text:
Q: Is there anything wrong with FileWriter? I don't know what's going on with the FileWriter, because it only writes out the HTML part, but nothing from the String array content. content stores a lot of long Strings. Is it because of Java's garbage collector?
I print out the content and everything is there, but FileWrter did not write anything from content to that file except the HTML part. I added System.out.println(k); inside the enhanced for-loop. content array is not null though.
public void writeHtml(String[] content) {
    File file = new File("final.html");
    try {
        try (FileWriter Fw = new FileWriter(file)) {
            Fw.write("<!DOCTYPE html PUBLIC \"-//W3C//DTD HTML 4.01 Transitional//EN\">\n"
                    + "\n"
                    + "\n"
                    + "<meta http-equiv=\"Content-Type\" content=\"text/html; charset=us-ascii\">\n"
                    + "<title>" + fileName +" for  The Delinquent</title>\n"
                    + "\n"
                    + "");
            for (String k : content) {
                Fw.write(k+"\n");
            }
            Fw.write("");
        }

    } catch (Exception e) {
        e.printStackTrack();
    }
}

How the final.html looks like after running the program:
<!DOCTYPE html PUBLIC "-//W3C//DTD HTML 4.01 Transitional//EN">

<meta http-equiv="Content-Type" content="text/html; charset=us-ascii">
<title>the_delinquent.txt for  The Delinquent</title>

I know content is not empty because I did this:
 for (String k: content) {
                System.out.println(k + "\n");
                bw.write(k + "\n");
            }

Everything printed out. so weird : (

A: You code is working. The only thing that prevents content to be written - empty content. It has no elements.

A: Your code iis basically correct, maybe the content array is empty.
The following is in modernized java style.
public void writeHtml(String[] content) {
    Path file = Paths.get("final.html");
    try (BufferedWriter fw = Files.newBufferedWriter(file, StandardCharsets.UTF_8)) {
        fw.write("<!DOCTYPE html>\n"
                + "\n"
                + "\n"
                + "<meta charset=UTF-8\">\n"
                + "<title>" + fileName + " for  The Delinquent</title>\n"
                + "\n"
                + "");
        fw.write("Content has: " + content.length + " strings.
\n");
        for (String k : content) {
            fw.write("* " + k + "
\n");
        }
        fw.write("\n");
    } catch (IOException e) {
        System.out.println("Error " + e.getMessage());
    }
}

*

*FileWriter is an old utility class that uses the default charset, so not portable. Better specify the charset to correspond to the charset in HTML.

*The encoding UTF-8 allows full Unicode range of characters, like comma like quotes (typical to MS Word). Java internally also uses Unicode, so it is a fine match.

*HTML 5 is the latest HTML version, now generally disposable.

*At one spot a typo /n entered.

*Multiple spaces and line breaks are converted to a single space. So I added
 for a line break.

Normally one would add to the method header throws IOException to let the caller handle any irregularities.

