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Viewing 1 to 30 of 5633
CURRENT
2017-12-12
Standard
AS6369/3
This is the solid flange design standard for the new AS6369 specification.
CURRENT
2017-12-12
Standard
AMS3050/3
The foundation specification (AMS3050) and this category specification (AMS3050/3) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Nickel only.
CURRENT
2017-12-12
Standard
AMS3050/1
The foundation specification (AMS3050) and this category specification (AMS3050/1) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Copper only.
CURRENT
2017-12-12
Standard
AMS3050/5
The foundation specification (AMS3050) and this category specification (AMS3050/5) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient PTFE only. For use only below 600 °F / 315 °C.
CURRENT
2017-12-12
Standard
AMS3050/2
The foundation specification (AMS3050) and this category specification (AMS3050/2) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Aluminum only.
CURRENT
2017-12-12
Standard
AMS3050/4
The foundation specification (AMS3050) and this category specification (AMS3050/4) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Molybdenum Disulphide; Graphite only.
CURRENT
2017-12-12
Standard
AMS3050/7
The foundation specification (AMS3050) and this category specification (AMS3050/7) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Copper+Graphite+Aluminum only.
CURRENT
2017-12-12
Standard
AMS3050/6
The foundation specification (AMS3050) and this category specification (AMS3050/6) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Nickel and Graphite only.
CURRENT
2017-12-12
Standard
AMS3050/9
The foundation specification (AMS3050) and this category specification (AMS3050/9) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Graphite+Calcium Fluoride only.
CURRENT
2017-12-12
Standard
AMS3050/8
The foundation specification (AMS3050) and this category specification (AMS3050/8) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Graphite+Aluminum only.
CURRENT
2017-12-12
Standard
AS6369/1
SCOPE IS UNAVAILABLE.
CURRENT
2017-12-12
Standard
AS6369/2
This is the sheet metal flange design standard for the new AS6369 specification.
CURRENT
2017-12-12
Standard
AS6369
This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 °F external ambient to +800 °F internal fluid.
CURRENT
2017-12-12
Standard
AS4716C
This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for O-ring seal glands for static and dynamic applications, and other seals.
2017-12-08
WIP Standard
AS85421B
Revision clarifies qualification/manufacturing details regarding initial form of fitting (standard near-net forgings, oversize forgings or bar stock). Additionally, replacing the lot-to-lot destructive testing with standardized periodic test procedures.
CURRENT
2017-12-07
Standard
AS1650E
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, and is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure. AS1650 was not designed for the new certification requirements for flammable leakage zones and fuel tanks for lightning protection and assembly redundancy. As such their use and installation may require additional efforts and equipment to support new FAA CFR compliance. The AS7510 flexible coupling should be the preferred coupling for use in flammable leakage zones and fuel tanks that require service life and functionality for lightning protection and part redundancy.
2017-12-07
WIP Standard
AS24586C
SCOPE IS UNAVAILABLE.
2017-12-07
WIP Standard
AS848A
No scope available.
2017-12-07
WIP Standard
AS7232A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made form a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600. Primarily for fastener applications requiring corrosion resistance and heat and oxidation resistance up to 2000 degrees F, but with reduced strength at the elevated temperatures. Rivets shall not be hand peened during driving.
2017-12-07
WIP Standard
MA1421A
This SAE Aerospace Standard (MA) establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module shaft or bearing retaining screw threads.
2017-12-07
WIP Standard
MA3344A
Scope is unavailable.
2017-12-07
WIP Standard
MA3350A
Scope is unavailable.
2017-12-07
WIP Standard
MA3287A
Scope is unavailable.
CURRENT
2017-11-30
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.
CURRENT
2017-11-30
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.
Viewing 1 to 30 of 5633

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