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Viewing 5761 to 5790 of 5859
HISTORICAL
1963-02-01
Standard
AS440
This SAE Aerospace Standard (AS) covers autoatic pilots intended for use on aircraft to automatically operate the primary and trim aerodynamic controls to maintain stable flight and/or to provide maneuvering about any of the three axes through servo control. Automatic control functions essential for primary or augmented flight control are excluded. To establish essential minimum safe performance standards for automatic pilots primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.3.
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
1963-01-01
Standard
J853_196301
This SAE Standard has been established to provide direction for the design and installation of a Vehicle Identification Number assigned to a passenger car or truck. In adhering to these standards, facility of application in factory production and appearance are matters for manufacturer control.
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
1962-11-15
Standard
ARP268C
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.
HISTORICAL
1962-11-15
Standard
ARP450A
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
1962-11-01
Standard
J839_196211
This SAE Recommended Practice establishes minimum performance requirements and test procedures for evaluating and testing passenger car side door latch systems. It is limited to tests that can be conducted on uniform test fixtures and equipment in commercially available laboratory test facilities. The test procedures and minimum performance requirements outlined in this document are based on currently available engineering data. It is intended that all portions of the document will be periodically reviewed and revised, as additional knowledge regarding vehicle latch performance under impact conditions is developed.
HISTORICAL
1962-07-01
Standard
AS425A
This Standard is intended to establish preferred abbreviations for use on panels, controls, instruments, displays, placards and markings. The recommendations apply to terms used in the flight deck of transport aircraft. The abbreviations, symbols and codes do not supersede those used in airworthiness regulations or aeronautical charts and documents. Where conflict is possible the operational context must be such as to resolve any ambiguity. If doubt exists, an alternative abbreviation or less truncated abbreviation should be used.
HISTORICAL
1962-07-01
Standard
ARP571A
The facilities covered in this bulletin are: Navigational equipment which makes use of radio or other electronic devices. Equipment for weather surveillance, anti-collision devices, etc. Air traffic control equipment. All air-borne communciations equipment both for communication within the aircraft and to points outside the aircraft.
HISTORICAL
1962-06-01
Standard
J831_196206
This SAE Standard contains the industry standard definitions for electrical equipment used in the generation of electric power onboard today's conventional road vehicles. It is intended to complement the electronic terminology that was formerly documented in SAE J1213 (canceled) and/or in other industry glossaries of electrical/electronic devices.
HISTORICAL
1962-04-01
Standard
J823_196204
This SAE Standard specifies the test procedure, test circuitry, and instruments required for measuring the performance of flashers used in motor vehicles.
CURRENT
1962-03-01
Standard
AS420B
This Aerospace Standard covers Flight Directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a pre-selected flight plan.
CURRENT
1962-03-01
Standard
AS446
This Aerospace Standard covers three basic types of cargo compartment fire detector instruments.
HISTORICAL
1962-02-15
Standard
AS400A
This Aerospace Standard covers three basic types of cargo compartment fire detector instruments. Basic Types - Definition of: Type I: Carbon Monoxide, an instrument which will actuate an alarm signal when the concentration of carbon monoxide in air exceeds a specified value. Type II: Smoke Detector, Electronic, an instrument operating on the principle of smoke particles modifying the relationship between a light beam and electronic light sensor which will actuate an alarm signal when the concentration of smoke in air exceeds a specified value. Type III: Smoke Detector, Visual, an instrument which, by visual means, will show in a positive manner the presence of smoke when the concentration of smoke in air exceeds a specified value.
HISTORICAL
1962-02-01
Standard
AS431A
This SAE Aerospace Standard (AS) covers three basic types of true mass flow indicating instruments. Each may consist of an indicator, transmitter and other auxiliary means such as a power supply or amplifier as required. This Aerospace Standard establishes the essential minimum safe performance standards for True Mass Fuel Flow Instruments primarily for use with turbine powered, subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3.
HISTORICAL
1961-12-31
Standard
ARP719
Gas for the purpose of this ARP shall be defined as the gaseous produces) resulting from the decomposition, dissociation, or combustion of liquid or solid mono or bi-propellants. Where other gases such as heated N2, H2, H2O (steam), etc., which may have similar physical and/or chemical properties as the defined "gas", are used to effect testing economies; they may be considered as being included in this ARP.
HISTORICAL
1961-12-01
Standard
ARP592
These recommendations cover the use of taper pins in taper pin terminal blocks, multi-contact electric connectors, and components designed to accept taper pins. Taper pins are intended to facilitate termination of a wire and are not to be employed as a quick-disconnect device. The mating portions of taper pins and taper pin receptacles shall be in accordance with Figure 1.
CURRENT
1961-11-30
Standard
ARP727
HISTORICAL
1961-06-01
Standard
AS414
This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: type I: ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. Type II: millivoltmeter type, operated and actuated by varying EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple. This document establishes the essential minimum safe performance standards for electrical type temperature instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4.
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.
CURRENT
1961-05-01
Standard
AS418A
This Aeronautical Standard covers the basic types of maximum allowable airspeed instruments which give a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots.
CURRENT
1961-04-01
Standard
AS445
This Aeronautical Standard covers the capacitance sensor type of instrument.
CURRENT
1960-11-15
Standard
AS391C
This Aeronautical Standard covers five basic types of airspeed instruments as follows:
CURRENT
1960-10-01
Standard
AS430
This Aeronautical Standard covers the following basic types of fire detection instruments, or combinations thereof, intended for use in protecting aircraft powerplant installation, auxiliary powerplants, combustion heaters and other installations where fuel, oil or similar fires may occur.
HISTORICAL
1960-07-15
Standard
AS393A
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
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
1960-03-01
Standard
J589_196003
A turn signal switch is that part of a turn signal system by which the operator of a vehicle causes the turn signal lamps to function. A Class A turn signal switch may be used on any vehicle but is intended for use on multipurpose passenger vehicles, trucks, and buses that are 80 in or more wide overall. A Class B turn signal switch is intended for use in passenger cars, motorcycles, and multipurpose passenger vehicles, trucks, and buses of less than 80 in overall width.
HISTORICAL
1960-03-01
Standard
AS407B
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
1960-03-01
Standard
ARP217A
This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment.
HISTORICAL
1960-01-01
Standard
J563_196001
This standard is intended to cover cigar or cigarette lighters as well as power outlets based on the form and dimensions of the cigar lighter, and accessory plugs for use in these devices. Components covered herein are designed to work in nominal 12 VDC systems. This standard is a full performance specification. It includes dimensional and operational parameters as well as performance characteristics which must be met when submitting a cigar lighter assembly, power outlet assembly, or plug for production approval. This standard constitutes an acceptance specification for these devices. This standard covers the operational, reliability, durability, acceptance, and testing requirements for a cigar lighter (also referred to as just "lighter") for installation in the passenger compartment of production vehicles.
Viewing 5761 to 5790 of 5859