redpajama_set_name: RedPajamaStackExchange


text:
Justia Regulation Tracker Department Of Transportation Federal Aviation Administration Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes, 3143-3146 [2016-31958]
Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes, 3143-3146 [2016-31958]
Download as PDF Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Rules and Regulations Before the accumulation of 18,000 total flight cycles, or within 13 years after the effective date of this AD, whichever occurs first, do the inspections specified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD, and all applicable corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787–81205–SB570018–00, Issue 001, dated July 1, 2015, except as required by paragraph (i) of this AD. Do all applicable corrective actions before further flight. (1) Do a detailed inspection for a machine mismatch condition of the stringer 1 fitting faying surface. (2) Do a detailed inspection of the faying surface of the aluminum T-chord common to the stringer 1 fitting for fretting damage. (3) Do an eddy current inspection for cracking of the fastener holes common to stringer fitting 1 and stringer fittings 5 through 11. (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (4) Except as required by paragraph (i) of this AD: For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (j)(4)(i) and (j)(4)(ii) apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (h) Modification, Inspection, and Repair (k) Related Information Concurrently with accomplishment of the requirements of paragraph (g) of this AD: Modify the stringer fitting fasteners, and do an eddy current inspection for cracking of the fastener holes, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787–81205–SB570018–00, Issue 001, dated July 1, 2015. If any crack is found, before further flight, repair using a method approved in accordance with the procedures specified in paragraph (j) of this AD. For more information about this AD, contact Allen Rauschendorfer, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425–917–6487; fax: 425– 917–6590; email: allen.rauschendorfer@ faa.gov. adversely affect the structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection and Corrective Actions sradovich on DSK3GMQ082PROD with RULES (i) Exception to Service Information Specifications Where Boeing Alert Service Bulletin B787– 81205–SB570018–00, Issue 001, dated July 1, 2015, specifies to contact Boeing for repair of cracking: Before further flight, repair the cracking using a method approved in accordance with the procedures specified in paragraph (j) of this AD. (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in paragraph (k)(1) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. VerDate Sep<11>2014 15:58 Jan 10, 2017 Jkt 241001 (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing Alert Service Bulletin B787– 81205–SB570018–00, Issue 001, dated July 1, 2015. (ii) Reserved. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110–SK57, Seal Beach, CA 90740; telephone 562–797–1717; Internet https:// www.myboeingfleet.com. (4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. PO 00000 Frm 00013 Fmt 4700 Sfmt 4700 3143 Issued in Renton, Washington, on December 15, 2016. Victor Wicklund, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016–31188 Filed 1–10–17; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2016–9113; Directorate Identifier 2016–NM–042–AD; Amendment 39–18772; AD 2017–01–05] RIN 2120–AA64 Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: We are adopting a new airworthiness directive (AD) for all Airbus Defense and Space S.A. Model CN–235, CN–235–100, CN 235–200, and CN–235–300 airplanes. This AD was prompted by reports of cracks in certain areas of the rear fuselage. This AD requires repetitive borescope and detailed visual inspections of the rear fuselage lateral beam and its external area, and repair if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective February 15, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publications listed in this AD as of February 15, 2017. ADDRESSES: For service information identified in this final rule, contact Airbus Defence and Space, Services/ Engineering Support, Avenida de ´ Aragon 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 31 27; email MTA.TechnicalService@Airbus.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. It is also available on the Internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2016– 9113. SUMMARY: E:\FR\FM\11JAR1.SGM 11JAR1 3144 Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Rules and Regulations Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2016– 9113; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone 800–647– 5527) is Docket Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM– 116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227– 1112; fax 425–227–1149. 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 all Airbus Defense and Space S.A. Model CN–235, CN–235–100, CN– 235–200, and CN–235–300 airplanes. The NPRM published in the Federal Register on September 29, 2016 (81 FR 66872). The NPRM was prompted by reports of cracks in certain areas of the rear fuselage. The NPRM proposed to require repetitive borescope and detailed visual inspections of the rear fuselage lateral beam and its external area, and repair if necessary. We are issuing this AD to address the unsafe condition on these products. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued Airworthiness Directive 2016–0064, dated April 4, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or ''the MCAI''), to correct an unsafe condition for all Airbus Defense and Space S.A. Model CN–235, CN–235–100, CN–235–200, and CN– 235–300 airplanes. The MCAI states: During a scheduled visual inspection accomplished in accordance with the CN– 235 Maintenance Review Board (MRB) Document task 53.160, cracking was found, affecting the rear fuselage lateral beam, both left hand (LH) and right hand (RH) sides. The investigation to determine the cause of these cracks is on-going. This condition, if not detected and corrected, could lead to failure of the affected components, resulting in reduced structural integrity of the fuselage. To address this potential unsafe condition, Airbus Defence and Space (D&S) issued Alert Operator Transmission (AOT) AOT–CN235– 53–0002 Revision 1 (hereafter referred to as 'the AOT' in this AD) to provide inspection instructions. For the reasons described above, this [EASA] AD requires repetitive inspections [special detailed inspection with a borescope and detailed visual] of the rear fuselage lateral beam and its external area and, depending on findings, [cracks or discrepancies], accomplishment of applicable corrective action(s) [repair]. You may examine the MCAI in the AD docket on the Internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2016– 9113. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public. Conclusion We reviewed the relevant data and determined that air safety and the public interest require adopting this AD as proposed except for minor editorial changes. We have determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for correcting 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 We reviewed Airbus Defense and Space Alert Operators Transmission (AOT), AOT–CN235–53–0002, Revision 1, dated September 17, 2015. This service information describes repetitive borescope and detailed visual inspection requirements for the rear fuselage lateral beam and its external area. 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 13 airplanes of U.S. registry. We estimate the following costs to comply with this AD: ESTIMATED COSTS Action Labor cost Inspection ................................ 2 work-hours × $85 per hour = $170 ..................................... We have received no definitive data that will enable us to provide cost estimates for the on-condition actions specified in this AD. sradovich on DSK3GMQ082PROD with RULES 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, VerDate Sep<11>2014 15:58 Jan 10, 2017 Jkt 241001 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. PO 00000 Frm 00014 Fmt 4700 Cost per product Parts cost Sfmt 4700 $0 $170 Cost on U.S. operators $2,210 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; E:\FR\FM\11JAR1.SGM 11JAR1 Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Rules and Regulations 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: § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ 2017–01–05 Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.): Amendment 39– 18772; Docket No. FAA–2016–9113; Directorate Identifier 2016–NM–042–AD. (a) Effective Date This AD is effective February 15, 2017. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Defense and Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model CN–235, CN–235–100, CN–235–200, and CN–235–300 airplanes, certificated in any category, all manufacturer serial numbers. (d) Subject Air Transport Association (ATA) of America Code 53, Fuselage. 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. (e) Reason This AD was prompted by reports of cracks in certain areas of the rear fuselage. We are issuing this AD to detect and correct cracks 3145 in the rear fuselage lateral beam and its external area; such cracking could lead to failure of the affected components, and result in reduced structural integrity of the fuselage. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Repetitive Inspections on the Fuselage Lateral Beam Within the compliance time specified in table 1 to paragraph (g) of this AD, and thereafter at intervals not to exceed the values specified in table 2 to paragraph (g) of this AD, as applicable to airplane model, accomplish the inspections as specified in paragraphs (g)(1) and (g)(2) of this AD, in accordance with the instructions of Airbus Defense and Space Alert Operators Transmission (AOT) AOT–CN235–53–0002, Revision 1, dated September 17, 2015. (1) A special detailed inspection for cracks and other discrepancies with a borescope of the rear fuselage lateral beam between frame (FR) 31 and FR 45, left-hand (LH) and righthand (RH) side. (2) A detailed visual inspection for cracks and other discrepancies of the external area of the rear fuselage lateral beam, LH and RH side. TABLE 1 TO PARAGRAPH (g) OF THIS AD—INITIAL INSPECTION COMPLIANCE TIME A or B, whichever occurs later A ........................................... B ........................................... Before exceeding 15,000 flight cycles or 15,000 flight hours, whichever occurs first since airplane first flight. Within 50 flight cycles or 50 flight hours, whichever occurs first after the effective date of this AD. TABLE 2 TO PARAGRAPH (g) OF THIS AD—REPETITIVE INSPECTION INTERVALS Repetitive interval (whichever occurs first, flight cycles or flight hours) Airplane models Model CN–235 and CN–235–100 airplanes ............................................ Model CN–235–200 airplanes .................................................................. Model CN–235–300 airplanes .................................................................. (h) Repair sradovich on DSK3GMQ082PROD with RULES If any crack or discrepancy is found during any inspection required by paragraph (g) of this AD: Before further flight, contact and obtain repair instructions from Airbus Defense and Space S.A. in accordance with paragraph (k)(2) of this AD, and within the compliance time indicated in those instructions, accomplish the repair accordingly, including any post-repair maintenance task(s), as applicable. (i) Continued Inspection of Repaired Areas Accomplishment of a repair on an airplane, as required by paragraph (h) of this AD, does not constitute terminating action for the repetitive inspections as required by paragraph (g) of this AD for that airplane, unless specified in the applicable repair instructions obtained in paragraph (h). (j) Credit for Previous Actions This paragraph provides credit for actions required by paragraphs (g) and (h) of this AD, VerDate Sep<11>2014 15:58 Jan 10, 2017 Jkt 241001 3,600 flight cycles or 3,100 flight hours. 3,600 flight cycles or 2,800 flight hours. 15,000 flight cycles or 15,000 flight hours. if those actions were performed before the effective date of this AD, using Airbus Defense and Space AOT AOT–CN235–53– 0002, dated August 28, 2015. (k) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM–116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1112; fax 425–227–1149. PO 00000 Frm 00015 Fmt 4700 Sfmt 4700 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 Branch, ANM– 116, Transport Airplane Directorate, FAA; or EASA; or Airbus Defense and Space S.A.'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 Airworthiness Directive 2016–0064, dated April 4, 2016, for related information. This MCAI may be found in the AD docket on the Internet at https://www.regulations.gov by E:\FR\FM\11JAR1.SGM 11JAR1 3146 Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Rules and Regulations searching for and locating Docket No. FAA– 2016–9113. