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DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT
- Aerospace Standard
- ARP920A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Recommended Practice (ARP) covers the design and installation requirements for pitot-static systems.
Recommended Content
Aerospace Standard | PRESSURE ALTIMETER SYSTEM MINIMUM SAFE PERFORMANCE STANDARD |
Aerospace Standard | Minimum Performance Standard for Mach Meters |
Aerospace Standard | Air Data Computers, MPS |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1A | Reciprocating Engine Powered Aircraft | |
TABLE 1B | Turbine Powered Aircraft (Subsonic) | |
TABLE 1C | Turbine Powered Aircraft (Supersonic) | |
TABLE 2 | ||
TABLE 3 | ||
TABLE 4 |
Issuing Committee
A-4 Aircraft Instruments Committee
The A-4 Committee is responsible for mechanical, electromechanical and electronic cockpit instrumentation standards applicable to all civil aircraft, with emphasis on minimum performance standards intended for reference in the Federal Aviation Administration (FAA) Technical Standard Orders (TSO).
A list of the technical reports developed by the A-4 Committee can be obtained by searching on 'aircraft instruments' and selecting 'standards', from the SAE Home Page. A-4 Standards For additional information about the A-4 Committee or SAE, contact Maureen Lemankiewicz mlemank@sae.org Let us contact you about suitable committee participation opportunities. Advise us of an industry issue for an SAE Technical Committee.Reference
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