Sandia Aerospace SAC 7-35 User Manual

Page 5

Advertising
background image

Section 1 General Description

1.1 INTRODUCTION

This manual describes the installation of the SANDIA aerospace SAC 7-35 Airdata Computer. It is
intended for use by FAA certified repair stations to install the SAC 7-35 Airdata Computer and in-
cludes both the mechanical and electrical installation information for the SAC 7-35. Calibration, sys-
tem configuration and checkout procedures are included. The installer should ensure that all functions
are operating according to their intended purpose in their particular installation.

1.1.1 Product Description

The SAC 7-35 is a solid state -1000 to 35,000 foot airdata computer and altitude encoder. With the addition
of a fuel flow transducer(s), the SAC 7-35 will also provide fuel flow data to systems capable of displaying that
information. The SAC 7-35 provides five data outputs that allow it to interface with a wide range of transpon-
ders, TAWS, MFD’s, Navigation Systems and a variety of other avionics products. The SAC 7-35 can also

be installed for use in a variety of converter functions. Contact factory for more information.

One ARINC 429 High Speed output, airdata and/or ADS-B.

Two RS-232 airdata output ports (including fuel flow or ADS-B).

Two RS-232 serial encoder outputs

Note: All four of the RS-232 outputs can be individually configured to match the system(s)
being interfaced.

One Gillham Grey code output for legacy transponders.

One SANDIA Altitude In-flight Monitoring (AIM) feature. With the addition of an optional

panel mounted switch and annunciator the AIM mode will monitor and advise the pilot if the
aircraft deviates from a selected altitude.

All calibration and configuration is accomplished via a lap top computer through the 6 pin Din connec-
tor on the front of the SAC 7-35.

SAC 7-35

Airdata Computer

Pitot

Static

OAT

Syncro Heading

Baro Pot *

Fuel **

GPS Track

Grey Code to Transponder

RS 232 Corresponding Alt. C

RS 232 Airdata A

RS 232 Airdata B

ARINC 429 Airdata

AIM (Altitude In-flight
Montoring)

* Optional
** Single or Twin

Figure 1-1

System Configuration

RS 232 Corresponding Alt. D

305586-00

4

Advertising