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4) Supply the voltage regulator with a stabilized power supply source adjustable within 24 and 36 V. 5) Vary the supply voltage, check that the voltage regulator triggers at 32 (+ 0.5 ; - 0) VDC and that the test wiring indicator light goes off. NOTE : In case of incorrect operation, replace the regulator (no setting is possible). 6) Remove the test wiring and install the regulator if removed. 7) Connect the regulator. 3. CHECK OF LOW VOLTAGE DETECTION SYSTEM (Figure 603) A. Tools and consumable materials - 1 stabilized power supply source adjustable within 24 and 36 V - Varnish (TB 07-901) B. Procedure 1) Disconnect the battery - refer to 24-30-02. 2) Supply the aircraft mains with a stabilized power supply source adjustable within 24 and 36 V. 3) At a 24 V supply voltage, the generation warning light located on advisory panel (1) is on. 4) Vary the supply voltage and check that the generation warning light goes off between 25.8 and 26.2 VDC. 5) If necessary, adjust adjustable resistor (3) of low voltage detection printed circuit (2) to set the triggering threshold. Once the setting completed, lock adjustable resistor (3) with varnish (TB 07-901). NOTE : Low voltage detection printed circuit (2) is located on fuse panel assembly (4), inspection door 212L - refer to 06-30-00. 6) Connect the battery - refer to 24-30-02. ADAB Validity : S / N 823 - 849, 888, 948 - 9999 24 30-00Page 603 (CG) OCT 02 |
