2010-04-20
P/N: 240-0008-00-02
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3.8.2
Electrical Load Analysis
The ADS600-B is powered via a separate circuit breaker. For aircraft with multiple power
buses, this circuit breaker is sourced from the non-essential bus. Circuits should be protected in
accordance with guidelines in AC 43.13-1B, Chapter 11.
An electrical load analysis should be completed on each aircraft prior to installation in
accordance with AC 43.13-1B, Chapter 11.
Table 3-7: Recommended Circuit Breaker
ADS600-B/ADS600-B-B
14 VDC
28 VDC
Circuit Breaker
3 AMP
2 AMP
The circuit breaker placard should be labeled “UAT.”
3.8.3
Mounting Check
3.8.4
Wiring Check
3.8.5
Functional Test
3.8.6
Weight and Balance
An aircraft weight and balance is required after installation of the ADS600-B. Follow the
guidelines in AC 43.13-1B, Chapter 10, Section 2. Update the aircraft equipment list indicating
the items relocated, added or removed. Table 3-8 identifies the weight of the ADS600-B
equipment.
Table 3-8: ADS600-B Weights
Item
Weight
ADS600-B Only
1.5lbs
ADS600-B (optional) Mounting bracket
0.1lbs