SAE AS417A PDF

Air Data Computers, MPS(NONCURRENT Nov 1996)

Guaranteed Safe Checkout

Description

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

Revision History

Related Info

AS417A
2008-02-16
Latest

Reaffirmed

AS417

1965-02-01
Historical
Issued

DOI: https://doi.org/10.4271/AS417A

Issuing Committee:

A-4 Aircraft Instruments Committee

Publisher:

SAE International

Pages: 13

History

AS417A	2008-02-16	Latest	Reaffirmed
AS417	1965-02-01	Historical	Issued

ISSUING COMMITTEE	A-4 Aircraft Instruments Committee
DATE	2008-02-16
DOI	https://doi.org/10.4271/AS417A
ISCURRENT	Current
PAGE	13
PUBLISHER	SAE International
REVISED	REAF. NONC.