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The SAC 7-35 has set the Air Data Computer standard for General Aviation aircraft, combining the accuracy
and performance demanded by today’s integrated avionics systems. The addition of the SAC 7-35 will unlock
the powerful features your new system is capable of providing to you. All with the quality and reliability you
have come to expect from
SANDIA aerospace
.
In addition to the airdata capabilities the -01 version of SAC 7-35 provides interface compatibility between
Garmin 400W/500W navigators and certain Mode S transponders for ADS-B operations.
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The new generation of integrated avionics have been designed to provide the pilot with a host of information to
make his flying safer and more economical. Such information as real time Winds Aloft which aid the pilot in
selecting the altitude that provides the best cruise performance. And with today’s rising fuel costs, this is
rapidly becoming a more and more important consideration. Density Altitude to help determine takeoff off
distances and make those important go, no-go decisions, particularly at high altitude airports and those with
short runways. Digital Outside Air Temperature simplifies temperature monitoring to determine when icing
conditions may exist. Fuel Flow data allows you to continually monitor your fuel used and watch any changes
in fuel consumption that may indicate engine problems.
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A full featured Air Data Computer enhancing the utility of your navigation system. The SAC 7-35 provides all
the performance of Airdata Computers costing thousands of dollars more. Altitude In-Flight Monitoring
(AIM) alerts the pilot whenever the aircraft deviates more than 100’ feet from a selected altitude. Certified
Altitude Encoder that provides both Gilliam Grey Code for legacy transponders and RS 232 outputs for modern
designs. With the addition of a fuel flow transducer(s) the SAC 7-35 supplies digital Fuel Flow information to
navigation systems that have Fuel Flow displays.
T
ECHNICAL
S
PECIFICATIONS
Electrical:
10-32 VDC
1 Amp Max
Mechanical:
4.87W x 5.62L x 1.89H
1.2 Lbs
Inputs:
ARINC 407 Synchro Heading
OAT
Pitot (Airspeed)
Static (Altitude)
Track, Mag Var & Ground Speed From On Board GPS
5 Volt Pot Baro
Fuel Flow, Pulse
GPS Position (-01 Version only)
Air Speed:
KTS:
40-450
MACH:
0.1-.99
Wind Speed:
0-200 Kts
Vertical Speed:
+/- 9999 Ft/min
+/- 20000 On ARINC Bus
Altitude:
35,000’ Max
Resolution:
Grey Code
100’
RS 232
10’
ARINC 429
10’
Accuracy:
-1000’
to
5000’
+25’
5001’
to
11000’
+30’
11001’
to
20000’
+35’
20001’
to
30000’
+50’
30001’
to
35000’
+75’
Fuel Flow:
Flow Rate
1-14400 GPH Per Side
K-Factor Range
500-130,000
Certification:
TSO C88a, ETSO C88a
TSO C106, ETSO C106
DO160E
DO178 Level C
DO254
3700 Osuna Rd NE
Suite 711
Albuquerque, NM 87109
www.sandia.aero
R4-022010-1000
SANDIA aerospace
SANDIA aerospace
SANDIA aerospace
SANDIA aerospace
SANDIA aerospace
SA
SA
SA
SA
SAC 7-35
C 7-35
C 7-35
C 7-35
C 7-35 Air Da
Air Da
Air Da
Air Da
Air Data Computer
ta Computer
ta Computer
ta Computer
ta Computer
Air Temp:
Range:
-60C to +60C
Accuracy:
+1.5
o
C
ADS-B
ARINC 743 Labels (-01 Version Only)
