81 FR 75687 - Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 211 (November 1, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 211 (November 1, 2016)
| Page Range | 75687-75689 | |
| FR Document | 2016-26184 |
[Federal Register Volume 81, Number 211 (Tuesday, November 1, 2016)] [Rules and Regulations] [Pages 75687-75689] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-26184] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-6990; Directorate Identifier 2016-NE-14-AD; Amendment 39-186990; AD 2016-22-10] RIN 2120-AA64 Airworthiness Directives; Turbomeca S.A. Turboshaft Engines AGENCY: Federal Aviation Administration (FAA), DOT. [[Page 75688]] ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Arriel 1, 1A, 1A1, 1A2, 1B, 1B2, 1C, 1C1, 1C2, 1D, 1D1, 1E, 1E2, 1K1, 1S, and 1S1 turboshaft engines. This AD requires removing the centrifugal impeller and replacing with a part eligible for installation. This AD was prompted by an anomaly that occurred during the grinding operation required by modification TU376, which increases the clearance between the rear curvic coupling of the centrifugal impeller and the fuel injection manifold. We are issuing this AD to prevent failure of the centrifugal impeller, uncontained centrifugal impeller release, damage to the engine, and damage to the helicopter. DATES: This AD becomes effective December 6, 2016. ADDRESSES: See the FOR FURTHER INFORMATION CONTACT section. 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-2016- 6990; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the mandatory continuing airworthiness information (MCAI), the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Philip Haberlen, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7770; fax: 781- 238-7199; email: [email protected]. 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 the specified products. The NPRM was published in the Federal Register on July 28, 2016 (81 FR 49575). The NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: Turbomeca reported an anomaly that was generated during the grinding operation associated to the application of modification TU376, which increases the clearance between the rear curvic coupling of the centrifugal impeller and the fuel injection manifold. This condition, if not corrected, could lead to crack initiation and propagation in the centrifugal impeller bore area, possibly resulting in centrifugal impeller failure, with consequent damage to, and reduced control of, the helicopter. To address this potential unsafe condition, the life of the affected centrifugal impellers was reduced and Turbomeca published Mandatory Service Bulletin (MSB) 292 72 0848 to inform operators about the life reduction and to provide instructions for the replacement of the affected centrifugal impellers. For the reasons described above, this AD requires replacement of each affected centrifugal impeller before it exceeds the applicable reduced life limit. You may obtain further information by examining the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-6990. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM (81 FR 49575, July 28, 2016) or on the determination of the cost to the public. Conclusion We reviewed the available data and determined that air safety and the public interest require adopting this AD as proposed. Related Service Information Turbomeca S.A. has issued Mandatory Service Bulletin (MSB) 292 72 0848, Version B, dated April 13, 2016. The MSB describes procedures for reducing the life limit of the centrifugal impellers affected by an anomaly that occurred during the grinding operation required by modification TU376. 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 3 engines installed on helicopters of U.S. registry. We also estimate that it would take about 22 hours per engine to comply with this AD. The average labor rate is $85 per hour. Required parts cost about $96,518 per engine. Based on these figures, we estimate the cost of this AD on U.S. operators to be $295,164. 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. 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 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 to the extent that it justifies making a regulatory distinction, 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. [[Page 75689]] Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2016-22-10 Turbomeca S.A.: Amendment 39-186990; Docket No. FAA-2016- 6990; Directorate Identifier 2016-NE-14-AD. (a) Effective Date This AD becomes effective December 6, 2016. (b) Affected ADs None. (c) Applicability This AD applies to certain Arriel 1, 1A, 1A1, 1A2, 1B, 1B2, 1C, 1C1, 1C2, 1D, 1D1, 1E, 1E2, 1K1, 1S, and 1S1 turboshaft engines, with modification TU376 installed. (d) Reason This AD was prompted by an anomaly that occurred during the grinding operation required by modification TU376, which increases the clearance between the rear curvic coupling of the centrifugal impeller and the fuel injection manifold. We