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Viewing 8641 to 8670 of 8780
HISTORICAL
1960-03-01
Standard
J726_196003
The air cleaner test code has been established to cover dry type and oil bath air cleaners used on internal combustion engines and to present a uniform method of determining and reporting air cleaner performance.
HISTORICAL
1960-03-01
Standard
ARP584
This SAE Aerospace Recommended Practice (ARP) encompasses design, analysis, fabrication, and installation of pressurized metal tubing used in fluid power systems to provide relative motion. Specific data given are for MIL-T_6845 tubing ranging from 1/4 to 1 in. (6.3 to 25 mm) to diameter used in 3000 psi (20.7 MPa) hydraulic or pneumatic system, Military Type I, II, III, or IV hydraulic systems applied to any type of vehicle. For information on design of coiled tube assemblies using Ti-3Al-2.5CWSR tubing, see ARP4146. The flexible configurations of tubing are intended for application to actuators that oscillate about a pivot, to areas of large structural deflection such as reservoirs installation, and to areas of extrement environment where flexible hose could not survive. The purpose of this document is to proide engineering guidance in designing metal tubing configurations that provide for large relative motion between contiguous points in fluid piping systems.
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
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
1959-11-15
Standard
ARP246A
Numbering as provided herein is intended for convenience in locating a particular unit in a group of like or similar units.
HISTORICAL
1959-11-01
Standard
ARP670
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
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.
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
ARP373A
HISTORICAL
1959-02-01
Standard
ARP368A
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
AS468
No scope available.
HISTORICAL
1957-11-15
Standard
AS472
No scope available.
HISTORICAL
1957-11-15
Standard
AS471
No scope available.
HISTORICAL
1957-11-15
Standard
AS470
No scope available.
HISTORICAL
1957-11-15
Standard
AS524
No scope available.
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
1957-11-01
Standard
AS473
No scope available.
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