Standard
ADAPTORS AND SEALS FOR PIPE CONNECTIONS TO AIRCRAFT PITOT/STATIC INSTRUMENTS AND ASSOCIATED EQUIPMENT
2018-04-19
CURRENT
TSC47-017_01
No Scope available.
Search Results
Standard
AGS3093 Pitot Connector (Plain 5/16" DIA.)
1970-05-22
CURRENT
AGS3093-6
No scope available.
Standard
AGS3422 Straight Union (Pitot)
1961-04-28
CURRENT
AGS3422-4
No scope available.
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
AIR TRANSPORT INDICATOR CASES AND MOUNTING
1976-12-15
CURRENT
ARINC408A
This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system. This standard defines mechanical dimensions and thermal standards for aircraft indicators and displays. Thermal interface data is included for indicators and their operating environment. These indicators may be stand alone or part of larger integrated display system.
Standard
AIRBORNE WAKE VORTEX SAFETY SYSTEMS
2013-03-26
WIP
ARP6267
This document recommends criteria for Airborne Wake Vortex Information Systems, including operational objectives, characteristics, and functional requirements. The recommendations in this document apply to transport aircraft, and describe the operational objectives of wake vortex information systems, situational displays, guidance systems, and avoidance/detection systems.
Standard
AIRBORNE WINDSHEAR SYSTEMS
1988-07-01
HISTORICAL
ARP4102/11
This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics and functional requirements. The recommendations of this document apply to transport aircraft, and describe the operational objectives of Windshear warning devices, situational displays, guidance systems and detection/avoidance systems.
Standard
AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS
1996-10-01
HISTORICAL
ARP4737A
This document establishes the minimum criteria for ground based aircraft deicing/anti-icing with fluids to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models.
Standard
AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS
1997-03-01
HISTORICAL
ARP4737B
This document establishes the minimum criteria for ground based aircraft deicing/anti-icing with fluids to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models.
Standard
AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS, FOR LARGE TRANSPORT AIRCRAFT
1992-10-01
HISTORICAL
ARP4737
This document provides information to assist in the preparation of particular airline aircraft ground deicing/anti-icing procedures and to ensure safe operation of large transport aircraft during adverse conditions conducive to aircraft icing on the ground, in accordance with aircraft manufacturers’ recommendations.
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 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:
