Search Results

Standard

AIR DATA COMPUTER

1965-02-01

HISTORICAL

AS417

This Aerospace Standard covers an air data computer characterized by the concept of transducing and computing the majority of air data requirements for an aircraft. The display instruments and other using subsystems are not considered in this scope except where they perform computing operations for output parameters as covered by this specification. The computer may accept the inputs and provide the outputs listed in paragraphs 2.1 and 2.2 respectively. The computer may also provide an altitude encoder output for IFF Mark X ¯ ¯ (SIF)/Air Traffic Control Radar Beacon System SIF/ATCRBS; in which case AS 855* "Altitude Device Providing Outputs for Automatic Pressure Altitude Reporting" shall be referred to for applicable minimum standards. (Note - Reference to air data computer in subsequent paragraphs will be designated as "instrument".)

Standard

AIRCRAFT INSTRUMENT AND INSTRUMENT SYSTEM STANDARDS: WORDING TERMINOLOGY, PHRASEOLOGY, ENVIRONMENT AND DESIGN STANDARDS FOR

1981-01-15

HISTORICAL

AIR818C

This AS covers __________ which measure and display __________ or This AS covers __________ basic types of (no capitals) instruments as follows: Note: Each type number to be followed by a brief description as it would if the scope were covering only a single type. As many types as required may be used.

Standard

AIRCRAFT INSTRUMENT STANDARDS: WORDING, TERMINOLOGY, PHRASEOLOGY AND ENVIRONMENTAL AND DESIGN REQUIREMENTS FOR

1991-05-01

HISTORICAL

AIR818

This Aerospace Standard covers ______________________________________________.

Standard

AIRCRAFT INSTRUMENT STANDARDS: WORDING, TERMINOLOGY, PHRASEOLOGY, ENVIRONMENT AND DESIGN STANDARDS FOR

1972-01-01

HISTORICAL

AIR818B

This Aerospace Standard covers ____________________ or SCOPE This Aerospace Standard covers ____________________ basic types of (no capitals) instruments as follows: NOTE: Each type number to be followed by a brief description. As many types as required may be used.

Standard

AIRSPEED INDICATOR (PITOT STATIC)

1954-12-01

HISTORICAL

AS391B

This Aeronautical Standard covers five basic types of airspeed instruments with indication range essentially as follows: TYPE I - 1 revolution TYPE II - 1 revolution (unequal scale) TYPE III - 1-1/2 to 1-3/4 revolutions TYPE IV - 7 revolutions TYPE V - 1-3/4 to 2 revolutions

Standard

AIRSPEED INDICATOR (PITOT STATIC)

1949-02-01

HISTORICAL

AS391A

This specification covers six types of instruments as follows: TYPE I - 30 - 250 miles per hour range TYPE II - 40 - 300 miles per hour range TYPE III - 50 - 400 miles per hour range TYPE IV - 50 - 450 miles per hour range TYPE V - 50 - 700 miles per hour range TYPE VI - 50 - 425 knots range

Standard

AIRSPEED INDICATOR (PITOT STATIC)

1947-07-01

HISTORICAL

AS391

This specification covers six types of instruments as follows:

Standard

AIRSPEED INDICATOR (PITOT STATIC) (RECIPROCATING ENGINE POWERED AIRCRAFT)

2008-02-16

CURRENT

AS391C

This Aeronautical Standard covers five basic types of airspeed instruments as follows:

Standard

AIRSPEED INSTRUMENTS

1987-05-01

HISTORICAL

AS8019

This standard covers Airspeed Instruments which display airspeed of an aircraft, as follows:

Standard

AIRSPEED TUBES ELECTRICALLY HEATED

1960-07-15

HISTORICAL

AS393A

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.

Standard

AIRSTREAM DEVIATION INSTRUMENT (ADI)

1991-05-01

HISTORICAL

ARP794

This recommended practice covers an instrument which measures and displays angle of deviation of the airstream dependent on mounting location on the aircraft.

Standard

ALTIMETER, PRESSURE ACTUATED SENSITIVE TYPE

1947-08-01

HISTORICAL

AS392

This specification covers two types as follows:

Standard

ALTITUDE ALERTING DEVICES AND SYSTEMS

1991-05-01

HISTORICAL

ARP1061

This 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

AUTOMATIC PILOT INSTALLATIONS

1991-05-01

HISTORICAL

ARP419

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

AUTOMATIC PILOTS

1991-05-01

HISTORICAL

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.

Standard

AUTOMATIC PILOTS

1947-08-01

HISTORICAL

AS402

This specification covers all gyroscopic and servo control types of automatic pilots intended for use on aircraft to operate automatically the control surfaces of the aircraft to maintain a stabilized flight attitude with respect to the longitudinal, lateral and vertical axes, and to provide for maneuvering the airplane through servo control.

Standard

AUTOMATIC PILOTS (Turbine Powered Subsonic Aircraft)

1996-09-01

HISTORICAL

AS440A

This SAE Aerospace Standard (AS) covers automatic pilots intended for use on aircraft to automatically operate the primary and trim aerodynamic controls to maintain stable flight and/or to provide maneuvering about any of the three axes through servo control. Automatic control functions essential for primary or augmented flight control are excluded.

Standard

AUTOMATIC PILOTS (Turbine Powered Subsonic Aircraft)

1963-02-01

HISTORICAL

AS440

This Aerospace Standard covers Automatic Pilots intended for use on aircraft to automatically operate the primary and trim aerodynamic controls to maintain stable flight and/or to provide maneuvering about any of the three axes through servo control. Automatic control functions essential for primary or augmented flight control are excluded.

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

Accelerometer Group, Counting (MS25447 and MS25448)

2012-08-22

CURRENT

AS22145A

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