are issuing this AD to prevent failure of the centrifugal impeller, uncontained centrifugal impeller release, damage to the engine, and damage to the helicopter. (e) Actions and Compliance Comply with this AD within the compliance times specified, unless already done. (1) Remove from service, any centrifugal impeller listed in Table 1 to paragraph (e) of this AD, before exceeding the applicable cycles since new (CSN) and replace with a centrifugal impeller not listed in Table 1 to paragraph (e) of this AD. Table 1 to Paragraph (e)--Centrifugal Impeller CSNs ------------------------------------------------------------------------ Part No. Serial No. CSN ------------------------------------------------------------------------ 0292254040...................................... 44 5,129 0292254040...................................... 1762FT 11,476 0292254050...................................... 1676CAR 6,281 0292254050...................................... 5333OTT 5,495 0292254050...................................... 5017OTT 5,491 0292254050...................................... 1136CAR 8,734 0292254050...................................... 3655OTT 4,600 0292254050...................................... 1757CAR 7,913 0292254050...................................... 1738CAR 10,640 0292254050...................................... 1149CAR 12,273 0292254050...................................... 2677OTT 11,145 0292254050...................................... 3109OTT 10,662 0292254050...................................... 3496OTT 5,562 0292254050...................................... 2074CAR 7,423 729225293A...................................... 290CAR 6,326 729225293A...................................... 1227FT 8,139 729225293A...................................... 504FB 4,600 729225293A...................................... 2517OTT 9,732 729225293A...................................... 2165OTT 6,163 729225293A...................................... 2194FT 11,461 729225293A...................................... 1331OTT 12,513 729225293A...................................... 1301FT 7,262 729225293A...................................... 1567FT 6,305 729225293A...................................... 783FB 8,307 729225293A...................................... 98OTT 9,492 ------------------------------------------------------------------------ (2) Reserved. (f) Alternative Methods of Compliance (AMOCs) The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: [email protected]. (g) Related Information (1) For more information about this AD, contact Philip Haberlen, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7770; fax: 781-238-7199; email: [email protected]. (2) Refer to MCAI, European Aviation Safety Agency AD 2016-0090, dated May 10, 2016, for more information. You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2016-6990. (h) Material Incorporated by Reference None. Issued in Burlington, Massachusetts, on October 24, 2016. Colleen M. D'Alessandro, Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2016-26184 Filed 10-31-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 211 / Tuesday, November 1, 2016 / Rules and Regulations 75687
Aviation Programs, describes in more FAA–2016–5423; Directorate Identifier A, paragraph 4.B., or Part B, paragraph 1.B.
detail the scope of the Agency’s 2016–NE–09–AD. of PW ASB PW4G–100–A73–45, dated
authority. February 16, 2016.
(a) Effective Date
We are issuing this rulemaking under This AD is effective December 6, 2016. (g) Alternative Methods of Compliance
the authority described in Subtitle VII, (AMOCs)
Part A, Subpart III, Section 44701: (b) Affected ADs The Manager, Engine Certification Office,
‘‘General requirements.’’ Under that None. FAA, may approve AMOCs for this AD. Use
section, Congress charges the FAA with the procedures found in 14 CFR 39.19 to
(c) Applicability
promoting safe flight of civil aircraft in make your request. You may email your
This AD applies to Pratt & Whitney (PW): request to: ANE-AD-AMOC@faa.gov.
air commerce by prescribing regulations
(1) PW4164, PW4168, and PW4168A
for practices, methods, and procedures model engines that have incorporated PW (h) Related Information
the Administrator finds necessary for Service Bulletin (SB) PW4G–100–72–214, For more information about this AD,
safety in air commerce. This regulation dated December 15, 2011, or PW SB PW4G– contact Besian Luga, Aerospace Engineer,
is within the scope of that authority 100–72–219, Revision No. 1, dated October 5, Engine Certification Office, FAA, Engine &
because it addresses an unsafe condition 2011, or original issue, and have fuel nozzles, Propeller Directorate, 1200 District Avenue,
that is likely to exist or develop on part number (P/N) 51J345, installed; Burlington, MA 01803; phone: 781–238–
products identified in this rulemaking (2) PW4168A model engines with Talon 7750; fax: 781–238–7199; email:
IIA outer combustion chamber assembly, P/ besian.luga@faa.gov.
action.
