Airworthiness Directives; Various Transport Airplanes, 55036-55041 [2019-22389]
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Federal Register / Vol. 84, No. 199 / Tuesday, October 15, 2019 / Rules and Regulations
provide interest credits is limited to the
extent that appropriations are available
to cover the cost of the assistance. The
Agency will notify the public of the
availability of assistance, changes in
application requirements, or changes in
the fee structure.
■ 4. Amend § 3565.5 by revising
paragraph (b) to read as follows:
§ 3565.5
Ranking and selection criteria.
*
*
*
*
*
(b) Priority projects. Priority will be
given to projects: In smaller rural
communities, in the neediest
communities having the highest
percentage of leveraging, having the
lowest interest rate, having the highest
ratio of 3–5-bedroom units to total units,
or on tribal lands. In addition, the
Agency may, at its sole discretion, setaside assistance for or rank projects that
meet important program goals.
Assistance will include both loan
guarantees and interest credits. Priority
projects must compete for set-aside
funds.
Subpart B—Guarantee Requirements
5. Amend § 3565.53 by revising
paragraph (c) to read as follows:
■
§ 3565.53
Guarantee fees.
9. Amend § 3565.302 by revising
paragraph (b) introductory text to read
as follows:
■
§ 3565.302
Allowable fees.
*
*
*
*
*
(b) Agency fees. The Agency will
charge one or more types of fees deemed
appropriate as reimbursement for
reasonable and necessary costs incurred
in connection with applications
received from lenders. Agency fees may
include, but are not limited to, the
following:
*
*
*
*
*
[FR Doc. 2019–22426 Filed 10–11–19; 8:45 am]
*
*
*
*
(c) Surcharge for guarantees on
construction advances. The Agency
may, at its sole discretion, charge an
additional fee on the portion of the loan
advanced during construction. If
applicable, this fee will be charged in
advance at the start of construction.
BILLING CODE 3410–XV–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0444; Product
Identifier 2019–NM–028–AD; Amendment
39–19756; AD 2019–20–03]
Subpart C—Lender Requirements
[Amended]
■
6. Amend § 3565.104 by removing the
last sentence.
RIN 2120–AA64
Subpart E—Loan Requirements
Airworthiness Directives; Various
Transport Airplanes
7. Section 3565.210 is revised to read
as follows:
■
§ 3565.210
Maximum interest rate.
The interest rate for a guaranteed loan
must not exceed the maximum
allowable rate specified by the Agency.
This interest rate must be fixed over the
term of the loan.
Subpart F—Property Requirements
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Subpart G—Processing Requirements
Bruce W. Lammers,
Administrator, Rural Housing Service.
*
§ 3565.104
modular or manufactured houses, or
multifamily structures. Manufactured
housing must meet Agency
requirements contained in 7 CFR part
1924, subpart A. The Agency will
guarantee proposals for new
construction or acquisition with
moderate or substantial rehabilitation of
at least $6,500 per dwelling unit. The
portion of guaranteed funds available
for acquisition with rehabilitation may
be limited.
8. Section 3565.252 is revised to read
as follows:
■
§ 3565.252
Housing types.
The property may include new
construction or rehabilitation of existing
structures. The units may be attached,
detached, semi-detached, row houses,
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Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for various
transport airplanes. This AD was
prompted by reports of smoke and
fumes in the flight deck. This AD
requires modification of certain
universal serial bus (USB) receptacles
located in the flight deck. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective November
19, 2019.
The Director of the Federal Register
approved the incorporation by reference
SUMMARY:
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of certain publications listed in this AD
as of November 15, 2019.
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 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.
It is also available on the internet at
https://www.regulations.gov by searching
for and locating Docket No. FAA–2019–
0444.
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–2019–
0444; 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 final rule,
the regulatory evaluation, any
comments received, and other
information. The address for Docket
Operations is 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: Dan
Rodina, Aerospace Engineer,
International Section, Transport
Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax 206–231–3225.
SUPPLEMENTARY INFORMATION:
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–
0259R1, dated February 7, 2019 (‘‘EASA
AD 2018–0259R1’’) (also referred to as
the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for the following airplanes on which
certain USB receptacles were installed
using certain Fokker service
information:
• Fokker Services B.V. Model F.27
Mark 050 airplanes.
• Fokker Services B.V. Model F28
Mark 3000 airplanes.
• Fokker Services B.V. Model F28
Mark 0070 and Mark 0100 airplanes.
• Airbus SAS Model A318–111
airplanes.
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• Airbus SAS Model A319–111, –112,
–114, –115, and –132 airplanes.
• Airbus SAS Model A320–211, –212,
–214, –231, –232, and –251N airplanes.
