[Federal Register Volume 84, Number 64 (Wednesday, April 3, 2019)]
[Rules and Regulations]
[Pages 12877-12880]
[FR Doc No: 2019-06284]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0205; Product Identifier 2019-CE-001-AD; Amendment
39-19598; AD 2019-05-15]
RIN 2120-AA64

Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Pilatus Aircraft Ltd. Model PC-7 airplanes. This AD results from
mandatory continuing airworthiness information (MCAI) issued by the
aviation authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as chafed and burned wires located under panel F5. We are
issuing this AD to require actions to address the unsafe condition on
these products.

DATES: This AD is effective April 23, 2019.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of April 23,
2019.
    We must receive comments on this AD by May 20, 2019.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: 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 Pilatus
Aircraft Ltd., Customer Technical Support (MCC), P.O. Box 992, CH-6371
Stans, Switzerland; telephone: +41 (0)41 619 67 74; fax: +41 (0)41 619
67 73; email: aircraft.com">[email protected]aircraft.com; internet: https://www.pilatus-aircraft.com/en. You may view this referenced service
information at the FAA, Policy and Innovation, 901 Locust, Kansas City,
Missouri 64106. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>. It is also available on the internet at
http://www.regulations.gov by searching for locating Docket No. FAA-
2019-0205.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0205; 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 regulatory evaluation, any comments received, and other
information. The street address for Docket Operations (telephone (800)
647-5527) is in the ADDRESSES section. Comments will be available in
the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA,
Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
doug.[email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    The Federal Office of Civil Aviation (FOCA), which is the aviation
authority for Switzerland, has issued AD HB-2019-002, dated January 28,
2019 (referred to after this as ``the MCAI''), to correct an unsafe
condition for certain serial-numbered Pilatus Aircraft Ltd. Model PC-7
airplanes. The MCAI states:

    During a scheduled inspection several chafed and burned wires
located under panel F5 were found.
    This condition, if not detected and corrected, could lead to
smoke/fume in the cockpit and in a possible in-flight fire.
    To address this potential unsafe condition, Pilatus Aircraft
Ltd. issued the [service bulletin] SB to provide applicable
inspection instructions.
    For the reason described above, this [FOCA] Airworthiness
Directive (AD) requires a visual inspection of the wires below the
panel F5 and, depending on findings, accomplishment of applicable
corrective action(s).

    FOCA advises that although aircraft are manufactured with
sufficient clearance between the wiring loom and the components
installed below access panel F5, the wiring looms may be moved when
components installed in the front instrument panel are removed and re-
installed during maintenance. As a result, the wiring looms can come
into contact with other equipment, causing chafing damage. You may
examine the MCAI on the internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2019-0205.

Related Service Information Under 1 CFR Part 51

    Pilatus Aircraft Ltd. has issued Pilatus PC-7 Service Bulletin No.
24-008, Rev. No. 1, dated December 20, 2018. The service information
contains procedures for inspecting the wires below access panel F5 for
chafing and contact with the casings of the line replacement unit
(LRU), panel edges, and environmental control system (ECS) hoses;
replacing exposed bare wires; repairing chafed wires by installing a
protective sleeve; inspecting the metal clips on the demist hoses to
make sure they are not in contact with the wiring looms; and if
necessary, adjusting the orientation of the metal clips to put their
sharp edges away from the wiring loom. The service information also
specifies reporting information to Pilatus Aircraft Ltd. so it can
determine if follow-on action will be necessary. This service
information is reasonably available because the interested parties have
access to it through their normal course of business or by the means
identified in the ADDRESSES section.

FAA's Determination and Requirements of the AD

    This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are issuing this AD because we
evaluated all information provided by the State of Design Authority and
determined the unsafe condition exists and is likely to exist or
develop on other products of the same type design.

