82 FR 55332 - Airworthiness Directives; Pilatus Aircraft Limited Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 223 (November 21, 2017)

Page Range		55332-55333
FR Document		2017-25006

We propose to adopt a new airworthiness directive (AD) for Pilatus Aircraft Limited Model PC-7 airplanes. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as the brakes remaining activated after release of the brake pedal. We are issuing this proposed AD to require actions to address the unsafe condition on these products.

Federal Register, Volume 82 Issue 223 (Tuesday, November 21, 2017)

[Federal Register Volume 82, Number 223 (Tuesday, November 21, 2017)]
[Proposed Rules]
[Pages 55332-55333]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-25006]


========================================================================
Proposed Rules
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains notices to the public of 
the proposed issuance of rules and regulations. The purpose of these 
notices is to give interested persons an opportunity to participate in 
the rule making prior to the adoption of the final rules.

========================================================================


Federal Register / Vol. 82, No. 223 / Tuesday, November 21, 2017 / 
Proposed Rules

[[Page 55332]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-1079; Product Identifier 2017-CE-039-AD]
RIN 2120-AA64


Airworthiness Directives; Pilatus Aircraft Limited Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
Pilatus Aircraft Limited Model PC-7 airplanes. This proposed AD results 
from mandatory continuing airworthiness information (MCAI) originated 
by an aviation authority of another country to identify and correct an 
unsafe condition on an aviation product. The MCAI describes the unsafe 
condition as the brakes remaining activated after release of the brake 
pedal. We are issuing this proposed AD to require actions to address 
the unsafe condition on these products.

DATES: We must receive comments on this proposed AD by January 5, 2018.

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: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: 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 proposed 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">techsupport@pilatus-aircraft.com; Internet: http://
www.pilatus-aircraft.com. You may review this referenced service 
information at the FAA, Policy and Innovation Division, 901 Locust, 
Kansas City, Missouri 64106. For information on the availability of 
this material at the FAA, call (816) 329-4148.

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-2017-
1079; 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 proposed AD, the regulatory evaluation, any comments 
received, and other information. The street address for the Docket 
Office (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: (816) 329-4059; fax: (816) 329-4090; email: 
[email protected].

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2017-1079; 
Product Identifier 2017-CE-039-AD'' at the beginning of your comments. 
We specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this proposed AD. We will consider 
all comments received by the closing date and may amend this proposed 
AD because of those comments.
    We will post all comments we receive, without change, to http://regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The Federal Office of Civil Aviation (FOCA), which is the aviation 
authority for Switzerland, has issued FOCA AD HB-2017-002, dated 
October 20, 2017 (referred to after this as ``the MCAI''), to correct 
an unsafe condition for Pilatus Aircraft Limited Model PC-7 airplanes. 
The MCAI states:

    This [FOCA] Airworthiness Directive (AD) is prompted due to a 
report where the brakes have remained activated after release of the 
brake pedals before taxing.
    Such a condition, if left uncorrected, could lead to an 
asymmetric braking and subsequent loss of directional control.
    In order to correct and control the situation, this [FOCA] AD 
requires the modification of the brake-pedal interconnecting tie-rod 
by removing the bonding straps and attachment hardware currently 
installed on the left and right brake-pedal interconnecting tie-
rods.

You may examine the MCAI on the Internet at http://www.regulations.gov 
by searching for and locating Docket No. FAA-2017-1079.

Related Service Information Under 1 CFR Part 51

    Pilatus Aircraft Limited has issued Pilatus Service Bulletin No. 
32-028, dated September 20, 2017. The service information describes 
procedures for removing the left and right brake pedal interconnecting 
tie rods. 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 of this 
NPRM.

FAA's Determination and Requirements of the Proposed 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 proposing this AD because 
we evaluated all information and determined the unsafe condition exists 
and is likely to exist or develop on other products of the same type 
design.

