Eagle ICA-D212-725, Instructions Manual

Page: 653 / 729

ICA-D212-725 (96)
Page 42 of 90
CHAPTER 96 – ELECTRICAL SYSTEM (96-00-00)

COPYRIGHT

2007 BY DART AEROSPACE LTD.

THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO ANY
OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision:
4
Date: 11.06.01
96.4.5.1 While supporting the inverter on its
mounting pad, install and secure mounting bolts
and washers.
96.4.5.2
Remove protective cap or tape from
electrical connector and engage and secure
connector.
96.4.5.3
Restore electrical power and
perform operational check.
96.4.6 Operational Check – Inverter
System and Inverter Caution Lights
96.4.6.1
Apply electrical power to the
helicopter electrical system.
96.4.6.2
Set INVERTER 1 switch ON and
INVERTER 2 switch to AUTO/ON (inverter blower
may run for a short time). Verify INVERTER 1
and INVERTER 2 caution lights are extinguished.
Use voltmeter on FUEL QTY CB to verify 115
VAC.
96.4.6.3
Open INV 1 PWR circuit breaker.
Verify INVERTER 1 caution light is illuminated.
Verify inverter blower runs.
96.4.6.4
Close INV 1 PWR circuit breaker.
Verify results described in step 96.4.6.2 are
obtained.
96.4.6.5
Open INV 2 PWR circuit breaker.
Verify INVERTER 2 caution light is illuminated.
96.4.6.6
Close INV 2 PWR circuit breaker.
Verify results described in step 96.4.6.2 are
obtained.
96.4.6.7
Turn electric power off. Close INV
1 PWR circuit breaker. Verify results described in
step 96.4.6.2 are obtained.