N 51J100, and fuel nozzles, P/N 51J345, with
serial numbers CGGUA19703 through (i) Material Incorporated by Reference
Regulatory Findings
CGGUA19718 inclusive or CGGUA22996 and (1) The Director of the Federal Register
This AD will not have federalism higher, installed; approved the incorporation by reference
implications under Executive Order (3) PW4168A–1D and PW4170 model (IBR) of the service information listed in this
13132. This AD will not have a engines with engine serial numbers P735001 paragraph under 5 U.S.C. 552(a) and 1 CFR
substantial direct effect on the States, on thru P735190 inclusive and fuel nozzles, P/ part 51.
the relationship between the national N 51J345, installed; and (2) You must use this service information
government and the States, or on the (4) PW4164–1D, PW4168–1D, PW4168A– as applicable to do the actions required by
1D, and PW4170 model engines that have this AD, unless the AD specifies otherwise.
distribution of power and
incorporated PW SB PW4G–100–72–220, (i) Pratt & Whitney (PW) Alert Service
responsibilities among the various Revision No. 4, dated September 30, 2011, or Bulletin PW4G–100–A73–45, dated February
levels of government. earlier revision, and have fuel nozzles, P/N 16, 2016.
For the reasons discussed above, I 51J345, installed. (ii) Reserved.
certify that this AD: (3) For PW service information identified
(1) Is not a ‘‘significant regulatory (d) Unsafe Condition in this AD, contact Pratt & Whitney Division,
action’’ under Executive Order 12866, This AD was prompted by nine instances 400 Main St., East Hartford, CT 06108;
(2) Is not a ‘‘significant rule’’ under of fuel leaks on PW engines with the Talon phone: 860–565–8770; fax: 860–565–4503.
DOT Regulatory Policies and Procedures IIB combustion chamber configuration (4) You may view this service information
(44 FR 11034, February 26, 1979), installed. We are issuing this AD to prevent at FAA, Engine & Propeller Directorate, 1200
failure of the fuel nozzles, which could lead District Avenue, Burlington, MA. For
(3) Will not affect intrastate aviation
to engine fire and damage to the airplane. information on the availability of this
in Alaska to the extent that it justifies material at the FAA, call 781–238–7125.
making a regulatory distinction, and (e) Compliance
(5) You may view this service information
(4) Will not have a significant Comply with this AD within the at the National Archives and Records
economic impact, positive or negative, compliance times specified, unless already Administration (NARA). For information on
on a substantial number of small entities done. the availability of this material at NARA, call
under the criteria of the Regulatory (1) Within 800 flight hours after the 202–741–6030, or go to: http://
Flexibility Act. effective date of this AD, and thereafter www.archives.gov/federal-register/cfr/ibr-
within every 800 flight hours accumulated on locations.html.
List of Subjects in 14 CFR Part 39 the fuel nozzles, do the following:
Issued in Burlington, Massachusetts, on
(i) Inspect all fuel nozzles, P/N 51J345. Use
Air transportation, Aircraft, Aviation Part A of PW Alert Service Bulletin (ASB) October 25, 2016.
safety, Incorporation by reference, PW4G–100–A73–45, dated February 16, Colleen M. D’Alessandro,
Safety. 2016, to do the inspection. Manager, Engine & Propeller Directorate,
(ii) For any fuel nozzle that fails the Aircraft Certification Service.
Adoption of the Amendment inspection, before further flight, remove and [FR Doc. 2016–26183 Filed 10–31–16; 8:45 am]
Accordingly, under the authority replace it with a part that is eligible for
BILLING CODE 4910–13–P
delegated to me by the Administrator, installation.
the FAA amends 14 CFR part 39 as (2) At the next shop visit after the effective
follows: date of this AD, and thereafter at each engine
shop visit, remove all fuel nozzles, P/N DEPARTMENT OF TRANSPORTATION
PART 39—AIRWORTHINESS 51J345, unless fuel nozzles were replaced
within the last 100 flight hours. Use Part B Federal Aviation Administration
DIRECTIVES
of PW ASB PW4G–100–A73–45, dated
February 16, 2016, to replace the fuel nozzles 14 CFR Part 39
■ 1. The authority citation for part 39
with parts eligible for installation.
continues to read as follows: [Docket No. FAA–2016–6990; Directorate
(f) Definitions Identifier 2016–NE–14–AD; Amendment 39–
Authority: 49 U.S.C. 106(g), 40113, 44701. 186990; AD 2016–22–10]
jstallworth on DSK7TPTVN1PROD with RULES
(1) For the purpose of this AD, an ‘‘engine
§ 39.13 [Amended] shop visit’’ means the induction of an engine RIN 2120–AA64
■ 2. The FAA amends § 39.13 by adding into the shop for any maintenance.
