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Viewing 15061 to 15090 of 15528
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.
1959-02-01
Standard
ARP373A
Scope is unavailable.
1959-02-01
Standard
AS127C
No scope available.
1959-02-01
Standard
AS125851A
No scope available
1959-02-01
Standard
AS125851
Scope unavailable.
1959-02-01
Standard
ARP426
These recommendations cover the mechanical and electrical installation and installation test procedures for Compass Systems of the type normally used in transport type aircraft. The recommendations in the ARP do not supersede any airworthiness requirements in Civil Air Regulations.
1959-02-01
Standard
AS402A
This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo control.
1959-02-01
Standard
AS404B
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
1959-01-01
Technical Paper
590303
ROBERT T. WESTMORELAND, PATRICK J. HANIFIN
1959-01-01
Technical Paper
590379
A. B. JONES
1959-01-01
Technical Paper
590056
L N. DeVos
INVOLUTE SPLINES enjoy three major advantages over their straight-sided counterparts: 1. New design concepts have given a more rational approach to clearances and errors. 2. Manufacturing is cheaper and more accurate. 3. Gaging is simpler. Thus, the involute spline standard of SAE and ASA continue to take precedence over the older straight-sided standards.
1959-01-01
Technical Paper
590243
F. H. POLLARD
1959-01-01
Technical Paper
590244
C. E. HAMLIN
1959-01-01
Technical Paper
590142
JOHN M. TYLER, THOMAS G. SOFRIN, JACK W. DAVIS
1959-01-01
Technical Paper
590400
JAMES W. SHEREECK, BRUCE A. KLNDGRM
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).
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).
1958-07-15
Standard
ARP502
No scope available.
1958-07-15
Standard
AS398A
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading Type II - Remote Indicating
1958-07-15
Standard
ARP433
This Aeronautical Recommended Practice covers Liquid Oxygen Quantity Indicators for use with associated Liquid Oxygen converters.
1958-07-15
Standard
AS405B
To specify minimum requirements for Fuel and Oil Quantity Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments.
1958-07-01
Standard
AS394A
To specify minimum requirements for pressure, actuated Climb Indicators for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This Aeronautical Standard covers four (4) basic types of direct indicating instruments as follows: TYPE I - Range 0-2000 feet per minute climb and descent, TYPE II - Range 0-3000 feet per minute climb and descent, TYPE III - Range 0-4000 feet per minute climb and descent, TYPE IV - Range 0-6000 feet per minute climb and descent.
1958-07-01
Standard
AS397A
To specify minimum requirements for non-magnetic gyroscopically stabilized direction indicators for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types as follows: Type I - Air Operated, Type II - Electrically Operated.
1958-07-01
Standard
AS396B
This Aeronautical Standard covers both direct and repeating type gyroscopically stabilized Bank and Pitch Indicating Instruments.
1958-07-01
Standard
AS399A
This Aeronautical Standard covers minimum requirements for gyroscopically stabilized Magnetic Direction Instruments for use in aircraft.
1958-05-01
Standard
J697_195805
This SAE Recommended Practice is intended as a guide for manufacturers and users of trailers, specifically full trailer(s) and/or converter dollies. Its inclusion in state, federal, or any laws or regulations where flexibility of revision is lacking is discouraged. Emergency safety is the basis of this recommendation. This SAE Recommended Practice covers the number, location, and method of attachment of safety chains for full trailers and/or converter dollies.
1958-04-01
Magazine
1958-02-15
Standard
ARP427
This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator. Type I - All material in this document applies to this classification only. Type II - Additional material for this classification will be added to superseding issues as the state of the art permits.
Viewing 15061 to 15090 of 15528

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