• Airbus SAS Model A321–211, –231,
–232, –251N and –253N airplanes.
• Airbus SAS Model A330–202, –223,
–243, –322 and –343 airplanes.
• Airbus SAS Model A340–312 and
–313 airplanes.
• ATR—GIE Avions de Transport
Re´gional Model ATR42–500 airplanes.
• ATR—GIE Avions de Transport
Re´gional Model ATR72–212 and –212A
airplanes.
• The Boeing Company Model 737–
300, –400, –500, –700, –800 and –900ER
series airplanes.
• The Boeing Company Model 757–
200 series airplanes.
• The Boeing Company Model 767–
200 and –300 series airplanes.
• The Boeing Company Model 777–
200LR series airplanes.
• Bombardier, Inc., Model CL–600–
2B16 (601–3A, 601–3R, and 604
Variants) airplanes.
• Bombardier, Inc., Model CL–600–
2C10 (Regional Jet Series 700, 701 &
702) airplanes.
• Bombardier, Inc., Model DHC–8–
202, –311, –315 and –402 airplanes.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to various transport airplanes.
The NPRM published in the Federal
Register on June 24, 2019 (84 FR 29414).
The NPRM was prompted by reports of
smoke and fumes in the flight deck due
to overheating of an Electronic Flight
Bag (EFB) USB receptacle. The NPRM
proposed to require modification of
certain USB receptacles located in the
flight deck.
The FAA is issuing this AD to address
smoke and fumes in the flight deck,
which could result in excessive
flightcrew workload and injury to flight
deck occupants. See the MCAI for
additional background information.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The following presents
the comments received on the NPRM
and the FAA’s response to each
comment.
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Support for the NPRM
The Air Line Pilots Association,
International (ALPA) indicated its
support for the NPRM.
Request To Revise Applicability
NetJets submitted two requests to
revise the applicability of the proposed
AD. The commenter’s first request was
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to exclude Bombardier Model CL–650
airplanes having serial numbers 6071
and subsequent. The commenter
provided a page from the Bombardier
Model CL–650 Illustrated Parts Catalog,
which shows that the USB part number
delivered on airplanes with those serial
numbers is not the affected USB part
number addressed in the proposed AD.
The commenter submitted a subsequent
request asking that all Model CL–650
airplanes be removed from the
applicability of the proposed AD. The
commenter stated that it had conducted
additional research and provided a list
of airplane models that have the affected
USB part installed that was created by
Fokker and only one Bombardier Model
CL–650 airplane, having serial number
(S/N) 5651, has the affected part
installed.
The FAA acknowledges the
commenter’s observation that a limited
number of Bombardier Model CL–650
airplanes (also known as Challenger 650
airplanes; a marketing designation for
the Model CL–600–2B16 (604 Variant)
airplanes beginning with S/N 6050 and
subsequent) may have the affected part
installed. However, the FAA does not
agree with the commenter’s request to
revise the applicability of this AD. Since
some of the CL–600–2B16 (604 Variant)
airplanes may have the affected part
installed, the requirements of this AD
apply to those airplanes. The FAA has
determined that it is the operators’
responsibility to conduct the necessary
review to determine if an airplane in its
fleet is affected by the requirements of
this AD. This AD applies to the
airplanes identified in figure 1 to
paragraph (c) of this AD, having an
affected part (defined in paragraph (g) of
this AD) installed as specified in the
applicable service information
identified in in figure 1 to paragraph (c)
of this AD. The FAA has not revised this
AD regarding this issue.
Request To Allow Records Review
NetJets requested that the proposed
AD include a provision to allow
operators to do a records review to
determine which airplanes have the
affected USB part installed.
The commenter provided pages from
the Bombardier Model CL–650
Illustrated Parts Catalog and pointed out
that specific serial numbers of
Bombardier Model CL–650 airplanes
were delivered with factory-installed
USB ports and are not affected by the
modification specified in the proposed
AD.
The FAA acknowledges the
commenter’s request. However, while
the manufacturers Illustrated Parts
Catalog is a valuable tool for operators
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to order replacement parts, it is not an
FAA approved document that identifies
an airplane delivered type design
configuration. A records review is one
way of determining if the affected part
is installed on an airplane if the review
can conclusively identify the affected
part. Paragraph (h) of this AD requires
modification of affected parts; this AD
does not specify any required method
for determining that an affected part is
installed on an airplane. Therefore,
operators can do an appropriate records
review or they can inspect the airplane
to determine if the affected part is
installed. The FAA has not revised this
AD regarding this issue.
