A—INSERT (372-2519-040) alM MOD COStNC HOD LOOP Br ahj b* SWITCHED 28 VDC 500 HZ 1 KHZ 2^ m• 4 • 8 • 10 KHZ 20 "40 • 80 • 100 KHZ 200 • 400 • 800 • 1 MHZ FREQ COMMON

AhOf RECEIVER No.l "—CoLLlH» ADF-60 CExISTI

601-5098-001

RF IHPOT A1INSERT (372-2519-040)

alM MODCOStNC HODLOOP Br

ahj b*

SWITCHED 28 VDC500 HZ1 KHZ^ m2 •4 •8 •10 KHZ20 "40 •80 •100 KHZ200 •400 •800 •1 MHZFREQ COMMONBFO

adf/aNt modeSELF TEST

SWITCHED 26 TACBEARINO Z

BEARING X• Y

R£C£IVe/t AUDIO Ht

POWER GROUND

antenna ground

CB-D390

Re50A20N

N173 Nl40nh^RE8A20M-'

RE3a24whT-Re4A24BLtf-RE2a24R£1a24

RE9a20N

THIS DwGSheet 2

R£33A20N'-^^h N191

rr

Ref405-3610

N727 -I

LH72N22

RE39a20N—

PT08SE-14-19S

Rcr 908-3610

ADF COMTROLLER No.lGables G-5497

H$3l26F-20-4lS

AUDIO OUT LO

AUDIO IN LO

AUDIO OUT HI

5V DlAL LlGHT8

EDGE lights

GROUND

26 VAC H-IN

28 VOC IN

100 KHZ200 •400 •800 •1 MHZFREQ COMMONBFO

AOr/Attr MODKSELF Tcsr

SWITCHCD 26 VACBEARING Z

BEARING X• Y

KUOlQ \.0

RecEtvem auo/o at

POWSR GROUND

ANTENNA GROUND

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RE3Za20

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ll»

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AUDIO OUT LO

AUDIO IN LO

AUDlO OUT HI

5V Dl AL LIGHTS

EDGE LIGHTS

GROUND

26 Vac h in

CB^346.

3^ (P39

•Re44B22- 28 VDC I M

€B~D390

NOTESi

!• Aircraft wiring installation in accordance with faaADVISORY CIRCULAR 43-13-Ia, CHAPTER 11, SECTIONS 1,2,3&7.

2* Allwireper HIL-W-22759 unless shielded.

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

4, All WiRE 24 AWG unless otherwise noted.

9. All wire shown * 22 awg.

6. All WIRE SHOWN ** 20 AWG.

7. All CIRCUIT breakers per MS22073.

8. All grounds grounded to grounding blocks at theappropriate radio rack.

9. Indicated wire at P6 are removed from P3RE (exist adf control)AND REINSERTED INTO P6, ONLY WIRES WITH WIRE NO.'s ARE REUSED, OTHERS ARE NEW

10. Replaces original Gables single control head»

11. Ref CanadaIR Dwg 601-70479 - ADF System.

12. Triaxial Cable by Havcg Industries, Pt No. 61-02478. (Existing Cable),

13. All wire or components shown # or are existing.

14. Existing A^^*-60A antenna replaced with dual aNT-60B,

15. ADF-l, ADF-2 CERTIFIED To TS0-C41c,

16. Change blocks lo, ii, 12, 13 from HRTB20E04 to HRTB20E03.

17* Splice wire rg66622 & rg66c22 bypassing existing block 13a, b, &.f.WIRE RG66D22 IS REMOVED (ReF 705-3610).

•i-T

pi LOT*3 SHI

rI AOr X BRQ X

AOr 1 BAG Y

AOF 1 BRG Z

BRQ REF HI

1 RefCanadair1 Owe 601-70479

CO.PILOT«S RHI

AOF 1 BRQ X

ADF 1 BRQ Y

AOF 1 BRQ 2

BRQ REF HI

Ref CanadaIrDwq •01-70479

PILOT'S HSI

AOF BRQ X

AOF BRQ Y

AOF REF

Ref CanaoaIrOwQ 601-70479

PUOT'S RHi

Ref 1R09-3610

AOF 1 BRQ X

AOF 1 BRQ Y

AOF 1 BRQ Z

BRQ REF Hi

CO-PtUOT'S RHl

tEF 1809-S610

ADF 1 BRQ X

ADF 1 BRQ Y

AOF 1 BRQ Z

BRQ REF HI

PILOT'S HSi

Aori 6*0 X

AOr 1 BRG Y

.Re43D22BLU

-RE42d22wht

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E43E22BLU

E42e22WHT

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fEl

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Ref CanadairDhq 601-70479

This 0wq Sht 1

RE73a24—

-RE62C20N-

RE41B20H

•RE74A24 5

ThIs Duq Sht i

Re43AA22BLU

•UE42AA22VHT

'Re40BB22WHT

-fiE4lAA22BLU

ADP 1 BKQ X

AOr 1 BRQ Y

AOF 1 BRQ X

BRQ RIP HI

IV

[I1

PILOT'S HSi

1

^i>r'X BM3 X

xor X BMS Y

3>ffe43B22BLU

B£42b22whT'

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IE40A22

FOR NOTES SEE SHEET 1.

THiS DuQ ShT 1

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