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (m)(3) and (m)(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) Airbus Defense and Space Alert Operators Transmission (AOT), AOT– CN235–53–0002, Revision 1, dated September 17, 2015. (ii) Reserved. (3) For service information identified in this AD, contact EADS–CASA, Military Transport Aircraft Division (MTAD), Integrated Customer Services (ICS), ´ Technical Services, Avenida de Aragon 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 55 05; email MTA.TechnicalService@casa.eads.net; Internet https://www.eads.net. (4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on December 27, 2016. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016–31958 Filed 1–10–17; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2013–1015; Directorate Identifier 2013–NE–37–AD; Amendment 39– 18768; AD 2017–01–01] RIN 2120–AA64 sradovich on DSK3GMQ082PROD with RULES Airworthiness Directives; Rolls-Royce plc Turbofan Engines Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. AGENCY: Examining the AD Docket We are superseding airworthiness directive (AD) 2014–05– 25 for all Rolls-Royce plc (RR) RB211- SUMMARY: VerDate Sep<11>2014 15:58 Jan 10, 2017 Jkt 241001 Trent 970–84, RB211-Trent 970B–84, RB211-Trent 972–84, RB211-Trent 972B–84, RB211-Trent 977–84, RB211Trent 977B–84, and RB211-Trent 980– 84 turbofan engines. AD 2014–05–25 required inspections of the low-pressure turbine (LPT) exhaust case and support assembly or tail bearing housing (TBH) to detect cracks or damage. This AD modifies the inspection schedule for the affected engines and adds an optional terminating action. This AD was prompted by RR performing additional analysis of inspection results and determining that the existing inspections need to be modified. We are issuing this AD to correct the unsafe condition on these products. DATES: This AD is effective January 26, 2017. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of January 26, 2017. We must receive any comments on this AD by February 27, 2017. 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. • 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– 1332–245418, or email: https:// www.rolls-royce.com/contact/civil_ team.jsp. You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781–238–7125. It is also available on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2013– 1015. You may examine the AD docket on the Internet at https:// www.regulations.gov by searching for PO 00000 Frm 00016 Fmt 4700 Sfmt 4700 and locating Docket No. FAA–2013– 1015; 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, regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800–647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781–238–7754; fax: 781–238–7199; email: robert.green@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ''Docket No. FAA– 2013–1015; Directorate Identifier 2013– NE–37–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 https:// 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. Discussion On February 27, 2014, we issued AD 2014–05–25, Amendment 39–17798 (79 FR 15665, March 21, 2014), ''AD 2014– 05–25,'' for all RR RB211-Trent 970–84, RB211-Trent 970B–84, RB211-Trent 972–84, RB211-Trent 972B–84, RB211Trent 977–84, RB211-Trent 977B–84, and RB211-Trent 980–84 turbofan engines. AD 2014–05–25 required inspections of the LPT exhaust case and support assembly or TBH to detect cracks or damage. AD 2014–05–25 resulted from an RR structural reanalysis indicating that the TBH may not retain full limit load capability in all fail-safe conditions. We issued AD 2014–05–25 to prevent failure of the E:\FR\FM\11JAR1.SGM 11JAR1
[Federal Register Volume 82, Number 7 (Wednesday, January 11, 2017)]
[Rules and Regulations]
[Pages 3143-3146]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[Docket No. FAA-2016-9113; Directorate Identifier 2016-NM-042-AD;
Amendment 39-18772; AD 2017-01-05]
RIN 2120-AA64
Airworthiness Directives; Airbus Defense and Space S.A. (Formerly
Known as Construcciones Aeronauticas, S.A.) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN 235-200, and
CN-235-300 airplanes. This AD was prompted by reports of cracks in
certain areas of the rear fuselage. This AD requires repetitive
borescope and detailed visual inspections of the rear fuselage lateral
beam and its external area, and repair if necessary. We are issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective February 15, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publications listed in this AD as of February
ADDRESSES: For service information identified in this final rule,
contact Airbus Defence and Space, Services/Engineering Support, Avenida
de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84;
fax +34 91 585 31 27; email MTA.TechnicalService@Airbus.com. You may
view this referenced service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call 425-227-1221. It is also
available on the Internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2016-9113.
[[Page 3144]]
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9113; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is Docket Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone 425-227-1112; fax 425-227-1149.
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to all Airbus Defense and
Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300
airplanes. The NPRM published in the Federal Register on September 29,
2016 (81 FR 66872). The NPRM was prompted by reports of cracks in
certain areas of the rear fuselage. The NPRM proposed to require
repetitive borescope and detailed visual inspections of the rear
fuselage lateral beam and its external area, and repair if necessary.
We are issuing this AD to address the unsafe condition on these
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued
Airworthiness Directive 2016-0064, dated April 4, 2016 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for all Airbus Defense
and Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300
airplanes. The MCAI states:
During a scheduled visual inspection accomplished in accordance
with the CN-235 Maintenance Review Board (MRB) Document task 53.160,
cracking was found, affecting the rear fuselage lateral beam, both
left hand (LH) and right hand (RH) sides. The investigation to
determine the cause of these cracks is on-going.
This condition, if not detected and corrected, could lead to
failure of the affected components, resulting in reduced structural
integrity of the fuselage.
To address this potential unsafe condition, Airbus Defence and
Space (D&S) issued Alert Operator Transmission (AOT) AOT-CN235-53-
0002 Revision 1 (hereafter referred to as `the AOT' in this AD) to
provide inspection instructions.
For the reasons described above, this [EASA] AD requires
repetitive inspections [special detailed inspection with a borescope
and detailed visual] of the rear fuselage lateral beam and its
external area and, depending on findings, [cracks or discrepancies],
accomplishment of applicable corrective action(s) [repair].
You may examine the MCAI in the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2016-
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for correcting 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
We reviewed Airbus Defense and Space Alert Operators Transmission
(AOT), AOT-CN235-53-0002, Revision 1, dated September 17, 2015. This
service information describes repetitive borescope and detailed visual
inspection requirements for the rear fuselage lateral beam and its
external area. 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 13 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Cost per      Cost on U.S.
Action                         Labor cost            Parts cost        product        operators
Inspection.........................  2 work-hours x $85 per hour              $0            $170          $2,210
= $170.
We have received no definitive data that will enable us to provide
cost estimates for the on-condition actions specified in this AD.
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
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 that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
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
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]
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive (AD):
2017-01-05 Airbus Defense and Space S.A. (Formerly Known as
Construcciones Aeronauticas, S.A.): Amendment 39-18772; Docket No.
FAA-2016-9113; Directorate Identifier 2016-NM-042-AD.
(a) Effective Date
This AD is effective February 15, 2017.
(b) Affected ADs
(c) Applicability
This AD applies to Airbus Defense and Space S.A. (formerly known
as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-
235-200, and CN-235-300 airplanes, certificated in any category, all
manufacturer serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Reason
This AD was prompted by reports of cracks in certain areas of
the rear fuselage. We are issuing this AD to detect and correct
cracks in the rear fuselage lateral beam and its external area; such
cracking could lead to failure of the affected components, and
result in reduced structural integrity of the fuselage.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Repetitive Inspections on the Fuselage Lateral Beam
Within the compliance time specified in table 1 to paragraph (g)
of this AD, and thereafter at intervals not to exceed the values
specified in table 2 to paragraph (g) of this AD, as applicable to
airplane model, accomplish the inspections as specified in
paragraphs (g)(1) and (g)(2) of this AD, in accordance with the
instructions of Airbus Defense and Space Alert Operators
Transmission (AOT) AOT-CN235-53-0002, Revision 1, dated September
(1) A special detailed inspection for cracks and other
discrepancies with a borescope of the rear fuselage lateral beam
between frame (FR) 31 and FR 45, left-hand (LH) and right-hand (RH)
side.
(2) A detailed visual inspection for cracks and other
discrepancies of the external area of the rear fuselage lateral
beam, LH and RH side.
Table 1 to Paragraph (g) of This AD--Initial Inspection Compliance Time
A or B, whichever occurs later
A............................  Before exceeding 15,000 flight cycles or
15,000 flight hours, whichever occurs
first since airplane first flight.
B............................  Within 50 flight cycles or 50 flight
hours, whichever occurs first after the
effective date of this AD.
Table 2 to Paragraph (g) of This AD--Repetitive Inspection Intervals
Repetitive interval (whichever
Airplane models               occurs first, flight cycles or
flight hours)
Model CN-235 and CN-235-100 airplanes..  3,600 flight cycles or 3,100
flight hours.
Model CN-235-200 airplanes.............  3,600 flight cycles or 2,800
Model CN-235-300 airplanes.............  15,000 flight cycles or 15,000
(h) Repair
If any crack or discrepancy is found during any inspection
required by paragraph (g) of this AD: Before further flight, contact
and obtain repair instructions from Airbus Defense and Space S.A. in
accordance with paragraph (k)(2) of this AD, and within the
compliance time indicated in those instructions, accomplish the
repair accordingly, including any post-repair maintenance task(s),
as applicable.
(i) Continued Inspection of Repaired Areas
Accomplishment of a repair on an airplane, as required by
paragraph (h) of this AD, does not constitute terminating action for
the repetitive inspections as required by paragraph (g) of this AD
for that airplane, unless specified in the applicable repair
instructions obtained in paragraph (h).
(j) Credit for Previous Actions
This paragraph provides credit for actions required by
paragraphs (g) and (h) of this AD, if those actions were performed
before the effective date of this AD, using Airbus Defense and Space
AOT AOT-CN235-53-0002, dated August 28, 2015.
(k) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Shahram
Daneshmandi, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone 425-227-1112; fax 425-227-1149. 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
(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
Branch, ANM-116, Transport Airplane Directorate, FAA; or EASA; or
Airbus Defense and Space S.A.'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 Airworthiness Directive 2016-0064, dated April 4, 2016,
for related information. This MCAI may be found in the AD docket on
the Internet at https://www.regulations.gov by
searching for and locating Docket No. FAA-2016-9113.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(3) and (m)(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) Airbus Defense and Space Alert Operators Transmission (AOT),
AOT-CN235-53-0002, Revision 1, dated September 17, 2015.
(ii) Reserved.
(3) For service information identified in this AD, contact EADS-
CASA, Military Transport Aircraft Division (MTAD), Integrated
Customer Services (ICS), Technical Services, Avenida de
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84;
fax +34 91 585 55 05; email MTA.TechnicalService@casa.eads.net;
Internet https://www.eads.net.
(4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on December 27, 2016.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification

