Standard
TUBE - PITOT, ELECTRICALLY HEATED
1998-02-01
HISTORICAL
AS5813
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Standard
TUBE - PITOT, ELECTRICALLY HEATED
2012-08-22
CURRENT
AS5813A
Standard
SYNCHROS
2008-02-16
CURRENT
ARP461B
This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros:
Standard
SYNCHROS
1959-11-15
HISTORICAL
ARP461A
This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros:
Standard
SUBSONIC AIRCRAFT INSTRUMENT STANDARDS: WORDING, TERMINOLOGY, PHRASEOLOGY, ENVIRONMENT AND DESIGN STANDARDS FOR
1966-08-01
HISTORICAL
AIR818A
This standard covers _________________________________________
Standard
Rate Gyro Assembly Configuration
2008-02-16
CURRENT
ARP727
Standard
PRECISION MOTOR TACHOMETER GENERATOR
2008-02-16
CURRENT
ARP667
This recommended practice establishes objectives for high performance control motor tachometer generators to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climatic conditions of heat, cold, shock, vibration, and humidity. Control motor tachometer generators larger than size 23 are not covered in this document.
Standard
Minimum Performance Standard for Direction Instrument, Non-Magnetic (Gyroscopically Stabilized)
2008-02-16
CURRENT
AS8021
This document establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Non-Magnetic Direction Instruments.
Standard
Maintenance of Pitot-Static Systems of Transport Aircraft
2020-02-20
CURRENT
AIR975B
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.
Standard
MINIMUM PERFORMANCE STANDARD STALL WARNING EQUIPMENT
1986-09-08
HISTORICAL
AS8014
This Aerospace Standard covers two basic Stall Warning Systems, one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to an arbitrary reference line. Each type of system includes, as a minimum, a sensor and the means for activating a device which warns the pilot of an impending stall.
Standard
MINIMUM PERFORMANCE STANDARD FOR TURN AND SLIP INSTRUMENT
2008-02-16
CURRENT
AS8004
This standard covers Turn and Slip Instruments which measure and display the rate of turn about the vertical axis and incorporate an integral slip indicator.
Standard
MINIMUM PERFORMANCE STANDARD FOR DIRECTION INSTRUMENT, MAGNETIC (GYROSCOPICALLY STABILIZED)
1983-06-01
HISTORICAL
AS8013
This document establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Magnetic Direction Instruments.
Standard
MINIMUM PERFORMANCE STANDARD FOR BANK & PITCH INSTRUMENTS
2008-02-16
CURRENT
AS8001
This Standard covers Bank and Pitch Instruments which measure and display the angular displacement of bank and pitch from a gyroscopic vertical reference. This reference may be pneumatically or electrically driven and be contained within the instrument display case or located remotely. Unless otherwise specified, whenever the term "Instrument" is used, it is to be understood to be the complete system of gyro component, any auxiliary equipment and display.
Standard
Indicator, Pressure, 1 1/2-Inch, Integrally Lighted
2012-08-22
CURRENT
AS23479A
This specification covers design requirements and all performance requirements for the procurement of single and dual hermetically sealed, integrally lighted, remote indicating, pressure indicators.
Standard
Indicator, Pressure, 1 1/2-Inch, Integrally Lighted
1999-05-01
HISTORICAL
AS23479
This specification covers design requirements and all performance requirements for the procurement of single and dual hermetically sealed, integrally lighted, remote indicating, pressure indicators.
Standard
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH (HARD MOUNTED)
1999-03-01
HISTORICAL
AS14114
Standard
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH (HARD MOUNTED)
2012-08-22
CURRENT
AS14114A
Standard
FLIGHT DIRECTORS
1954-12-01
HISTORICAL
AS420
This Aeronautical 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.
Standard
FIRE AND HEAT DETECTORS
1947-12-01
HISTORICAL
AS401
This specification covers the following basic types of instruments, or combinations thereof, intended for use in protecting aircraft power plant installations, auxiliary power plants, combustion heaters and other installation where fuel, oil or similar fires may occur.
Standard
FIRE AND HEAT DETECTORS
1949-10-01
HISTORICAL
AS401A
This specification covers the following basic types of instruments, or combinations thereof, intended for use in protecting aircraft power plant installations, auxiliary power plants, combustion heaters and other installation where fuel, oil or similar fires may occur.