FAA's Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because
chafing of electrical cables through the insulation could lead to
arching, which may cause smoke or fumes in the cockpit and result in a
possible in-flight fire. Therefore, we find good cause that notice and
opportunity for prior public comment are impracticable. In addition,
for the reason stated above, we find that good cause exists for making
this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2019-0205; Product
Identifier 2019-CE-001-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD because of
those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

Costs of Compliance

    We estimate that this AD will affect 18 products of U.S. registry.
We also estimate that it would take about 3.5 work-hours per product to
comply with the inspection requirement of this AD and 5 minutes to
comply with the reporting requirement of this AD. The average labor
rate is $85 per work-hour.
    Based on these figures, we estimate the cost of the inspection and
reporting requirement in this AD on U.S. operators to be $5,481, or
$304.50 per product.
    In addition, we estimate the labor and parts costs for the follow-
on actions as necessary:

     Repairing chafed wires and installing a protective sleeve
would take about 1.5 work-hours for a cost of $127.50 per product.
     Replacing burnt or bare wires would take about 4 work-
hours and require parts costing approximately $2,000 for a cost of
$2,340.
     Adjusting metal clips would take about .5 work-hour for a
cost of $42.50.
    We have no way of determining the number of products that may need
these actions.

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 small airplanes, gliders,
balloons, airships, domestic business jet transport airplanes, and
associated appliances to the Director of the Policy and Innovation
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 adding the following new airworthiness
directive (AD):

2019-05-15 Pilatus Aircraft Ltd: Amendment 39-19598; Docket No. FAA-
2019-0205; Product Identifier 2019-CE-001-AD.

(a) Effective Date

    This AD becomes effective April 23, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Pilatus Aircraft Ltd. Model PC-7 airplanes,
manufacturer serial number (MSN) 101 through MSN 537, MSN 548
through MSN 609, and MSN 613 through MSN 618, certificated in any
category.

(d) Subject

    Air Transport Association of America (ATA) Code 24: Electric
Power.

(e) Reason

    This AD was prompted by mandatory continuing airworthiness
information (MCAI) issued by the aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as chafed and
burned wires located under panel F5. We are issuing this AD to
detect and correct chafed and burned wires under panel F5, which
could lead to smoke or fumes in the cockpit and result in a possible
in-flight fire.

 (f) Actions and Compliance

    Unless already done, do the following actions in paragraphs
(f)(1) through (2).
    (1) Within the next 120 days after the effective date of this
AD, do the following inspections:
    (i) Visually inspect all wires below access panel F5 for signs
of chafing and contact with the casings of the line replacement
units (LRUs), panel edges, or environmental control system (ECS)
hoses. If there is any chafing or contact, before further flight, do
all corrective actions by following the Accomplishment Instructions,
paragraphs 3.B.(2) through 3.B.(3), in Pilatus PC-7 Service Bulletin
No. 24-008, Rev. No. 1, dated December 20, 2018.
    (ii) Visually inspect the metal clips on the demist hoses for
signs of contact with the wiring looms. If there is any contact,
before further flight, adjust the clips by following the
Accomplishment Instructions, paragraph 3.B.(5), in Pilatus PC-7
Service Bulletin No. 24-008, Rev. No. 1, dated December 20, 2018.
    (2) Within 10 days after completing the inspections required in
paragraph (f)(1)(i) and (ii) of this AD or within the next 10 days
after the effective date of this AD, whichever occurs later, report
the results of the inspections, both negative and positive, to
Pilatus Aircraft Ltd. at the address listed in paragraph (i)(3) of
this AD. On the report, include whether there were any chafed wires,
casing contacts that needed to be relocated, or metal clip
adjustments. You may use the Service Bulletin Evaluation Sheet in
Pilatus PC-7 Service Bulletin No. 24-008, Rev. No. 1, dated December
20, 2018, for this purpose, but include the above findings of the
inspection.

(g) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
Small Airplane Standards Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. Send information to ATTN: Doug Rudolph, Aerospace Engineer,
FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas
City, Missouri 64106; telephone:<PHONE_NUMBER>; fax: (816) 329-
4090; email: [email protected]. Before using any approved AMOC on
any airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must
instead be accomplished using a method approved by the Manager,
Small Airplane Standards Branch, FAA, or the Federal Office of Civil
Aviation (FOCA).
    (3) Reporting Requirements: A federal agency may not conduct or
sponsor, and a person is not required to respond to, nor shall a
person be subject to a penalty for failure to comply with a
collection of information subject to the requirements of the
Paperwork Reduction Act unless that collection of information
displays a currently valid OMB Control Number. The OMB Control
Number for this information collection is 2120-0056. Public
reporting for this collection of information is estimated to

be approximately 5 minutes per response, including the time for
reviewing instructions, searching existing data sources, gathering
and maintaining the data needed, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory as required by this AD; the nature and
extent of confidentiality to be provided, if any. Send comments
regarding this burden estimate or any other aspect of this
collection of information, including suggestions for reducing this
burden to: Information Collection Clearance Officer, Federal
Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX
76177-1524.

