Part 21 Report - 1997-551

ACCESSION #: 9709040119 Information & Support Services P.O. Box 3707 Seattle, WA 98124-2207 August 27, 1997 G-1151-SJA-97-395 Document Control Desk United States Nuclear Regulatory Commission Washington, D.C. 20555 Reference: a) Boeing Letter G-1151-RSO-92-365 dated August 31, 1992; R. S. Orr to the NRC Operations Center b) NRC Letter Docket No. 99901227 dated August 12, 1992; L. J. Norrholm to R. S. Orr; Subject: Response to 10 CFR 21 Inquiry Dear Sir or Madam: In accordance with the reference correspondence and 10 CFR 21, Boeing is sending the NRC the attached error notice(s) received from our former software suppliers. Because of unknown current addresses, the following former customers were not notified: Reactor Controls, Inc. Echo Energy Consultants, Inc. Nuclear Applications and Systems Analysis Company (Japan) Nuclear Power Services Error notices have been sent to our other former customers. Very truly yours, Sandra J. Andrews Nuclear Administrator Phone: (206) 865-6248 FAX: (206) 865-4851 Mail Stop: 7A-33, or e-mail: Sandra.Andrews@PSS.Boeing.com Enclosure(s): GTSTRUDL Program Report Form 97.07 Georgia Institute of Technology GTSTRUDL [Registered Copy] AUG 26 1997 August 19, 1997 Attention: Nuclear Administrator Boeing Information & Support Services P.O. Box 24346, M/S 7A-33 Seattle, Washington 98124-0346 RE: GT STRUDL Dear Sir or Madam: Enclosed please find copies of GTSTRUDL PROGRAM REPORT FORM 97.07 and a GTSTRUDL QA CUSTOMER ACKNOWLEDGEMENT FORM. Please sign and return the GTSTRUDL QA CUSTOMER ACKNOWLEDGEMENT FORM to acknowledge receipt of the GTSTRUDL Program Report. Thank you for reviewing the Program Report and for returning the Acknowledgement Form. Best regards, CASE Center David C. Key Configuration Control Manager Enclosures Computer Aided Structural Engineering Center Phone: (404) 894-2260 School of Civil & Environmental Engineering Fax: (404) 894-8014 Atlanta, Georgia 30332-0355 USA casec@ce.gatech.edu A Unit of the University System of Georgia GTSTRUDL Program Report Form GPRF No.: DATE: FROM: Computer-Aided Structural Engineering Center Georgia Institute of Technology Atlanta, Georgia 30332-0355 SEVERITY LEVEL: _ URGENT Problem results in incorrect answers which may not be apparent or job aborts and cannot be recovered within the session or job. _ SERIOUS Problem results in incorrect answers which are obvious or problem prevents completion of a particular user's task. _ MINOR Problem can be worked around or problem poses high frustration factor. _ INFORMATIVE Documentation error, program usage tip, user inconveniences. Date Problem Confirmed August 18, 1997 Date Notification Sent Computers PC Operating System DOS, Windows NT, Windows 95 Version All versions up to and including 97.01 Target Release for Correction 98.01 Mgr. ASD Signature Title R & D Division Michael H. Swanger Typed or Printed Name Date of Signature Signature Title Professional Services Division Typed or Printed Name Date of Signature Rev. 2.2 GTSTRUDL Program Report Form (Continued) GPRF No.: DATE: DESCRIPTION: The NONLINEAR ANALYSIS CONTINUE command will abort if a new load is created or a previously inactive load is newly activated prior to execution. This is not a valid operation. The NONLINEAR ANALYSIS CONTINUE command expects results to be available for the currently active load from previous NONLINEAR ANALYSIS or NONLINEAR ANALYSIS CONTINUE commands. An example of the command sequence that causes the abort follows: UNITS KIPS INCHES LOADING 1 JOINT LOADS 1 TO 10 FORCE Y -10.0 MAXIMUM NUMBER OF CYCLES 10 CONVERGENCE TOLERANCE DISPLACEMENT 0.001 NONLINEAR ANALYSIS $ $ Loading 2 is a new load with no results from a previous analysis. $ NONLINEAR ANALYSIS CONTINUE expects results to be available. $ LOAD 2 JOINT LOADS 1 TO 10 FORCE Y -20.0 LOAD LIST 2 NONLINEAR ANALYSIS CONTINUE The correct way to do this is shown below: UNITS KIPS INCHES LOADING 1 JOINT LOADS 1 TO 10 FORCE Y -10.0 Rev. 2.2 MAXIMUM NUMBER OF CYCLES 10 CONVERGENCE TOLERANCE DISPLACEMENT 0.001 NONLINEAR ANALYSIS $ $ The total joint loads applied to joints 1 to 10 is -20.0 kips in the global Y direction. $ Use CHANGES and ADDITIONS modes to add an additional -10.0 kips to $ loading 1. $ CHANGES LOAD 2 ADDITIONS JOINT LOADS 1 TO 10 FORCE Y -10.0 LOAD LIST 1 NONLINEAR ANALYSIS CONTINUE Rev. 2.2 *** END OF DOCUMENT ***

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