redpajama_set_name: RedPajamaCommonCrawl


text:
Isomeric and β -decay spectroscopy of Ho 173,174
J. J. Liu, J. Lee, H. Watanabe, S. Nishimura, G. X. Zhang, J. Wu, P. M. Walker, P. H. Regan, P. A. Söderström, H. Kanaoka, Z. Korkulu, P. S. Lee, A. Yagi, A. C. Dai, F. R. Xu, D. S. Ahn, T. Alharbi, H. Baba, F. Browne, A. M. Bruce
R. J. Carroll, K. Y. Chae, Zs Dombradi, P. Doornenbal, A. Estrade, N. Fukuda, E. Ideguchi, N. Inabe, T. Isobe, S. Kanaya, I. Kojouharov, F. G. Kondev, T. Kubo, S. Kubono, N. Kurz, I. Kuti, S. Lalkovski, G. J. Lane, C. S. Lee, E. J. Lee, G. Lorusso, G. Lotay, C. B. Moon, I. Nishizuka, C. R. Nita, A. Odahara, Z. Patel, V. H. Phong, Zs Podolyák, O. J. Roberts, H. Sakurai, H. Schaffner, C. M. Shand, Y. Shimizu, T. Sumikama, H. Suzuki, H. Takeda, S. Terashima, Zs Vajta, J. J. Valiente-Dobón, Z. Y. Xu
β-decay spectroscopy of Ho173,174 (Z = 67, N = 106,107) was conducted at Radioactive Isotope Beam Factory at RIKEN by using in-flight fission of a 345-MeV/u U238 primary beam. A previously unreported isomeric state at 405 keV with half-life of 3.7(12) μs and a spin and parity of (3/2+) is identified in Ho173. Moreover, a new state with a spin and parity of 9- was discovered in Er174. The experimental log ft values of 5.84(20) and 5.25(18) suggest an allowed-hindered β decay from the ground state of Ho174 to the Kπ=8- isomeric state in Er174. Configuration-constrained potential energy surface (PES) calculations were performed and the predictions are in reasonable agreement with the experimental results.
Physical Review C
https://doi.org/10.1103/PhysRevC.102.024301
This measurement was carried out at the RIBF operated by RIKEN Nishina Center and CNS, University of Tokyo, the EUROBALL Owners Committee for the loan of germanium detectors, the PreSpec Collaboration for the readout electronics of the cluster detectors. Part of the WAS3ABi was supported by the Rare Isotopes Science Project which is funded by MSIP and NRF of Korea. This work was supported by JSPS KAKENHI Grants No. 24740188, No. 25247045, and No. 25287065, STFC (UK authors), the UK National Measurement Office (P.H.R.), the U.S. Department of Energy, Office of Science, Office of Nuclear Physics under Contract No. DE-AC02-06CH11357 (F.G.K.), NRF Korea Grants No. 2016R1D1A1A09917463, No. 2017M2A2A6A02071071 (C.S.L.), No. 2019R1F1A1058370, and No. 2016R1A5A1013277 (K.Y.C.), and Science Foundation Ireland under Grant No. 12/IP/1288 (O.J.R.).
© 2020 American Physical Society.
Copyright 2020 Elsevier B.V., All rights reserved.
10.1103/PhysRevC.102.024301
Dive into the research topics of 'Isomeric and β -decay spectroscopy of Ho 173,174'. Together they form a unique fingerprint.
parity Physics & Astronomy 100%
industrial plants Physics & Astronomy 60%
spectroscopy Physics & Astronomy 58%
half life Physics & Astronomy 58%
radioactive isotopes Physics & Astronomy 57%
flight Physics & Astronomy 52%
fission Physics & Astronomy 52%
Liu, J. J., Lee, J., Watanabe, H., Nishimura, S., Zhang, G. X., Wu, J., Walker, P. M., Regan, P. H., Söderström, P. A., Kanaoka, H., Korkulu, Z., Lee, P. S., Yagi, A., Dai, A. C., Xu, F. R., Ahn, D. S., Alharbi, T., Baba, H., Browne, F., ... Xu, Z. Y. (2020). Isomeric and β -decay spectroscopy of Ho 173,174. Physical Review C, 102(2), [024301]. https://doi.org/10.1103/PhysRevC.102.024301
Liu, J. J. ; Lee, J. ; Watanabe, H. et al. / Isomeric and β -decay spectroscopy of Ho 173,174. In: Physical Review C. 2020 ; Vol. 102, No. 2.
@article{d79b5a7eac69498fa1795317eec627e2,
title = "Isomeric and β -decay spectroscopy of Ho 173,174",
abstract = "β-decay spectroscopy of Ho173,174 (Z = 67, N = 106,107) was conducted at Radioactive Isotope Beam Factory at RIKEN by using in-flight fission of a 345-MeV/u U238 primary beam. A previously unreported isomeric state at 405 keV with half-life of 3.7(12) μs and a spin and parity of (3/2+) is identified in Ho173. Moreover, a new state with a spin and parity of 9- was discovered in Er174. The experimental log ft values of 5.84(20) and 5.25(18) suggest an allowed-hindered β decay from the ground state of Ho174 to the Kπ=8- isomeric state in Er174. Configuration-constrained potential energy surface (PES) calculations were performed and the predictions are in reasonable agreement with the experimental results.",
author = "Liu, {J. J.} and J. Lee and H. Watanabe and S. Nishimura and Zhang, {G. X.} and J. Wu and Walker, {P. M.} and Regan, {P. H.} and S{\"o}derstr{\"o}m, {P. A.} and H. Kanaoka and Z. Korkulu and Lee, {P. S.} and A. Yagi and Dai, {A. C.} and Xu, {F. R.} and Ahn, {D. S.} and T. Alharbi and H. Baba and F. Browne and Bruce, {A. M.} and Carroll, {R. J.} and Chae, {K. Y.} and Zs Dombradi and P. Doornenbal and A. Estrade and N. Fukuda and E. Ideguchi and N. Inabe and T. Isobe and S. Kanaya and I. Kojouharov and Kondev, {F. G.} and T. Kubo and S. Kubono and N. Kurz and I. Kuti and S. Lalkovski and Lane, {G. J.} and Lee, {C. S.} and Lee, {E. J.} and G. Lorusso and G. Lotay and Moon, {C. B.} and I. Nishizuka and Nita, {C. R.} and A. Odahara and Z. Patel and Phong, {V. H.} and Zs Podoly{\'a}k and Roberts, {O. J.} and H. Sakurai and H. Schaffner and Shand, {C. M.} and Y. Shimizu and T. Sumikama and H. Suzuki and H. Takeda and S. Terashima and Zs Vajta and Valiente-Dob{\'o}n, {J. J.} and Xu, {Z. Y.}",
note = "Funding Information: This measurement was carried out at the RIBF operated by RIKEN Nishina Center and CNS, University of Tokyo, the EUROBALL Owners Committee for the loan of germanium detectors, the PreSpec Collaboration for the readout electronics of the cluster detectors. Part of the WAS3ABi was supported by the Rare Isotopes Science Project which is funded by MSIP and NRF of Korea. This work was supported by JSPS KAKENHI Grants No. 24740188, No. 25247045, and No. 25287065, STFC (UK authors), the UK National Measurement Office (P.H.R.), the U.S. Department of Energy, Office of Science, Office of Nuclear Physics under Contract No. DE-AC02-06CH11357 (F.G.K.), NRF Korea Grants No. 2016R1D1A1A09917463, No. 2017M2A2A6A02071071 (C.S.L.), No. 2019R1F1A1058370, and No. 2016R1A5A1013277 (K.Y.C.), and Science Foundation Ireland under Grant No. 12/IP/1288 (O.J.R.). Publisher Copyright: {\textcopyright} 2020 American Physical Society. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.",
doi = "10.1103/PhysRevC.102.024301",
journal = "Physical Review C",
Liu, JJ, Lee, J, Watanabe, H, Nishimura, S, Zhang, GX, Wu, J, Walker, PM, Regan, PH, Söderström, PA, Kanaoka, H, Korkulu, Z, Lee, PS, Yagi, A, Dai, AC, Xu, FR, Ahn, DS, Alharbi, T, Baba, H, Browne, F, Bruce, AM, Carroll, RJ, Chae, KY, Dombradi, Z, Doornenbal, P, Estrade, A, Fukuda, N, Ideguchi, E, Inabe, N, Isobe, T, Kanaya, S, Kojouharov, I, Kondev, FG, Kubo, T, Kubono, S, Kurz, N, Kuti, I, Lalkovski, S, Lane, GJ, Lee, CS, Lee, EJ, Lorusso, G, Lotay, G, Moon, CB, Nishizuka, I, Nita, CR, Odahara, A, Patel, Z, Phong, VH, Podolyák, Z, Roberts, OJ, Sakurai, H, Schaffner, H, Shand, CM, Shimizu, Y, Sumikama, T, Suzuki, H, Takeda, H, Terashima, S, Vajta, Z, Valiente-Dobón, JJ & Xu, ZY 2020, 'Isomeric and β -decay spectroscopy of Ho 173,174', Physical Review C, vol. 102, no. 2, 024301. https://doi.org/10.1103/PhysRevC.102.024301
Isomeric and β -decay spectroscopy of Ho 173,174. / Liu, J. J.; Lee, J.; Watanabe, H. et al.
In: Physical Review C, Vol. 102, No. 2, 024301, 03.08.2020.
T1 - Isomeric and β -decay spectroscopy of Ho 173,174
AU - Liu, J. J.
AU - Watanabe, H.
AU - Nishimura, S.
AU - Zhang, G. X.
AU - Wu, J.
AU - Walker, P. M.
AU - Regan, P. H.
AU - Söderström, P. A.
AU - Kanaoka, H.
AU - Korkulu, Z.
AU - Lee, P. S.
AU - Yagi, A.
AU - Dai, A. C.
AU - Xu, F. R.
AU - Ahn, D. S.
AU - Alharbi, T.
AU - Baba, H.
AU - Browne, F.
AU - Bruce, A. M.
AU - Carroll, R. J.
AU - Chae, K. Y.
AU - Dombradi, Zs
AU - Doornenbal, P.
AU - Estrade, A.
AU - Fukuda, N.
AU - Ideguchi, E.
AU - Inabe, N.
AU - Isobe, T.
AU - Kanaya, S.
AU - Kojouharov, I.
AU - Kondev, F. G.
AU - Kubo, T.
AU - Kubono, S.
AU - Kurz, N.
AU - Kuti, I.
AU - Lalkovski, S.
AU - Lane, G. J.
AU - Lee, C. S.
AU - Lee, E. J.
AU - Lorusso, G.
AU - Lotay, G.
AU - Moon, C. B.
AU - Nishizuka, I.
AU - Nita, C. R.
AU - Odahara, A.
AU - Patel, Z.
AU - Phong, V. H.
AU - Podolyák, Zs
AU - Roberts, O. J.
AU - Sakurai, H.
AU - Schaffner, H.
AU - Shand, C. M.
AU - Shimizu, Y.
AU - Sumikama, T.
AU - Suzuki, H.
AU - Takeda, H.
AU - Terashima, S.
AU - Vajta, Zs
AU - Valiente-Dobón, J. J.
AU - Xu, Z. Y.
N1 - Funding Information: This measurement was carried out at the RIBF operated by RIKEN Nishina Center and CNS, University of Tokyo, the EUROBALL Owners Committee for the loan of germanium detectors, the PreSpec Collaboration for the readout electronics of the cluster detectors. Part of the WAS3ABi was supported by the Rare Isotopes Science Project which is funded by MSIP and NRF of Korea. This work was supported by JSPS KAKENHI Grants No. 24740188, No. 25247045, and No. 25287065, STFC (UK authors), the UK National Measurement Office (P.H.R.), the U.S. Department of Energy, Office of Science, Office of Nuclear Physics under Contract No. DE-AC02-06CH11357 (F.G.K.), NRF Korea Grants No. 2016R1D1A1A09917463, No. 2017M2A2A6A02071071 (C.S.L.), No. 2019R1F1A1058370, and No. 2016R1A5A1013277 (K.Y.C.), and Science Foundation Ireland under Grant No. 12/IP/1288 (O.J.R.). Publisher Copyright: © 2020 American Physical Society. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.
N2 - β-decay spectroscopy of Ho173,174 (Z = 67, N = 106,107) was conducted at Radioactive Isotope Beam Factory at RIKEN by using in-flight fission of a 345-MeV/u U238 primary beam. A previously unreported isomeric state at 405 keV with half-life of 3.7(12) μs and a spin and parity of (3/2+) is identified in Ho173. Moreover, a new state with a spin and parity of 9- was discovered in Er174. The experimental log ft values of 5.84(20) and 5.25(18) suggest an allowed-hindered β decay from the ground state of Ho174 to the Kπ=8- isomeric state in Er174. Configuration-constrained potential energy surface (PES) calculations were performed and the predictions are in reasonable agreement with the experimental results.
AB - β-decay spectroscopy of Ho173,174 (Z = 67, N = 106,107) was conducted at Radioactive Isotope Beam Factory at RIKEN by using in-flight fission of a 345-MeV/u U238 primary beam. A previously unreported isomeric state at 405 keV with half-life of 3.7(12) μs and a spin and parity of (3/2+) is identified in Ho173. Moreover, a new state with a spin and parity of 9- was discovered in Er174. The experimental log ft values of 5.84(20) and 5.25(18) suggest an allowed-hindered β decay from the ground state of Ho174 to the Kπ=8- isomeric state in Er174. Configuration-constrained potential energy surface (PES) calculations were performed and the predictions are in reasonable agreement with the experimental results.
U2 - 10.1103/PhysRevC.102.024301
DO - 10.1103/PhysRevC.102.024301
JO - Physical Review C
JF - Physical Review C
Liu JJ, Lee J, Watanabe H, Nishimura S, Zhang GX, Wu J et al. Isomeric and β -decay spectroscopy of Ho 173,174. Physical Review C. 2020 Aug 3;102(2). 024301. https://doi.org/10.1103/PhysRevC.102.024301