[[Page 55333]]

Costs of Compliance

    We estimate that this proposed AD will affect 18 products of U.S. 
registry. We also estimate that it would take about 2.5 work-hours per 
product to comply with the basic requirements of this proposed AD. The 
average labor rate is $85 per work-hour.
    Based on these figures, we estimate the cost of the proposed AD on 
U.S. operators to be $3,825, or $212.50 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 small airplanes and domestic 
business jet transport airplanes to the Director of the Policy and 
Innovation Division.

Regulatory Findings

    We determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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


Sec.  39.13   [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

Pilatus Aircraft Limited: Docket No. FAA-2017-1079; Product 
Identifier 2017-CE-039-AD.

(a) Comments Due Date

    We must receive comments by January 5, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Pilatus Aircraft Limited Model PC-7 
airplanes, manufacturer serial numbers 101 through 618, certificated 
in any category.

(d) Subject

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

(e) Reason

    This AD was prompted by mandatory continuing airworthiness 
information (MCAI) originated by an aviation authority of another 
country to identify and correct an unsafe condition on an aviation 
product. The MCAI describes the unsafe condition as the brakes 
remaining activated after release of the brake pedal. We are issuing 
this AD to prevent the brakes from remaining activated after the 
brake pedal has been released, which could lead to asymmetric 
braking and subsequent loss of control.

(f) Actions and Compliance

    Unless already done, within the next 90 days after the effective 
date of this AD, modify the brake pedal interconnecting tie rods by 
removing the bonding straps and attachment hardware following 
sections A, B, and C of the Accomplishment Instructions in Pilatus 
Service Bulletin 32-028, dated September 20, 2017.

(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: (816) 329-4059; 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 be 
accomplished using a method approved by the Manager, Small Airplane 
Standards Branch, FAA; or the Federal Office of Civil Aviation 
(FOCA), which is the aviation authority for Switzerland.

(h) Related Information

    Refer to MCAI FOCA AD HB-2017-002, dated October 20, 2017; and 
Pilatus Service Bulletin No. 32-028, dated September 20, 2017, for 
related information. You may examine the MCAI on the Internet at 
http://www.regulations.gov by searching for and locating Docket No. 
FAA-2017-1079. For service information related to 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">techsupport@pilatus-aircraft.com; 
Internet: http://www.pilatus-aircraft.com. You may review this 
referenced service information at the FAA, Policy and Innovation 
Division, 901 Locust, Kansas City, Missouri 64106. For information 
on the availability of this material at the FAA, call (816) 329-
4148.

    Issued in Kansas City, Missouri, on November 9, 2017.
Pat Mullen,
Acting Deputy Director, Policy & Innovation Division, Aircraft 
Certification Service.
[FR Doc. 2017-25006 Filed 11-20-17; 8:45 am]
 BILLING CODE 4910-13-P

