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HISTORICAL
1984-10-01
Standard
AIR975
In efforts to increase the accuracy and reliability of altimetry, speed measurement and other aspects of air data, a great deal of attention and money have been expended on new and refined pressure transducing and computing systems and on the standards by which they are calibrated. So much progress has been made in this that the limiting factor is, or may soon be, the sensing and transmitting in the aircraft of the pressures to be transduced. Until the appearance of References 1-13 and 18 there was little guidance available on the maintenance of pitot and static systems. This report presents what information is available, suggests limits, and lists the principal original papers on the subject.
HISTORICAL
1984-10-01
Standard
J1282_198410
This SAE Recommended Practice is intended to provide the minimum acceptable criteria for snowmobile hand brake control systems. This recommendation is not intended to cover competition vehicles nor is it intended to limit development of new and/or improved technology in controls. Although these recommendations are primarily addressed to hand control systems using an outer flexible conduit with a multiple strand inner cable or hydraulic type brake control system, the basic requirements of freedom of movement, strength, material, etc., will apply to any system.
HISTORICAL
1984-10-01
Standard
J1222_198410
This SAE Recommended Practice provides minimum requirements and performance criteria for devices to prevent runaway snowmobiles due to malfunction of the speed control system.
CURRENT
1984-09-01
Standard
AS8008
This Aerospace Standard covers Flight Director Equipments which display to the pilot a computed command for the operation of an aircraft in accordance with selected Mode(s). The term “Equipment” may include controls, displays, computers, etc. and may include sensors if furnished as a part of the Flight Director.
HISTORICAL
1984-09-01
Standard
AIR1800
This document covers the field of civilian, commercial and military airplanes and helicopters. This summary of tail bumper design approaches may be used by design personnel as a reference and guide for future airplanes and helicopters that require tail bumpers. Those described herein will consist of simple rub strips, structural loops with a wear surface for runway contact, retractable installations with replaceable shock absorbers and wear surfaces and complicated retractable tail landing gears with shock strut, wheels and tires. The information will be presented as a general description of the installation, its components and their functions.
HISTORICAL
1984-09-01
Standard
ARP1817
This recommended practice describes an industrial battery, lead acid type, for use in electric powered ground support equipment.
HISTORICAL
1984-09-01
Standard
ARP1816
This SAE Aerospace Recommended Practice (ARP) describes two general types of Ground Support Equipment (GSE) battery chargers. The conventional industrial battery charger typically requiring up to 8 hours to recharge a 100% discharged battery, hereafter called “Conventional Charger”. The other type a fast battery charger typically used as an opportunity charger for ground support equipment, hereafter called “Fast Charger”. Recommendations that apply to both types will refer generically to “charger”.
HISTORICAL
1984-08-01
Standard
J930_198408
This SAE Standard applies to all types of heavy-duty storage batteries for use on off-road machines as described in SAE J1116. Included are definitions of industry terms, test procedures, general requirements, application recommendations, standard sizes, overall dimensions, and electrical values.
CURRENT
1984-07-06
Standard
ARIC715-3
This standard describes the characteristics of a PA AMP designed for installation in commercial aircraft. Its function is to amplify control voice, music and internally generated chime audio signals to drive the aircraft cabin loudspeaker system.
CURRENT
1984-07-06
Standard
ARIC719-5
This standard sets forth characteristics of a new-generation HF/SSB System intended for installation in all types of commercial transport aircraft. Covers requirements for airborne transmitter-receiver equipment capable of transmitting and receiving HF radio intelligence.
HISTORICAL
1984-07-01
Standard
AMS3593
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified-polyvinylidene-fluoride plastic in the form of semi-rigid, extra-thin-wall, heat-shrinkable tubing.
HISTORICAL
1984-06-01
Standard
J1399_198406
This SAE Recommended Practice establishes minimum requirements for electric tachometer systems with and without hourmeter or revolution counter, for general applications as follows: Class 1-Passenger Car Class 2-Bus and Truck Class 3-Off-Road vehicles
HISTORICAL
1984-06-01
Standard
J1377_198406
This SAE Recommended Practice covers the transmission output shaft mounted signal rotor and sensor mounting hole used for electronic speed sensing on Class 6, 7, and 8 highway vehicles.
HISTORICAL
1984-06-01
Standard
J1167_198406
This SAE Recommended Practice establishes test procedures and performance requirements for stop lamp switches intended for use in an AC or a DC circuit on motorcycles. In service use may impose specific conditions on the switch which can affect its functional life. Those conditions should be replicated, as necessary, during the testing described in this document to ensure the adequate functioning of the device.
HISTORICAL
1984-06-01
Standard
AIR784B
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine.
HISTORICAL
1984-06-01
Standard
J1113_198406
This SAE Recommended Practice establishes uniform laboratory measurement techniques for the determination of the susceptibility to undesired electromagnetic sources of electrical, electronic, and electromechanical ground-vehicle components. It is intended as a guide toward standard practice, but may be subject to frequent change to keep pace with experience and technical advances, and this should be kept in mind when considering its use.
HISTORICAL
1984-06-01
Standard
J378_198406
This SAE Recommended Practice covers the requirements for all marine inboard engine wiring, wiring assemblies, wiring components, and wiring connectors connected to microprocessors associated with the operation of the propulsion system, operating at 50 V or less.
HISTORICAL
1984-05-01
Standard
ARP1199A
This Aerospace Recommended Practice provides technical and application information needed by the designers of aircraft electric systems and support equipment for the selection of overcurrent protective devices. It provides definitions to permit comparisons of various electric circuit protective devices. Included also are recommended procedures for periodic inspection.
HISTORICAL
1984-05-01
Standard
J392_198405
This SAE Recommended Practice pertains to electrical systems of motorcycles both with and without batteries. Purpose This document provides minimum illumination voltage values for all motorcycle classifications as specified in SAE J213 describes test procedures to determine that these voltages are maintained.
HISTORICAL
1984-04-01
Standard
J253_198404
This document defines the test conditions, procedures, and performance specifications for 6-,12-, and 24-V manually actuated headlamp switches (circuit breaker(s) may be incorporated for circuit overload protection).
HISTORICAL
1983-12-01
Standard
J551_198312
This SAE Standard covers the measurement of broadband electromagnetic radiation over the frequency range of 30 to 1000 MHz from a vehicle or other device powered by an internal combustion engine or electric motor. Operation of all engines (main and auxiliary) of a vehicle or device is included. All equipment normally operating when the engine is running is also included except operator-controlled equipment, which is excluded. The recommended level applies only to complete vehicles or devices in their final manufactured form. Vehicle mounted rectifiers used for battery charging in electric vehicles are included in this document when operated in their charging mode.
CURRENT
1983-10-31
Standard
ARIC703-2
The characteristics of a TCCS within the Automatic Flight System are defined in this standard for throttle control. The standard also provides general and specific design guidance for the development and installation of a TCCS.
HISTORICAL
1983-09-01
Standard
AIR1810
This document examines the most important considerations relative to the use of proximity sensing systems for applications on aircraft landing gear. In general, the recommendations included are applicable to other demanding aircraft sensor installations where the environment is equially severe. The purpose of this SAE Aerospace Information Report (AIR) is to suggest specification, application, performance, and validation criteria for solid-state proximity sensing systems used for environmentally severe applications on aircraft landing gear.
HISTORICAL
1983-08-01
Standard
J538_198308
The negative side of the storage battery shall be securely and adequately grounded so that the voltage drop to the starting motor is held within the limits specified in the current edition of SAE J541.
CURRENT
1983-07-25
Standard
ARIC596-4
This standard describes the system requirements for a ground-to-air SELCAL system. The purpose of the system is to permit the selective calling of individual aircraft over normal radio communications circuits linking the ground station with the aircraft. The elements comprising the overall system are: ground selective calling unit (coder), ground-to-air transmitter (HF or VHF), airborne receiver (HF or VHF), airborne selective calling unit (decoder), annunciator panel, and code selection panel.
HISTORICAL
1983-07-01
Standard
J541_198307
The scope of this SAE Recommended Practice is to describe the maximum recommended voltage drop for starting mortor circuits for 6 V through 32 V starters.
HISTORICAL
1983-07-01
Standard
ARP670A
HISTORICAL
1983-06-01
Standard
J56_198306
The purpose of this SAE Recommended Practice is to provide a standard test procedure for the development of alternator output performance, and a standard form for plotting performance curves.