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GA - 620 - GYPSUM AREA SEPARATION FIREWALLS Organization: GA
Date: 2011-01-01
Description: The clips on the non-fire side are protected by the Gypsum Area Separation Firewall and will continue to support the Gypsum Area Separation Firewall, allowing it to remain intact, protecting the neighboring unit.
SAE AMS3374 - SEALING COMPOUND AIRCRAFT FIREWALL, SILICONE Organization: SAE
Date: 2013-11-01
Description: Application These products are used primarily for sealing aircraft firewall structures against passage of air, vapors, and flames but usage is not limited to such applications.
TIA-455-172 - FOTP-172 FLAME RESISTANCE OF FIREWALL CONNECTOR - ANSI APPROVAL WITHDRAWN MARCH, 2004 Organization: TIA
Date: 1986-04-01
Description: 1.0 INTENT This procedure provides for a test to determine the ability of a cabled and mated connector (plug and receptacle) to resist firewall environments, such as flame or ignition of gases.
SAE AMS3381 - SEALING COMPOUND, AIRCRAFT FIREWALL, NON-SILICONE Organization: SAE
Date: 2014-05-01
Description:   Application These products are used primarily for sealing aircraft firewall structures against passage of air, vapors, and flames but usage is not limited to such applications.
PACKT - CONFIGURING IPCOP FIREWAL - CONFIGURING IPCOP FIREWALLS: CLOSING BORDERS WITH OPEN SOURCE Organization: PACKT
Date: 2006-10-01
Description: Anyone interested in securing their networks with IPCop â€" from those new to networking and firewalls, to networking and IT Professionals with previous experience of IPCop.
SAE AS5127/2 - (R) TEST METHOD FOR AEROSPACE FIREWALL SEALANT FLAME PENETRATION Organization: SAE
Date: 2014-05-01
Description: This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193.
SAE AMS3374/1 - SEALING COMPOUND, ONE-PART SILICONE (TYPE 1) AIRCRAFT FIREWALL Organization: SAE
Date: 2011-02-01
Description: Application: This product is used primarily for sealing aircraft firewall structures against passage of air and vapors. The cured compound shall remain an effective sealant at all temperatures between −65 and +400 °F (−54 to +204 °C) and shall be able to withstand a flash temperature of 2000 °F (1093 °C).
SAE AMS3374/4 - SEALING COMPOUND TWO-PART, POLYSULFIDE (TYPE 4) FIREWALL SEALANT Organization: SAE
Date: 2011-02-01
Description: Application: This product is used primarily for sealing aircraft firewall structures against passage of air and vapors. The cured compound shall remain an effective sealant at all temperatures between −65 and +400 °F (−54 to +204 °C) and shall be able to withstand a flash temperature of 2000 °F (1093 °C).
SAE AMS3374/3 - SEALING COMPOUND TWO-PART, CONDENSATION CURED (TYPE 3) FIREWALL SEALANT Organization: SAE
Date: 2011-02-01
Description: Application: This product is used primarily for sealing aircraft firewall structures against passage of air and vapors. The cured compound shall remain an effective sealant at all temperatures between −65 and +400 °F (−54 to +204 °C) and shall be able to withstand a flash temperature of 2000 °F (1093 °C).
ECIA - EIA-364-45 - TP-45C FIREWALL FLAME TEST PROCEDURES FOR ELECTRICAL CONNECTORS Organization: ECIA
Date: 2012-11-01
Description: This standard establishes a test method to determine the ability of a mated pair of electrical firewall connectors to resist specified flame and vibration conditions during 20 minutes of exposure by preventing flames from breaching the firewall through the connectors and providing specific electrical performance for the first 6 minutes.
ECIA - EIA/ECA-364-45 - TP-45A FIREWALL FLAME TEST PROCEDURE FOR ELECTRICAL CONNECTORS Organization: ECIA
Date: 2000-05-01
Description: This standard establishes a test method to determine the ability of a mated electrical firewall connector to resist specified flame and vibration during a 20 minute exposure by preventing the flame from breaching the firewall through the connector, and providing specified electrical performance for the first 6 minutes of the 20 minute exposure.
SAE AMS3374/2 - SEALING COMPOUND TWO-PART, ADDITION CURED SILICONE (TYPE 2) FIREWALL SEALANT Organization: SAE
Date: 2011-02-01
Description: Application: This product is used primarily for sealing aircraft firewall structures against passage of air and vapors. The cured compound shall remain an effective sealant at all temperatures between −65 and +400 °F (−54 to +204 °C) and shall be able to withstand a flash temperature of 2000 °F (1093 °C).
PACKT - DESIGNING AND IMPLEM LINU - DESIGNING AND IMPLEMENTING LINUX FIREWALLS AND QOS USING NETFILTER, IPROUTE2, NAT AND L7-FILTER Organization: PACKT
Date: 2006-10-31
Description: supportAnnotations]--> with some understanding of Linux security threats and issues, or any one interested in securing their systems behind a firewall. Basic knowledge of Linux is presumed but other than that this book shows you how to do the rest, from configuring your system to dealing with security breaches.
SAE-ITC - SAE ITC TS335 - FIRE PROOF, FIREWALL - FORMERLY ADS TS335 Organization: SAE-ITC
NPFC - MIL-S-38249 - SEALING COMPOUND, FIREWALL Organization: NPFC
AFNOR - NF Z74-262 - PROTECTION PROFILE - PERSONAL FIREWALL Organization: AFNOR
Date: 2009-10-01
AFNOR - NF Z74-263 - PROTECTION PROFILE - IP INTERCONNECTION FIREWALL Organization: AFNOR
Date: 2009-10-01
ISO/IEC DIS 29341-24-11 - INFORMATION TECHNOLOGY - UPNP DEVICE ARCHITECTURE PART 24-11: INTERNET GATEWAY DEVICE CONTROL PROTOCOL - LEVEL 2 - WIDE AREA NETWORK INTERNET PROTOCOL V6 - FIREWALL CONTROL SERVICE Organization: ISO
Date: 2015-09-03
Description: This service supports the management IPv6 firewall pinholes in Internet gateway devices independent of the WAN access type (PPP, DHCP, ...).
ECIA - SP4524 - FIREWALL FLAME TEST PROCEDURE FOR ELECTRICAL CONNECTORS - COMMENT PERIOD EXPIRES: MAY 17, 1999 Organization: ECIA
Date: 1999-03-15
NASA-STD-2813 - NASA FIREWALL STRATEGY ARCHITECTURE, STANDARDS AND PRODUCTS - INACTIVE PER EMAIL FROM NASA 1/11/2008. OCIO CONSIDERS THIS TECHNICAL STANDARD AS OBSOLETE. Organization: NASA
Date: 1997-08-19

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