KPN 030-1014- 55
PIIISI
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~PI962
I. MIC INTERCOM IS NOT USED. INTERCOM IS PROVIIED BY USING EXT. MOOE OF KMA 20 AND
CONNECTING RAMPHAI~ OUTPUT TO A RESISTOR LOAD.
2. RAMP HAILER AND AIRCRAFT SPEAKER SHIELDS SHOULD E1E CONIIIECTED
TO PIN I AT KMA 20.
3. UN~ESS NOTED. A~L WiRES 24 AWG MIN IMUM.
4. AL~ ANTENNA COAX IS RG 58 AIU.
S. UN~ESS OTHERWISE SPECIFIED.ALL SYSTEM GROUNDS ARE AIRFRAME GROUNDS.
6. POWER BUSS CIRCUIT BREAKERS ARE "TOBE MOUNTED IN THE AIRCRAFT BREAKER
PANEL OR INSTRUMENT PANEL SUCH THAT THEY WILL BE ACCESSIBLE IN FLIGHT
AND SAFE FROM PHYSICAL OAMAGE.
7. THIS INTERCONflECT ORAWING IS FOR KMA 20', SIN 11233 AND ABOVE. KMA 20',
511I 11232 AND BELOW WILL REOUIREAN EXT.8n.
LOAD
RESIS10R FOR RAMPHAIL
OUTPUT. SEE
"'STAL~
&U~LETIN
""
56.
8. AP~ICAiLE TO
K"A
2~-09.-10.-11 .-13 AND,-14 ONlY.
9. TX-RX INTERCONNECT WIRING IS NECESSARY WHEN BOTH COMM ANT. ARE TOP MOUNTED. BOTH
COMM ANT. ARE BOTTOM MOUNTED OR IN DUA~ COMM INSTA~TIONS IN FABRIC AIRCRAFT.
REFER "TO
ANTENNA INSTA~LATION RECOMMENDATIONS.
10. AIRCRAFT POWER WIRING SHOU~ 8E
TWO'"
18 AWG
"TO
THE CIRCUIT BREAKER AND POWER
GROUND SHOULD BE
TWO'"
IB AWG TO GROUND.
II. SWITCHED A/C POWER. PINS J AND 8 AND 27.SV POWER PINS HAND 7. MUST BE ~UMPERED
TOGETHER WITH... 20 AWG MINIMUM.
IZ. FOR REMOTE FREQUENCY TRANSFER I REMOTE FREOUENCY RECALL (06~.IDZ HO/ll1l21
OR FIELC MOD I~. A MOMENTARY GROUND
AT PIN E WILL CAUSE THE RADIC
Te'
INCREMENT
TO THE NEX: F~::C:U::NCY !N MErI.CF"cYAND 01SPLLY
IT I~J THE
STay WINDOW. A MOMENTARY
GRCIJND AT F-IN
6 wiLL TRANSFER TI-tE USE toNO STBY. FREOUENCIES. A TWC POSITION
SPRING L.OADED FcOCKER
SWITCH CR TWO SEPARATE MOMENTARY PUSHBUTTON
SWITCHES
MI.Y 9E USED AT THE INSTI.~LERS
OPTION.
J
PI961
~AGC
TESTIREMOTE
6 REMOTE X FER
INC---O
~OR
a
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