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PART NO.

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DESCRIPTION

REVISION DESCRIPTION BY DATE

TOLERANCE

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APPROVED A.PPROVED A/71 ft DATE DWG. NO. REV, SHEETo.i_£oCii-3l-aa-2o*ZS-01 — \of1

THIS PRINT IS OUR EXCLUSIVE PROPERTY NO COPYING OR REPRODUCING RETURN ON REQUEST

battery temp indicatorFoxTronics BTI-600-103a

HS3126-12-10S [0H12| Jl

J1 fWlll MS3126F-14-15STEST RUN

♦9V TEST

TEMP PROSE IN A

9V0C INST LIOHTS

OROUNO

WARN L18HT DIM

28VDC POWER IN

150* HOT OUTPUT

A|RCR/iFT ELECTRICAL DISTRIBUTION BOX

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Ref3008-3610

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Ref2008-3610

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SWITCHLITES BYAerospace Optics

Diodes areSylvania ECG-125

BATTERY PROBE

ANNUNCIATOR TEST BOX

Ref 2010-3610

CO-PI LOT*3 INBOARD PANEL

1CB-Bl7di

28VDCBuss 2

Ref 1905-3610

3, KC.I&-II

fiATTEPy CHARGER

Ref CanaoairOwe G01-SOo74

BATTERY AHP METERCot-T CO-2021

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SIGNAL ♦

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GROUND

Shunt is a Emoro HA-300-50 ♦20VDC

Ref Canada Ir Owe 601*50674

NOTES:

PHOTOS INBOARD PANEL

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1. Aircraft wiring installation in accordance vith faaADVISORY circular 43-13-1a, CHAPTER 11, SECTIONS 1,2,3, A 7.

2. All wire per MlL*V>22759 unless shielded.

3. All shielded wire per MlL-C-27500TG,

4. All wire 24 awq unless shown otherwise.

5. All wire shown * 22 awq.

6. All wire shown •• 20 awg.

7. All CIRCUIT BREAKERS PER HS22073*

8. All wire or components shown | or C,J existing.

9. All grounds grounded to grounding olocks at theappropriate radio rack.

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