And now here was a chance to mold—or at the very least unleash—the next one, a 24-year-old from Athens who stands 6'11", with arms that spread wider than he is tall, who can play all five positions and conjures comparisons as disparate as Scottie Pippen and Shaquille O'Neal. Better yet, this unicorn—whose name the rest of the league was finally learning to pronounce (YAHN-iss an-tay-to-KOON-poh)—was just entering his prime, his talents not yet fully exploited, the league still unsure how to best adapt.
One of their origin stories is familiar by now. How Charles and Veronica Antetokounmpo came from Nigeria to Greece in 1991 and raised four sons, hawking handbags on the street and constantly fearing deportation. How Giannis, the second oldest, kept growing, signed with a semi-pro team at 16 and went 15th to the Bucks in the 2013 draft. How he agreed to stay only after he was assured that his family would be able join him. How he arrived in Milwaukee at 18, joyous and disbelieving, reveling in every cheeseburger and convenience store and tweeting things like, "I just taste for the first time a smothie. . MAN GOD BLESS AMERICA" [sic]. How he became a regular starter in his second season and made the All-Star team in his fourth. How he became a hero, the best kind of immigrant story (one Disney is said to be making into a movie).
Most coaches start out mimicking their mentors. Pop ran a variation on the motion offense, and Bud did the same in Atlanta. Over time, though, he tinkered. He had long admired the triangle: how players read and reacted, how opposing defenses had no idea whom to double-team when. "F—— beautiful!" he says. He knew its era had passed, but the principles of spontaneity remained timeless. So, after years of having his big men run to the rim in transition—the hallmark of Duncan-era Spurs—he instructed Al Horford and Paul Millsap to peel off to the corners to create space. (Recalls Budenholzer, "My assistants looked at me like someone stole my brain.") The court opened up, the ball moved and everyone launched from deep. The symbolic highlight: when four Atlanta starters made the 2015 All-Star team.
Now Budenholzer envisioned what he calls "positionless motion." No bigs or wings or guards. Just five players, all interchangeable, creating a glorious "randomness." Don Nelson aspired to this 30 years ago, and George Karl preached playing in space with minimal structure. But while Nellie dreamed of a quintet of 6'9″ do-everything players, Budenholzer wanted to try it with the roster at hand, which meant everyone from the 6'1″ Bledsoe to the 7-foot Lopez. Five blue boxes appeared on the practice court, arrayed around the three-point line. "Basically, stand here," Bud says. Anyone could be in any box; just don't muck up the paint.
But offense was never the problem under Bud's predecessor, Jason Kidd. It was defense where the Bucks faltered. And yet Horst says that of all the coaches who interviewed for the job, only Budenholzer focused on D. It made sense. In Atlanta the accolades came for his offense; quietly, he also oversaw three top five defen-sive seasons in a row. He is Vince's son, after all. Now he had ideas. "Watching the tape, I think Giannis had taken a step back." He wanted to challenge his star—to cover more ground, to win Defensive Player of the Year, to guard each position if needed. And so far Giannis has, swatting, swiping and lurking like a giant gargoyle atop the rim. He had never averaged more than 10 rebounds; he's now grabbing 10.3 on the defensive end alone. He may well win that DPOY award.
Up close, his proportions are disconcerting, like one of those flip books where the top and bottom half change with each page. A compact, muscled torso perches atop two stringy legs. When he palms the ball he does it as Connie Hawkins once did, waving it around as the rest of us might a slightly deflated balloon, swallowed in hands that measure a foot from his pinkie tip to the top of his thumb. Since entering the league Giannis has grown almost three inches. He can almost grab the rim without jumping and once blocked a shot with his elbow. Pat Connaughton, a backup guard and the Bucks' resident weight room enthusiast, recently said he and Giannis do pull-ups wearing 88-pound vests and add 66 pounds to their triceps dips. The result: Giannis can looks less like a human basketball player and more like something Pixar created; in the next Space Jam, he'd be a Monstar.
Ah, yes, the shooting. It seems unfair to harp on his one flaw, but there it is. This year Giannis is shooting 24.5% from behind the arc on 2.7 attempts per game, putting him on pace for one of the 10 worst high-volume seasons in history, amid chuckers like Charles Barkley and Josh Smith. And yet, to reach their goal, the Bucks might Giannis need to jack more.
Even so, just the promise of Giannis becoming a wing shooter allows Bud to experiment. Against the Kings he rolls out the team's newest acquisition, 6'10" Nikola Mirotic, another tall sniper who allows Budenholzer to go, as he says "counterculture," combating smallball lineups with Lopez, Giannis, Mirotic and the 6'8″ Middleton. Once, Bud went even bigger. When Brogdon and Bledsoe were out against the Jazz, he says he "channeled my inner Nellie" and ran out a lineup that stood 7 feet, 6'11", 6'10", 6'10" and 6'8″. It's not something he plans to do often—they've only been together 22 possessions—but the results were intriguing: Their point differential per 100 possessions was 119.6. "It was f—— beautiful!" says Bud. "I just love that we can go so many different directions." Of course, he notes, this only works because of Giannis.


The Sharif family on Wednesday broke their silence on Begum Kulsoom Nawaz's health, who was reported to have been diagnosed with throat cancer, with Maryam Nawaz taking to Twitter to update followers regarding her well-being.
In a series of tweets, Maryam said the former first lady was diagnosed with lymphoma, a type of cancer that starts in the lymph nodes.
Maryam added that due to early diagnosis, doctors are optimistic that the disease can be treated successfully.
She also thanked her supporters for their prayers.
Kulsoom, who is PML-N's candidate for the NA-120 seat, had unexpectedly departed for London on August 17 for a medical checkup.
She left hours before she was meant to appear before the Election Commission of Pakistan for the scrutiny of her nomination papers. The by-polls for the NA-120 seat, which fell vacant after the disqualification of Nawaz Sharif, are scheduled to be held on September 17.
Since Kulsoom may not be able to run her election campaign due to her ailment, Maryam Nawaz will be overseeing the electioneering as MNA Hamza Shahbaz, who has so far been the lead strategist for the by-polls held in Punjab, has also left for London.
Earlier, Shahbaz Sharif, Nawaz Sharif's younger brother, also tweeted his "best wishes and prayers" for his sister-in-law's "quick recovery".
Lot of prayers for the First Lady and wishing her a quick recovery.
Keep yourself away from politics, just relax, and eat healthy food. Let your immune system to fight cancer. Anxiety, worries and political pressures not good for the health of our fisrt lady.
Can we also pray for countless, less privileged souls, whose cancers will go unnoticed until it's too late to help. And this, largely due to an acute lack of national facilities resulting from industrial level money laundering and theft from the national exchequer. Get well soon Begum Kalsoom.
I wish her health and recovery. Cancer is reverse-able through a healthy ketogenic diet. Cancer's food and energy source is sugar and carbs. The body's primary source of energy is glucose which can be replaced by ketons through ketogenic diet. The results is, unlike the normal cells the cancerous cells do not have metabolic flexibility to metabolize ketons. So the cancer gets starved.
Normally diagnosis of this nature is only shared with the close family and not with the patient. The immense pressure of having cancer has physical and emotional impact on the patient. Whereas concerns, prayers and well wishes of the followers and loved ones are great, however, it seems that there may also be intent to gain sympathy and political ground. Sad.
Pray for her full recovery.
Beat wishes to her and we pray for her recovery. I wish that she could be treated in our own country and not had to go abroad. PMLN government should invest in hospitals and schools and not waste money on road network. Priority shold be health, education and poor people.
Prayers and best wishes to KS for a speedy recovery. She should do some project for the good of the poor like building a hospital like Shaukat Khanum so her name can live for ever.
What example does the exPM and his wife give when they run overseas to seek treatment yet Pakistan has cancer hospitals and heart specialists but its not good enough for those who have power and money...wake up Pakistan to reality and vote for those leaders who put Pakistan first NOT their bank accounts!!! The irony here is that Pakistani drs are the ones treating them in London hospitals!!!
Hodgkin's lymphoma is often curable. She is not at an advanced stage of cancer.
May our brave bhabi get well soon.


