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Viewing 151 to 180 of 35602
2017-10-26
WIP Standard
ARP6812
This SAE Aerospace Recommended Practice (ARP) covers the functional, design, construction, and test requirements for Brake Temperature Monitoring Systems (BTMS), and sometimes referred to as Brake Temperature Indication Systems (BTIS). The BTMS is limited to aircraft where a dispatch indication and brake temperature indication is required. The scope of this BTMS equipment shall be limited to the 1) brake temperature sensor or indicator, 2) temperature reference measurement, if required, and 3) processing and communication of brake temperature. This recommended practice will not address cockpit ergonomics and aircraft operating procedures.
2017-10-26
WIP Standard
AS23053/10A
SCOPE IS UNAVAILABLE.
CURRENT
2017-10-26
Standard
AS101A
NO SCOPE AVAILABLE
2017-10-26
WIP Standard
AMS5797E
This specification covers a corrosion and heat-resistant cobalt alloy in the form of covered welding electrodes.
2017-10-25
WIP Standard
ARP1340B
This document specifies those requirements and procedures for periodic tests to insure maintenance of balance machine capabilities for balancing jet engine components.
2017-10-25
WIP Standard
ARP1840C
This document establishes two types of engine transport devices: Type A: For split engine pack transport (mainly lower deck) Type B: For full engine transport (mainly main deck)
2017-10-25
WIP Standard
ARP4166A
This Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible, reusable, water-vaporproof cover for environmental protection of internal combustion engines, major components, and other military and commercial items.
2017-10-25
WIP Standard
ARP4898A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.
2017-10-25
WIP Standard
ARP4732A
This SAE Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible nonreuseqble waterproof cover for shipment of aircraft engines, major components, and other military and commercial items not intended for storage; items to be removed within fourteen (14) days.
2017-10-25
WIP Standard
AMS5768L
This specification covers a corrosion and heat-resistant iron-chromium-nickel-cobalt alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
2017-10-25
WIP Standard
AMS5788G
This specification covers a corrosion and heat-resistant cobalt alloy in the form of welding rods, coating rods, or wrought wire.
2017-10-25
WIP Standard
AMS5860G
This specification covers a corrosion and moderate heat-resistant steel in the form of sheet, strip, and plate.
2017-10-25
WIP Standard
ARP826A
This document covers resolvers which are used to perform coordinate transformations as well as sine and cosine computations. It includes both the categories of compensated and uncompensated resolvers which perform these functions. Linear resolvers are also included because of their similarity to resolvers.
2017-10-25
WIP Standard
AS18013A
No scope available.
2017-10-25
WIP Standard
AMS5925B
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
2017-10-25
WIP Standard
AS5135A
This SAE Aerospace Standard (AS) describes the characteristics of a desiccant port installed through the flat wall of a shipping and storage container. With the cover removed, the desiccant port shall provide access to the interior of the container for installation and removal of desiccant.
2017-10-25
WIP Standard
AIR1213A
The scope of this report is limited to a discussion of candidate radioisotope power systems which are presently in varying stages of development, and is oriented principally towards aerospace applications.
2017-10-25
WIP Standard
AIR5709A
To present the results of a survey taken concerning future applications for high-temperature electronics and sensors.
2017-10-25
WIP Standard
ARP4729A
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 VDC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
2017-10-25
WIP Standard
AIR34B
The scope of this SAE Aerospace Information Report (AIR) is to present a guide for the determination of probable power output and the effect on the aircraft system that will be experienced when operating three-phase motors with one phase open. Unfortunately, the above subject cannot be resolved by specific rules. Modern aircraft or missile electrical systems are composed of a wide variety of electrical and electronic components. These components react differently under identical impetus due to the latitude of their design. This latidue of design must be allowed wherever possible to the accessory designer due to the various specification requirements. Therefore, it cannot be over-emphasized that the effect on the airplane or missile system, as well as motor operation, of three-phase motors on two-phase power must be thoroughly investigated.
2017-10-25
WIP Standard
ARP497B
In order to ease the equipment design engineer's problem and at the same time provide a basis for more accurate comparable measurements between manufacturer and user, this recommended practice sets up "standard conditions" for design assurance testing and tabulated values which differ from previous publications by requiring the motor to be in a warmed-up condition which approximates its average use temperature. These conditions and the basic tests to which the tabulated characteristics refer are grouped in section 2.2 (Design Assurance) and compose a complete list of defining characteristics of the motor. This recommendation establishes objectives for high performance control motors to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climate conditions of heat, cold, shock, vibration, altitude, and humidity.
2017-10-25
WIP Standard
AMS5792C
This specification covers a blend of tungsten carbide-cobalt aggregate, a nickel alloy, and a nickel aluminum aggregate in the form of powder.
2017-10-25
WIP Standard
AMS5805J
This specification covers a corrosion and heat resistant steel in the form of welding wire.
2017-10-25
WIP Standard
AMS5773F
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
2017-10-25
WIP Standard
AMS5780F
This specification covers a corrosion and moderate heat-resistant steel in the form of welding wire.
2017-10-25
WIP Standard
AMS5828H
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
2017-10-25
WIP Standard
AMS5808D
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
2017-10-25
WIP Standard
AMS5811E
This specification covers a corrosion and heat resistant steel in the form of welding wire.
Viewing 151 to 180 of 35602