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Viewing 271 to 300 of 35892
CURRENT
2017-11-21
Standard
AS5316
This SAE Aerospace Standard (AS) specifies the general requirements for data recording procedures, packaging, and storing of elastomeric seals and seal assemblies which include an elastomeric element prior to the seal being assembled into hardware components. NOTE: The requirement for packaging is an integral part of the controlled storage procedure and provides a means of positive product identity from the time of manufacture to the time of assembly into a component.
CURRENT
2017-11-21
Standard
ARP6807
The intent of the SAE Aerospace Recommended Practice (ARP) is to provide a process for users to identify the part number of AS7928 terminal lugs installed in civilian or military applications, although it can also can be used to identify terminals that have been stored incorrectly. This ARP is subject to change to keep pace with experience and technical advances of AS7928 terminals. A current set of tables are provided to list and identify current AS7928 terminal lug configurations per the associated specification detail sheet and terminal lug configuration. Specific configuration details, graphic, size and marking information for each individual terminal lug is provided to assist the product user with accurate selection for replacement or identification.
CURRENT
2017-11-21
Standard
AS6294/1
This document establishes common industry practices and recommended screening, qualification, and lot acceptance testing of Plastic Encapsulated Microcircuits (PEMs) for use in space application environments.
CURRENT
2017-11-21
Standard
AS6495B
CURRENT
2017-11-21
Standard
AMS2431/1F
This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of conditioned cast steel shot with a hardness of 45 to 52 HRC.
CURRENT
2017-11-21
Standard
AIR5867
This report revises ARD50015 document to the AIR format. This report, as was the original, is intended to complement ARP1420C and AIR1419C documents issued by the SAE S-16 Committee on spatial total-pressure distortion. These previous documents addressed only total-pressure distortion and excluded total temperature distortion. The subject of inlet total temperature distortion is addressed in this report with some background and identification of the problem area. The status of past efforts is reviewed, and an attempt is made to define where we are today. Deficiencies, voids, and limitations in knowledge and test techniques for total temperature distortion are identified.
CURRENT
2017-11-21
Standard
AMS3330C
This specification covers a fluorosilicone (FVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
CURRENT
2017-11-21
Standard
AMS3329C
This specification covers a fluorosilicone (FVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
CURRENT
2017-11-21
Standard
AMS6501E
This specification covers a maraging steel in the form of welding wire.
CURRENT
2017-11-21
Standard
AMS6302K
This specification covers an aircraft‐quality, low‐alloy, heat‐resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
2017-11-21
Standard
AMS4916L
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness (see 8.6).
CURRENT
2017-11-20
Standard
AMS3382D
This specification covers two classes (durometers) of tetrafluoroethylene/propylene rubber (FEPM) in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7255 or AMS7256 specification, as appropriate.
CURRENT
2017-11-20
Standard
AMS2451/11B
This specification covers the requirements for brush plating of cobalt by electrodeposition.
CURRENT
2017-11-20
Standard
AIR1419C
This document addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the development of techniques used to assess engine stability margins in the presence of inlet total-pressure distortion. Specific performance and stability issues that are covered by this document include total-pressure recovery and turbulence effects and steady and dynamic inlet total-pressure distortion.
CURRENT
2017-11-20
Standard
AMS6951
This specification covers a titanium alloy in the form of sheet 0.025 through 0.100 inches (0.63 through 2.54 mm) inclusive in thickness (see 8.5).
CURRENT
2017-11-20
Standard
AS931C
CURRENT
2017-11-20
Standard
AMSQQA200/4C
This specification covers the specific requirements for aluminum alloy 5083 bar, rod, shapes, tube, and wire produced by extrusion.
CURRENT
2017-11-20
Standard
AMS3331C
This specification covers a fluorosilicone (FVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
2017-11-18
WIP Standard
AIR26B
This SAE Aerospace Information Report (AIR) records the dimensions for the No. 70-90, 70L-90, 80-100 and 80L-100 dual rotation propeller shaft ends, which have been deleted from ARP375.
2017-11-18
WIP Standard
AIR809B
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between methods I and II.
2017-11-18
WIP Standard
AIR1471B
The purpose of this SAE Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when a common torque value per size is the objective.
2017-11-18
WIP Standard
AS3216B
No scope available.
2017-11-18
WIP Standard
AS3215B
Scope not available.
2017-11-18
WIP Standard
AS4847B
This design standard provides information on the use of self-locking shank nuts, thread sizes .1640-36 thru .3750-24, together with details of flange hole and abutment shoulder for their installation.
2017-11-18
WIP Standard
ARP674D
Groove designs presented herein are applicable for use with the following MS metal O-ring gaskets, or to dimensionally equivalent gaskets of other materials: a. AMS 5570 or AMS 5576 Plain 1. MS9141 - 0.035 tube x 0.006 wall 2. MS9142 - 0.062 tube x 0.006 wall 3. MS9202 - 0.062 tube x 0.010 wall 4. MS9203 - 0.094 tube x 0.006 wall 5. MS9204 - 0.094 tube x 0.010 wall 6. MS9205 - 0.125 tube x 0.010 wall b. AMS 5570 or AMS 5576 Silver Pl. 1. MS9371 - 0.035 tube x 0.006 wall 2. MS9372 - 0.062 tube x 0.006 wall 3. MS9373 - 0.062 tube x 0.010 wall 4. MS9374 - 0.094 tube x 0.006 wall 5. MS9375 - 0.094 tube x 0.010 wall 6. MS9376 - 0.125 tube x 0.010 wall
2017-11-18
WIP Standard
ARP676A
No scope available.
Viewing 271 to 300 of 35892