SAE AS417A

Anotace textu normy SAE AS417A :

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

SUBJECT TAXONOMY: CAD, CAM, and CAE, Avionics, Aircraft instruments, Flight control systems, Air data computers, Flight management systems, Displays, Smoke detection, Instrument panels, Parts, Safety, Fire detection, Tests and Testing
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard