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Viewing 4831 to 4860 of 4905
HISTORICAL
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.
HISTORICAL
1958-07-01
Standard
AS399A
This Aeronautical Standard covers minimum requirements for gyroscopically stabilized Magnetic Direction Instruments for use in aircraft.
CURRENT
1958-07-01
Standard
AS394A
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
CURRENT
1958-07-01
Standard
AS396B
This Aeronautical Standard covers both direct and repeating type gyroscopically stabilized Bank and Pitch Indicating Instruments.
HISTORICAL
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.
HISTORICAL
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.
HISTORICAL
1958-05-01
Standard
J577_195805
This SAE Recommended Practice provides procedures, and information to conduct vibration (impact) tests on lighting devices and their components as well as other safety equipment used on vehicles.
CURRENT
1958-02-15
Standard
ARP464
HISTORICAL
1958-02-15
Standard
ARP427
This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist 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.
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
ARP419
These recommendations cover the mechanical and electrical installation and installation test procedures for automatic pilots of the type normally used in transport type aircraft. The material in this ARP does not supercede any airworthiness requirement in the Civil Air Regulations.
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.
HISTORICAL
1957-08-15
Standard
ARP495
This Aerospace Recommended Practice (ARP) establishes criteria for design and installation of devices which will ensure rapid and effective occupant evacuation in the event of an emergency. This ARP deals with emergency evacuation devices installed for the purpose of rapidly assisting the occupants to the ground or water from emergency exits and/or wings. NOTE: This document is not intended to specify design methods, mechanisms or equipment to be used in accomplishment of the objectives set forth herein.
HISTORICAL
1957-08-15
Standard
ARP496
This document describes the engineering requirements for the assembly and installation of tube couplings used on aircraft fuel and pneumatic systems. In case of conflict between this document and an engineering drawing, the provisions of the engineering drawing shall prevail.
HISTORICAL
1956-12-15
Standard
AS418
This Aeronautical Standard establishes the essential minimum safe requirements for pitot-static type of Maximum Allowable Airspeed Instruments primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the instruments to the environmental conditions specified in paragraph 3.3. This Aeronautical Standard covers the basic types of maximum allowable airspeed instruments which give a continuous indication of both indicated air speed and maximum allowable airspeed not exceeding 650 knots.
HISTORICAL
1956-12-15
Standard
AS412A
This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
HISTORICAL
1956-12-15
Standard
AS405A
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
1956-12-01
Standard
AS452
The purpose of this standard is to establish optimum standards for crew demand and pressure-breathing oxygen mask assemblies for use by crew members in civil aircraft. This standard covers both general type and quick-donning type mask assemblies in the following classes: a. Class A, oronasal, demand b. Class B, oronasal, pressure-demand c. Class C, full face, demand d. Class D, full face, pressure-demand
HISTORICAL
1956-12-01
Standard
AIR64
This AIR is intended as a status report on the of E.C.S. to date in dealing with the problem of equipment cooling in present and immediate future civil transport aircraft. Subsequent revisions to this AIR will follow as more information is gathered on this subject.
HISTORICAL
1956-03-15
Standard
ARP85C
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
1955-07-01
Standard
ARP461
This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros: 26 volt, 400 cycle synchros 115 volt, 400 cycle synchros 115 volt, 60 cycle synchros
HISTORICAL
1954-12-15
Standard
AS408A
This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating, Type II - Remote Indicating. This Aerospace Standard does not apply to engine mounted torque meter systems.
HISTORICAL
1954-12-15
Standard
AS407A
To specify minimum requirements for Fuel Flowmeters for use primarily 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 two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
HISTORICAL
1954-12-15
Standard
AS404A
To specify minimum requirements for Electric Tachometers 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 magnetic drag tachometers with or without built-in synchroscopes.
Viewing 4831 to 4860 of 4905