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Viewing 7231 to 7260 of 7276
HISTORICAL
1948-11-01
Standard
AS405
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments. 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.
HISTORICAL
1948-08-01
Standard
ARP85B
Air Condiitioning System - General - Dealing with design features. Air Conditioning Equipment - Commercial Passenger - Delaing with features. Applicable only to commercial passenger carrying aircraft. Desirable Design Features - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1948-07-01
Standard
AMS2645
This specification has been declared 'SUPERSEDED' by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of ASTM E 1417.
CURRENT
1948-03-01
Standard
AS236
CURRENT
1948-03-01
Standard
AS234
CURRENT
1948-03-01
Standard
AS196
CURRENT
1948-03-01
Standard
ARP175
HISTORICAL
1947-12-01
Standard
AMS6372A
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
HISTORICAL
1947-12-01
Standard
AS393
The purpose of this Aeronautical Standard is to specify minimum requirements for pitot-static type of electrically heated Airspeed Tubes primarily for use in reciprocating engine powered civil transport 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 - Pitot Pressure, straight and L-shaped, 12 and 14 volt nominal, 2 wire circuit. Type II - Pitot and Static Pressured, straight and L-shaped, 12 and 24 volt nominal, 2 wire circuit.
HISTORICAL
1947-08-01
Standard
AS392
This specification covers two (2) basic types of instruments as follows: Type I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude. Type II - Range 50,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude.
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
1946-11-01
Standard
AMS3626
This specification covers one type of methyl methacrylate in the form of extrusions, compression moldings, and injection moldings. These products have been used typically for parts requiring good dimensional stability, a high degree of optical clarity, and good resistance to outdoor weathering, but usage is not limited to such applications.
HISTORICAL
1946-04-01
Standard
AMS2640B
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1945-10-01
Standard
AMS6372
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
HISTORICAL
1944-11-01
Standard
AMS2601B
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2602A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2605A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2607A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-11-01
Standard
AMS2606B
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1944-08-01
Standard
AMS2640A
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1944-05-01
Standard
AS84A
This SAE Aerospace Standard (AS) defines an involute with a 30? pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the root.
HISTORICAL
1943-11-01
Standard
ARP159
Viewing 7231 to 7260 of 7276