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Viewing 8641 to 8670 of 8840
HISTORICAL
1962-11-01
Standard
AS692
This specification establishes the performance, qualification, acceptance limits, and identification for aeronautical engine high tension spark igniters.
HISTORICAL
1962-11-01
Standard
ARP755
This SAE Aerospace Recommended Practice (ARP) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives.
HISTORICAL
1962-10-30
Standard
AS534
HISTORICAL
1962-10-30
Standard
AS532
HISTORICAL
1962-10-30
Standard
AS533
HISTORICAL
1962-10-30
Standard
AS516
HISTORICAL
1962-10-30
Standard
AS515
HISTORICAL
1962-10-30
Standard
AS517
HISTORICAL
1962-10-15
Standard
ARP763
This specification covers ground type hydropneumatic pressure accumulators for use in ground support hydraulic systems at rated pressures ranging up to 5,000 psi including details pertinent to the design, fabrication, and performance of the accumulators.
HISTORICAL
1962-09-01
Standard
AS701
No scope available.
CURRENT
1962-09-01
Standard
AIR781
A general discussion is presented herein, to outline the starter functions which are necessary for a successful engine start. In addition, sample calculations are included to illustrate an accepted method of determining the engine starting time from known data. Further consideration is then given to the relationship between starter torque output and engine pad strength and a generalized formula is presented for calculating the theoretical transient torque peaks for a simplified starter-engine system. Sample calculations for actual tests are included, and the results of these calculations are compared with measured values.
HISTORICAL
1962-08-30
Standard
ARP743
This method describe the procedure for (1) sampling air in contamination controlled spaces for air-borne particulate contamination 5u or greater in size and for (2) the microscopic determination of the concentration and size range distribution of the particulate material removed from the air sample.
HISTORICAL
1962-06-30
Standard
ARP704
HISTORICAL
1962-06-30
Standard
ARP716
To establish recommended gap settings for aircraft piston engine spark plugs.
CURRENT
1962-06-01
Standard
ARP489A
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
1962-04-01
Standard
J816_196204
CURRENT
1962-03-01
Standard
AS420B
This Aerospace Standard covers Flight Directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a pre-selected flight plan.
HISTORICAL
1962-02-01
Standard
AIR737
This report lists military and industry specifications and standards which are used in Aero/Space Hydraulic and Pneumatic Systems. It is intended as a supplement to Specifications MIL-H-5440 and MIL-P-5518. Only those hardware standards which have been specifically designed for hydraulic or pneumatic use are listed. Revisions and amendments which are current for these specifications and standards are not listed.
HISTORICAL
1962-01-15
Standard
AS269C
This SAE Aerospace Standard (AS) provides material identification codes for aluminum alloys, copper alloys, carbon steels, alloy steels, titanium alloys, corrosion resistant materials, and heat resistant materials that are used to make AN, MS, and AS engine and propeller standard utility parts. This document also provides similar material codes for company parts (such as nuts, bolts, etc.) having design configuration similar to other company parts or the engine and propeller standard utility parts (AN, MS, and AS) that are not of the same material.
HISTORICAL
1962-01-01
Standard
ARP680A
This recommended practice covers a series of stands that may be used for assembly, disassembly and maintenance; incorporating the following design criteria: a collapsible frame construction, envelope dimensions, attachment shear pad configuration and gear box and caster specifications.
HISTORICAL
1962-01-01
Standard
ARP260B
HISTORICAL
1961-12-31
Standard
ARP719
Gas for the purpose of this ARP shall be defined as the gaseous produces) resulting from the decomposition, dissociation, or combustion of liquid or solid mono or bi-propellants. Where other gases such as heated N2, H2, H2O (steam), etc., which may have similar physical and/or chemical properties as the defined "gas", are used to effect testing economies; they may be considered as being included in this ARP.
HISTORICAL
1961-12-15
Standard
ARP748
HISTORICAL
1961-12-15
Standard
AS28A
This specification covers aircraft reciprocating engine shielded and unshielded spark plugs.
HISTORICAL
1961-10-15
Standard
ARP480
This document lists recommended noun titles for drawings of support equipment and provides definition for each. The use of secondary modifiers to distinguish a part from similar parts is also covered.
HISTORICAL
1961-10-15
Standard
ARP219
This procedure will be generally applicable to three classes of hydraulic components as listed below:
HISTORICAL
1961-08-01
Standard
ARP741
This recommended practice considers many facets of testing which have a bearing on obtaining accurate, repeatable engine performance data. These are: TEST CELL CONFIGURATIONS TEST CELL INSTRUMENTATION ENGINE PERFORMANCE CORRECTION FACTORS TEST CELL EFFECTS INSTRUMENTATION CALIBRATION CORRELATION TEST PROGRAM
HISTORICAL
1961-07-01
Standard
AMS3388A
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).
HISTORICAL
1961-07-01
Standard
AMS3389A
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
1961-07-01
Standard
AMS3386A
This specification covers a synthetic rubber in the form of soft wall, smooth bore, collapsing-type hose. This hose has been used typically for fueling aircraft from tank trucks or pits where the hose will be rolled flat for stowage on a reel, but usage is not limited to such applications. Not recommended for operating pressures higher than 125 psi (862 kPa).
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