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This Standard covers air data equipment (hereinafter designated the instrument) which when connected to sources of aircraft electrical power, static pressure, total pressure and outside air temperature (singly or in combination) provides some or all of the following computed air data output signals:
| Pressure Altitude* | Total Temperature* |
| Pressure Altitude (Reporting) | Altitude Rate |
| Baro-Corrected Pressure Altitude* | Overspeed Warning |
| Vertical Speed* | Altitude Hold |
| Computed Airspeed* | Airspeed Hold |
| Mach Number* | Mach Hold |
| Maximum Allowable Airspeed* | qc (impact pressure) |
| Static Air Temperature (*when used as an alternate for total temperature) | True Airspeed Others |
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2008-02-16 |
| ICS | 49.090 : On-board equipment and instruments
|
| Number of pages | 13 |
| Replace | SAE AS 417:1965-02-01 |
| Set | AEROPAKS10U-10 |
| Year | 2008 |
| Document history | |
| Country | USA |
| Keyword | SAE 417;SAE AS417A;SAE AS417A;SAE AS 417 |