Request To Include Supplemental Type
Certificate (STC) Number
Net Jets requested that the proposed
AD include the STC number for any
USB receptacle that was installed on an
airplane using the FAA-approved STC
process. The commenter observed that
including the STC number would aid in
its research to determine which
airplanes in its fleet would be affected
by the requirements specified in the
proposed AD.
The FAA acknowledges the
commenter’s request. Figure 1 to
paragraph (c) of this AD already
includes the applicable STC numbers
for USB receptacles installed using the
FAA-approved STC process. Because a
USB receptacle could have been
installed using a means other than an
STC, it is the operator’s responsibility to
conduct the review necessary to
determine if an airplane in its fleet is
affected by the requirements of this AD.
The FAA has not revised this AD
regarding this issue.
Conclusion
The FAA reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
final rule as proposed, except for minor
editorial changes. The agency has
determined that these minor changes:
• Are consistent with the intent that
was proposed in the NPRM for
addressing the unsafe condition; and
• 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 modifying the
electronic flight bag USB receptacles
located in the flight deck, including
current limiting and overheat
protection. These documents are
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• Fokker Services Engineering
Bulletin EBA340–0005, Revision 0,
Sequence 8, dated July 27, 2018.
• Fokker Services Engineering
Bulletin EBAT72–0013, Revision 0,
Sequence 7, dated July 27, 2018.
• Fokker Services Engineering
Bulletin EBB737–0156, Revision 3,
Sequence 3, dated February 25, 2019.
• Fokker Services Engineering
Bulletin EBB757–0020, Revision 1,
Sequence 3, dated October 2, 2018.
• Fokker Services Engineering
Bulletin EBB767–0023, Revision 1,
Sequence 3, dated October 3, 2018.
• Fokker Services Engineering
Bulletin EBB777–0009, Revision 1,
Sequence 3, dated October 3, 2018.
distinct since they apply to different
airplane models.
• Fokker Services F28 Generic
Service Bulletin SBF28–46–002,
Revision 0, dated July 27, 2018.
• Fokker Services F50/60 Generic
Service Bulletin SBF50–46–006,
Revision 0, dated July 27, 2018.
• Fokker Services F100/700 Generic
Service Bulletin SBF100–46–008,
Revision 0, dated July 27, 2018.
• Fokker Services Engineering
Bulletin EBA320–0167, Revision 2,
Sequence 4, dated December 13, 2018.
• Fokker Services Engineering
Bulletin EBA330–0011, Revision 0,
Sequence 9, dated July 27, 2018.
• Fokker Services Engineering
Bulletin EBCL60–0010, Revision 1,
Sequence 3, dated August 30, 2018.
• Fokker Services Engineering
Bulletin EBDHC8–0035, Revision 1,
Sequence 4, dated December 13, 2018.
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
The FAA estimates that this AD
affects 14 airplanes of U.S. registry. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS *
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
3 work-hours × $85 per hour = $255 ..........................................................................................
$0
$255
$3,570
* The FAA has received no definitive data on the parts costs for the required actions.
According to the manufacturer, some
or all of the costs of this AD may be
covered under warranty, thereby
reducing the cost impact on affected
individuals. The FAA does not control
warranty coverage for affected
individuals. As a result, the FAA has
included all known costs in our cost
estimate.
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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.
The FAA is 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.
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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
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) Will not affect intrastate aviation
in Alaska, and
(3) 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.
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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 adding
the following new airworthiness
directive (AD):
■
2019–20–03 Transport Category Airplanes:
Amendment 39–19756; Docket No.
FAA–2019–0444; Product Identifier
2019–NM–028–AD.
(a) Effective Date
This AD is effective November 19, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes identified
in figure 1 to paragraph (c) of this AD,
certificated in any category, having an
affected part (defined in paragraph (g) of this
AD) installed as specified in the applicable
service information identified in figure 1 to
paragraph (c) of this AD.
BILLING CODE 4910–13–P
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Federal Register / Vol. 84, No. 199 / Tuesday, October 15, 2019 / Rules and Regulations
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BILLING CODE 4910–13–C
(d) Subject
Air Transport Association (ATA) of
America Code 46, Information systems.
(e) Reason
This AD was prompted by reports of smoke
and fumes in the flight deck. The FAA is
issuing this AD to address smoke and fumes
in the flight deck, which could result in
excessive flightcrew workload and injury to
flight deck occupants.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Definition
For the purpose of this AD, an ‘‘affected
part’’ is a universal serial bus (USB)
receptacle manufactured by Lone Star
Aviation, Corporation, having part number
LS03–05050–A.
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(h) Modification
Within 12 months after the effective date
of this AD, modify each affected part in
accordance with the Accomplishment
Instructions of the applicable Fokker Services
B.V. service information identified in
paragraphs (h)(1) through (13) of this AD.
(1) Fokker Services Engineering Bulletin
EBA320–0167, Revision 2, Sequence 4, dated
December 13, 2018.
(2) Fokker Services Engineering Bulletin
EBA330–0011, Revision 0, Sequence 9, dated
July 27, 2018.
(3) Fokker Services Engineering Bulletin
EBA340–0005, Revision 0, Sequence 8, dated
July 27, 2018.
(4) Fokker Services Engineering Bulletin
EBAT72–0013, Revision 0, Sequence 7, dated
July 27, 2018.
(5) Fokker Services Engineering Bulletin
EBB737–0156, Revision 3, Sequence 3, dated
February 25, 2019.
(6) Fokker Services Engineering Bulletin
EBB757–0020, Revision 1, Sequence 3, dated
October 2, 2018.
(7) Fokker Services Engineering Bulletin
EBB767–0023, Revision 1, Sequence 3, dated
October 3, 2018.
(8) Fokker Services Engineering Bulletin
EBB777–0009, Revision 1, Sequence 3, dated
October 3, 2018.
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(9) Fokker Services Engineering Bulletin
EBCL60–0010, Revision 1, Sequence 3, dated
August 30, 2018.
(10) Fokker Services Engineering Bulletin
EBDHC8–0035, Revision 1, Sequence 4,
dated December 13, 2018.
(11) Fokker Services F28 Generic Service
Bulletin SBF28–46–002, Revision 0, dated
July 27, 2018.
(12) Fokker Services F50/60 Generic
Service Bulletin SBF50–46–006, Revision 0,
dated July 27, 2018.
(13) Fokker Services F100/700 Generic
Service Bulletin SBF100–46–008, Revision 0,
dated July 27, 2018.
(i) Parts Installation Prohibition
After modification of an airplane as
required by paragraph (h) of this AD, no
person may install an affected part on that
airplane.
(j) Credit for Previous Actions
This paragraph provides credit for the
actions specified in paragraph (h) of this AD,
if those actions were performed before the
effective date of this AD using the applicable
service information specified in paragraphs
(j)(1) through (7) of this AD.
(1) Fokker Services Engineering Bulletin
EBA320–0167, Revision 1, dated August 30,
2018.
(2) Fokker Services Engineering Bulletin
EBDHC8–0035, Revision 0, dated July 27,
2018.
(3) Fokker Services Engineering Bulletin
EBB737–0156, Revision 1, dated August 30,
2018.
(4) Fokker Services Engineering Bulletin
EBB737–0156, Revision 2, dated October 3,
2018.
(5) Fokker Services Engineering Bulletin
EBB757–0020, Revision 0, dated July 27,
2018.
(6) Fokker Services Engineering Bulletin
EBB767–0023, Revision 0, dated July 27,
2018.
(7) Fokker Services Engineering Bulletin
EBB777–0009, Revision 0, dated July 27,
2018.
(k) 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
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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 (l)(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: 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
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.
(l) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2018–0259R1, dated February 7, 2019, 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–2019–0444.
(2) For more information about this AD,
contact Dan Rodina, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax 206–
231–3225.
(3) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (m)(3) and (4) of this AD.
(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 Services Engineering Bulletin
EBA320–0167, Revision 2, Sequence 4, dated
December 13, 2018.
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(ii) Fokker Services Engineering Bulletin
EBA330–0011, Revision 0, Sequence 9, dated
July 27, 2018.
(iii) Fokker Services Engineering Bulletin
EBA340–0005, Revision 0, Sequence 8, dated
July 27, 2018.
(iv) Fokker Services Engineering Bulletin
EBAT72–0013, Revision 0, Sequence 7, dated
July 27, 2018.
(v) Fokker Services Engineering Bulletin
EBB737–0156, Revision 3, Sequence 3, dated
February 25, 2019.
(vi) Fokker Services Engineering Bulletin
EBB757–0020, Revision 1, Sequence 3, dated
October 2, 2018.
(vii) Fokker Services Engineering Bulletin
EBB767–0023, Revision 1, Sequence 3, dated
October 3, 2018.
(viii) Fokker Services Engineering Bulletin
EBB777–0009, Revision 1, Sequence 3, dated
October 3, 2018.
(ix) Fokker Services Engineering Bulletin
EBCL60–0010, Revision 1, Sequence 3, dated
August 30, 2018.
(x) Fokker Services Engineering Bulletin
EBDHC8–0035, Revision 1, Sequence 4,
dated December 13, 2018.
