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Viewing 8641 to 8670 of 8783
HISTORICAL
1960-03-01
Standard
AS291B
This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the latest issue of the American Standards Association publication ASA B46.1.
HISTORICAL
1960-03-01
Standard
ARP603
This Aerospace Recommended Practice (ARP) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.
HISTORICAL
1960-03-01
Standard
ARP581
This recommended practice covers a rail concept stand that may be used for horizontal disassembly and reassembly, and maintenance, incorporating certain design features which are defined herein. These features include the rail dimensions and width, length and height of stand to insure compatibility with rail concept type transport and positioning trailers.
HISTORICAL
1960-03-01
Standard
AS107C
This standard provides a method for the application of surface finish control primarily to aircraft engine and propeller parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.
HISTORICAL
1960-03-01
Standard
AS177A
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
HISTORICAL
1960-01-01
Standard
AMS3380
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid. Primarily for fluid lines operating in service up to 230 degrees C (446 degrees F) and under pressures up to 1500 psi (10,342 kPa).
CURRENT
1959-11-15
Standard
ARP591
Conventional Representation provides established drafting practice for showing various common part elements which are a compromise between complete pictorial representation and complete symbolization. The use of conventional representation materially reduces drafting time and thus increases drafting economy without impairing the clarity of the drawing.
HISTORICAL
1959-11-15
Standard
ARP246A
Numbering as provided herein is intended for convenience in locating a particular unit in a group of like or similar units.
HISTORICAL
1959-11-15
Standard
ARP510
To standardize Turbine and Compressor rotor blade drawing data and blade marking requirements for the purpose of classifying blades with respect to their moment weight.
HISTORICAL
1959-11-01
Standard
ARP670
HISTORICAL
1959-02-01
Standard
ARP373A
HISTORICAL
1959-02-01
Standard
ARP368A
CURRENT
1959-02-01
Standard
ARP265A
This Aeronautical Recommended Practice provides a standard method for locating and dimensioning the airfoil portions of parts such as blades, and vanes. This method will apply to blades, or vanes with or without a base. The forms of attachment are varied; therefore, the blade bases shown in the following figures are for illustration only. All dimensions and notes shown pertaining to the common functional point, line or plane are considered to be applied to a datum, on or off the part, irrespective of the form of attachment.
HISTORICAL
1959-02-01
Standard
AS595
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps, used in civil aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjunction with this AS for each pump.
HISTORICAL
1959-02-01
Standard
ARP575
These recommendations are written to cover the subject of obtaining filter patch test samples from aircraft hydraulic pumps of the categories shown below. The same procedure shall apply regardless of the pump drive category.
HISTORICAL
1959-02-01
Standard
AS127C
HISTORICAL
1959-02-01
Standard
AS567
This SAE Aerospace Standard (AS) covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained. The practices cover the types of retaining devices described in the following sections: a. Section 3: safety cable and safety wire; b. Section 4: key washers; and c. Section 5: cotter pins.
HISTORICAL
1958-08-01
Standard
AMS3389
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 250 psi (1724 kPa).
HISTORICAL
1958-08-01
Standard
AMS3388
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
CURRENT
1958-02-15
Standard
ARP464
HISTORICAL
1958-02-15
Standard
ARP24A
This SAE Aerospace Recommended Practice (ARP) provides analytical and test methods for determining pressure drop in fluid systems such as hydraulic, fluid, oil, and coolant used in aerospace vehicles. Determining pressure drop by analytical and test results will be discussed.
HISTORICAL
1957-11-15
Standard
ARP484
HISTORICAL
1957-11-15
Standard
ARP492
This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for th epurpose of determining their resistance to eterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L). The procedure recommended herin is based on experience gathered by a number of laboratories conducting component qualification tests to MIL-E-5009, currently MIL-E-5007. It is intendd to produce a uniform reproducible steady state test condition for fuel pump cavitation testing as required by various military engine specifications. This test is NOT intended to establish altitude, climb rate, starting, or other transient performance of the article tested.
HISTORICAL
1957-11-15
Standard
AS524
No scope available.
HISTORICAL
1957-11-15
Standard
AS471
No scope available.
HISTORICAL
1957-11-15
Standard
AS472
No scope available.
HISTORICAL
1957-11-15
Standard
AS470
No scope available.
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