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SAE International - ARP920A

DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT

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Organization: SAE International
Publication Date: 1 October 1996
Status: active
description:

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

Document History

ARP920A
October 1, 1996
DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT
This SAE Aerospace Recommended Practice (ARP) covers the design and installation requirements for pitot-static systems.

References

This document references:
ARP921 - FLIGHT TEST PROCEDURES FOR STATIC PRESSURE SYSTEMS INSTALLED IN SUBSONIC TRANSPORT AIRCRAFT
Published by SAE International on August 10, 2011
This Aerospace Recommended Practice covers the test procedures and equipment for performing flight testing on pitot-static systems installed in subsonic transport type aircraft.
This document references:
AS390 - Pitot or Pitot-Static Pressure Tubes, Electrically Heated (Turbine Powered Sub-Sonic Aircraft)
Published by SAE International on February 16, 2008
This aerospace standard covers the following basic instrument types:
This document references:
AS393 - AIR SPEED TUBES ELECTRICALLY HEATED
Published by SAE International on December 1, 1947
This specification covers the following basic types: Type I - Pitot Pressure, Straight and L-shaped, 12 and 24 volt nominal, 2 wire circuit. Type II - Pitot and Static Pressures, Straight and...
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