text:
cask :v1 => 'gopanda' do
  version :latest
  sha256 :no_check

  url 'http://pandanet-igs.com/gopanda2/installer/stable/mac-32/gopanda2-mac-32.zip'
  homepage 'http://pandanet-igs.com/communities/gopanda2'
  license :unknown    # todo: improve this machine-generated value

  app 'GoPanda2.app'
end

redpajama_set_name: RedPajamaGithub


After hovering at alpha for a few months, we're looking to move the Fiscal Data Package specification to version 0.3.0 by 31 January 2016.
We would like to request interested parties read the current spec and raise any comments they have on the issue tracker. We are looking to solve the most pressing issues for a 0.3.0 release. Please note, that even after the deadline, the specification will still be evolving. As such, comments that don't make the 0.3.0 release could possibly be included in a future release.
In parallel with this, we are seeking to define and refine a process for reviewing and accepting contributions. Please see the following pull request for details: #122.


text:
Late-onset nonketotic hyperglycinemia caused by a novel homozygous missense mutation in the GLDC gene
Late-onset nonketotic hyperglycinemia caused by a novel homozygous missense mutation in the GLDC... Brunel-Guitton, Catherine; Casey, Brett; Coulter-Mackie, Marion; Vallance, Hilary; Hewes, Deborah; Stockler-Ipsiroglu, Sylvia; Mercimek-Mahmutoglu, Saadet 2011-06-01 00:00:00 Nonketotic hyperglycinemia (NKH) is an inborn error of the glycine metabolism. A 9-year-old boy with learning disability and intermittent choreoathetosis during febrile illnesses had elevated plasma glycine level and CSF/plasma glycine ratio (0.044) and a novel homozygous missense mutation (c.605C > T; p.Ala202Val) in the GLDC gene, confirming the diagnosis of NKH. This is the first report of late-onset NKH with a confirmed underlying genetic defect. NKH should be in the differential diagnosis of intermittent choreoathetosis. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Molecular Genetics and Metabolism Elsevier http://www.deepdyve.com/lp/elsevier/late-onset-nonketotic-hyperglycinemia-caused-by-a-novel-homozygous-1pTkdbDrUL
Brunel-Guitton, Catherine; Casey, Brett; Coulter-Mackie, Marion; Vallance, Hilary; Hewes, Deborah; Stockler-Ipsiroglu, Sylvia; Mercimek-Mahmutoglu, Saadet
Molecular Genetics and Metabolism
, Volume 103 (2) – Jun 1, 2011
/lp/elsevier/late-onset-nonketotic-hyperglycinemia-caused-by-a-novel-homozygous-1pTkdbDrUL
Molecular Genetics and Metabolism /
Volume 103 Issue 2
10.1016/j.ymgme.2011.02.009
Nonketotic hyperglycinemia (NKH) is an inborn error of the glycine metabolism. A 9-year-old boy with learning disability and intermittent choreoathetosis during febrile illnesses had elevated plasma glycine level and CSF/plasma glycine ratio (0.044) and a novel homozygous missense mutation (c.605C > T; p.Ala202Val) in the GLDC gene, confirming the diagnosis of NKH. This is the first report of late-onset NKH with a confirmed underlying genetic defect. NKH should be in the differential diagnosis of intermittent choreoathetosis.
Molecular Genetics and Metabolism – Elsevier
Published: Jun 1, 2011
Nonketotic hyperglycinemia
Hamosh, A.; Johnston, M.V.
Structural and expression analyses of normal and mutant mRNA encoding glycine decarboxylase: three-base deletion in mRNA causes nonketotic hyperglycinemia
Kure, S.; Narisawa, K.; Tada, K.
The glycine cleavage system structure of a cDNA encoding human H-protein, and partial characterization of its gene in patients with hyperglycinemias
Koyata, H.; Hiraga, K.
Isolation and sequence determination of cDNA encoding human T-protein of the glycine cleavage system
Hayasaka, K.; Nanao, K.; Takada, F.; Okamura-Ikeda, K.; Motokawa, Y.
Localization of the human dihydrolipoamide dehydrogenase gene (DLD) to 7q31–q32
Scherer, S.W.; Otulakowski, G.; Robinson, B.H.; Tsui, L.C.
Nonketotic hyperglycinemia (glycine encephalopathy): laboratory diagnosis
Applegarth, D.A.; Toone, J.R.
Biochemical and molecular investigations of patients with nonketotic hyperglycinemia
Toone, J.R.; Applegarth, D.A.; Coulter-Mackie, M.B.; James, E.R.
Atypical variants of nonketotic hyperglycinemia
Dinopoulos, A.; Matsubara, Y.; Kure, S.
Comprehensive mutation analysis of GLDC, AMT, and GCSH in nonketotic hyperglycinemia
Kure, S.; Kato, K.; Dinopoulos, A.; Gail, C.; deGrauw, T.J.; Christodoulou, J.; Bzduch, V.; Kalmanchey, R.; Fekete, G.; Trojovsky, A.; Plecko, B.; Breningstall, G.; Tohyama, J.; Aoki, Y.; Matsubara, Y.
Treatment of late-onset nonketotic hyperglycinemia: effectiveness of imipramine and benzoate
Wiltshire, E.J.; Poplawski, N.K.; Harrison, J.R.; Fletcher, J.M.
Late-onset nonketotic hyperglycinemia with leukodystrophy and an unusual clinical course
Chiong, M.A.; Procopis, P.; Carpenter, K.; Wilcken, B.
Nonketotic hyperglycinemia: analyses of glycine cleavage system in typical and atypical cases
Hayasaka, K.; Tada, K.; Fueki, N.; Nakamura, Y.; Nyhan, W.L.; Schmidt, K.; Packman, S.; Seashore, M.R.; Haan, E.; Danks, D.M.
Adult nonketotic hyperglycinemia (NKH) crisis presenting as severe chorea and encephalopathy
Hall, D.A.; Ringel, S.P.
Blindness due to non-ketotic hyperglycinemia: report of a 38-year-old, the oldest case to date
Tanaka, Y.; Miyazaki, M.; Tsuda, M.; Murai, K.; Kuzuhara, S.
Late-onset nonketotic hyperglycinemia and spinocerebellar degeneration
Steiman, G.S.; Yudkoff, M.; Berman, P.H.; Blazer-Yost, B.; Segal, S.
Late-onset nonketotic hyperglycinemia: a case report
Hasegawa, T.; Shiga, Y.; Matsumoto, A.; Takeda, A.; Itoyama, Y.
Juvenile non-ketotic hyperglycinemia in three siblings
Cole, D.E.C.; Meek, D.C.
Familial neuromuscular disease with nonketotic hyperglycinemia
Bank, W.J.; Morrow, G.
Atypical nonketotic hyperglycinemia with normal cerebrospinal fluid to plasma glycine ratio
Jackson, A.H.; Applegarth, D.A.; Toone, J.R.; Kure, S.; Levy, H.L.
Nonketotic hyperglycinemia: studies in an atypical variant
Singer, H.S.; Valle, D.; Hayasaka, K.; Tada, K.
Structure of P-protein of the glycine cleavage system: implications for nonketotic hyperglycinemia
Nakai, T.; Nakagawa, N.; Maoka, N.; Masui, R.; Kuramitsu, S.; Kamiya, N.
Persistent NKH with transient or absent symptoms and a homozygous GLDC mutation
Korman, S.H.; Boneh, A.; Ichinohe, A.; Kojima, K.; Sato, K.; Ergaz, Z.; Gomori, J.M.; Gutman, A.; Kure, S.
Neonatal epileptic encephalopathy caused by mutations in the PNPO gene encoding pyridox(am)ine 5′-phosphate oxidase
Mills, P.B.; Surtees, R.A.; Champion, M.P.; Beesley, C.E.; Dalton, N.; Scambler, P.J.; Heales, S.J.; Briddon, A.; Scheimberg, I.; Hoffmann, G.F.; Zschocke, J.; Clayton, P.T.
Increased cerebrospinal fluid glycine: a biochemical marker for a leukoencephalopathy with vanishing white matter
van der Knaap, M.S.; Wevers, R.A.; Kure, S.; Gabreëls, F.J.; Verhoeven, N.M.; van Raaij-Selten, B.; Jaeken, J.
Transient nonketotic hyperglycinemia and defective serotonin metabolism in a child with neonatal seizures
Lin, F.Y.; Gascon, G.G.; Hyland, K.; Chugani, H.; Chugani, D.
A novel missense mutation in a neonate with nonketotic hyperglycinemia
Meyer, S.; Acquaviva, C.; Shamdeen, M.G.; Haas, D.; Vianey-Saban, C.
Lower sensitivity to stress and altered monoaminergic neuronal function in mice lacking the NMDA receptor epsilon 4 subunit
Miyamoto, Y.; Yamada, K.; Noda, Y.; Mori, H.; Mishina, M.; Nabeshima, T.
Hyperglycinuria and hyperglycinemia in two siblings with mild developmental delays
Frazier, D.M.; Summer, G.K.; Chamberlin, H.R.
Nonketotic hyperglycinemia: atypical clinical and biochemical manifestations
Steiner, R.D.; Sweetser, D.A.; Rohrbaugh, J.R.; Dowton, S.B.; Toone, J.R.; Applegarth, D.A.
Atypical nonketotic hyperglycinemia confirmed by assay of the glycine cleavage system in lymphoblasts
Christodoulou, J.; Kure, S.; Hayasaka, K.; Clarke, J.T.
Brunel-Guitton, C., Casey, B., Coulter-Mackie, M., Vallance, H., Hewes, D., Stockler-Ipsiroglu, S., & Mercimek-Mahmutoglu, S. (2011). Late-onset nonketotic hyperglycinemia caused by a novel homozygous missense mutation in the GLDC gene. Molecular Genetics and Metabolism, 103(2), 193-196.
Brunel-Guitton, Catherine, Brett Casey, Marion Coulter-Mackie, Hilary Vallance, Deborah Hewes, Sylvia Stockler-Ipsiroglu, and Saadet Mercimek-Mahmutoglu. "Late-onset nonketotic hyperglycinemia caused by a novel homozygous missense mutation in the GLDC gene." Molecular Genetics and Metabolism 103.2 (2011): 193-196.


