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SAE AIR4004 - GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR Organization: SAE
Date: 2015-07-01
Description: Recent field experience has indicated significant problems with some types of wire and cables as routed on aircraft landing gear. This SAE Aerospace Information Report (AIR) is intended to identify environmental concerns the designer should consider, materials that appear to be most suitable for use in these areas, routing, clamping, and other protection techniques that are appropriate in these applications.
ASME B107.18M - PLIERS (WIRE TWISTER) Organization: ASME
Date: 1996-01-01
Description: This Standard is intended to cover the general dimensional and functional characteristics for wire twister pliers, which are used primarily for twisting safety wires on critical equipment on aircraft, automotive equipment, and for other similar applications.
ASME B107.18 - PLIERS: WIRE TWISTER Organization: ASME
Date: 2003-09-05
Description: This Standard is intended to cover the general dimensional and functional characteristics for wire twister pliers, which are used primarily for twisting safety wires (lock wire) on critical equipment on aircraft, automotive equipment, and for other similar applications.
ARINC 822A - ON-GROUND AIRCRAFT WIRELESS COMMUNICATION Organization: ARINC
Date: 2016-07-14
Description: Document Scope This specification addresses the following types of IPv4-based connections between an aircraft on the ground and the airline’s network infrastructure: Connections based on IEEE 802.11 wireless LAN standards Connections using cellular technologies: 3G, Universal Mobile Telecommunications System (UMTS), 4G, and Long Term Evolution (LTE) This specification does not address the following technologies, nor does it preclude their future addition based on market demand: Wired connections to the aircraft at the gate, e.g., powerline communications AeroMACS, an aviation implementation of IEEE 802.16e (WiMAX) that uses protected spectrum to carry safety communications 5G cellular IPv6 Elements necessary for interoperability in the radio and network layers are addressed while methods for application data transfer are out of scope.
SAE/TP - 2007-01-3900 - AN ELECTRO – MECHANICAL ACTUATOR FOR GENERAL AVIATION AIRCRAFT Organization: SAE/TP
Date: 2007-09-17
Description: Due to the focus of applicability in General Aviation aircraft and corresponding certification efforts the ECS requires the development of a highly integrated, absolutely safety critical, all-electric full fly-by-wire platform with low risk investment capability for both supplier and customer.
ASTM F2799 - STANDARD PRACTICE FOR MAINTENANCE OF AIRCRAFT ELECTRICAL WIRING SYSTEMS Organization: ASTM
Date: 2014-05-01
Description: This philosophy stresses the importance of protective measures when working on or around wire bundles and connectors. It stresses how important it is to protect EWIS during structural repairs, (STC) installations, or other alterations by ensuring that metal shavings, debris, and contamination resulting from such work are removed.
SAE AMS1424 - (R) DEICING/ANTI-ICING FLUID, AIRCRAFT SAE TYPE 1 Organization: SAE
Date: 2016-05-01
Description: Application The fluid is generally used heated either diluted with water, or as supplied, for the removal of deposits of frost, ice, and snow on exterior aircraft surfaces prior to take off. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated.
ASTM F2639 - STANDARD PRACTICE FOR DESIGN, ALTERATION, AND CERTIFICATION OF AIRCRAFT ELECTRICAL WIRING SYSTEMS Organization: ASTM
Date: 2015-08-01
Description: Protections and Cautions—This practice provides guidance for developing actions and cautionary statements to be added to maintenance instructions for the protection of wire and wire configurations. Maintenance personnel will use these enhanced procedures to minimize contamination and accidental damage to electrical wiring interconnection system (EWIS) while working on aircraft.
SAE/TP - 2006-01-3091 - AIRCRAFT ELECTRICAL SYSTEM MONITORING WITH ARC FAULT CIRCUIT PROTECTION AND AUTOMATIC FAULT LOCATION Organization: SAE/TP
Date: 2006-11-07
Description: As electrical systems on-board commercial and military aircraft grow in complexity they must also be designed for enhanced safety and functionality.
SAE R-285 - THE WORLD'S MOST SIGNIFICANT AND MAGNIFICENT AIRCRAFT EVOLUTION OF THE MODERN AIRPLANE - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: SAE
Date: 2000-07-21
Description: The pioneers tried everything and anything for power plant, structural design, and aerodynamic configuration—frequently without regard to the basic principles of physics, engineering, and aeronautics, or their possible effect on flight performance, handling characteristics, and safety. Over time, aircraft utility and performance developed not only through aerodynamic refinement but also as permitted by the pace of structural, control-system, and power-plant design.
SAE ARP6001 - AEROSPACE - PASSIVE SIDE STICK UNIT GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS Organization: SAE
Date: 2012-07-01
Description: This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic "passive" side stick that could be used for fly by wire transport and business aircraft. It addresses the following: • The functions to be implemented • The geometric and mechanical characteristics • The mechanical and electrical interfaces • The safety and certification requirements
SAE AS4461 - ASSEMBLY AND SOLDERING CRITERIA FOR HIGH QUALITY/HIGH RELIABILITY SOLDERING WIRE AND CABLE TERMINATION IN AEROSPACE VEHICLES Organization: SAE
Date: 2016-07-01
Description: Strain Relief The use of solder devices for wire or cable terminations in aircraft requires strain relief in all applications or designs with no strain on the solder terminations.