(h) Related Information

    Refer to MCAI FOCA AD HB-2019-002, dated January 28, 2019, for
related information. You may examine the MCAI on the internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2019-0205.

(i) 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) Pilatus Aircraft Ltd. PC-7 Service Bulletin No. 24-008, Rev.
No. 1, dated December 20, 2018.
    (ii) [Reserved]
    (3) For Pilatus Aircraft Ltd. service information identified in
this AD, contact Pilatus Aircraft Ltd., Customer Technical Support
(MCC), P.O. Box 992, CH-6371 Stans, Switzerland; phone: +41 (0)41
619 67 74; fax: +41 (0)41 619 67 73; email: aircraft.com">[email protected]aircraft.com; internet: https://www.pilatus-aircraft.com/en.
    (4) You may view this service information at the FAA, Policy and
Innovation, 901 Locust, Kansas City, Missouri 64106. For information
on the availability of this material at the FAA, call (816) 329-
4148. It is also available on the internet at http://www.regulations.gov by searching for locating Docket No. FAA-2019-
0205.
    (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<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Kansas City, Missouri, on March 25, 2019.
Melvin J. Johnson,
Aircraft Certification Service, Deputy Director, Policy and Innovation
Division, AIR-601.
[FR Doc. 2019-06284 Filed 4-2-19; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 84, Number 42 (Monday, March 4, 2019)]
[Rules and Regulations]
[Pages 7269-7271]
[FR Doc No: 2019-03411]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0963; Product Identifier 2018-NM-135-AD; Amendment
39-19566; AD 2019-03-14]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Dassault Aviation Model FAN JET FALCON and FAN JET FALCON SERIES C, D,
E, F, and G airplanes. This AD was prompted by a determination that new
and more restrictive airworthiness limitations and maintenance
requirements are necessary. This AD requires revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations and maintenance
requirements. We are issuing this AD to address the unsafe condition on
these products.

DATES: This AD is effective April 8, 2019.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 8,
2019.

ADDRESSES: For service information identified in this final rule,
contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606; telephone<PHONE_NUMBER>; internet
http://www.dassaultfalcon.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<PHONE_NUMBER>. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0963.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0963; 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 (phone:<PHONE_NUMBER>) 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: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Dassault Aviation
Model FAN JET FALCON and FAN JET FALCON SERIES C, D, E, F, and G
airplanes. The NPRM published in the Federal Register on November 23,
2018 (83 FR 59326). The NPRM was prompted by a determination that new
and more restrictive airworthiness limitations and maintenance
requirements are necessary. The NPRM proposed to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations and
maintenance requirements. We are issuing this AD to address, among
other things, fatigue cracking and damage in principal structural
elements; such fatigue cracking and damage could result in 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 AD
2018-0193, dated September 3, 2018 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for certain Dassault Aviation Model FAN JET
FALCON and FAN JET FALCON SERIES C, D, E, F, and G airplanes. The MCAI
states:

    In June 1988, the Federal Aviation Administration sponsored a
conference on ageing aircraft, during which the decision was taken
to pay particular attention to those. The ATA [Air Transport
Association] and the AIA [Aerospace Industries Association]
committed themselves to identify and to set up procedures to ensure
continued structural integrity on ageing aircraft. Prompted by these
actions, Dassault developed the SSIP [Supplemental Structural
Inspection Program], aiming to guarantee the airworthiness of the
Fan Jet Falcon aeroplane which reach and exceed half of the Limit of
Validity. The airworthiness limitations and certification
maintenance instructions for the affected Fan Jet Falcon aeroplanes,
which are approved by EASA, are currently defined and published in
the ALS [airworthiness limitations section]. These instructions have
been identified as mandatory for continued airworthiness.
    Failure to accomplish these instructions could result in an
unsafe condition.
    Previously, EASA issued AD 2008-0221 to require accomplishment
of the maintenance tasks, and implementation of the airworthiness
limitations, as specified in ALS at Revision 7.
    Since that [EASA] AD was issued, Dassault issued ALS Revisions 8
and 9, which introduced new and more restrictive maintenance
requirements and/or airworthiness limitations.
    For the reason described above, this [EASA] AD takes over the
requirements for Fan Jet Falcon aeroplanes from EASA AD 2008-0221
and requires accomplishment of the actions specified in the ALS.
    Once new [EASA] ADs have been published for all the types
addressed by EASA AD 2008-0221, EASA plans to cancel that AD.