55332

Proposed Rules Federal Register
Vol. 82, No. 223

Tuesday, November 21, 2017

This section of the FEDERAL REGISTER For service information identified in post a report summarizing each
contains notices to the public of the proposed this proposed AD, contact PILATUS substantive verbal contact we receive
issuance of rules and regulations. The Aircraft Ltd., Customer Technical about this proposed AD.
purpose of these notices is to give interested Support (MCC), P.O. Box 992, CH–6371
persons an opportunity to participate in the Discussion
Stans, Switzerland; phone: +41 (0)41
rule making prior to the adoption of the final
rules.
619 67 74; fax: +41 (0)41 619 67 73; The Federal Office of Civil Aviation
email: techsupport@pilatus- (FOCA), which is the aviation authority
aircraft.com; Internet: http:// for Switzerland, has issued FOCA AD
DEPARTMENT OF TRANSPORTATION www.pilatus-aircraft.com. You may HB–2017–002, dated October 20, 2017
review this referenced service (referred to after this as ‘‘the MCAI’’), to
Federal Aviation Administration information at the FAA, Policy and correct an unsafe condition for Pilatus
Innovation Division, 901 Locust, Kansas Aircraft Limited Model PC–7 airplanes.
14 CFR Part 39 City, Missouri 64106. For information The MCAI states:
on the availability of this material at the This [FOCA] Airworthiness Directive (AD)
[Docket No. FAA–2017–1079; Product
FAA, call (816) 329–4148. is prompted due to a report where the brakes
Identifier 2017–CE–039–AD]
Examining the AD Docket have remained activated after release of the
RIN 2120–AA64 brake pedals before taxing.
You may examine the AD docket on Such a condition, if left uncorrected, could
Airworthiness Directives; Pilatus the Internet at http:// lead to an asymmetric braking and
Aircraft Limited Airplanes www.regulations.gov by searching for subsequent loss of directional control.
and locating Docket No. FAA–2017– In order to correct and control the
AGENCY: Federal Aviation 1079; or in person at the Docket situation, this [FOCA] AD requires the
Administration (FAA), Department of Management Facility between 9 a.m. modification of the brake-pedal
Transportation (DOT). and 5 p.m., Monday through Friday, interconnecting tie-rod by removing the
ACTION: Notice of proposed rulemaking bonding straps and attachment hardware
except Federal holidays. The AD docket currently installed on the left and right brake-
(NPRM). contains this proposed AD, the pedal interconnecting tie-rods.
regulatory evaluation, any comments
SUMMARY: We propose to adopt a new You may examine the MCAI on the
received, and other information. The
airworthiness directive (AD) for Pilatus Internet at http://www.regulations.gov
street address for the Docket Office
Aircraft Limited Model PC–7 airplanes. by searching for and locating Docket No.
(telephone (800) 647–5527) is in the
This proposed AD results from FAA–2017–1079.
ADDRESSES section. Comments will be
mandatory continuing airworthiness
available in the AD docket shortly after Related Service Information Under 1
information (MCAI) originated by an
receipt. CFR Part 51
aviation authority of another country to
FOR FURTHER INFORMATION CONTACT:
identify and correct an unsafe condition
Doug Rudolph, Aerospace Engineer, Pilatus Aircraft Limited has issued
on an aviation product. The MCAI
FAA, Small Airplane Standards Branch, Pilatus Service Bulletin No. 32–028,
describes the unsafe condition as the
901 Locust, Room 301, Kansas City, dated September 20, 2017. The service
brakes remaining activated after release
Missouri 64106; telephone: (816) 329– information describes procedures for
of the brake pedal. We are issuing this
4059; fax: (816) 329–4090; email: removing the left and right brake pedal
proposed AD to require actions to
doug.rudolph@faa.gov. interconnecting tie rods. This service
address the unsafe condition on these
SUPPLEMENTARY INFORMATION: information is reasonably available
products.
because the interested parties have
DATES: We must receive comments on Comments Invited access to it through their normal course
this proposed AD by January 5, 2018. We invite you to send any written of business or by the means identified
ADDRESSES: You may send comments by relevant data, views, or arguments about in the ADDRESSES section of this NPRM.
any of the following methods: this proposed AD. Send your comments FAA’s Determination and Requirements
• Federal eRulemaking Portal: Go to to an address listed under the of the Proposed AD
http://www.regulations.gov. Follow the ADDRESSES section. Include ‘‘Docket No.
instructions for submitting comments. FAA–2017–1079; Product Identifier This product has been approved by
• Fax: (202) 493–2251. 2017–CE–039–AD’’ at the beginning of the aviation authority of another
• Mail: U.S. Department of your comments. We specifically invite country, and is approved for operation
Transportation, Docket Operations, M– comments on the overall regulatory, in the United States. Pursuant to our
30, West Building Ground Floor, Room economic, environmental, and energy bilateral agreement with this State of
asabaliauskas on DSKBBXCHB2PROD with PROPOSALS

W12–140, 1200 New Jersey Avenue SE., aspects of this proposed AD. We will Design Authority, they have notified us
Washington, DC 20590. consider all comments received by the of the unsafe condition described in the
• Hand Delivery: U.S. Department of closing date and may amend this MCAI and service information
Transportation, Docket Operations, M– proposed AD because of those referenced above. We are proposing this
30, West Building Ground Floor, Room comments. AD because we evaluated all
W12–140, 1200 New Jersey Avenue SE., We will post all comments we information and determined the unsafe
Washington, DC 20590, between 9 a.m. receive, without change, to http:// condition exists and is likely to exist or
and 5 p.m., Monday through Friday, regulations.gov, including any personal develop on other products of the same
except Federal holidays. information you provide. We will also type design.