(2) For the purpose of this AD, a part that Airworthiness Directives; Turbomeca
the following new airworthiness
is ‘‘eligible for installation’’ is a fuel nozzle, S.A. Turboshaft Engines
directive (AD): with a P/N other than 51J345, that is FAA-
2016–22–05 Pratt & Whitney Division: approved for installation or a fuel nozzle, P/ AGENCY:Federal Aviation
Amendment 39–18694; Docket No. N 51J345, that meets the requirements of Part Administration (FAA), DOT.
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![Federal Register / Vol. 81, No. 211 / Tuesday, November 1, 2016 / Rules and Regulations 75689
§ 39.13 [Amended] (2) Reserved. Electronic Submissions
■ 2. The FAA amends § 39.13 by adding (f) Alternative Methods of Compliance Submit electronic objections in the
the following new airworthiness (AMOCs) following way:
directive (AD): The Manager, Engine Certification Office, • Federal eRulemaking Portal: http://
2016–22–10 Turbomeca S.A.: Amendment FAA, may approve AMOCs for this AD. Use www.regulations.gov. Follow the
39–186990; Docket No. FAA–2016–6990; the procedures found in 14 CFR 39.19 to instructions for submitting comments.
Directorate Identifier 2016–NE–14–AD. make your request. You may email your Objections submitted electronically,
request to: ANE-AD-AMOC@faa.gov.
(a) Effective Date
including attachments, to http://
(g) Related Information www.regulations.gov will be posted to
This AD becomes effective December 6, the docket unchanged. Because your
(1) For more information about this AD,
2016.
contact Philip Haberlen, Aerospace Engineer, objection will be made public, you are
(b) Affected ADs Engine Certification Office, FAA, Engine & solely responsible for ensuring that your
Propeller Directorate, 1200 District Avenue, objection does not include any
None.
Burlington, MA 01803; phone: 781–238–
confidential information that you or a
(c) Applicability 7770; fax: 781–238–7199; email:
philip.haberlen@faa.gov. third party may not wish to be posted,
This AD applies to certain Arriel 1, 1A, such as medical information, your or
1A1, 1A2, 1B, 1B2, 1C, 1C1, 1C2, 1D, 1D1, (2) Refer to MCAI, European Aviation
Safety Agency AD 2016–0090, dated May 10, anyone else’s Social Security number, or
1E, 1E2, 1K1, 1S, and 1S1 turboshaft engines,
with modification TU376 installed.
2016, for more information. You may confidential business information, such
examine the MCAI in the AD docket on the as a manufacturing process. Please note
(d) Reason Internet at http://www.regulations.gov by that if you include your name, contact
This AD was prompted by an anomaly that searching for and locating it in Docket No. information, or other information that
FAA–2016–6990.
occurred during the grinding operation identifies you in the body of your
required by modification TU376, which (h) Material Incorporated by Reference objection, that information will be
increases the clearance between the rear None. posted on http://www.regulations.gov.
curvic coupling of the centrifugal impeller • If you want to submit an objection
and the fuel injection manifold. We are Issued in Burlington, Massachusetts, on
issuing this AD to prevent failure of the October 24, 2016. with confidential information that you
centrifugal impeller, uncontained centrifugal Colleen M. D’Alessandro, do not wish to be made available to the
impeller release, damage to the engine, and Manager, Engine & Propeller Directorate,
public, submit the objection as a
damage to the helicopter. Aircraft Certification Service. written/paper submission and in the
[FR Doc. 2016–26184 Filed 10–31–16; 8:45 am]
manner detailed (see ‘‘Written/Paper
(e) Actions and Compliance
Submissions’’ and ‘‘Instructions’’).