text:
News Yet another mysterious abduction by a black van in Turkey's capital
Yet another mysterious abduction by a black van in Turkey's capital
Hasan Kala, an academic who was fired from his job at Çankırı Karatekin University by a government decree under a state of emergency declared in the aftermath of a controversial coup attempt on July 15, 2016 over his alleged links to the Gülen movement, was reportedly abducted by an unknown group of people on Saturday night.
Associate Professor Hasan Kala
According to information shared by Turkish social media accounts, Associate Professor Kala was abducted after being forced into a black Transporter van in Ankara's Batıkent district at 11:30 p.m. on July 21, 2018.
Thirteen people have reportedly been abducted in Turkey, 11 of them kidnapped in Ankara by National Intelligence Organization (MİT)-affiliated paramilitary forces that work with total impunity. The mysterious kidnappings in Turkey are bringing back fears of the enforced disappearances by state agencies in the mid-1990s.
Opposition politicians put the number at eight, while Turkey's Human Rights Association (İHD), an independent NGO, said it had documented 10 cases as of May, 2017. Another two abductions are alleged to have taken place in June 2017. On Aug. 3, 2017 Human Rights Watch (HRW) called on Turkish Justice Minister Abdülhamit Gül in a letter to investigate the abductions and possibly enforced disappearances in Ankara of at least four men who have been missing since March 2017.
The Stockholm Center for Freedom (SCF) has so far documented 18 individual cases of disappearance since 2016 that show a systematic and deliberate campaign of kidnappings by elements within the Turkish security and intelligence services as part of intimidation campaign to silence critical and independent voices and kill the right to dissent.
In the 1990s, at the height of the state's brutal war against terrorists of the outlawed Kurdistan Workers' Party (PKK), security forces disappeared hundreds of civilians, most of them Kurds. Often, they were tortured. Some victims' bodies were eventually found; in many cases, their fate remains unknown to this day. Over the years, the ECtHR found the Turkish state responsible in numerous cases.
Turkey survived a controversial military coup attempt on July 15, 2016 that killed 249 people. Immediately after the putsch, the Justice and Development Party (AKP) government along with President Recep Tayyip Erdoğan pinned the blame on the Gülen movement.
Fethullah Gülen, who inspired the movement, strongly denied having any role in the failed coup and called for an international investigation into it, but President Erdoğan — calling the coup attempt "a gift from God" — and the government initiated a widespread purge aimed at cleansing sympathizers of the movement from within state institutions, dehumanizing its popular figures and putting them in custody.
Turkey has suspended or dismissed more than 150,000 judges, teachers, police and civil servants since July 15. On December 13, 2017 the Justice Ministry announced that 169,013 people have been the subject of legal proceedings on coup charges since the failed coup.
Turkish Interior Minister Süleyman Soylu announced on April 18, 2018 that the Turkish government had jailed 77,081 people between July 15, 2016 and April 11, 2018 over alleged links to the Gülen movement.


text:
More on Cash Transfers to Reduce HIV among Adolescents
My recent blog on cash transfers as a tool for HIV prevention among adolescent girls and young women left out results from a number of recent evaluations that illustrate the importance of program design and, in particular, targeting the transfers to the poorest households in getting results in wellbeing.
Tia Palermo, a social policy specialist with the Transfer Project at UNICEF Office of Research-Innocenti and UNC-Chapel Hill, wrote with an update, which I'm pleased to share with her permission:
Widely demonstrated to reduce poverty and improve food security, school enrolment, selected health outcomes, resilience, and productive activities, the emerging consensus has been that cash transfers may also have the potential to facilitate safe transitions to adulthood, including delaying sexual debut, pregnancy and marriage, and reducing HIV risk among adolescents. Furthermore, concerns about unintended consequences, such as that cash transfers incentivize increases in fertility, people will spend the cash on alcohol and tobacco, and recipients will stop working have been largely debunked.
Four recent studies emerging from India and South Africa have challenged the prevailing narrative about the benefits of cash transfers for adolescents and raised concerns about unintended consequences. One study suggests that a conditional cash transfer programme in India targeted to households, conditional on certain behaviours among adolescent girls increased the likelihood of marriage as soon as the girls turned 18. Another study, also from India, found that a cash transfer programme conditional on childbirth delivery at a health facility was successful at its stated aim but inadvertently increased the probability of pregnancy or childbirth over a three-year period among women in target areas. A third programme in South Africa (HPTN 068), targeted to adolescent girls and their caregivers conditional on girls' school attendance, aimed to reduce HIV infections, and a study evaluating this programme found no impacts on either school attendance or HIV rates. Finally, another study, CAPRISA 007, provided life skills training and cash incentives with the aim of reducing HIV and HSV-2 infection among rural high school students in South Africa was found to reduce HSV-2 incidence but had no impact on HIV incidence.
So what does all this mean for cash transfer programmes?
To understand the implications of these findings, we should consider three key points: 1) programme characteristics such as objectives, delivery and targeting matter, 2) context matters, and 3) cash transfers are not a silver bullet. Once these points are taken into consideration, the potential for cash transfers to facilitate safe transitions to adulthood remains clear.
Programme objectives, delivery, and targeting matter
Programme objectives, delivery, and targeting are important, particularly if we are to compare apples to apples. Programmes in India were specifically designed to motivate certain behaviours (e.g., institutional delivery and delayed marriage). They were targeted/narrow programmes consisting of one-time payments for complying with desired behaviours. Conversely, government-run cash transfer programmes in Africa are designed with the broader aims of reducing poverty and investing in human capital. To achieve these aims, African government programmes are targeted to the poorest and most vulnerable households, and consist of regular-interval payments which continue over time. This regularity of payments allows households to become more forward-thinking and invest in children's schooling and productive activities. One-time payments which reward specific behaviours are unlikely to have the same impacts. Regarding concerns about fertility incentives, a programme which aims to increase institutional delivery (and thus women can only qualify when pregnant) is likely to have different impacts on fertility than programs which aim to improve food security and investments in human capital more broadly. In fact, rigorous research from Latin America and Africa demonstrates no, or very few, impacts on fertility of conditional and unconditional cash transfers to date.
Targeting, or decisions about who receives the programme benefits, also matters. The South African programmes (HPTN 068 and CAPRISA 007) did not explicitly target the poorest households (indeed, girls in HPTN 068 had to be in school and know how to use computers to qualify and youth in CAPRISA 007 were sampled from secondary schools), but large-scale government-run cash transfers almost always do (it should be noted that there is a large-scale, successful government-run programme in South Africa). Since girls in both treatment and control arms of the HPTN 068 study attended school at high rates throughout the duration of the study, and since CAPRISA 007 sampled from in-school secondary students, schooling as a protective pathway was unlikely in these contexts. Conversely, evidence from government programmes across Africa have shown that cash transfers have large, positive impacts on secondary school attendance. So if school turns out to be protective against sexual debut, risky behaviours, and marriage, then we can still expect other cash transfer programmes (either those with different targeting mechanisms, aims, or in other contexts) to impact these outcomes through the schooling pathway. HPTN 068 did however find that the programme reduced the frequency of sex and risk of unprotected sex and intimate partner violence, and CAPRISA 007 reduced HSV-2 incidence, suggesting that there were positive impacts of these programmes. Further, a study examining the government's Child Support Grant in South Africa found that cash transfers reduced adolescent pregnancy and sexual activity .
Context matters
Across countries and regions, characteristics such as social norms (e.g., gender preference in schooling, norms around marriage age, etc.), levels of poverty, and quality of government institutions may differ, and all of these are likely to affect how cash can influence outcomes. For example, before we discount the ability of cash transfers to delay marriage, we should consider contexts of marriage markets. In India, it is customary for brides' families to pay dowries to the grooms' family. Conversely, in Africa, brideprice is more common, whereby the bride's family receives a large payment or goods at the time of the marriage. So although a programme which financially rewarded families at a girls' 18th birthday for not having married her off earlier induced immediate marriage (likely because families found themselves able to pay a dowry), this does not mean that smaller, predictable cash transfers over a sustained period cannot delay marriage. Indeed, the latter type of programme addresses structural poverty and may shift underlying behaviours. Thus, these programmes may delay marriage through pathways such as reduced school dropout and reduced economic insecurity, a driver of early marriage.
Not a silver bullet
Finally, it is important to remember that cash transfers are not a silver bullet. While they do allow households to meet basic food needs, become more forward-looking, and invest in human capital by demanding more services (education and health), programmes can only achieve these aims if adequate services exist in the first place. Thus, cash transfer programmes need to be implemented in conjunction with improvements to supply-side factors like availability and quality of schools and health facilities, as well as improvements in markets and economic opportunities.
The good news and looking forward
Cash transfers won't solve all problems, but there is still good reason to believe that they can facilitate safe transitions to adulthood. New evidence from the Transfer Project demonstrates the ability of government cash transfer programmes in Africa to delaysexual debut,pregnancy, and improve adolescents' mental health. Other evidence in the region also suggests that cash transfers may also reduce adolescent girls' engagement intransactional sex, reduceHIV infection, and delay marriage. Researchers from the Transfer Project are working with governments and local partners to evaluate impacts on the safe transition to adulthood infive African countries. Data are still being analysed, and a lot ofnew evidence is still being generated on the ability of programmes to reduce risk of violence and risky behaviours, delay pregnancy and marriage, and examine impacts on schooling and work. So even though a lot of questions are still unanswered, there is good reason to believe that these programs may facilitate safe transitions to adulthood.
The Transfer Project works to provide rigorous evidence on programme impacts in an effort to inform future programme design and scale-up. Find more information on the Transfer Project's research on cash transfers here or on Twitter (@TransferProjct).
The Birdsall House Conference Series on Gender Equality
Global Childcare in 2022: Taking Stock & What's Next
Megan O'Donnell
Sumitra Mishra
Was Your Teacher Sexist?
Susannah Hares et al.
How Social Protection Programs Can Help to Tackle Gender-Based Violence
Alessandra Heinemann et al.


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7 Best Anime Like Classroom Of The Elite That You Should Watching Update 01/2023
An enjoyable high school anime, "Classroom of the Elite" Depending on their grades, pupils are assigned to different classes in the school. Class A is for the well-to-do, whereas class D is for the down-and-out. Class D students, on the other hand, are free to organize and rebel. It's amusing to watch how individuals act in such a competitive environment. Looking for more shows with comparable topics and ideas to what you saw in this anime? You've come to the perfect spot! We've put up a list of the greatest anime that we think are similar to 'Classroom of the Elite'. Anime like 'Classroom of the Elite' may be found on Netflix, Crunchyroll, and Hulu.
7. Prison School (2015)
In my opinion, "Prison School" is one of the best ecchi anime I've seen. Even though fan service and inappropriate moments are prevalent, they are not the exclusive source of entertainment in this anime. Animation and plot are both top-notch, and the characters are both amusing and relatable. 'Prison School' and 'Classroom of the Elite' both take place at a high school, which is why they're both on this list. Students are divided into groups according to school regulations. Discipline and adhering to school rules are more important than academic performance when it comes to class segregation.
Earlier this year, Hachimitsu Private Academy became a co-ed institution. It was once the most esteemed all-girls boarding school in the country. Five new boys have applied to this school as a result of the recent change. All-girls underground student council members aren't happy about the change, so they decide to expel the male students. After being caught spying on a girl while she was having a shower, the males discover that they have dug themselves a grave. They are subsequently sent to the school's prison, which is located within the grounds of the institution. Now, if they behave themselves, they will be allowed to attend school as normal. Apparently, the council members, on the other hand, are not ready to allow that to happen. Is it possible for them to make it through their time in the Prison School?
6. Baka to Test to Shoukanjuu (2010)
An enjoyable high school anime, 'Baka to Test to Shoukanjuu' It's a terrific show that's both amusing and visually appealing. In an effort to keep things from becoming tedious, the figures are dressed up in a variety of bright colors. 'Classroom of the Elite' and this anime share many similarities. Both of these stories take place in a high school setting. High achievers are separated from the rest of the pupils in these institutions by a set of restrictions. Students at the higher levels are treated with greater respect and have access to more resources at school than those at the lower levels. In both series, the main character strives to improve his class rank by accumulating as many points as possible.
The students at Fumizuki Gakuen's High School are divided into groups based on their grades. Prodigies are in Class A and losers are in Class F. Class A students have access to luxurious amenities, such as leather chairs and climate control, while those in Class F must make do with scuffed-up mats. Class F student Akihisa Yoshii has a plan to defeat the elites by enlisting the help of the fantastical creatures his academy can conjure.
5. Mahouka Koukou no Rettousei (2014)
Another anime for high school students is 'Mahouka Koukou no Rettousei.' It's about magic, the supernatural, and science fiction. It's a fun show with some beautiful images. 'Classroom of the Elite' and this anime share many similarities. Both anime focus on the lives of high school students. Students at the high school are separated based on their academic achievements. Students of a lesser level are undervalued and must work hard to improve their standing. In this anime, you'll see a lot of magic. Rather than the stuff of fairy tales and folklore, it is now polished technology that is used in people's everyday lives.
Magic is taught at First High School, a high-ranking institution that teaches pupils. On the basis of their achievement on the admissions tests, the school divides students into two groups. The Blooms outperform the Weeds, who struggle mightily. As a result, Tatsuya is placed in the Weeds class, whereas Miyuki, his cousin, is placed in the Blooms class. To be fair, Tatsuya isn't completely illiterate. He possesses a good deal of technical expertise and a solid fighting style. In addition, he has developed a unique set of magic skills. Anime focuses on students at an all-girls school.
4. Kakegurui (2017)
'Kakegurui' is a lot of fun to see. Throughout the show, there are numerous moments that heighten the tension. It's always a treat to watch an anime with a strong female lead in charge. The show's animation is quite good. Overall, the show has a vibrant and eye-catching aesthetic. Classroom of the Elites shares several similarities with this film. Neither anime is set outside of a school. Money is a status symbol among students at both schools, and those with more money are held in more regard than those from lower socioeconomic backgrounds.
Unlike other private schools, Hyakkaou Private Academy doesn't focus much emphasis on academics. To put it another way, school teaches pupils how to succeed in the real world. Of course, regular classes continue throughout the day. Although it's tedious, this isn't the major point of the article. There is nothing more thrilling than nighttime. High stakes gambling takes place during these hours. In this academy, money is king, and winning means a lot of money. Incoming freshman Yumeko Jabami is a newcomer to the school. She's beautiful and naive, but her unconventional attitude to gaming could make her the gambling queen at the school….
3. Grisaia no Kajitsu (2014)
A harem anime, 'Grisaia no Kajitsu,' can be described as such. It does, however, take a different path from the majority of harem anime. A logical and emotional build-up is used rather than a blatant attempt to make attractive female characters fall in love with the male protagonist. The show also features a lot of drama and a lot less humour than you may expect. Because of how the characters are developed, this anime is on my list. It is the backstories of the characters in both 'Classroom of The Elite' and 'Grisaia no Kajitsu' that give these works their complexity and depth.
There are several characters in this story that are connected to Mihama Academy. However, this institution differs from others in that it only has five pupils (all of whom are female) and a principal. This school accepts Yuuji Kazami as a student. He avoids interacting with others and prefers to be alone. However, in a classroom with a limited number of pupils sharing a similar area, there are bound to be interactions. Yuuji learns a lot about these girls and realizes that they are all unhappy individuals who may be headed for the bottom of the heap. It's hard to help others when you've got your own problems to deal with.
2. Ansatsu Kyoushitsu (2015)
"Ansatsu Kyoushitsu" is a great show that's full of laughs and surprises. A lot of effort has gone into the animation and character designs. Because of its similarities to 'Classroom of the Elite', it has been included on this list. The first thing to note is that both anime take place at a high school. Students in these shows are separated into groups based on their performance. Students at the bottom rungs of the academic ladder are motivated to rise to the top by a lack of consideration for their accomplishments.
In Kunugigaoka Middle School's Class 3-E, there are many underachievers and misfits. They are students who have failed to meet the standards or who have broken them. But they had no idea that they would be able to save the entire human race.. Half of the moon is wiped off by an unknown entity with a top speed of Mach 20. Unless he is killed, he pledges to do the same to Earth. That doesn't mean his nature is. He intends to give the assassins enough time to carry out their plan. In addition, he plans to instruct the kids of Class 3-E, providing them enough opportunity to assassinate him in the process. Do they have what it takes? Should they attempt to assassinate their all-time favorite professor?
1. Yahari Ore no Seishun Love Comedy wa Machigatteiru. (2013)
'Yahari Ore no Seishun Love Comedy wa Machigatteiru.' is set in a high school, like 'Classroom of The Elite.' The main protagonists in this anime are expected to join a club, despite the lack of guidelines on student segregation. Like in 'Classroom of the Elite,' the backstories of these characters are extremely relevant. Narcissism and semi-nihilism characterize Hachiman Hikigaya. It's as though he's the only one who knows the real meaning of life, and everyone else is simply playing tricks on him. In a writing assignment, he composes an essay ridiculing contemporary social interactions. His teacher, however, is not amused and forces him to join the Volunteer Service club, which aids other children in need in the local community. This group also includes Yukino Yukinoshita. She is socially awkward and possesses an icy demeanor. Does this person have the character to help others? How useful or detrimental will it be for Hachiman to see the world objectively and pessimistically?
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