(xi) Fokker Services F28 Generic Service
Bulletin SBF28–46–002, Revision 0, dated
July 27, 2018.
(xii) Fokker Services F50/60 Generic
Service Bulletin SBF50–46–006, Revision 0,
dated July 27, 2018.
(xiii) Fokker Services F100/700 Generic
Service Bulletin SBF100–46–008, Revision 0,
dated July 27, 2018.
(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 technicalservices@
fokker.com; internet https://
www.myfokkerfleet.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,
email fedreg.legal@nara.gov or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
September 27, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–22389 Filed 10–11–19; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
15:53 Oct 11, 2019
Jkt 250001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0693; Product
Identifier 2017–NE–43–AD; Amendment 39–
19758; AD 2019–20–05]
RIN 2120–AA64
Airworthiness Directives; Rolls-Royce
Deutschland Ltd & Co KG (Type
Certificate Previously Held by RollsRoyce plc) Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is superseding
airworthiness directive (AD) 2018–15–
01 for certain Rolls-Royce plc (RR) Trent
1000–A, Trent 1000–C, Trent 1000–D,
Trent 1000–E, Trent 1000–G, Trent
1000–H, Trent 1000–A2, Trent 1000–C2,
Trent 1000–D2, Trent 1000–E2, Trent
1000–G2, Trent 1000–H2, Trent 1000–
J2, Trent 1000–K2, and Trent 1000–L2
model turbofan engines. AD 2018–15–
01 required certain engines susceptible
to intermediate-pressure turbine (IPT)
blade failure not be installed on an
airplane together with other engines
with IPT blades of the same cyclic life.
This AD requires removal of the IPT
blade set at lower cyclic life limits and
replacing it with a blade set eligible for
installation. This AD also expands the
applicability to include additional Trent
1000 turbofan engine models. This AD
was prompted by the determination that
certain IPT blades are susceptible to
shank corrosion which leads to cracking
and possible blade separation. The FAA
is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective October 30,
2019.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of October 30, 2019.
The FAA must receive any comments
on this AD by November 29, 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
https://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.
SUMMARY:
PO 00000
Frm 00025
Fmt 4700
Sfmt 4700
55041
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this AD, contact Rolls-Royce plc,
Corporate Communications, P.O. Box
31, Derby, England, DE24 8BJ; phone:
011–44–1332–242424; fax: 011–44–
1332–249936; email: https://www.rollsroyce.com/contact/civil_team.jsp;
internet: https://customers.rollsroyce.com/public/rollsroycecare. You
may view this service information at the
FAA, Engine and Propeller Standards
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call 781–238–7759. It is also
available on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0693.
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–2019–
0693; 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 AD, the
mandatory continuing airworthiness
information (MCAI), regulatory
evaluation, any comments received, and
other information. The street address for
Docket Operations is listed above.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Martin Adler, Aerospace Engineer, ECO
Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: 781–
238–7088; fax: 781–238–7157; email:
martin.adler@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued AD 2018–15–01,
Amendment 39–19333 (83 FR 34755,
July 23, 2018), (‘‘AD 2018–15–01’’), for
certain RR Trent 1000–A, Trent 1000–C,
Trent 1000–D, Trent 1000–E, Trent
1000–G, Trent 1000–H, Trent 1000–A2,
Trent 1000–C2, Trent 1000–D2, Trent
1000–E2, Trent 1000–G2, Trent 1000–
H2, Trent 1000–J2, Trent 1000–K2, and
Trent 1000–L2 model turbofan engines.
AD 2018–15–01 prohibited the
installation of engines susceptible to IPT
blade failure on an airplane together
with other engines with IPT blades of
the same cyclic life. AD 2018–15–01
resulted from new operating restrictions
E:\FR\FM\15OCR1.SGM
15OCR1
]]>Agencies
[Federal Register Volume 84, Number 199 (Tuesday, October 15, 2019)]
[Rules and Regulations]
[Pages 55036-55041]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-22389]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0444; Product Identifier 2019-NM-028-AD; Amendment
39-19756; AD 2019-20-03]
RIN 2120-AA64
Airworthiness Directives; Various Transport Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
various transport airplanes. This AD was prompted by reports of smoke
and fumes in the flight deck. This AD requires modification of certain
universal serial bus (USB) receptacles located in the flight deck. The
FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective November 19, 2019.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 15,
2019.
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 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. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0444.
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-2019-
0444; 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 final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations is 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: Dan Rodina, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax 206-231-3225.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2018-0259R1, dated February 7, 2019 (``EASA AD 2018-0259R1'') (also
referred to as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for the following
airplanes on which certain USB receptacles were installed using certain
Fokker service information:
Fokker Services B.V. Model F.27 Mark 050 airplanes.
