Search Results

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

Rate Gyro Assembly Configuration

2008-02-16

CURRENT

ARP727

Standard

Altitude Alerting Devices and Systems

2008-02-16

HISTORICAL

ARP1061A

This SAE Aerospace Recommended Practice (ARP) provides performance criteria for Altitude Alerting Devices and Systems. These devices can be self-contained or receive remote altitude information and can have integral or remote barometric corrections. Only the generation of the alerting signals is covered by this recommended practice and not the details of the visual or audio alerts operated by these signals. It is recommended that the system’s operational correspondence between the selected altitude settings of the Altitude Alerting Device and the Altitude Level Indication normally used to control the aircraft should not exceed ±250 ft RSS throughout the operating range of the device.

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

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

Manifold Pressure Indicating Instruments

2008-02-16

CURRENT

AS411B

This Aerospace Standard covers two basic types of manifold pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating

Standard

Compass System Installations

2008-02-16

HISTORICAL

ARP426A

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.

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 General Aviation Flight Recorder

2008-02-16

CURRENT

AS8039A

This standard covers three (3) basic types of flight recorders as defined below: All requirements specified in Sections 3, 4, 5, 6 and 7 of this standard shall be applicable to all recorder types unless otherwise noted.

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

TACHOMETER INSTRUMENTS (Indicator and Generator)

2008-02-16

CURRENT

AS432B

This SAE Aerospace Standard (AS) covers tachometer instruments (RPM indicator, 0-110 percent RPM and 0-120 percent RPM indicators and generator) for remote indication of engine speed.

Standard

Pressure Instruments - Fuel, Oil and Hydraulic (Reciprocating Engine Powered Aircraft)

2008-02-16

CURRENT

AS408C

This Aeronautical Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating This Aerospace Standard does not apply to engine mounted torque meter systems.

Standard

MANIFOLD PRESSURE INSTRUMENTS

2008-02-16

CURRENT

AS8042

This Standard covers two basic types of manifold pressure instruments:

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

Compass; Magnetic, Pilot’s Standby

1999-04-01

HISTORICAL

AS5604

This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot’s standby compasses as specified herein.

Standard

DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT

1996-10-01

CURRENT

ARP920A

This SAE Aerospace Recommended Practice (ARP) covers the design and installation requirements for pitot-static systems.

Standard

MINIMUM PERFORMANCE STANDARD TEMPERATURE INSTRUMENTS

1996-09-01

CURRENT

AS8005A

This SAE Aerospace Standard (AS) applies to all temperature instruments used in aircraft applications and environments. The word “instrument” as used in this Standard encompasses only the display device and does not include the temperature sensors. Examples of the types of instruments covered are as follows:

Standard

MANIFOLD PRESSURE INDICATING INSTRUMENTS

1993-05-01

HISTORICAL

AS411A

This Aerospace Standard covers two basic types of manifold pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating

Standard

TOTAL TEMPERATURE MEASURING INSTRUMENTS (TURBINE POWERED SUBSONIC AIRCRAFT)

1991-05-01

HISTORICAL

AS793

This standard covers three basic types of total-temperature-measuring instruments used as a means of determining the total temperature developed by adiabatic heating of the air due to motion of the aircraft through the air.

Standard

DIRECTIONAL INDICATING SYSTEM (TURBINE POWERED SUBSONIC AIRCRAFT)

1991-05-01

HISTORICAL

ARP416

This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy.