Search Results

Standard

VERTICAL VELOCITY INSTRUMENT (Rate-of-Climb)

1978-10-01

HISTORICAL

AS8016

This AS covers Vertical Velocity Instruments which display the rate of change of pressure altitude of an aircraft, as follows:

Standard

Temperature Measurement, Well Insert Type

2020-04-14

CURRENT

ARP175A

Standard

TEMPERATURE MEASUREMENT, WELL INSERT TYPE

2008-02-16

HISTORICAL

ARP175

Standard

Single-Degree-of-Freedom Spring-Restrained Rate Gyros

2008-02-16

CURRENT

AS1104

This specification covers that gyroscopic instrument normally defined as a "subminiature rate gyro." The rate gyro, when subjected to an angular rate about its input axis, provides an AC output voltage proportional to the angular rate. The subminiature size category generally includes gyro instruments of one (1) inch diameter or less and three and one-half (3 1/2) inches length or less. This specification defines the requirements for a subminiature spring-restrained, single-degree-of-freedom rate gyro for aircraft, missile, and spacecraft applications.

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

Pressure Ratio Instruments

2008-02-16

CURRENT

ARP427A

This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator.

Standard

PRESSURE RATIO INSTRUMENTS

1991-05-01

HISTORICAL

ARP427

This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator.

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

Minimum Performance Standard for Automatic Pressure Altitude Digitizer Equipment

2008-02-16

CURRENT

AS855

All automatic altitude reporting digitizer equipment manufactured under this standard shall comply with the requirements as specified up to its maximum range as indicated on the equipment nameplate.

Standard

Minimum Performance Standard Stall Warning Equipment

2020-12-22

CURRENT

AS8014A

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 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 MACH METERS

1978-10-01

HISTORICAL

AS8018

This AS covers subsonic and supersonic Mach Meter instruments which, when connected to sources of static (Ps), and total (Pt), or impact (Pt-Ps), pressure provide indication of Mach number. These instruments are known as Type A. This AS also covers servo-operated repeater or digital display instruments which indicate Mach number when connected to the appropriate electrical output of a Mach transducer of Air Data Computer. These instruments are known as Type B.

Standard

MINIMUM PERFORMANCE STANDARD FOR FUEL AND OIL QUANTITY INDICATING SYSTEM COMPONENTS

2008-02-16

CURRENT

AS8029

This AS defines components in "Capacitance Sensor" and "Non-Capacitance Sensor" type Fuel and Oil Quantity Indicating Systems. "Non-Capacitance" systems may employ any measurement technique current in the art including, but not restricted to, float, ultra-sonic and fiber optic devices. The definition of the individual components contained herein is related to the specified Total Installed System accuracy of the entire Fuel or Oil Quantity Indicating System which is a part of the airframe manufacturer's type certification approval data. This data shall be available from the subject airframe manufacturer as published in the operating manual for the aircraft type, model number and configuration. The Fuel or Oil Quantity Indicating System may incorporate optimum compensation based upon measurement of dielectric constant, temperature or density to correct for variations in fuel or oil characteristics due to temperature grade variations or additives.

Standard

MINIMUM PERFORMANCE STANDARD FOR DIRECTION INSTRUMENT, MAGNETIC (GYROSCOPICALLY STABILIZED)

2008-02-16

CURRENT

AS8013A

This SAE Aerospace Standard (AS) establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Magnetic Direction Instruments.

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

Liquid Oxygen Quantity Instruments

2008-02-16

CURRENT

ARP433A

This Aeronautical Recommended Practice covers Liquid Oxygen Quantity Indicators for use with associated Liquid Oxygen converters.

Standard

LIQUID OXYGEN QUANTITY INSTRUMENTS

1991-05-01

HISTORICAL

ARP433

This Aeronautical Recommended Practice covers Liquid Oxygen Quantity Indicators for use with associated Liquid Oxygen converters.

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.