Refine Your Search

Topic

Search Results

Standard

Aerospace Vehicle Wiring, Lessons Learned

2017-06-05
WIP
AIR6808
This SAE Aerospace Information Report (AIR) is limited to the requirements of AS50881 and examines these requirements providing rationale behind them. SAE AS50881 is only applicable to the aircraft electrical wiring and interconnect system (EWIS). Pods and other devices that can be attached to an aircraft that are considered as aircraft equipment design. The AS50881 scope does not include attached devices, but does include the interface between the pod and aircraft wiring. Paragraph 3.3.5 addresses components such as antennas and other similar equipment that was once supplied as GFAE.
Standard

Mitigating Wire Insulation Damage During Processing and Handling

2009-12-30
CURRENT
AIR5717
Wire and cable products progress through a series of handling or operational steps from the time they leave the manufacturer, and until a finished harness or assembly is ready for installation on a vehicle. Throughout these many steps, environmental or processing conditions may be present which can generate damage detrimental to the wire or cable and/or its intended application.
Standard

Hot Stamp Wire Marking Concerns for Aerospace Vehicle Applications

2017-01-24
CURRENT
AIR5575A
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
Standard

Hot Stamp Wire Marking Concerns for Aerospace Vehicle Applications

2002-06-25
HISTORICAL
AIR5575
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
Standard

Transmission Lines, Transverse Electromagnetic Mode

2016-01-09
CURRENT
ARP81490A
This document covers the general recommendations for Transverse Electromagnetic Mode (TEM) Transmission Lines intended for use in airborne systems (see 6.2.14). For U.S military applications, TEM Transmission Lines shall meet the requirements in accordance with MIL-T-81490. The follow index lists the recommended requirements and methods covered by the Aerospace Recommended Practice (ARP):
Standard

Recommended Test Fluids for Electrical Components Used on Aircraft Exterior or for Ground Support Near Aircraft

1998-04-01
HISTORICAL
ARP5062
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommended test fluids for testing of electrical components used on aircraft exterior or for ground support near aircraft. These fluids were selected based on a consolidation of test fluids used by military and commercial sources and on review of national and international component specifications. These recommendations are general guidelines. Safety factors for any unusual testing applications or operating conditions should be given special consideration by the designer. The test fluids provided are intended to be recommendations and are not intended to limit or supersede those recommended by aircraft or ground support equipment manufacturers.
Standard

Recommended Test Fluids for Electrical Components Used on Aircraft Exterior or for Ground Support Near Aircraft

2012-11-21
CURRENT
ARP5062A
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommended test fluids for testing of electrical components used on aircraft exterior or for ground support near aircraft. These fluids were selected based on a consolidation of test fluids used by military and commercial sources and on review of national and international component specifications. These recommendations are general guidelines. Safety factors for any unusual testing applications or operating conditions should be given special consideration by the designer. The test fluids provided are intended to be recommendations and are not intended to limit or supersede those recommended by aircraft or ground support equipment manufacturers.
X