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Viewing 1591 to 1620 of 14315
HISTORICAL
1947-08-01
Standard
AS399
This specification covers minimum requirements for gyroscopically stabilized (or integrated) magnetic direction indicators for use in aircraft.
HISTORICAL
1947-08-01
Standard
AS402
To specify minimum requirements for Automatic Pilots primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. 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.
HISTORICAL
1947-08-01
Standard
AS394
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.
HISTORICAL
1947-08-01
Standard
AS396
To specify the minimum requirements for gyroscopically stabilized Bank and Pitch Indicators for ue in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.4.
HISTORICAL
1947-07-01
Standard
AS398
To specify minimum requirements for non-stabilized magnetic direction instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading, Type II - Remote Indicating.
CURRENT
1947-07-01
Standard
AS395
HISTORICAL
1947-07-01
Standard
AS391
This Aeronautical Standard covers five basic types o fairspeed instruments as follows: Type I - 1 revolution Type II - 1 revolution (unequal scale) Type III - 1 1/2 to 1 3/4 revolutions Type IV - 7 revolutions Type V - 1 3/4 to 2 revolutions
HISTORICAL
1947-02-01
Standard
AS397
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.
HISTORICAL
1944-05-01
Standard
AIR4
HISTORICAL
1944-05-01
Standard
ARP147
This ARP provides the definition of terms commonly used in aircraft environmental control system (ECS) design and analysis. Many of the terms may be used as guidelines for establishing standard ECS nomenclature. Some general thermodynamic terms are included that are frequently used in ECS analysis, but this document is not meant to be an inclusive list of such terms.
HISTORICAL
1943-11-01
Standard
ARP85A
This specification is written to cover heating and ventilating equipment under four main classifications, namely; A. HEATING AND VENTILATING EQUIPMENT - GENERAL - Dealing with features applicable to all makes and uses. B. HEATING AND VENTILATING EQUIPMENT - MILITARY - Dealing with features applicable only to military aircraft. C. HEATING AND VENTILATING EQUIPMENT - COMMERCIAL - Dealing with features applicable only to commercial aircraft. D. DESIRABLE DESIGN FEATURES - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1943-01-01
Standard
ARP89
The recommendations of this SAE Aerospace Recommended Practice (ARP) for aircraft compartment automatic temperature control systems are primarily intended to be applicable to occupied or unoccupied compartments of civil and miliary aircraft.
HISTORICAL
1943-01-01
Standard
ARP85
Viewing 1591 to 1620 of 14315