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Viewing 13171 to 13200 of 13384
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
1957-11-15
Standard
ARP494A
HISTORICAL
1957-11-15
Standard
ARP484
HISTORICAL
1957-11-15
Standard
AS524
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
1957-11-01
Standard
ARP485
HISTORICAL
1957-11-01
Standard
AIR34
The scope of this SAE Aerospace Information Report (AIR) is to present a guide for the determination of probable power output and the effect on the aircraft system that will be experienced when operating three-phase motors with one phase open. Unfortunately, the above subject cannot be resolved by specific rules. Modern aircraft or missile electrical systems are composed of a wide variety of electrical and electronic components. These components react differently under identical impetus due to the latitude of their design. This latidue of design must be allowed wherever possible to the accessory designer due to the various specification requirements. Therefore, it cannot be over-emphasized that the effect on the airplane or missile system, as well as motor operation, of three-phase motors on two-phase power must be thoroughly investigated.
HISTORICAL
1957-11-01
Standard
AS473
No scope available.
HISTORICAL
1957-11-01
Standard
AS469
No scope available.
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
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
1956-12-15
Standard
ARP243A
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
1956-12-15
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
AS418
This Aeronautical Standard covers the basic type of maximum allowable airspeed indicators used to indicate continuously both the indicated airspeed and the maximum allowable airspeed in the ranges shown below;
CURRENT
1956-12-01
Standard
AIR47
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
1956-12-01
Standard
AS452
This specification covers the types of oxygen masks considered satisfactory for use in commercial transport aircraft at altitudes up to 25,000 ft. The types of masks covered are:
HISTORICAL
1956-03-15
Standard
ARP489
This specification establishes the requirements for shielded, detachable high tension spark plug leads for reciprocating engines.
HISTORICAL
1956-03-15
Standard
ARP450
This ARP sets forth design and operational recommendations relative to the integrated alerting system to be implemented on the flight deck. It is intended that through the adoption of the design objectives and recommendations incorporated herein, a consistent and effective industry standard will result. Safety of flight is greatly enhanced by an alerting system designed to provide early crew recognition of flight crew operational error as well as aircraft system or component status or malfunction. The alerting system therefore relates to aircraft configuration and flight regime as well as the aircraft systems. To fulfill this objective, the flight deck alerting system must attract the attention of the crew, must state with clarity the nature and location of the problem, must be highly reliable and thoroughly responsive to the operational requirements and environment.
HISTORICAL
1956-03-15
Standard
ARP268B
The purpose of this document is to set forth the recommendations of SAE Committee S-7 relative to the location and actuation of flight deck controls. These recommendations are intended to minimize confusion and distraction and thereby reduce transition training time, crew errors, fatigue, and other factors detrimental to flight safety and efficiency. In arriving at these recommendations, the committee carefully reviewed the work of the flight deck layout panel of the Aircraft Committee of the Munitions Board, the recommendations and requirements of the Civil Aeronautics Board, the Federal Aviation Agency, the requirements of the airline operators, the aircraft manufacturers, etc. In cases where conflicting opinions existed, suitable compromises were made. The recommendations of this document apply to commercial type, multi-engine transport aircraft which utilize reciprocating or turbine type powerplants and which are operated in subsonic, transonic, or supersonic speed regimes.
CURRENT
1956-03-15
Standard
ARP467
HISTORICAL
1956-03-15
Standard
ARP476
HISTORICAL
1956-03-15
Standard
ARP89B
This recommended practice covers automatic cabin temperature control systems of the following types for pressurized and unpressurized cabins:
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.
Viewing 13171 to 13200 of 13384

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