    The unsafe condition is fatigue cracking and damage in principal
structural elements; such fatigue cracking and damage could result in
reduced structural integrity of the airplane. Because we determined
that a separate FAA AD should be issued for each airplane model due to
different ALS requirements, we did not issue an AD that corresponded to
EASA AD 2008-0221.
    You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0963.

Comments

    We gave the public the opportunity to participate in developing
this final rule. We have considered the comment received; the
commenter, Bienvenu Badinenganyi, stated no objection to the NPRM.

Conclusion

    We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this final rule as proposed, except for minor editorial changes. We
have 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

    Dassault has issued Chapter 5-40-01, Airworthiness Limitations, DMD
44729, Revision 9, dated November 29, 2017, of the Dassault Aviation
Falcon 20 Maintenance Manual. This service information includes life
limits for certain airframe components, and describes airworthiness
limitations for safe life limits and certification maintenance
requirements. This service information is reasonably available because
the interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    We estimate that this AD affects 61 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:
    We have determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although we recognize that this number may vary from operator to
operator. In the past, we have estimated that this action takes 1 work-
hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet, we have determined
that a per-operator estimate is more accurate than a per-airplane
estimate. Therefore, we estimate the total cost per operator to be
$7,650 (90 work-hours x $85 per work-hour).

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
    This 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) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

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

2019-03-14 Dassault Aviation: Amendment 39-19566; Docket No. FAA-
2018-0963; Product Identifier 2018-NM-135-AD.

(a) Effective Date

    This AD is effective April 8, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Dassault Aviation Model FAN JET FALCON and
FAN JET FALCON SERIES C, D, E, F, and G airplanes, certificated in
any category, all serial numbers, on which the Dassault Fan Jet
Falcon Supplemental Structural Inspection Program (Dassault Service
Bulletin (SB) 730), has been embodied into the airplane's
maintenance program.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

(e) Reason

    This AD was prompted by a determination that new and more
restrictive airworthiness limitations and maintenance requirements
are necessary. We are issuing this AD to address, among other
things, fatigue cracking and damage in principal structural
elements; such fatigue cracking and damage could result in reduced
structural integrity of the airplane.

(f) Compliance

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

(g) Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the airworthiness limitations specified in Chapter 5-40-
01, Airworthiness Limitations, DMD 44729, Revision 9, dated November
29, 2017, of the Dassault Aviation Falcon 20 Maintenance Manual. The
initial compliance time for accomplishing the actions is at the
applicable time specified in Chapter 5-40-01, Airworthiness
Limitations, DMD 44729, Revision 9, dated November 29, 2017, of the
Dassault Aviation Falcon 20 Maintenance Manual; or within 90 days
after the effective date of this AD; whichever occurs later. Where
the threshold column in the table in paragraph B, Mandatory
Maintenance Operations, of Chapter 5-40-01, Airworthiness
Limitations, DMD 44729, Revision 9, dated November 29, 2017, of the
Dassault Aviation Falcon 20 Maintenance Manual specifies a
compliance time in years, those compliance times start from the date
of issuance of the original airworthiness certificate or date of
issuance of the original export certificate of airworthiness.

(h) No Alternative Actions or Intervals

    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 and intervals are approved as an
alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (i)(1) of this AD.

(i) 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 (j)(2) of this AD. Information
may be emailed to<EMAIL_ADDRESS>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 European Aviation
Safety Agency (EASA); or Dassault Aviation's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.

(j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0193, dated September 3, 2018, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2018-0963.
    (2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax<PHONE_NUMBER>.

(k) 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) Chapter 5-40-01, Airworthiness Limitations, DMD 44729,
Revision 9, dated November 29, 2017, of the Dassault Aviation Falcon
20 Maintenance Manual.
    (ii) [Reserved]
    (3) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone<PHONE_NUMBER>; internet http://www.dassaultfalcon.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<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Des Moines, Washington, on February 21, 2019.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-03411 Filed 3-1-19; 8:45 am]
 BILLING CODE 4910-13-P