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Electricity – made understandable. Starting to “build the electrical system”. A more simple electrical schematic. Electricity. 28 volt system (1) 10 ampere battery Located under nose baggage compartment floor (2) 75 amp belt driven alternators (1) each Alternator Control Units
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Electricity • 28 volt system • (1) 10 ampere battery • Located under nose baggage compartment floor • (2) 75 amp belt driven alternators • (1) each Alternator Control Units • Regulate voltage, shut down alternator in the event it begins to produce excessive (32+) voltage, parallels the two alternators
Routing • Power from battery continuously available to hot battery bus • Grd Clearance • Courtesy lights • Nose baggage compartment light
Routing - 2 • Power available from battery through master switch, to the 80 amp circuit breaker on to the tie bus • Tie Bus • 2 Main buss circuit breakers • 1 non-ess circuit breaker • 2 avionics circuit breakers
ELECTRICITY • INTERIOR LIGHTS • Overhead dome rheostats • Switch, Panel & Avionics rheostats • Switch • Switch backlighting • Panel • Post lights • Stby instruments • EL • Flap indicator
Avionics rheostat • Stby Nav Head internal lighting • Trim Master Switch • Audio Panel lighted buttons • Txp buttons • Autopilot buttons • Stby Att gyro ON switch • Stby instrument backlighting if aircraft electrical fails
Annunciator Panel Day • Self dimming or bright override • Switch Panel lights • Self dimming • Night dimming • Gear down lights • PFD & MFD bezel button outlines • Speed Brakes
PFD & MFD • Manual dimming by button at top right of unit • TXP display • Own photocell • GNS 430 • Auto-dimming by photocell?