Fokker Services B.V. Model F28 Mark 3000 airplanes.
Fokker Services B.V. Model F28 Mark 0070 and Mark 0100
airplanes.
Airbus SAS Model A318-111 airplanes.
[[Page 55037]]
Airbus SAS Model A319-111, -112, -114, -115, and -132
airplanes.
Airbus SAS Model A320-211, -212, -214, -231, -232, and -
251N airplanes.
Airbus SAS Model A321-211, -231, -232, -251N and -253N
airplanes.
Airbus SAS Model A330-202, -223, -243, -322 and -343
airplanes.
Airbus SAS Model A340-312 and -313 airplanes.
ATR--GIE Avions de Transport R[eacute]gional Model ATR42-
500 airplanes.
ATR--GIE Avions de Transport R[eacute]gional Model ATR72-
212 and -212A airplanes.
The Boeing Company Model 737-300, -400, -500, -700, -800
and -900ER series airplanes.
The Boeing Company Model 757-200 series airplanes.
The Boeing Company Model 767-200 and -300 series
airplanes.
The Boeing Company Model 777-200LR series airplanes.
Bombardier, Inc., Model CL-600-2B16 (601-3A, 601-3R, and
604 Variants) airplanes.
Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series
700, 701 & 702) airplanes.
Bombardier, Inc., Model DHC-8-202, -311, -315 and -402
airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to various transport
airplanes. The NPRM published in the Federal Register on June 24, 2019
(84 FR 29414). The NPRM was prompted by reports of smoke and fumes in
the flight deck due to overheating of an Electronic Flight Bag (EFB)
USB receptacle. The NPRM proposed to require modification of certain
USB receptacles located in the flight deck.
The FAA is issuing this AD to address smoke and fumes in the flight
deck, which could result in excessive flightcrew workload and injury to
flight deck occupants. See the MCAI for additional background
information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comments
received on the NPRM and the FAA's response to each comment.
Support for the NPRM
The Air Line Pilots Association, International (ALPA) indicated its
support for the NPRM.
Request To Revise Applicability
NetJets submitted two requests to revise the applicability of the
proposed AD. The commenter's first request was to exclude Bombardier
Model CL-650 airplanes having serial numbers 6071 and subsequent. The
commenter provided a page from the Bombardier Model CL-650 Illustrated
Parts Catalog, which shows that the USB part number delivered on
airplanes with those serial numbers is not the affected USB part number
addressed in the proposed AD. The commenter submitted a subsequent
request asking that all Model CL-650 airplanes be removed from the
applicability of the proposed AD. The commenter stated that it had
conducted additional research and provided a list of airplane models
that have the affected USB part installed that was created by Fokker
and only one Bombardier Model CL-650 airplane, having serial number (S/
N) 5651, has the affected part installed.
The FAA acknowledges the commenter's observation that a limited
number of Bombardier Model CL-650 airplanes (also known as Challenger
650 airplanes; a marketing designation for the Model CL-600-2B16 (604
Variant) airplanes beginning with S/N 6050 and subsequent) may have the
affected part installed. However, the FAA does not agree with the
commenter's request to revise the applicability of this AD. Since some
of the CL-600-2B16 (604 Variant) airplanes may have the affected part
installed, the requirements of this AD apply to those airplanes. The
FAA has determined that it is the operators' responsibility to conduct
the necessary review to determine if an airplane in its fleet is
affected by the requirements of this AD. This AD applies to the
airplanes identified in figure 1 to paragraph (c) of this AD, having an
affected part (defined in paragraph (g) of this AD) installed as
specified in the applicable service information identified in in figure
1 to paragraph (c) of this AD. The FAA has not revised this AD
regarding this issue.
Request To Allow Records Review
NetJets requested that the proposed AD include a provision to allow
operators to do a records review to determine which airplanes have the
affected USB part installed.
The commenter provided pages from the Bombardier Model CL-650
Illustrated Parts Catalog and pointed out that specific serial numbers
of Bombardier Model CL-650 airplanes were delivered with factory-
installed USB ports and are not affected by the modification specified
in the proposed AD.
The FAA acknowledges the commenter's request. However, while the
manufacturers Illustrated Parts Catalog is a valuable tool for
operators to order replacement parts, it is not an FAA approved
document that identifies an airplane delivered type design
configuration. A records review is one way of determining if the
affected part is installed on an airplane if the review can
conclusively identify the affected part. Paragraph (h) of this AD
requires modification of affected parts; this AD does not specify any
required method for determining that an affected part is installed on
an airplane. Therefore, operators can do an appropriate records review
or they can inspect the airplane to determine if the affected part is
installed. The FAA has not revised this AD regarding this issue.
