Sandia SAC 7-35 Air Data Computer

Available within 5 days

2866,70 3468,71  Excl. VATIncl. VAT

Sandia SAC 7-35 Air Data Computer contains an altitude encoder, altitude alerting, fuel flow, and air data computer. FAA TSO’d.

Condition Factory New
Certification FAA 8130 or EASA Form 1
Warranty 24 Months
Part Number: 705548-00 Category:

Available within 5 days

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  • Pick up from our store (LKHS Airport)

Convenient Pickup at LKHS – Whether You Arrive by Car or Plane

Description

Sandia SAC 7-35 Air Data Computer – Performance You Can Count On

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.

You can depend on Sandia Aerospace products to provide years of reliable service. And every product is backed by a three-year warranty and personal service support.

 

Sandia SAC 7-35 Functions

  • Altitude Encoder. The SAC 7-35 is FAA TSO Approved as an altitude encoder. It provides standard Gillham Grey code for legacy transponders and RS-232 data for the new generations of transponders.
  • Altitude Alerting. The SAC 7-35 has SANDIA Aerospace’s exclusive AIM (Altitude Inflight Monitoring) that alerts the pilot anytime he deviates more than 100 feet from his selected altitude.
  • Fuel Flow. Combined with a fuel flow transducer (two for a twin) and your SAC 7-35 provides all the fuel flow data your navigation systems need to monitor your fuel situation.
  • Airdata Computer. The SAC 7-35 is a full-up TSO’d Airdata Computer offering all of the functions and capabilities of systems costing thousands of dollars more

 

SAC 7-35 Package Includes

  • Air Data Computer
  • Tray Connectors
  • OAT Probe
  • Installation manual

Specification

Technical Overview

Certification

TSO C88a, ETSO C88a TSO C106, ETSO C106 DO160E DO178 level C DO254

Electrical

10 – 32 VDC @ 1 amp, max

Inputs

ARINC 407 Synchro Heading OAT Pitot (airspeed) Static (Altitude) Track, Mag, Var & Ground from on-board GPS 5-volt pot baro Fuel flow, pulse

Air Speed

KTS: 40 – 450 MACH: 01 – 0.99

Wind Speed

0 – 200 KTS

Vertical Speed

±9,999 ft/min ±20,000 on ARINC bus

Air Temperature

-60°C to 60°C

Max Altitude

35,000 FT

Resolution

100 ft (Grey Code) 10 ft (RS-232) 10 ft (ARINC 429)

Accuracy

±25 ft (-1,000 to 5,000 ft) ±30 ft (5,001 to 11,000 ft) ±35 ft (11,001 to 20,000 ft) ±50 ft (20,001 to 30,000 ft) ±75 ft (30,001 to 35,000 ft)

Fuel Flow

Flow rate: 1 – 14,400 GPH per side K-factor range: 500 – 130,000

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