SAE AMS3388 - HOSE, AIRCRAFT FUELING, ACRYLONITRILE BUTADIENE (NBR) RUBBER SINGLE WIRE BRAID REINFORCED, CHLOROPRENE COVERED, NONCOLLAPSING Organization: SAE
Date: 1993-10-01
Description: Application: This hose has been used typically for fueling aircraft, but usage is not limited to such applications.
SAE AMS3389 - HOSE, AIRCRAFT FUELING, ACRYLONITRILE BUTADIENE (NBR) RUBBER DOUBLE WIRE BRAID REINFORCED, CHLOROPRENE COVERED, NONCOLLAPSING Organization: SAE
Date: 1993-10-01
Description: Application: This hose has been used typically for fueling aircraft, but usage is not limited to such applications.
UL 62841-3-4 - UL STANDARD FOR SAFETY ELECTRIC MOTOR-OPERATED HAND-HELD TOOLS, TRANSPORTABLE TOOLS AND LAWN AND GARDEN MACHINERY – SAFETY – PART 3-4: PARTICULAR REQUIREMENTS FOR TRANSPORTABLE BENCH GRINDERS - FIRST EDITION Organization: UL
Date: 2016-12-23
Description: Addition: This part of IEC 62841 applies to transportable bench grinders that can be equipped with one or two accessories as follows: – type 1 grinding wheels in accordance with ISO 603-4:1999 with a diameter not exceeding 310 mm and a thickness not exceeding 55 mm; – wire brushes with a diameter not exceeding 310 mm and a thickness not exceeding 55 mm; – polishing wheels with a diameter not exceeding 310 mm; and with a peripheral speed of any accessory between 10 m/s and 50 m/s.
DS/EN 60335-2-76/A1 - HOUSEHOLD AND SIMILAR ELECTRICAL APPLIANCES - SAFETY - PART 2-76: PARTICULAR REQUIREMENTS FOR ELECTRIC FENCE ENERGIZERS Organization: DS
Date: 2006-09-22
Description: This standard deals with the safety of electric fence energizers, the rated voltage of which is not more thatn 250 V and by means of which fence wires in agricultural, domestic or fedral animal control fences and security fences may be electrified or monitores.
CENELEC - EN 60335-2-76 - HOUSEHOLD AND SIMILAR ELECTRICAL APPLIANCES – SAFETY PART 2-76: PARTICULAR REQUIREMENTS FOR ELECTRIC FENCE ENERGIZERS - INCORPORATES AMENDMENT A2: 2015 Organization: CENELEC
Date: 2005-02-01
Description: This International Standard deals with the safety of electric fence energizers, the rated voltage of which is not more than 250 V and by means of which fence wires in agricultural, domestic or feral animal control fences and security fences may be electrified or monitored.
CEI EN 62282-5-1 - FUEL CELL TECHNOLOGIES PART 5-1: PORTABLE FUEL CELL POWER SYSTEMS - SAFETY Organization: CEI
Date: 2013-07-01
Description: This standard does not apply to portable fuel cell power systems that are a) permanently connected (hard wired) to the electrical distribution system, b) permanently connected to a utility fuel distribution system, c) exporting power to the grid, d) for propulsion of road vehicles, e) intended to be used on board passenger aircraft.
CENELEC - EN 62282-5-1 - FUEL CELL TECHNOLOGIES - PART 5-1: PORTABLE FUEL CELL POWER SYSTEMS - SAFETY Organization: CENELEC
Date: 2012-11-01
Description: This standard does not apply to portable fuel cell power systems that are a) permanently connected (hard wired) to the electrical distribution system, b) permanently connected to a utility fuel distribution system, c) exporting power to the grid, d) for propulsion of road vehicles, e) intended to be used on board passenger aircraft Fuel cells that provide battery charging for hybrid vehicles where the battery provides power and energy for propulsion of the vehicle are not included in the scope of this standard The following fuels and fuel feedstocks are considered within the scope of this standard: • natural gas; • liquefied petroleum gas, such as propane and butane; • liquid alcohols, for example methanol, • ethanol; • gasoline; • diesel; • kerosene; • hydrogen; • metals (e.g.
IEC 62282-5-1 - FUEL CELL TECHNOLOGIES – PART 5-1: PORTABLE FUEL CELL POWER SYSTEMS – SAFETY - EDITION 2.0 Organization: IEC
Date: 2012-09-01
Description: This standard does not apply to portable fuel cell power systems that are a) permanently connected (hard wired) to the electrical distribution system, b) permanently connected to a utility fuel distribution system, c) exporting power to the grid, d) for propulsion of road vehicles, e) intended to be used on board passenger aircraft.

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