Comply with this AD within the BILLING CODE 4910–13–P
compliance times specified, unless already Written/Paper Submissions
done. Submit written/paper submissions as
(1) Remove from service, any centrifugal DEPARTMENT OF HEALTH AND
impeller listed in Table 1 to paragraph (e) of
follows:
HUMAN SERVICES • Mail/Hand delivery/Courier (for
this AD, before exceeding the applicable
cycles since new (CSN) and replace with a Food and Drug Administration written/paper submissions): Division of
centrifugal impeller not listed in Table 1 to Dockets Management (HFA–305), Food
paragraph (e) of this AD. 21 CFR Parts 73 and 74 and Drug Administration, 5630 Fishers
Lane, Rm. 1061, Rockville, MD 20852.
TABLE 1 TO PARAGRAPH (e)— [Docket No. FDA–2016–F–0821] • For written/paper objections
CENTRIFUGAL IMPELLER CSNS submitted to the Division of Dockets
Listing of Color Additives Exempt Management, FDA will post your
Part No. Serial No. CSN
From Certification; Titanium Dioxide objection, as well as any attachments,
and Listing of Color Additives Subject except for information submitted,
0292254040 .......... 44 5,129 to Certification; [Phthalocyaninato (2-)] marked and identified, as confidential,
0292254040 .......... 1762FT 11,476 Copper if submitted as detailed in
0292254050 .......... 1676CAR 6,281
AGENCY: Food and Drug Administration, ‘‘Instructions.’’
0292254050 .......... 5333OTT 5,495
0292254050 .......... 5017OTT 5,491 HHS. Instructions: All submissions received
0292254050 .......... 1136CAR 8,734 ACTION: Final rule. must include the Docket No. FDA–
0292254050 .......... 3655OTT 4,600 2016–F–0821 for ‘‘Listing of Color
0292254050 .......... 1757CAR 7,913 SUMMARY: The Food and Drug Additives Exempt From Certification;
0292254050 .......... 1738CAR 10,640 Administration (FDA or we) is Titanium Dioxide and Listing of Color
0292254050 .......... 1149CAR 12,273 amending the color additive regulations Additives Subject to Certification;
0292254050 .......... 2677OTT 11,145 to provide for the safe use of titanium [Phthalocyaninato (2-)] Copper.’’
0292254050 .......... 3109OTT 10,662 dioxide and [phthalocyaninato (2-)] Received objections will be placed in
0292254050 .......... 3496OTT 5,562 copper to color orientation marks for the docket and, except for those
0292254050 .......... 2074CAR 7,423 intraocular lenses. This action is in
729225293A ......... 290CAR 6,326 submitted as ‘‘Confidential
response to a petition filed by Milton W. Submissions,’’ publicly viewable at
729225293A ......... 1227FT 8,139
729225293A ......... 504FB 4,600
Chu, M.D. http://www.regulations.gov or at the
729225293A ......... 2517OTT 9,732 DATES: This rule is effective December 2, Division of Dockets Management
jstallworth on DSK7TPTVN1PROD with RULES
729225293A ......... 2165OTT 6,163 2016. See section IX for further between 9 a.m. and 4 p.m., Monday
729225293A ......... 2194FT 11,461 information on the filing of objections. through Friday.
729225293A ......... 1331OTT 12,513 Submit either electronic or written • Confidential Submissions—To
729225293A ......... 1301FT 7,262 objections and requests for a hearing by submit an objection with confidential
729225293A ......... 1567FT 6,305 December 1, 2016. information that you do not wish to be
729225293A ......... 783FB 8,307
729225293A ......... 98OTT 9,492
ADDRESSES: You may submit objections made publicly available, submit your
and requests for a hearing as follows: objections only as a written/paper
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Document Created: 2016-11-01 02:36:37
Document Modified: 2016-11-01 02:36:37
| 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 | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD becomes effective December 6, 2016. | |
| Contact | Philip Haberlen, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7770; fax: 781- 238-7199; email: [email protected] | |
| FR Citation | 81 FR 75687 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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