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VERTICAL VELOCITY INSTRUMENT (Rate-of-Climb)
- Aerospace Standard
Published September 01, 1996 by SAE International in United States
Digital Standard available
Downloadable datasets availableAnnotation ability available
This AS covers Vertical Velocity Instruments which display the rate of change of pressure altitude of an aircraft, as follows:
Type A - Direct reading, self-contained, pressure actuated
Type B - Electrically or electronically operated, self-contained, pressure actuated
Type C - Electrically or electronically operated, input from a remote pressure sensor
|Aerospace Standard||AIRSPEED INSTRUMENTS|
|Aerospace Standard||ALTIMETER, PRESSURE ACTUATED SENSITIVE TYPE|
Data Sets - Support Documents
|TABLE 1||Test Rate Test Rate|
The A-4 Committee/Sub-Committees are 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).
|J916||This document is not part of the subscrption.|
|RTCADOC.DO-160||This document is not part of the subscrption.|
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