Request To Include Supplemental Type Certificate (STC) Number
Net Jets requested that the proposed AD include the STC number for
any USB receptacle that was installed on an airplane using the FAA-
approved STC process. The commenter observed that including the STC
number would aid in its research to determine which airplanes in its
fleet would be affected by the requirements specified in the proposed
AD.
The FAA acknowledges the commenter's request. Figure 1 to paragraph
(c) of this AD already includes the applicable STC numbers for USB
receptacles installed using the FAA-approved STC process. Because a USB
receptacle could have been installed using a means other than an STC,
it is the operator's responsibility to conduct the review necessary to
determine if an airplane in its fleet is affected by the requirements
of this AD. The FAA has not revised this AD regarding this issue.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule as proposed, except for minor
editorial changes. The agency has determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
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 modifying the electronic flight bag USB
receptacles located in the flight deck, including current limiting and
overheat protection. These documents are
[[Page 55038]]
distinct since they apply to different airplane models.
Fokker Services F28 Generic Service Bulletin SBF28-46-002,
Revision 0, dated July 27, 2018.
Fokker Services F50/60 Generic Service Bulletin SBF50-46-
006, Revision 0, dated July 27, 2018.
Fokker Services F100/700 Generic Service Bulletin SBF100-
46-008, Revision 0, dated July 27, 2018.
Fokker Services Engineering Bulletin EBA320-0167, Revision
2, Sequence 4, dated December 13, 2018.
Fokker Services Engineering Bulletin EBA330-0011, Revision
0, Sequence 9, dated July 27, 2018.
Fokker Services Engineering Bulletin EBA340-0005, Revision
0, Sequence 8, dated July 27, 2018.
Fokker Services Engineering Bulletin EBAT72-0013, Revision
0, Sequence 7, dated July 27, 2018.
Fokker Services Engineering Bulletin EBB737-0156, Revision
3, Sequence 3, dated February 25, 2019.
Fokker Services Engineering Bulletin EBB757-0020, Revision
1, Sequence 3, dated October 2, 2018.
Fokker Services Engineering Bulletin EBB767-0023, Revision
1, Sequence 3, dated October 3, 2018.
Fokker Services Engineering Bulletin EBB777-0009, Revision
1, Sequence 3, dated October 3, 2018.
Fokker Services Engineering Bulletin EBCL60-0010, Revision
1, Sequence 3, dated August 30, 2018.
Fokker Services Engineering Bulletin EBDHC8-0035, Revision
1, Sequence 4, dated December 13, 2018.
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
The FAA estimates that this AD affects 14 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions *
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
3 work-hours x $85 per hour = $255........................... $0 $255 $3,570
----------------------------------------------------------------------------------------------------------------
* The FAA has received no definitive data on the parts costs for the required actions.
According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in our cost estimate.
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.
The FAA is 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 and
associated appliances to the Director of the System Oversight Division.
Regulatory Findings
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) Will not affect intrastate aviation in Alaska, and
(3) 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):
2019-20-03 Transport Category Airplanes: Amendment 39-19756; Docket
No. FAA-2019-0444; Product Identifier 2019-NM-028-AD.
(a) Effective Date
This AD is effective November 19, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes identified in figure 1 to
paragraph (c) of this AD, certificated in any category, having an
affected part (defined in paragraph (g) of this AD) installed as
specified in the applicable service information identified in figure
1 to paragraph (c) of this AD.
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[[Page 55039]]
[GRAPHIC] [TIFF OMITTED] TR15OC19.000
[[Page 55040]]
[GRAPHIC] [TIFF OMITTED] TR15OC19.001
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(d) Subject
Air Transport Association (ATA) of America Code 46, Information
systems.
(e) Reason
This AD was prompted by reports of smoke and fumes in the flight
deck. The FAA is issuing this AD to address smoke and fumes in the
flight deck, which could result in excessive flightcrew workload and
injury to flight deck occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definition
For the purpose of this AD, an ``affected part'' is a universal
serial bus (USB) receptacle manufactured by Lone Star Aviation,
Corporation, having part number LS03-05050-A.
(h) Modification
Within 12 months after the effective date of this AD, modify
each affected part in accordance with the Accomplishment
Instructions of the applicable Fokker Services B.V. service
information identified in paragraphs (h)(1) through (13) of this AD.
(1) Fokker Services Engineering Bulletin EBA320-0167, Revision
2, Sequence 4, dated December 13, 2018.
(2) Fokker Services Engineering Bulletin EBA330-0011, Revision
0, Sequence 9, dated July 27, 2018.