VerDate Sep<11>2014 18:16 Nov 20, 2017 Jkt 244001 PO 00000 Frm 00001 Fmt 4702 Sfmt 4702 E:\FR\FM\21NOP1.SGM 21NOP1

Federal Register / Vol. 82, No. 223 / Tuesday, November 21, 2017 / Proposed Rules 55333

Costs of Compliance Procedures (44 FR 11034, February 26, Pilatus Service Bulletin 32–028, dated
1979), September 20, 2017.
We estimate that this proposed AD
will affect 18 products of U.S. registry. (3) Will not affect intrastate aviation (g) Other FAA AD Provisions
We also estimate that it would take in Alaska, and The following provisions also apply to this
about 2.5 work-hours per product to (4) Will not have a significant AD:
comply with the basic requirements of economic impact, positive or negative, (1) Alternative Methods of Compliance
this proposed AD. The average labor on a substantial number of small entities (AMOCs): The Manager, Small Airplane
rate is $85 per work-hour. under the criteria of the Regulatory Standards Branch, FAA, has the authority to
Based on these figures, we estimate Flexibility Act. approve AMOCs for this AD, if requested
the cost of the proposed AD on U.S. using the procedures found in 14 CFR 39.19.
List of Subjects in 14 CFR Part 39 Send information to ATTN: Doug Rudolph,
operators to be $3,825, or $212.50 per Aerospace Engineer, FAA, Small Airplane
product. Air transportation, Aircraft, Aviation
Standards Branch, 901 Locust, Room 301,
safety, Incorporation by reference, Kansas City, Missouri 64106; telephone:
Authority for This Rulemaking Safety. (816) 329–4059; fax: (816) 329–4090; email:
Title 49 of the United States Code doug.rudolph@faa.gov. Before using any
The Proposed Amendment
specifies the FAA’s authority to issue approved AMOC on any airplane to which
rules on aviation safety. Subtitle I, Accordingly, under the authority the AMOC applies, notify your appropriate
section 106, describes the authority of delegated to me by the Administrator, principal inspector (PI) in the FAA Flight
the FAA Administrator. ‘‘Subtitle VII: the FAA proposes to amend 14 CFR part Standards District Office (FSDO), or lacking
Aviation Programs,’’ describes in more 39 as follows: a PI, your local FSDO.
detail the scope of the Agency’s (2) Contacting the Manufacturer: For any
authority. PART 39—AIRWORTHINESS requirement in this AD to obtain corrective
We are issuing this rulemaking under DIRECTIVES actions from a manufacturer, the action must
be accomplished using a method approved
the authority described in ‘‘Subtitle VII, by the Manager, Small Airplane Standards
Part A, Subpart III, Section 44701: ■ 1. The authority citation for part 39
continues to read as follows: Branch, FAA; or the Federal Office of Civil
General requirements.’’ Under that Aviation (FOCA), which is the aviation
section, Congress charges the FAA with Authority: 49 U.S.C. 106(g), 40113, 44701. authority for Switzerland.
promoting safe flight of civil aircraft in
§ 39.13 [Amended] (h) Related Information
air commerce by prescribing regulations
for practices, methods, and procedures ■ 2. The FAA amends § 39.13 by adding Refer to MCAI FOCA AD HB–2017–002,
the Administrator finds necessary for the following new AD: dated October 20, 2017; and Pilatus Service
Bulletin No. 32–028, dated September 20,
safety in air commerce. This regulation Pilatus Aircraft Limited: Docket No. FAA– 2017, for related information. You may
is within the scope of that authority 2017–1079; Product Identifier 2017–CE– examine the MCAI on the Internet at http://
because it addresses an unsafe condition 039–AD. www.regulations.gov by searching for and
that is likely to exist or develop on (a) Comments Due Date locating Docket No. FAA–2017–1079. For
products identified in this rulemaking service information related to this AD,
We must receive comments by January 5,
action. contact PILATUS Aircraft Ltd., Customer
2018.
This AD is issued in accordance with Technical Support (MCC), P.O. Box 992, CH–
authority delegated by the Executive (b) Affected ADs 6371 Stans, Switzerland; phone: +41 (0)41
Director, Aircraft Certification Service, None. 619 67 74; fax: +41 (0)41 619 67 73; email:
as authorized by FAA Order 8000.51C. techsupport@pilatus-aircraft.com; Internet:
(c) Applicability http://www.pilatus-aircraft.com. You may
In accordance with that order, issuance
This AD applies to Pilatus Aircraft Limited review this referenced service information at
of ADs is normally a function of the the FAA, Policy and Innovation Division, 901
Compliance and Airworthiness Model PC–7 airplanes, manufacturer serial
numbers 101 through 618, certificated in any Locust, Kansas City, Missouri 64106. For
Division, but during this transition information on the availability of this
category.
period, the Executive Director has material at the FAA, call (816) 329–4148.
delegated the authority to issue ADs (d) Subject
Issued in Kansas City, Missouri, on
applicable to small airplanes and Air Transport Association of America November 9, 2017.
domestic business jet transport (ATA) Code 32: Landing Gear. Pat Mullen,
airplanes to the Director of the Policy (e) Reason Acting Deputy Director, Policy & Innovation
and Innovation Division. Division, Aircraft Certification Service.
This AD was prompted by mandatory
Regulatory Findings continuing airworthiness information (MCAI) [FR Doc. 2017–25006 Filed 11–20–17; 8:45 am]
originated by an aviation authority of another
We determined that this proposed AD BILLING CODE 4910–13–P
country to identify and correct an unsafe
would not have federalism implications condition on an aviation product. The MCAI
under Executive Order 13132. This describes the unsafe condition as the brakes
proposed AD would not have a remaining activated after release of the brake DEPARTMENT OF JUSTICE
substantial direct effect on the States, on pedal. We are issuing this AD to prevent the
the relationship between the national brakes from remaining activated after the Drug Enforcement Administration
asabaliauskas on DSKBBXCHB2PROD with PROPOSALS

