplished thereafter at the applicable interval specified in
Fokker Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items
and Safe Life Items,'' Issue 8, released March 17, 2011. Doing the
revision required by paragraph (k) of this AD terminates the
requirements of this paragraph.
(1) Within 3 months after December 20, 2012 (the effective date
of AD 2012-22-15).
(2) At the time specified in Fokker Report SE-623, ``Fokker 70/
100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8,
released March 17, 2011.
(h) Retained Corrective Actions, With Specific Delegation Approval
Language
This paragraph restates the requirements of paragraph (j) of AD
2012-22-15, with specific delegation approval language. If any
discrepancy, as defined in Fokker Report SE-623, ``Fokker 70/100
Airworthiness Limitation Items and Safe Life Items,'' Issue 8,
released March 17, 2011, is found during accomplishment of any task
specified in Fokker Report SE-623, ``Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,'' Issue 8, released March 17,
2011: Within the applicable compliance time specified in Fokker
Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items and
Safe Life Items,'' Issue 8, released March 17, 2011, accomplish the
applicable corrective actions in accordance with Fokker Report SE-
623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life
Items,'' Issue 8, released March 17, 2011, except as required by
paragraphs (h)(1) and (h)(2) of this AD.
(1) If no compliance time is identified in Fokker Report SE-623,
``Fokker 70/100 Airworthiness Limitation Items and Safe Life
Items,'' Issue 8, released March 17, 2011, accomplish the applicable
corrective actions before further flight.
(2) If any discrepancy is found and there is no corrective
action specified in Fokker Report SE-623, ``Fokker 70/100
Airworthiness Limitation Items and Safe Life Items,'' Issue 8,
released March 17, 2011: Before further flight, contact the Manager,
International Section, Transport Standards Branch, FAA; or the
European Aviation Safety Agency (EASA); or Fokker B.V. Services'
EASA Design Organization Approval (DOA); for approved corrective
actions, and accomplish those actions before further flight.
(i) Retained ``No Alternative Actions or Intervals,'' With a New
Exception
This paragraph restates the requirements of paragraph (k) of AD
2012-22-15, with a new
[[Page 8331]]
exception. Except as required by paragraph (k) of this AD, after
accomplishing the revision 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 (m)(1) of this AD.
(j) Retained Method of Compliance With AD 2008-06-20 R1, With Revised
Compliance Language
This paragraph restates the terminating action specified in
paragraph (m) of AD 2012-22-15, with revised compliance language.
Accomplishing the actions specified in paragraph (g) of this AD
terminates the requirements of paragraphs (f)(1) through (f)(5) of
AD 2008-06-20 R1.
(k) New Requirement of This AD: Maintenance or Inspection Program
Revision
Within 30 days of the effective date of this AD, revise the
maintenance or inspection program, as applicable, to incorporate the
airworthiness limitations specified in Fokker Services B.V.
Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue
17, issued April 26, 2017. Accomplishing the revision required by
this paragraph terminates the requirements of paragraph (g) of this
AD. Accomplishing the revision required by this paragraph also
terminates the requirements of paragraph (g) of AD 2012-12-07.
(1) The initial compliance times for the tasks specified in
Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/100
ALI's and SLI's,'' Issue 17, issued April 26, 2017, are at the later
of the applicable compliance times specified in Fokker Services B.V.
Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue
17, issued April 26, 2017, or within 30 days after the effective
date of this AD, whichever is 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 EASA; or Fokker B.V.
Service's EASA DOA. If approved by the DOA, the approval must
include the DOA-authorized signature.
(l) No Alternative Actions or Intervals
After the maintenance or inspection program, as applicable, has
been revised as required by paragraph (k) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions or intervals are approved as an AMOC in accordance with the
procedures specified in paragraph (m)(1) of this AD.
(m) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (n)(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: As of the effective date of
this AD, 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 EASA; or Fokker B.V. Services' EASA DOA. If approved
by the DOA, the approval must include the DOA-authorized signature.
(n) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive AD 2017-0095, dated May 30,
2017, for related information. This MCAI may be found in the AD
docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2016-9435.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone
425-227-1137; fax 425-227-1149.
(o) 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.
(3) The following service information was approved for IBR on
April 3, 2018.
(i) Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/
100 ALI's and SLI's,'' Issue 17, issued April 26, 2017.
(ii) Reserved.
(4) The following service information was approved for IBR on
December 20, 2012 (77 FR 68063, November 15, 2012).
(i) Fokker Report SE-623, ``Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,'' Issue 8, released March 17,
2011.
(ii) Reserved.
(5) 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
https://www.myfokkerfleet.com.
(6) You may view this service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information
on the availability of this material at the FAA, call 425-227-1221.
(7) 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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on February 9, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-03430 Filed 2-26-18; 8:45 am]
BILLING CODE 4910-13-P
