Criteria

Text:
Content:
Display:

Results

Viewing 5671 to 5700 of 5751
HISTORICAL
1961-12-01
Standard
ARP592
The purpose of these recommendations is to provide a guide to designers and users of electric equipment for the use of taper pins designed to make electrical connections. 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 terminations of a wire and are not to be employed as a quick-disconnect device.
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
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
1960-03-01
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
1960-01-01
Standard
J565_196001
This SAE Standard provides test procedures, performance requirements, and guidelines for semiautomatic headlamp beam switching devices.
HISTORICAL
1960-01-01
Standard
J564_196001
This SAE Standard J564 defines the test conditions, procedures and performance specification for 6, 12, and 24 V manually actuated headlamp beam control switches.
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.
HISTORICAL
1959-11-15
Standard
ARP461A
This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros:
HISTORICAL
1959-11-01
Standard
ARP670
No scope available.
HISTORICAL
1959-02-01
Standard
AS404B
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
HISTORICAL
1959-02-01
Standard
AS402A
This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo control.
CURRENT
1959-02-01
Standard
AS392C
This Aeronautical Standard covers two (2) basic types of instruments as follows: TYPE I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude. TYPE II- Range 50,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude.
HISTORICAL
1959-02-01
Standard
ARP426
These recommendations cover the mechanical and electrical installation and installation test procedures for Compass Systems of the type normally used in transport type aircraft. The recommendations in the ARP do not supersede any airworthiness requirements in Civil Air Regulations.
CURRENT
1958-07-15
Standard
AS403A
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
1958-07-15
Standard
AS398A
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading Type II - Remote Indicating
HISTORICAL
1958-07-15
Standard
ARP433
This Aeronautical Recommended Practice covers Liquid Oxygen Quantity Indicators for use with associated Liquid Oxygen converters.
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
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.
Viewing 5671 to 5700 of 5751