Search Results

Standard

Barometry for Altimeter Calibration

2020-02-20

CURRENT

AIR1075B

This SAE Aerospace Information Report (AIR) is concerned only with aspects directly relating to available accuracy. While well-designed photoelectric, inductive or capacitive readers and pressure regulators, and other accessories are highly desirable for convenience and production rate, they are considered to be outside the scope of this AIR.

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

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

GYROSCOPE, DISPLACEMENT, ROLL AND PITCH (HARD MOUNTED)

2012-08-22

CURRENT

AS14114A

Standard

COMPASS, MAGNETIC, PILOT'S STANDBY

2012-08-22

CURRENT

AS17983A

Standard

Direction Instrument, Non-Magnetic, Stabilized Type (Directional Gyro)

2012-08-22

CURRENT

AS397B

This Aeronautical Standard covers two basic types as follows: Type I - Air Operated Type II - Electrically Operated

Standard

Automatic Pilot Installations

2008-02-16

HISTORICAL

ARP419A

These recommendations cover the mechanical and electrical installation and installation test procedures for automatic pilots of the type normally used in transport type aircraft. The material in this ARP does not supercede any airworthiness requirement in the Civil Air Regulations.

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

Attitude Instruments, Pitch and Roll Part I Minimum Performance Standard for Equipment

2008-02-16

CURRENT

AS1162

This Aerospace Standard covers two basic types of pitch and roll indicating instruments as follows: Type I: Direct coupled to gyro Type II: Electrical repeating

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

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

Direction Instrument, Non-Magnetic, Stabilized Type (Directional Gyro)

2008-02-16

HISTORICAL

AS397A

This Aeronautical Standard covers two basic types as follows: Type I - Air Operated Type II - Electrically Operated

Standard

Bank and Pitch Instruments (Indicating Stabilized Type) (Gyroscopic Horizon, Attitude Gyro)

2008-02-16

CURRENT

AS396B

This Aeronautical Standard covers both direct and repeating type gyroscopically stabilized Bank and Pitch Indicating Instruments.

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

Overhaul Facilities for Aircraft Instruments

2002-12-16

CURRENT

ARP421

Standard

COMPASS, MAGNETIC, PILOT’S STANDBY

1999-07-01

HISTORICAL

AS17983

Standard

Accelerometer Group, Counting (MS25447 and MS25448)

1999-07-01

HISTORICAL

AS22145

This specification covers the design and performance requirements for a single axis, four load-factor level counting accelerometer group referred to hereafter as “equipment.”

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.