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HISTORICAL
1964-08-01
Standard
ARP842
This recommended practice sets forth the design objectives for handling qualities applicable to transport aircraft operating in the subsonic, transonic and supersonic speed range. These objectives are not necessarily applicable to rotor or VTOL aircraft.
HISTORICAL
1964-08-01
Standard
AS861
This standard covers all types of oxygen breathing equipment used in non-military aircraft. It is intended that this standard supplement the requirements of the detail specification or drawings of specific components or assemblies, e.g., regulators, masks, cylinders, etc. Where a conflict exists between this and detail specifications, detail specifications shall take precedence.
HISTORICAL
1964-06-20
Standard
ARP493
This recommended practice is intended to recommend the basic shapes and dimensions for knobs used in aircraft. Two basic types of knobs, the bar shape and the round shape, are described, as well as several widely used variations of these two basic shapes.
HISTORICAL
1964-04-01
Standard
J881_196404
This SAE Standard covers minimum dimensional relations for sheaves, drums, and wire rope for mobile, construction type lift cranes.
HISTORICAL
1964-03-01
Standard
J885_196403
This report reviews current quantitative data on human tolerance levels without recommending specific limits. Data developed on humans (including cadavers) are presented where available; however, in many cases animal data are provided where no suitable human results have been reported. This report confines itself, as much as possible, to information of direct use to the automotive designer and tester. Data of only academic interest are largely omitted; therefore, J885 should not be considered as a complete summary of all available biomechanical data. Most of the data cited in this report applies to adult males since little information is available on women or children. The summary data provided in the tables should be considered with the accompanying descriptive test. This material explains the manner in which the data were obtained and provides an insight as to their limitations.
HISTORICAL
1964-02-01
Standard
AIR805
The purpose of this information report is to present factors which affect the design and development of jet blast windshield rain removal systems for commercial transport aircraft. A satisfactory analytical approach to the design of these systems has not yet been developed. Although detailed performance data are available for some test configurations, rain removal systems will generally be unique to specific aircraft. This, then, requires a preliminary design for the system based on available empirical data to be followed with an extensive laboratory development program.
HISTORICAL
1963-12-01
Standard
ARP699B
This Recommended Practice is intended to outline the design, installation, testing, and field maintenance criteria for a high temperature metal pneumatic duct system, for use as a guide in the aircraft industry. These recommendations are to be considered as currently applicable and necessarily subject to revision from time to time, as a result of the rapid development of the industry.
CURRENT
1963-11-01
Standard
J879
HISTORICAL
1963-11-01
Standard
J879_196311
HISTORICAL
1963-05-01
Standard
ARP731
The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish recommendations for the design, installation and testing of air vehicle vapor cycle refrigeration systems. These recommendations are representative of the refrigerant cycles.
HISTORICAL
1963-01-31
Standard
AIR728
This publication outlines general design concepts considered the minimum acceptable standards for use in electrical and electronic equipment. The objective is increased reliability of the equipment without penalizing the aircraft performance.
HISTORICAL
1962-12-01
Standard
AIR746
This document supplements ARP85, to extend its use in the design of ECS for supersonic transports. The ECS provides an environment controlled within specified operational limits of comfort and safety, for humans, animals and equipment. These limits include pressure, temperature, humidity, conditioned air velocity, ventilation rate, thermal radiation, wall temperature, audible noise, vibration, and composition (ozone, contaminants, etc.) of the environment. The ECS is comprised of equipment, controls, and indicators that supply and distribute conditioned air to the occupied compartments. This system is defined within the ATA 100 specification, Chapter 21. It interfaces with the pneumatic system (Chapter 36 of ATA 100), at the inlet of the air conditioning system shutoff valves.
HISTORICAL
1962-11-01
Standard
J73_196211
HISTORICAL
1962-06-30
Standard
ARP499A
HISTORICAL
1962-01-01
Standard
ARP695
This Aerospace Recommended Practice provides criteria for design with respect to overall safety, particularly to afford minimum risk exposure to flight attendants and passengers from injuries due to: A. Routine use of galley installations B. Galley components becoming dislodged under routine or abnormal operating conditions and under survivable crash or ditching conditions C. Malfunctions of, or defects in, galleys or associated galley equipment. NOTE: It is not the purpose of this Aerospace Recommended Practice to specify the design methods or specific design to be followed in the accomplishment of the stated objectives.
HISTORICAL
1961-08-15
Standard
ARP85D
Air Conditioning System - General - Dealing with Design Features
HISTORICAL
1961-06-01
Standard
ARP693
This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a) single engine personal and/or liaison type; b) light twin engine; c) large multiengine propeller; d) large multiengine turbojet; e) military high performance fighter and attack; and f) helicopter. The purpose of this document is to provide certain basic considerations and design criteria for installation of landing and taxiing light systems for night operation.
HISTORICAL
1961-04-01
Standard
J765_196104
This SAE Standard may be used for all revolving cranes wherein the capacity of the crane to support loads is based on its resistance to overturning. it is not applicable to cranes wherein the capacity of the crane is based on structural strength or available hoisting power. The purpose of this test is to determine the maximum capacity of a crane to counterbalance loads applied on its hook block. The capacity of the crane is reported in terms of the load in kilograms (pounds) and its corresponding radius in meters (feet) for a specified position of the upperstructure with respect to the mounting.
HISTORICAL
1960-06-01
Standard
AIR32A
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
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
1957-07-01
Standard
J80_195707
This SAE Recommended Practice covers the requirements for rubber floor mats made from five types of rubber compounds as required by the physical property requirements of the application.
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
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
1954-12-15
Standard
AS264C
The desired system for aircraft instrument panel and cockpit lighting is one that will furnishlight of adequate intensity and distribution under all conditions of external lighting so that the crew may read instrumentation, placards, check lists, manuals, maps, instrument color coding, distinguish controls, etc., without undue interference with their vision outside of the aircraft.
HISTORICAL
1952-08-15
Standard
AIR32
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
Viewing 1231 to 175 of 175