Eagle ICA-D212-725, Instructions Manual

Page: 726 / 729

ICA-D212-725 (98)
Page
19 of 21
CHAPTER 98 –WIRE DIAGRAMS (98-00-00)
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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:
3
Date: 09.05.20
DC LOAD ANALYSIS
EQUIPMENT
NUMBER
OF UNITS AMPS/UNIT
TOTAL
AMPS
NORMAL
OPS
ENGINE IGNITION SYS.
Igniter Unit 1 1.50 1.50 1.50
Solenoid-Valve Igniter 1 0.75 0.75 0.75
Relay-Starter 1 4.50 4.50
TOTAL 6.75 2.25
MISCELLANEOUS
Windshield Wiper 2 3.10 6.20 6.20
Relay-Cargo Hook 1 0.20 0.20 0.20
Hourmeter 1 0.00 0.00
Logging Door Lights 3 0.04 0.12
Aux Power Connector 1 15.00 15.00
TOTAL 21.52 6.40
AVIONICS
Audio Controller 2 0.50 1.00 1.00
Transponder 1 3.00 3.00 3.00
Blind Encoder 1 2.00 2.00 2.00
GNS-430 GPS 1 3.00 3.00 3.00
GNS-430 VHF Comm 1 5.00 5.00 5.00
#2 VHF Comm 1 10.00 10.00 10.00
FM Radio 2 2.00 4.00 1.00
USFS Panel 1 5.00 5.00 1.00
AA34 Interface 1 1.00 1.00 0.50
Sackafoam 1 5.00 5.00
PA Controller 1 3.00 3.00 3.00
PA Amp 1 5.00 5.00 5.00
TOTAL 47.00 25.50
TOTAL AMPERES
BASIC HELICOPTER 214.41 123.64
Figure 98-7. DC Load Analysis Chart (Sheet 3 of 4)
For S/N except 30687, 30576, 30931, 30817 and 30599