Government and the States, or on the brake pedal has been released, which could
distribution of power and lead to asymmetric braking and subsequent 21 CFR Part 1308
responsibilities among the various loss of control.
[Docket No. DEA–474]
levels of government. (f) Actions and Compliance
For the reasons discussed above, I Unless already done, within the next 90 Schedules of Controlled Substances:
certify this proposed regulation: days after the effective date of this AD, Temporary Placement of Cyclopropyl
(1) Is not a ‘‘significant regulatory modify the brake pedal interconnecting tie Fentanyl into Schedule I
action’’ under Executive Order 12866, rods by removing the bonding straps and
(2) Is not a ‘‘significant rule’’ under attachment hardware following sections A, B, AGENCY:Drug Enforcement
the DOT Regulatory Policies and and C of the Accomplishment Instructions in Administration, Department of Justice.

VerDate Sep<11>2014 18:16 Nov 20, 2017 Jkt 244001 PO 00000 Frm 00002 Fmt 4702 Sfmt 4702 E:\FR\FM\21NOP1.SGM 21NOP1

Document Created: 2017-11-21 00:43:12
Document Modified: 2017-11-21 00:43:12

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Proposed Rules
Action		Notice of proposed rulemaking (NPRM).
Dates		We must receive comments on this proposed AD by January 5, 2018.
Contact		Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; fax: (816) 329-4090; email: [email protected]
FR Citation		82 FR 55332
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

82 FR 55332 - Airworthiness Directives; Pilatus Aircraft Limited Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 82, Issue 223 (November 21, 2017)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration