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ASQ SW1005 - ANSI/ISO/ASQC Q9000-1994 SERIES STANDARD ELECTRONIC VERSION FOR WINDOWS Organization: ASQ
ASQ SW1014 - ANSI/ISO/ASQC Q9000-1994 SERIES STANDARDS - LAN VERSION FOR WINDOWS Organization: ASQ
ASQ SW1052 - ANSI/ISO/ASQC Q9000-1994 SERIES STANDARDS FOR WINDOWS 95 *INCLUDES 3 1/2" DISK, USER'S MANUAL & INSTALLATION INSTRUCTIONS* Organization: ASQ
ASQ SW1063 - ANSI/ISO/ASQC Q9000-1994 SERIES STANDARDS FOR WINDOWS 95 *INCLUDES 3 1/2" DISK, USER'S MANUAL & INSTALLATION INSTRUCTIONS* *LAN VERSION - UNLIMITED NUMBER OF USERS AT SINGLE SITE* Organization: ASQ
IWCA - BOMA I-14.1 - BOMA I-14 WINDOW CLEANING SAFETY STANDARD FOR EQUIPMENT MANUFACTURERS, DESIGNERS AND INSTALLERS (THIS GUIDEBOOK FOCUSES ON THE ASPECTS OF THE ANSI/IWCA STANDARD THAT IMPACTS COMMERCIAL PROPERTY PROFESSIONALS) Organization: IWCA
UL 199J OUTLINE - UL OUTLINE FOR INVESTIGATION FIRE TESTING OF SPECIFIC APPLICATION SPRINKLERS FOR USE ON WINDOWS - ISSUE 1 Organization: UL
Date: 2014-05-16
Description:   These sprinklers have not been investigated for use as a substitute for fire protection rated glazing materials investigated in accordance with ANSI/UL 9, Fire Tests of Window Assemblies.
ASTM E1996 - STANDARD SPECIFICATION FOR PERFORMANCE OF EXTERIOR WINDOWS, CURTAIN WALLS, DOORS, AND IMPACT PROTECTIVE SYSTEMS IMPACTED BY WINDBORNE DEBRIS IN HURRICANES Organization: ASTM
Date: 2014-10-01
Description: This specification covers exterior windows, glazed curtain walls, doors, and impact protective systems used in buildings located in geographic regions that are prone to hurricanes.
ASTM E1886 - STANDARD TEST METHOD FOR PERFORMANCE OF EXTERIOR WINDOWS, CURTAIN WALLS, DOORS, AND IMPACT PROTECTIVE SYSTEMS IMPACTED BY MISSILE(S) AND EXPOSED TO CYCLIC PRESSURE DIFFERENTIALS Organization: ASTM
Date: 2013-10-01
Description: This test method covers the performance of exterior windows, curtain walls, doors, and impact protective systems impacted by missile(s) and subsequently subjected to cyclic static pressure differentials.
CTA - EIA/CEA-860 - DEVICE PLUG-IN INTERFACE TO EIA-709.1 NETWORK TOOLS - FORMERLY EIA/CEA-860 Organization: CTA
Date: 2001-01-01
Description: Network tool software and device plug-in software properly implementing their appropriate sides of the interfaces described in this specification interoperate on Microsoft® Windows® and Windows NT® platforms using the Component Object Model (COM) technology for interoperability.
CTA-860 - DEVICE PLUG-IN INTERFACE TO EIA-709.1 NETWORK TOOLS - FORMERLY CEA-860-A; INCLUDES ACCESS TO ADDITIONAL CONTENT Organization: CTA
Date: 2002-12-01
Description: Network tool software and device plug-in software properly implementing their appropriate sides of the interfaces described in this specification interoperate on Microsoft® Windows® and Windows NT® platforms using the Component Object Model (COM) technology for interoperability.
UL - 1815 BULLETIN - UL STANDARD FOR SAFETY NONDUCTED HEAT RECOVERY VENTILATORS - COMMENTS DUE: SEPTEMBER 02, 2011 Organization: UL
Date: 2011-07-18
Description: These requirements cover heat recovery ventilators that may be mounted through a wall or ceiling, or in a window. These requirements cover heat recovery ventilators that may employ short ducts intended to bring air to and from the equipment.
UL 1815 - UL STANDARD FOR SAFETY NONDUCTED HEAT RECOVERY VENTILATORS - FIFTH EDITION Organization: UL
Date: 2012-02-29
Description: These requirements cover heat recovery ventilators that may be mounted through a wall or ceiling, or in a window.  These requirements cover heat recovery ventilators that may employ short ducts intended to bring air to and from the equipment.
ESDU 00036 - AIRCRAFT PERFORMANCE PROGRAM PART 6: EXAMPLES OF APPLICATION PROGRAMS APP02 AND APP03 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00031 - AIRCRAFT PERFORMANCE PROGRAM PART 1: INTRODUCTION TO THE COMPUTER PROGRAMS FOR AIRCRAFT PERFORMANCE EVALUATION Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00033 - AIRCRAFT PERFORMANCE PROGRAM PART 3: BRIEF GUIDE PROGRAMS APP02, APP03 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00039 - AIRCRAFT PERFORMANCE PROGRAM PART 9: TESTING PROGRAMS APP02 AND APP03 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00037 - AIRCRAFT PERFORMANCE PROGRAM PART 7: ERROR MESSAGES PROGRAMS APP02 AND APP03 Organization: ESDU
Date: 2009-04-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00034 - AIRCRAFT PERFORMANCE PROGRAM PART 4: BRIEF FORM OF INPUT AND OUTPUT PROGRAMS APP02, APP03 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00035 - AIRCRAFT PERFORMANCE PROGRAM PART 5: DETAILED INPUT AND OUTPUT PROGRAM APP02 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.
ESDU 00038 - AIRCRAFT PERFORMANCE PROGRAM PART 8: DESCRIPTION OF APP02 Organization: ESDU
Date: 2013-10-01
Description: The programs are written in ANSI FORTRAN and are supplied as compiled executable binary (*.EXE) files for use under any 32-bit or 64-bit Microsoft Windows operating system. The suite of programs uses SI units internally.

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