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T.O. GR1F16CJ1 188 Electrical System Controls and Indicators C
DF (Typical) CONTROL/INDICATOR POSITION/INDICATION FUNCTION 2. FLCS PMG Indicator Light FLCS PMG (amber) In flight-None of the FLCS branches are receiving power from the FLCS PMG On ground-FLCS PMG power is not avail able at one or more FLCS branches. Light is delayed 60 seconds after initial NLG WOW 3. MAIN GEN Indicator Light MAIN GEN (amber) Indicates external power or main generator not connected to one or both nonessential ac buses 4. STBY GEN Indicator Light STBY GEN (amber) Indicates standby generator power is not available 5. EPU GEN Indicator Light EPU GEN (amber) Indicates the EPU has been commanded on but the EPU generator is not providing power to both emergency ac buses. The light does not function with the EPU switch in OFF (WOW) and the engine running 6. EPU PMG Indicator Light EPU PMG (amber) Indicates the EPU has been commanded on but EPU PMG power is not available to all branches of the FLCS 7. ACFT BATT Indicator Lights FAIL (amber) In flight-indicates aircraft battery failure (20V or less) On ground-indicates aircraft battery or bat tery charger failure. Light is delayed 60 seconds after MLG WOW TO FLCS (amber) In flight-indicates battery bus power is going to one or more FLCS branches and volt age is 25V or less On ground-indicates battery bus power is going to one or more FLCS branches FLCS RLY (amber) Indicates that voltage on one or more of the four FLCC branches connected to the aircraft battery is inadequate (below 20V) or that one or more FLCC branches are not connected to the battery Figure 130.(Sheet 2) |