(3) Fokker Services Engineering Bulletin EBA340-0005, Revision
0, Sequence 8, dated July 27, 2018.
(4) Fokker Services Engineering Bulletin EBAT72-0013, Revision
0, Sequence 7, dated July 27, 2018.
(5) Fokker Services Engineering Bulletin EBB737-0156, Revision
3, Sequence 3, dated February 25, 2019.
(6) Fokker Services Engineering Bulletin EBB757-0020, Revision
1, Sequence 3, dated October 2, 2018.
(7) Fokker Services Engineering Bulletin EBB767-0023, Revision
1, Sequence 3, dated October 3, 2018.
(8) Fokker Services Engineering Bulletin EBB777-0009, Revision
1, Sequence 3, dated October 3, 2018.
(9) Fokker Services Engineering Bulletin EBCL60-0010, Revision
1, Sequence 3, dated August 30, 2018.
(10) Fokker Services Engineering Bulletin EBDHC8-0035, Revision
1, Sequence 4, dated December 13, 2018.
(11) Fokker Services F28 Generic Service Bulletin SBF28-46-002,
Revision 0, dated July 27, 2018.
(12) Fokker Services F50/60 Generic Service Bulletin SBF50-46-
006, Revision 0, dated July 27, 2018.
(13) Fokker Services F100/700 Generic Service Bulletin SBF100-
46-008, Revision 0, dated July 27, 2018.
(i) Parts Installation Prohibition
After modification of an airplane as required by paragraph (h)
of this AD, no person may install an affected part on that airplane.
(j) Credit for Previous Actions
This paragraph provides credit for the actions specified in
paragraph (h) of this AD, if those actions were performed before the
effective date of this AD using the applicable service information
specified in paragraphs (j)(1) through (7) of this AD.
(1) Fokker Services Engineering Bulletin EBA320-0167, Revision
1, dated August 30, 2018.
(2) Fokker Services Engineering Bulletin EBDHC8-0035, Revision
0, dated July 27, 2018.
(3) Fokker Services Engineering Bulletin EBB737-0156, Revision
1, dated August 30, 2018.
(4) Fokker Services Engineering Bulletin EBB737-0156, Revision
2, dated October 3, 2018.
(5) Fokker Services Engineering Bulletin EBB757-0020, Revision
0, dated July 27, 2018.
(6) Fokker Services Engineering Bulletin EBB767-0023, Revision
0, dated July 27, 2018.
(7) Fokker Services Engineering Bulletin EBB777-0009, Revision
0, dated July 27, 2018.
(k) 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 (l)(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 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.
(l) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0259R1, dated February 7, 2019, 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-2019-0444.
(2) For more information about this AD, contact Dan Rodina,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax 206-231-3225.
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(3) and (4) of this AD.
(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 Services Engineering Bulletin EBA320-0167, Revision
2, Sequence 4, dated December 13, 2018.
[[Page 55041]]
(ii) Fokker Services Engineering Bulletin EBA330-0011, Revision
0, Sequence 9, dated July 27, 2018.
(iii) Fokker Services Engineering Bulletin EBA340-0005, Revision
0, Sequence 8, dated July 27, 2018.
(iv) Fokker Services Engineering Bulletin EBAT72-0013, Revision
0, Sequence 7, dated July 27, 2018.
(v) Fokker Services Engineering Bulletin EBB737-0156, Revision
3, Sequence 3, dated February 25, 2019.
(vi) Fokker Services Engineering Bulletin EBB757-0020, Revision
1, Sequence 3, dated October 2, 2018.
(vii) Fokker Services Engineering Bulletin EBB767-0023, Revision
1, Sequence 3, dated October 3, 2018.
(viii) Fokker Services Engineering Bulletin EBB777-0009,
Revision 1, Sequence 3, dated October 3, 2018.
(ix) Fokker Services Engineering Bulletin EBCL60-0010, Revision
1, Sequence 3, dated August 30, 2018.
(x) Fokker Services Engineering Bulletin EBDHC8-0035, Revision
1, Sequence 4, dated December 13, 2018.
(xi) Fokker Services F28 Generic Service Bulletin SBF28-46-002,
Revision 0, dated July 27, 2018.
(xii) Fokker Services F50/60 Generic Service Bulletin SBF50-46-
006, Revision 0, dated July 27, 2018.
(xiii) Fokker Services F100/700 Generic Service Bulletin SBF100-
46-008, Revision 0, dated July 27, 2018.
(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 https://www.myfokkerfleet.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, email [email protected] or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on September 27, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-22389 Filed 10-11-19; 8:45 am]
BILLING CODE 4910-13-P
